JP6141368B2 - Nozzle and nozzle holder for aerosol generator - Google Patents

Description

(Cross-reference of related applications)
This application claims priority from US non-provisional application 11 / 315,951 filed on December 22, 2005 and published as publication number US-2007-0144514-A1 on June 28, 2007. It is a continuation application. This previous non-provisional application 11 / 315,951 is fully incorporated herein by reference.

(Government support)
This invention was made with US government support from the National Institutes of Health, National Heart, Lung and Blood Institute under grant number HL78281. The US government has certain rights in this invention.

(Technical field)
The present invention relates to a small portable device for the generation of respirable dry particles concentrated from an aqueous solution or suspension.

There is an ever increasing demand for the supply of large quantities of biologics and other drugs to the respiratory tract by aerosol. Many devices that generate liquid aerosols may not work well with high molecular weight molecules or during high concentration. In addition, some of these devices can break down molecules during aerosolization. These restrictions, along with the requirement to reduce the use of fluorocarbons, led to the development of dry powder inhalers. In these devices, the “blister” or capsule containing the drug breaks, and the powdered drug together with the contained additives is used, for example, by vortex resulting from inhalation or aerosolization by other mechanical means such as sonication. Distributed. To the additive is added an active agent to assist in aerosolizing these lumps. Some examples, such as Exhubra®, for example, constitute about 70% of the weight of the mixture. The use of additives results in molding costs, safety pharmacology costs and potential unwanted side effects. Dry powders containing these active agents are most often generated using a spray drying method. Spray drying has been commonly used for many years. They generally consist of generating aerosol at the top of a vertical cylindrical tower where warm gas is added to the aerosol mist internally in the same or opposite direction. The output cyclone is used to collect the resulting powder. Additives are added to the collected powder to aid dispersion. The mixture is placed in a dry powder inhaler DPI. This means has some limitations:
(A) The resulting powder particles stored must be stable and desirably durable to high humidity.
(B) Additives must be formulated that are easily dispersed.
(C) When two chemicals are formed individually, the size of the drug particles is generally smaller than the size of the additive.
(D) The inhalable mixture is limited to the capsule size, not the inhalation volume.
(E) The spray-drying method has an efficiency of about 60% and a supply efficiency to the lungs with a dry powder inhaler of 30%, resulting in a loss of about 80% of the active agent.
(F) Rapid inhalation results in aerosolization of the majority of the powder in the capsule but results in a lot of attachment to the mouth and throat. Slow inhalation results in many attachments deep into the lungs, but results in low efficiency of aerosolization of the powder in the capsule. These results cause large variability in single doses, resulting in both efficiency and safety concerns.

  These results are overcome in a series of steps as described herein by a device that generates a liquid aerosol, drys it, concentrates it, and delivers the remaining dry aerosol of the active agent to the lungs. Is possible. Rather than a commercial size, lab equipment should be realized with a height of 70 inches and a weight of 50-80 kilograms. It should be noted that the spray tower is vertically oriented in all these devices. A small cylindrical device would best be provided with a small horizontal drying chamber.

  If the particle density is less than 1, higher mass delivery to the lungs than can be obtained with solid drug particles can be achieved with aerosols of the same aerodynamic diameter (Edwards 1996). The formation of such particles is the subject of many patents, including US Pat. No. 7,435,408. Large porous particles have been generated by spray drying a mixture of polyester and an active agent such as insulin. These spray-dried aerosols are generally generated by collecting them as standard spray-drying techniques and powders. In order to generate low density particles, a liquid with a lower molecular weight than the ultrahigh molecular weight additive in the solvent evaporates faster than the diffusion of the high molecular weight component. The resulting particles are hollow or have an open gas space that creates a geometric diameter greater than the aerodynamic diameter. These aerosols are generally collected using a cyclone. The particles so delivered need to be re-aerosolated later in order to be inhaled by the patient. As already mentioned, using this technique, only a small portion of the original drug is delivered to the lungs. This specification describes how the dilution of the aerosol plume is performed using a heated counter-flow gas jet coaxial in the opposite direction of the coaxial axis of the aerosol plume. Describe whether it can be diluted quickly to near the source. In addition, an annulus of diluent gas transports the aerosol along the evaporation chamber from the generator to the virtual concentrator. This document also describes how the evaporation of water particles in this perturbed plume can be increased by the supply of infrared radiation from a source outside the evaporation chamber.

  US Non-Provisional Application 11 / 315,951 (Yeastes et al.) Filed Dec. 22, 2005 and published as publication number US-2007-01445514-A1-this priority is claimed against this application Has described a dry powder aerosol generator and processing system that aerosolizes, evaporates, concentrates and delivers a dry powder aerosol containing all of the dissolved solutes. The specification describes details of improvements to these systems and subsequent new discoveries about the generation of pure protein respirable aerosols of density less than 1 in small devices. . This device eliminates the need for spray drying, cyclonic collection, additive mixing and placement in dry powder containers. Improvements to this system are detailed herein. The significant attenuation of the integrated gas flow resistance allows the use of a blower that is only 2 × 2 × 1 inches, improving the portability of the device. The assembly friction fit structure eliminates the use of large diameter O-rings, can easily seal the evaporation chamber, and makes it very easy to assemble by a sick patient. Lightweight heaters with flow resistance and low thermal inertia have been developed to allow functionality within 1 minute of turning on and improve portability. The backflow tube is centered within the concentrator to ensure ease of assembly and accurate alignment with the aerosol jet axis, thus improving performance reliability. An additional heating element for warming the nozzle and backflow gas is included, allowing more rapid evaporation of the aerosol plume. The focus reflector is included in the infrared heat source, and reduces the required power of the infrared heater. This and the above improvements reduce all the power used by the device. These and other functional practical improvements are detailed herein. At the same time, they make the device more portable, more functional, easier, more cost-effective and new for the generation of new particles for rapid inhalation that was previously impossible. Offer a lot of possibilities.

  Virtual impaction is used as an aerosol concentration means (US Pat. No. 4,767,524, Pillai and Years, 1994). There are several improvements in these structures, including the use of slit apertures instead of round apertures (Marple and Robo 1986). Applicant's patent application 2007014445 uses information for the design of concentrators with a radial slit with a cut-off diameter of 2.5 microns. The present disclosure discloses how to concentrate a broad mass of particles within the respiratory tract. This range is typically 1-5 microns, but may cover a range of 0.5-10 microns. According to Marple and Robow, a 1 mm aperture slit for capturing particles larger than 1 micron is required to be compared with a 2.6 mm slit for concentrating particles larger than 2.5 microns. This potentially increases the pressure head required to accelerate the aerosol passing through the slit. An open parabolic inlet was incorporated into the structure to dampen the pressure head upstream of the concentrator. It should be noted that Seshadri (AAAR 2006) points to using a parabolic inlet profile along with sheath gas flow to reduce wall loss and potentially increase the concentration factor. As already mentioned, in this disclosure they are incorporated to reduce the upstream pressure required to operate the concentrator. Shekarrizz (US Pat. No. 7,178,380) discloses a concentrator with an uneven accelerating wall along with a side injection port and claims reduced clogging. The concentrator is an input of 15 liters / minute, which is only a fraction of the flow rate in this device--typically 100 to 300 liters / minute, but higher or lower flow rates are possible. Use flow rate. The device does not have or need an injection port proposed to prevent clogging. Alternatively, US Pat. Nos. 7,261,007 and 5,858,043 describe concentric slits to reduce termination effects. When concentric slits are used, it is extremely difficult to exhaust the gas rather than using the small structure of the present application.

The first objective of the present disclosure results in generating an aqueous (or other solvent at high vapor pressure) aerosol in a small practical device and then rapidly evaporating the aqueous aerosol by dilution and heating. To provide a means to concentrate the particles and deliver them at a flow rate that fits the full range of standard expiratory flow.
A second objective of the present disclosure is to eliminate high pressure coupling so that the device can be easily assembled and disassembled for cleaning.
A third object of the present invention is to reduce the resistance to gas flow through the device in order to allow the construction of a small device using a small blower for supplying diluent gas.
A fourth object of the present disclosure is to minimize gas and / or aerosol leakage between the various elements of the device--the junction between each element while the structure is fully maintained. is there.
A fifth object of the present disclosure is to facilitate the supply of counterflow gas that is exactly coaxial with the aerosol plume and in the opposite direction with respect to the aerosol plume.
A sixth object of the present disclosure is to provide heated compressed gas to both the nozzle and the backflow tube while minimizing heat loss.
A seventh object of the present disclosure is to provide local radiant heat to newly formed aqueous aerosol particles from a source outside the evaporation chamber at the minimum infrared absorption wavelength of water.
An eighth object of the present disclosure is that the device has different easily replaceable nozzle holder structures that allow compressed gas to be delivered through a central opening or to surround a central fluid stream. Is to be able to be used together.
A ninth object of the present disclosure is to have these nozzle holders adjusted for use in a flow conditioner and to have the ability to include compressible fluid containers instead of fluid inlets.
The tenth object of the present disclosure is to provide a high-speed gas flow that is heated while flowing in one direction in a small device, and then the perturbation due to the aerosol plume and backflow gas is possible To provide a uniform slow flow in the direction.
The eleventh object of the present disclosure is to efficiently concentrate respiratory aerosols greater than 0.5 microns with minimal pressure loss between input and exhaust gases.
A twelfth object of the present disclosure is to facilitate assembly and disassembly while maintaining high precision alignment of the shaft and rotation.
The thirteenth object of the present disclosure is to prevent aerosol particles in the concentrator exhaust gas stream from polluting the atmosphere.
A fourteenth object of the present disclosure is to minimize aerosol deposition due to turbulence at the output of the concentrator.
A fifteenth object of the present disclosure is to provide an efficient means of delivering a concentrated aerosol at the output by means of the parabolic shaped nature of the output cone.
The sixteenth object of the present disclosure is to concentrate at a small positive pressure that provides pressure support for patients with problems in generating sufficient inhalation pressure, and flow rates that trigger other dry powder inhalers. It is to provide an aerosol.

(Outline of the present invention)
According to the first aspect of the present invention, these and other objects include a step of supplying a first volumetric flow rate of pressurized gas, a step of preheating the first volumetric flow rate of said pressurized gas, and a first step of dilution gas. Supplying a second volumetric flow rate, preheating a second volumetric flow rate of the dilution gas, supplying a third volumetric flow rate of fluid, a first volumetric flow rate of the pressurized gas, and a third volume of the fluid. A step of generating a concentrated first aerosol by discharging at least a portion of the volumetric flow rate through a nozzle; and the concentrated first aerosol so that the concentrated first aerosol is suppressed; Supplying a fourth volumetric flow rate of gas in the opposite direction; mixing the suppressed first aerosol with a second volumetric flow rate of the dilution gas to generate a diluted second aerosol; Generate aerosol with The method is achieved by the present invention using.

  According to the second aspect of the present invention, these and other objects are nozzles for generating aerosols from fluids and gases, the direction of gas flow from the cone apex of the wet cone-shaped gas outlet channel toward the cone base. At least one wet cone-shaped gas outlet channel connected to the nozzle gas supply channel at the apex of the cone and at least one annular circumference around the cone base connected to the nozzle fluid supply channel And a fluid outlet port.

In accordance with the third aspect of the present invention, these and other objects are achieved by a nozzle holder comprising a first end associated with a nozzle holder fluid injection port and a second end including the nozzle described above. The nozzle holder includes a barrel (barrel) with a cylindrical barrel bore having an internal cylindrical barrel bore and the inner cylinder barrel diameter, scan Temu (stem), and a cylindrical top portion having a perfect fit outer cylindrical top surface to the cylindrical barrel hole walls A cylindrical body having a plurality of circumferentially spaced grooves connected to a ring-shaped fluid outlet port.

In accordance with the fourth aspect of the present invention, these and other objects include a first inlet configured to generate and dilute an aerosol and accommodate a first volumetric flow rate of pressurized gas; A second inlet configured to receive a two volume flow rate, a third inlet configured to receive a fluid to be converted to aerosol, and connected to the first and third inlets; a nozzle having a nozzle orifice (orifice) for outputting one aerosol, a first diluent gas flow partitioner having a first opening set through the first flow partitioner, apart from the first dilution gas flow partitioner opened is disposed, and a second dilution gas flow partitioner having a second opening set through the second flow partitioner, wherein the nozzle orifice, said second dilution gas flow per It is achieved by the present invention using a flow conditioner that is placed in close proximity to the tensioner.

  In accordance with the fifth aspect of the present invention, these and other objects are concentrators for increasing particle concentration in an aerosol stream, which contain a first aerosol volumetric flow rate and are configured to a first cumulative cross-sectional size. In addition, a plurality of entry openings extending in the radial direction of the slit shape, and a slit shape configured to deliver the first aerosol volume flow rate and have a second cumulative cross-sectional size smaller than the first cumulative cross-sectional size A sculptured acceleration plate having a plurality of radially extending acceleration plate exit apertures, and a second aerosol volumetric flow with a high particle concentration and configured to a third cumulative cross-sectional size; A plurality of deceleration plate input openings extending in the radial direction in a slit shape, and a fourth cumulative section that delivers the second aerosol volume flow rate and is larger than the third cumulative cross-sectional size A sculptured deceleration plate having a slit shape and extending radially in a slit shape, the sculptured deceleration plate comprising a plurality of sculptured acceleration channels, Extending between the acceleration plate input openings and the plurality of acceleration plate outlet openings, and a plurality of sculpted deceleration channels extending between the plurality of deceleration plate input openings and the plurality of deceleration plate outlet openings, The plurality of acceleration plate exit openings are spaced from the base surface on the exit side of the acceleration plate, and the plurality of engraved deceleration channel input openings are spaced from the base surface on the input side of the deceleration plate. The gap is provided between the acceleration plate base surface and the deceleration plate base surface, and the gap is Configured to deliver a third volumetric flow rate of particle concentration, wherein the plurality of acceleration plate outlet openings substantially overlap the plurality of deceleration plate input openings, the plurality of openings being in the middle of each acceleration and deceleration plate The plurality of apertures can be achieved by the present invention using a concentrator that includes at least two different length apertures that extend radially from a location near the outer edge of each acceleration plate and deceleration plate. It is done.

FIG. 1 shows the elements for generating a dry warm dilution gas and delivering it to the flow conditioner, and for heating the hot gas and delivering it to the nozzle holder and backflow tube. A perspective view is shown. FIG. 2A shows a perspective view of a first embodiment of a nozzle holder. FIG. 2B shows a longitudinal sectional view of the nozzle holder shown in FIG. 2A. FIG. 2C shows a side view of the nozzle holder shown in FIG. 2A. FIG. 2D shows a longitudinal cross-sectional view of a second embodiment of the nozzle holder in which the knob on the nozzle holder described in FIGS. 2A, 2B and 2C has been replaced with a cartridge containing liquid to be aerosolized. FIG. 3A is an exploded perspective view of the nozzle body and an annulus that exactly fits the stem protruding from the nozzle body. FIG. 3B shows a partial longitudinal sectional view of the nozzle, designated T in FIG. 3D, within the neck of the barrel of the nozzle holder. FIG. 3C shows a longitudinal cross-sectional view of the nozzle holder indicated by RR in FIG. 3E. FIG. 3D shows a longitudinal section view of the nozzle holder that is rotated 90 degrees compared to FIG. 3C and coincides with the side view of FIG. 3F of the longitudinal section view indicated by PP. FIG. 3E shows a front end view of the nozzle and barrel and the RR cross section of FIG. 3C. 3F shows a side view of the nozzle holder illustrating the PP cross section shown in FIG. 3D. FIG. 4A shows an exploded perspective view of the flow conditioner manifold and nozzle holder, and the relationship of the nozzle holder and flow conditioner insertion into the manifold. FIG. 4B illustrates the cross-sectional view shown in FIG. 4C as well as showing a front view of the flow conditioner. 4C shows an exploded longitudinal cross-sectional view, indicated by YY in FIG. 4B of the flow conditioner as illustrated in FIG. 4B, and a cross-sectional view of the nozzle holder at the opening of the container to be inserted. Figure 5 A is a test and H-H cross-sectional view also shown as a flow conditioning manifold and flow partitioner 5B, the shows the relationship between the flow adjusting manifold and vaporization chamber walls. The compressed gas flow path to the nozzle holder and backflow tube is shown. 5B illustrates a cross-sectional view of the flow conditioner shown in FIG. 5A as well as showing a front view of the flow conditioner shown in FIG. 5A. FIG. 5C shows an exploded perspective view of the flow conditioner. It shows the details of the flow conditioner and the backflow tube. FIG. 5D shows a cross-sectional view (F-F) shown in FIG. 5E of the flow conditioner along with the evaporation chamber, the accelerator plate of the virtual impactor aerosol concentrator, and the interrelationship of these elements of the device. Longitudinal section). FIG. 5E shows a cross-sectional view of the concentrator, illustrating a longitudinal cross-sectional view of the flow conditioner, evaporation chamber and concentrator acceleration plate shown in FIGS. 5D and 5F. FIG. 5F shows a longitudinal cross-sectional view, indicated by JJ in FIG. 5E, of the flow conditioner, evaporation chamber and concentrator acceleration plate shown in FIG. 5E. FIG. 6A shows a flow conditioner, evaporation chamber, concentrator, output cone, infrared lamp and reflector—depicted in FIG. 6B showing the interrelationship between these elements—indicated by JJ in FIG. 6B. FIG. FIG. 6B shows a rear view of the flow conditioner, evaporation chamber, concentrator, output cone, infrared lamp and reflector shown in FIG. 6A. FIG. 6C shows a bottom perspective view of the elements listed in FIG. 6A showing the positional relationship with each other. FIG. 6D shows a top perspective view of the elements listed in FIG. 6A showing their positional relationship. FIG. 7A illustrates the difference between the nozzle length and the sculptured structure, and a female rugged cross placed centrally for accurate alignment of the acceleration plate and the cross raised above the deceleration plate. The perspective view of the output side of the acceleration plate which performs is shown. FIG. 7B shows a perspective view of the input side of the reduction plate showing the difference between the reduction nozzle length and the sculpted structure and the male raised cross for accurate alignment of the reduction plate and the acceleration plate. FIG. 7C shows a longitudinal cross-sectional view, shown as a KK cross-section in FIG. 7D, of the evaporation chamber, concentrator and aerosol output cone—shown in FIG. 7D showing the interrelationship of these elements. FIG. 7D shows a cross-sectional side view of the evaporation chamber, concentrator, and output cone illustrated in FIG. 7C. FIG. 7E shows a rear cross-sectional view of the evaporation chamber, concentrator, and output cone illustrated in FIG. 7F. FIG. 7F shows a longitudinal cross-sectional view, designated H-H, in FIG. 7E of the evaporation chamber, concentrator, and output cone.

(Detailed Description of the Invention)
According to a preferred embodiment of the present invention, liquid is evaporated from the second aerosol to generate a third aerosol comprising dry powder, gas and vapor. However, the aerosol may include residual liquid aerosol in addition to the dry particles.

  According to another preferred embodiment of the invention, the infrared radiation is applied to the evaporation of the liquid. However, it is also possible to dry the aerosol by utilizing other forms of heat transfer, such as convection or a combination of radiation and convection.

  According to another preferred embodiment of the present invention, the pre-heating of the first volumetric flow rate of the pressurized gas is via a gap between the inner cylindrical wall of the tube and the outer cylindrical wall of the tapered elongated infrared bulb. Deriving a first volume flow. This has proven very effective for efficient heat transfer in combination with low flow resistance, especially when the infrared bulb is tapered in the direction of flow. However, it is possible to use other forms of preheating, for example heating of the gas spray tube from the outside.

  According to another preferred embodiment of the present invention, the temperature of the first volume flow preheating is measured and controlled by a controller that controls the power supply to the elongated infrared bulb. However, since the volumetric flow rate is known and therefore the parameters related to heat transfer are also known, open loop control is also possible in which it is carried out without measuring the temperature.

  According to another preferred embodiment of the present invention, the preheating of the second volume flow of the dilution gas is performed via the gap between the inner cylindrical wall of the tube and the outer cylindrical wall of the tapered elongated infrared bulb. Including directing two volume flow rates. In a similar manner as preheating the second volume flow, other forms of heat transfer are possible.

  According to another preferred embodiment of the present invention, the temperature of the second volume flow preheating is measured and controlled by a second controller that controls the power supply to the elongated infrared bulb. Again, both open and closed loop control is possible, and in open loop control the control may be implemented without measuring temperature.

  According to another desirable embodiment of the present invention, the first volume flow rate of the pressurized gas is different from the first partial pressurized gas volume flow rate fed into the nozzle for generating the concentrated first aerosol. The second partial pressurized gas volume flow rate supplied as the fourth volume flow rate in the tube is divided into the second partial volume flow rate, the second partial volume flow rate is discharged through the backflow tube outlet port and the discharge direction related to the concentrated first aerosol Is discharged in the opposite direction. Instead of dividing the first volumetric flow rate, it is also possible to supply a fourth volumetric flow rate that is discharged from the separation source, for example from a pressurized vessel or a compressor, via a backflow tube.

  According to another preferred embodiment of the present invention, the second volumetric flow rate of the dilution gas is such that the first partial dilution gas volumetric flow rate supplied through the central portion of the flow partitioner and the flow partitioner And a second partial dilution gas volume flow rate supplied through the peripheral portion. This helps to form the desired shape of the aerosol plume in the middle, then mixed with the second partial dilution gas volume flow, and also helps to avoid aerosol deposition on any wall of the device. However, an alternative means of realizing a second volume flow that is not divided.

  According to another preferred embodiment of the invention, the second volume flow of the dilution gas is generated by means of a blower or a fan. This has the advantage of a low cost and a very small structure. The blower can generate a high volume flow at a relatively low pressure. However, in the alternative, any other dilution gas source may be used, for example a compressor or a pressurized gas container such as a bottle.

  According to other desirable embodiments of the present invention, the second volumetric flow rate of the dilution gas may be dried upstream of the blower in a drying chamber containing a disposable desiccant. This facilitates device operation even in relatively high humidity environments. However, by appropriately sizing heat transfer and dilution air volume flow, such desiccants may not be necessary even in high humidity environments.

  According to another preferred embodiment of the present invention, the partial second aerosol may be generated by mixing the first aerosol with the first partial dilution gas volume flow.

  According to another preferred embodiment of the present invention, a concentrated dry powder fourth aerosol is generated that is only 10-30% of the volume flow rate of the third aerosol but contains at least 75% of the dry particles of the third aerosol. By doing so, the third aerosol is concentrated. This allows the use of a high volume flow rate of the diluent gas, thus allowing rapid evaporation of the aerosol, and only a low volume flow rate where the concentrated dry powder aerosol can be easily inhaled by the patient. However, it contains most of the dry powder. This also allows the use of a low vapor pressure gas, for example air, but nevertheless a high evaporation rate can be achieved.

  According to another preferred embodiment of the present invention, the deceleration vortex is damped in the concentrated dry powder fourth aerosol in the vortex damping chamber. This allows for a quicker and easier restriction of the suction volume flow while generating a uniform distribution of particles within the suction volume flow. According to another preferred embodiment of the present invention, the concentrated dry powder fourth aerosol is limited in a cone-shaped collector prior to outputting the fourth aerosol to the patient for inhalation by the patient. The Desirably, the vortex damping chamber is in the direction of flow beyond a certain distance prior to restricting the flow towards the outlet connected to the mouthpiece or mask that allows the patient to inhale the restricted flow. It is desirable to extend.

  According to another preferred embodiment of the invention, the fourth volume flow of gas is preheated. If the fourth volume flow is generated by being separated from the first volume flow, such preheating may be achieved by preheating the first volume flow prior to separation. However, alternative means of heating the fourth volume flow separately, such as similar forms such as the first and second volume flows described above, are possible. Depending on how large the fourth volume flow rate is, it is possible to dispense with heating of the fourth volume flow rate.

  According to another preferred embodiment of the nozzle of the present invention, the nozzle comprises a cylindrical stem having an outer stem wall having an outer stem diameter, and an annulus having an annulus hole wall having an inner annulus diameter slightly larger than the outer stem diameter; The cylindrical stem extends through the annulus hole and includes a wet cone-shaped gas outlet channel, and the annular fluid outlet port is formed by an annular gap between the annulus hole wall and the outer stem wall. . Desirably, the difference between the internal annulus diameter and the external stem diameter is 0.006-0.8 mm, resulting in an annular gap width of 0.003-0.4 mm. This makes it possible to benefit from the capillary force for the fluid to move from the nozzle to the location where the fluid is aerosolized.

  According to another preferred embodiment of the nozzle of the present invention, the annulus has a front surface extending substantially perpendicular to the annular fluid outlet port. This annulus is precisely manufactured to the internal diameter required to facilitate assembly and maintain a slight tolerance between the annulus hole and stem so that the nozzle can benefit from capillary forces. Therefore, the annulus can be manufactured separately from the remaining part of the nozzle. However, as an alternative, it is also possible to integrate this part as an integral part of the nozzle holder or barrel.

According to another preferred embodiment of a nozzle of the present invention, annular scan wall holes and other stem wall despite wetted readily by the fluid, the front surface of the annulus is hydrophobic. This is advantageous for directing the fluid to the location where it is converted to an aerosol. However, in the alternative, a standard surface is also possible and the pressure differential and so that the induction of the fluid into the location where it is aerosolized does not require a particularly easily wet or hydrophobic surface. It may function simply by capillary action.

  According to another preferred embodiment of the nozzle of the present invention, the diameter of the cone base of the wet cone-shaped gas outlet channel is such that the stem ends within a sharp annular edge at the cone base of the wet cone-shaped gas outlet channel. , Substantially equal to the entire outer stem diameter. This is due to both capillary forces and pressure differences, through the gap between the stem and annulus, quickly over the edge and into the cone, where it is aerosolized near the top of the cone inside the cone, i.e. within the stem. Enable. Easy wet / hydrophobic surfaces support this fluid flow. However, in the alternative, the edges need not be sharp so that a cone that does not occupy the full diameter of the stem is also considered a possible structure.

  According to another preferred embodiment of the nozzle of the present invention, the cone-shaped gas outlet channel has an angular range of 15 to 80 degrees. The ideal cone shape varies with a number of different parameters, such as the flow rate, the size of the gap between the annulus and the stem, and the speed of the gas stream that aerosolizes the fluid. A particularly advantageous angle for the cone is 45 degrees. Preferably, the cone base has a diameter of 1 to 2 mm and the nozzle gas supply channel has a diameter of 0.05 mm to 1 mm.

  According to another preferred embodiment of the nozzle holder of the present invention, the nozzle body includes a cylindrical nozzle body base having an outer nozzle body base diameter, and the annular fluid supply channel is formed between the outer cylindrical nozzle body base surface and the cylindrical shape. Formed between the wall of the barrel hole. Although the gas flow is directed in a centrally located channel, it transports fluid near the periphery of the barrel forward in the annular more peripheral channel. However, other alternative configurations of fluid channels are possible, for example a longitudinal fluid channel that runs parallel to the center of the barrel.

  According to another preferred embodiment of the nozzle holder of the present invention, the barrel is connected to the nozzle gas supply channel and supplies a plurality of radii for supplying gas to a central gas supply channel having a diameter several times larger than the diameter of the nozzle gas supply channel. Directional gas supply channel. This allows an efficient radial gas supply while the gas flows parallel to the central channel of the barrel. However, other structures of gas supply are possible, for example an axial gas supply in a direction parallel to the fluid supply.

  According to another preferred embodiment of the nozzle holder of the present invention, the nozzle holder contacts the first end of the nozzle holder and has a disposable part having a knob for inserting / removing the nozzle holder into / from the aerosol generator container. Designed as This makes it possible to prevent pre-packaging of inhalable medicaments and misuse such as dosage mistakes. However, alternative means are also possible for the supply of fluid containing the drug from the bulk container, for example clinical use.

  According to another preferred embodiment of the nozzle holder of the present invention, the barrel has an outer cylindrical surface configured to fit within the aerosol generator container. For this purpose, the barrel size may be sized so that only a specific prepackaged nozzle holder fits the container. Especially for home use, such a pre-package structure is highly preferred to avoid misuse and unintentional use of wrong drugs. Desirably, the nozzle holder and fluid cartridge are pre-assembled as a single-use unit.

  According to another preferred embodiment of the nozzle holder of the present invention, the nozzle holder fluid injection port is a Luer fitting configured to receive a disposable fluid cartridge. However, in the alternative, any other fluid tight fitting works.

  According to a preferred embodiment of the present invention, the nozzle is an integral part of a detachable nozzle holder that is detachably attached to the flow conditioner. This allows the replacement of units with nozzles and nozzle holders for each delivery session to avoid contamination problems and unintentional delivery of drug residues by the patient.

  According to another preferred embodiment of the present invention, a removal nozzle holder with an essential nozzle is retained in a flow conditioner in a centering vessel having a length to width ratio greater than 1. Is a disposable part. This has the advantage that the nozzle is exactly centered as intended, so that a symmetrical plume of the aerosol can be distributed. In addition, it is possible to control so that only specific nozzles are inserted into specific containers, so that the use of wrong nozzles is avoided. This may be particularly important when the drug is prepackaged as a disposable joint in a container where the disposable nozzle is connected to the nozzle holder. However, other centering structures with a width ratio longer or shorter than 1 are possible, or alternative centering structures that allow precise orientation of the other nozzles.

  According to another preferred embodiment of the present invention, the container is an elongated cylindrical hole extending beyond the first flow partitioner, and the nozzle holder is a cylindrical portion having an outer cylindrical surface and seals. In this case, it is inserted into an elongated cylindrical hole having a plurality of ring-shaped grooves corresponding to a plurality of O-rings in contact with the outer cylindrical surface of the nozzle holder. Desirably, at least two spaced apart O-rings and a circumferential groove are provided in an elongated cylindrical hole between the two O-rings to provide a first volumetric flow rate of pressurized gas. At least a portion is directed through a groove into a plurality of openings in the nozzle holder connected to a nozzle holder pressurized gas channel that supplies the nozzle with pressurized gas for forming a first aerosol. Such an arrangement has the advantage that a gas, for example air, can be supplied in the radial direction, leaving more room for insertion or removal of the nozzle holder in the axial direction without any obstruction by the gas supply. Furthermore, it allows unobstructed access in the axial direction for connection to a fluid supply or for insertion into an integrated device including a nozzle, nozzle holder and fluid container. However, alternative arrangements are also possible, for example an axial or inclined gas supply.

  According to another preferred embodiment of the present invention, the first flow divider connected to the first inlet has a first partial volume supplied with a first volume flow of pressurized gas to a removable nozzle holder. A second partial volume directed into the backflow tube having a backflow tube outlet port that is substantially coaxial with the nozzle holder with the essential nozzle and with the essential nozzle, and directed in the opposite direction of the nozzle to generate backflow Divide the flow rate. The advantage of this configuration is that the initial aerosol formed by the first partial volume flow is suppressed by the second partial volume flow. Desirably, the first volume flow may be preheated before the first volume flow is divided into the first and second partial volume flows. This reduces the number of heaters. However, other configurations are possible, i.e. a completely separate source connected to the nozzle and the backflow tube, respectively, which can heat either or both of the volumetric flow rates or neither.

  According to another preferred embodiment of the present invention, the second flow divider directs the second volume flow of dilution gas to the central region of the second dilution gas flow partitioner through the second dilution gas flow partitioner. The remaining second through the space between the first partial dilution gas volume flow, the first dilution gas flow partitioner, and the second dilution gas flow partitioner through the second dilution gas flow partitioner near the peripheral region. A partial dilution gas volume flow rate is provided in the space between the first dilution gas flow partitioner and the second dilution gas flow partitioner for division into the partial dilution gas volume flow rate. This arrangement has the advantage of providing a good initial mixing phenomenon, and optionally an aerosol suppressed by dilution air. The flow in the more peripheral region realizes that the constrained aerosol plume is not only mixed to produce the desired flow profile, but also provides additional control of this flow profile. This is desirable in practice to avoid deposition of aerosols on the flow conditioner or evaporation chamber walls. However, other configurations are possible in which the dilution gas flow is not divided into two partial dilution air flows in the central and peripheral regions. Several different parameters, such as the flow rate, the amount of liquid aerosolized per minute, may determine whether division into a central and peripheral flow is useful.

  According to another preferred embodiment of the present invention, the central region of the second dilution gas flow partitioner is on the side of the second dilution gas flow partitioner from which the second partial volume flow of dilution gas exits the second flow partitioner. It has a depressed concave shape. This structure has been found to help avoid aerosol deposition on the second diluent gas flow partitioner. However, depending on the parameters, alternative structures such as a planar or convex shape on the front surface of the second dilution gas flow partitioner are possible.

  According to another preferred embodiment of the present invention, the outer periphery of the central region of the second dilution gas flow partitioner protrudes beyond the peripheral region of the second flow partitioner, and the flow partitioner's during assembly and disassembly A rim is provided to facilitate positioning and removal. Desirably, the rim comprises a cylindrical surface having a circular retaining groove. Such a structure is extremely quick with the concave shape described above, which allows the rim in the central region of the second diluent gas flow partitioner to be lifted over the peripheral region of the second diluent gas flow partitioner. Accomplished. In the alternative, other configurations for introducing and removing the second flow partitioner are possible, such as discrete protrusions spaced apart from each other.

  According to another preferred embodiment of the present invention, the second flow divider is ring-shaped and extends through the space between the first dilution gas flow partitioner and the second dilution gas flow partitioner, A plurality of radial openings are provided through which the first partial dilution gas volume flow partitioner towards the central region of the dilution gas flow partitioner passes. Desirably, the first and second diluent gas flow partitioners and the second flow divider form one of a pre-assembled assembly group and an integral component. This enables a structural robust structure, and the ring-shaped divider can have a spacer function between the first and second flow partitioners, or the first flow partitioner, the second flow partitioner. And the entire group including the ring-shaped divider can be integrally formed as a single component. The cumulative size of the plurality of holes provided in the divider determines how much of the partially diluted air flow goes to the center. In alternative means, other configurations, such as columns spaced apart between the first and second flow partitioners, or any form or shape that can divide the desired amount of flow towards the center of the second flow partitioner. Channels are also possible.

  According to another preferred embodiment of the present invention, the outer periphery of the first dilution gas flow partitioner enters the space between the first and second dilution gas flow partitioners through the first dilution gas flow partitioner. Formed by a plurality of merlons arranged circumferentially by a plurality of slots through which a second volume flow of dilution gas passes. Preferably, the first dilution gas flow partitioner is inserted into a cylindrical housing having an inner cylindrical wall, and the plurality of melons are surrounded by the plurality of slots, the plurality of melons and the cylindrical wall around the second flow partitioner. A close fit with the housing so as to be close to or in contact with the inner wall so that a plurality of openings are defined along. The space between the first and second dilution gas flow partitioners may function as a pressure equalization chamber. In addition, a plurality of spaced slots make the flow even. However, alternative structures are possible, for example, individual holes spaced along the circumference of the first diluent gas flow partitioner, instead of a plurality of melons and grooves.

  According to another preferred embodiment of the invention, the backflow tube comprises a substantially straight injection end that extends substantially parallel to the nozzle holder, passes through the first and second flow partitioners, and exits the backflow tube. End at the outer end with a 180 degree bend leading to the port. Desirably, the substantially straight injection end may comprise a positioning plate insertable into the positioning slot. With these measures, the outlet port is precisely aligned with the nozzle so that a symmetrical plume of aerosol is formed around the nozzle.

  According to another preferred embodiment of the present invention, the first injection port and the second injection port each pressurize to preheat at least one of a first volume flow of pressurized gas and a second volume flow of dilution gas. Connected to at least one of each pressurized gas and dilution gas heating chamber having gas and dilution gas heaters. The heating of the various streams is individually controlled as desired. However, depending on various parameters, such as the amount of liquid evaporated per minute, the gas used for evaporation, the liquid to be evaporated, all or any desired range of evaporation can be achieved without preheating any gas volume flow. It can also be achieved.

According to another preferred embodiment of the present invention, the plurality of dilution gas heaters are elongated infrared bulbs having tapered ends, and each heating chamber is a tube having an individual internal tube wall, and a dilution gas The second volumetric flow rate is guided through the gap between each infrared bulb and the inner tube wall, and the flow resistance of the second flow rate of this dilution gas is 200 liters / minute and is on the order of 13 mmH ₂ O. It is. This turns out to be a very efficient heater while low flow resistance is provided at the same time. However, other heating forms are possible, for example electrical heating by convection by enclosing the gas supply tube with an electric resistance heating coil.

  According to another preferred embodiment of the present invention, the blower has a dilution gas heating connected to the second injection port for supplying a second volume flow of dilution gas through the heating chamber into the second injection port. Provided upstream of the chamber. Such a blower can provide a high volume flow of dilution air. However, alternative gas sources such as compressors and gas bottles are possible.

According to another preferred embodiment of the present invention, the second volumetric flow rate of the dilution gas is 100 to 200 liters / minute, and the pressure loss across the flow conditioner and opposite the second inlet is 200 liters / minute. Minutes, on the order of 2 inches H ₂ O. This low pressure drop allows a high power compressor to be substituted by a simple blower that occupies only a small amount of compressor size and power consumption.

  According to another preferred embodiment of the present invention, the first group of the plurality of longer slit-shaped openings extends from a position near the center to a position near the outer periphery of the acceleration plate and the deceleration plate, and more The second group of the plurality of short slit-shaped openings extends from a position spaced from the center toward a position close to the outer periphery. This results in the slit-shaped openings having at least two different lengths, i.e. from their respective positions near the center of the acceleration plate and near the center of the deceleration plate. One length that extends all the way to the perimeter, and the other set of openings is shorter, extending from this offset position to the perimeter from a position that is only radially offset relative to the center. This slit distribution achieves that the cumulative aperture surface near the periphery is as close to the center of the acceleration and deceleration plates. This is the same as the cumulative width of the radial channel formed by the gap between the base surface on the exit side of the accelerator plate and the base surface on the input side of the deceleration plate while keeping the total flow resistance of the concentrator low. It is a measure that makes it possible to become. Such radial discharge channels extend between the engraved portions that provide acceleration and deceleration channels. However, in the alternative, not all channels may extend all the way to the perimeter. In addition to slit-shaped openings, it is also possible to provide other shaped openings, for example circular or triangular openings. A plurality of slit-shaped openings have been found to be particularly effective in providing an unobstructed radial discharge channel, and the use of different lengths as described above, for each substantially uniform plate surface area. It is particularly effective in maintaining an open surface that exceeds the overall circular acceleration and deceleration plates.

  According to another preferred embodiment of the present invention, the third group of intermediate slit-shaped openings is a length between the first and second groups of longer and shorter openings, respectively. , Extending from a position spaced from the center toward a position close to the outer periphery, and a distance from the center extending from a position shorter than the distance of the second group of the plurality of slit-shaped openings. This is another desirable variation, in which case it includes a third group of openings, even more even opening surfaces compared to the projected plate surface. To achieve a distribution of.

  According to another preferred embodiment of the present invention, the first group of slit-shaped openings of the plurality of openings includes four slit-shaped openings arranged on the circumference at an angle of 90 degrees to each other, The third group of the plurality of slit-shaped openings is on the circumference at an angle of 90 degrees with each other and at an angle of 45 degrees with respect to the adjacent slit-shaped openings of the first group of the plurality of slit-shaped openings. And the second group of the plurality of slit-shaped openings is at an angle of 45 degrees to each other and is adjacent to the first and third groups of the plurality of slit-shaped openings, respectively. It includes eight slit-shaped openings arranged on the circumference at an angle of 22.5 degrees with respect to the slit-shaped openings. While a uniform distribution of radial channels is achieved to enable low flow resistance leakage of the exhaust volume flow as exhaust gas, this angular distribution is in addition, compared to the projected plate surface, opening Achieve the goal of uniform surface distribution.

  According to another preferred embodiment of the present invention, the acceleration and deceleration plates are arranged with respect to each other in the radial and circumferential directions so that the acceleration and deceleration plates are arranged parallel to each other and spaced apart from each other by a side gap. For the alignment of the connector, the connector is one of the raised locator of the deceleration plate and the corresponding uneven container of the acceleration plate, or the raised locator of the acceleration plate and the corresponding one of the deceleration plate. The alignment includes an angular orientation in the circumferential direction, configured to have one of the concave and convex containers, such that the acceleration plate outlet opening is substantially aligned with the deceleration plate input opening. For minimum flow resistance, it is very important that the exit opening of the acceleration plate overlaps exactly with the exit opening of the deceleration plate. This requires precise alignment of the acceleration and deceleration plates in the radial and circumferential (angular) directions. In addition, the raised locator-uneven container-joint ensures that the gap between the acceleration plate and the deceleration plate, especially between the outlet opening of the acceleration plate and the input opening of the deceleration plate, is accurate for all outlet openings-input openings-pairs. This is useful in positioning the acceleration plate and the deceleration plate exactly parallel to each other. However, this parallelism may be established alone or in addition to the locator-container-joint by means of a spigot on the periphery of the acceleration and deceleration plates.

  According to another preferred embodiment of the present invention, the raised locator and the corresponding rugged container are cross-shaped. Other shapes such as squares, rectangles or triangles are possible, but the cruciform has so much space that can be used for multiple split-shaped apertures to achieve low flow resistance. Without occupying it allows a particularly precise orientation of the acceleration and deceleration plates with respect to each other.

  According to another preferred embodiment of the present invention, the slit-shaped acceleration plate outlet opening is 0.4-1.6 mm wide, the deceleration plate input opening is 0.6-2 mm wide, The accumulated length is 10-25 cm and the gap between the acceleration plate base surface and the deceleration plate base surface is 0.8-2 cm. Of course, other dimensions are also acceptable. However, the interrelationship of the various dimensions optimizes the objective of achieving low flow resistance, while at the same time achieving high efficiency aerosol particle concentration, eg, at low volume flow rates that can be rapidly inhaled by the patient. Optimize this goal. Desirably, the second volume flow comprises 10-20% of the first volume flow and the third volume flow comprises 80-90% of the first volume flow. Desirably, the concentrator is from a concentration efficiency such that 85% of the first volume flow of particles is included in the second volume flow and the third volume flow includes only 15% of the particles from the first volume flow. Become. However, in some situations, lower efficiencies, such as 70% efficiency, may be acceptable. Acceptable efficiency can be driven by various parameters, such as drug cost or acceptable delivery rates. Similarly, the percentage of volumetric flow divided into useful volumetric flow that can be inhaled by the patient and excretory volumetric flow may vary over a relatively wide range.

According to another preferred embodiment of the present invention, the assembled acceleration plate and deceleration plate are surrounded by a cowling having a radial opening through which a third volume flow is directed to the outlet port. This provides a further means for low flow resistance discharge of the exhaust volume flow. Desirably, the flow pressure drop across all the concentrators is 1 mmH ₂ O or less with a gas flow rate up to 250 liters / minute with an output aerosol flow of 40 liters / minute.

  According to another preferred embodiment of the present invention, at least some of the plurality of deceleration channels gradually become wider from the input opening in the direction of the exit opening of the deceleration plate, and the walls of the deceleration channel are linear, convex or It consists of one of the parabolic shapes. Similarly, at least some of the plurality of acceleration channels gradually narrow from the input opening in the direction of the exit opening of the deceleration plate, and the walls of the acceleration channel consist of one of a linear shape, a convex shape or a parabolic shape. In particular, the parabolic shape has been found to provide low flow resistance.

  According to another preferred embodiment of the invention, the vortex damping chamber is configured to dampen the deceleration vortex before the aerosol is compressed into the output port by the cone-shaped collector. Desirably, the cone-shaped collector has a parabolic wall. Useful volumetric flow compression is not necessarily required, but this configuration, in particular, exceeds the length the vortex damping chamber is in the direction of flow, e.g., equal to about half the diameter of the deceleration plate, When extended, there is the advantage of equalizing particle distribution and reduced deposits. This measure also reduces flow resistance. However, in an alternative arrangement, it is possible to provide no flow restriction and provide flow directly from the exit of the deceleration plate to the destination, for example in the suction mask.

Here, the present disclosure describes how a relatively high volume (up to 300 l / min) of low pressure aerosol is concentrated. The plurality of slits are arranged radially so that the exhaust gas is passively delivered between the slits in the radial direction. Such a configuration has many advantages. That is,
(A) Dilution gas is supplied by a small (2 inch x 2 inch x 1 inch) gas blower or fan.
(B) The device does not require an airtight high pressure seal, thus allowing easy assembly and disassembly for cleaning and maintenance.
(C) Since the exhaust gas does not require a negative pressure source, it is delivered at atmospheric pressure.
(D) The local counter-current jet is structurally stable with a precisely reproducible coaxial alignment.
(E) locally heated jets and backflow gases, in combination with local infrared irradiation, in addition to enhancing the device's ability to produce particles of density less than 1 gram / cc, reducing wall loss; Provide rapid drying of aerosols leading to increased efficiency.

  Devices that generate aerosols from liquids in refillable containers have problems with maintaining cleanliness. Devices used for various inhalations may be unpredictable about nozzle or orifice clogging or may have reduced output. This is a serious problem, especially when large molecules such as proteins, surfactants, as well as other large molecules are aerosolized. These problems are overcome in the present disclosure through the integration of replaceable or disposable cartridges into an integral single-pass nozzle.

In aerosol generator of the present invention, for purposes of illustration of the aerosol generator assembly group below, immediately Chi, nozzle and nozzle holder with container, flow conditioner with flow partitioner, reflux tube and evaporation chamber, Virtual impactors, vortex damping chambers, and aerosol delivery cones must be identified. These assembly groups are responsible for the generation of concentrated dry aerosols from aqueous (or high vapor pressure solvent) solutions or suspensions of materials so that the resulting aerosol becomes a dry concentrated aerosol containing the original solute or suspended material. Mutually affects the formation of portable small devices for In particular, it relates to procedures that demonstrate that this can be achieved in practical small portable devices. Furthermore, this device, which allows for very rapid evaporation of the solvent near the base of the aerosol plume, facilitates the generation of protein particles with a density of less than one.

  A major configuration limitation throughout the embodiments of the present invention is to fully operate the device with a diluent gas slightly above atmospheric pressure. This has two powerful advantages over a portable concentrated aerosol delivery system for patient use. First, very small fans or blowers for limited pressure heads are incorporated into the size, weight and noise considerations. Second, the use of low pressure mounting components allows easy assembly and disassembly for cleaning and maintenance.

  Another structural criterion is to supply heated compressed gas to the nozzle and backflow tube for the effect of evaporating the solvent as soon as possible. Another structural standard is to incorporate a replaceable removable nozzle holder and nozzle. This increases the commercial adaptability and functionality of the device. This flow conditioner is compact and has a very low resistance to gas flow.

  The device features (a) a small two-stage flow conditioner with an indispensable container for receiving a replaceable nozzle holder, (b) a backflow compressed gas divider and a backflow tube, (c) low gas flow resistance. And a temperature inertia gas heater, (d) near infrared irradiation, (e) for particles larger than 0.5 microns, low resistance, high efficiency aerosol concentrator, (f) low resistance extraction gas filtering function, and (g) Includes an aerodynamically designed collection “cone” for collecting concentrated output aerosol. The instrument version of this device can be used to adjust the parameters of the aerosol drying process for a particular solute (suspension) / solvent solution delivered as a respiratory aerosol. The present invention can be used for drug delivery that does not require the use of additives where re-aerosolization of the powder drug is often required. Bio-therapeutics containing proteins can be delivered directly to the patient. The generated particles may have a particle density of less than 1 or a tap density of less than 0.04.

The compressed gas is supplied to the pressure regulator via a quick disconnect. The compressed gas from the adjuster passes through a heater and a port on the flow conditioner manifold. Within the manifold, the flow has two paths: a. Towards the nozzle holder and towards the aerosol generator nozzle, b. The outlet port is redirected to a backflow tube that is aligned with the same axis as the nozzle. The low pressure gas source is provided by a small blower at a very high flow rate (100 to 300 liters / minute). (Alternatively, a source of pressurized gas may be used.) This gas passes through the heater and enters a port on the manifold of the two-stage flow conditioner. This flow conditioner ensures a uniform flow in the combined Pyrex® or quartz evaporation chamber. Gas from the two-stage flow conditioner enters this evaporation chamber. Infrared radiation from the infrared lamp and the reflector adjacent to the evaporation chamber pass through the chamber, is reflected by the second focal reflector, and is sent to the opposite side of the chamber. This evaporation chamber is coupled to a virtual impactor aerosol concentrator. The gas enters through the acceleration slit nozzle of the acceleration nozzle plate. A very small amount of gas containing most of the particles exits the concentrator through a collection deceleration nozzle in a virtual impaction plate. These deceleration nozzles are precisely aligned with the acceleration nozzles. The resulting aerosol from the deceleration nozzle loses most of its kinetic energy during vortex formation in a damping chamber connected to the concentrator outlet. Then, the aerosol flows through the aerosol collection cone with a tape over path, aerosol exits from the end. The main part of the gas flow exits the gap between the acceleration nozzle and the deceleration nozzle in each of the acceleration nozzle plate and the deceleration nozzle plate. This exhaust gas flows to an optional filter in the plenum to remove residual suspended particles in the exhaust gas. Alternatively, for use in locations where a sufficient supply of compressed gas is available, the quick disconnect for compressed gas is via a T-shaped fitting, two pressure regulators, for high pressure gas, Coupled to, for low pressure gas. The high pressure regulator is coupled to the manifold of the two stage flow conditioner via a gas heater as described above. This compressed gas is redirected in two paths as described above. The low pressure regulator is connected to the dilution gas heater as described above and then to the flow conditioner.

The compressed gas provides energy for the aerosolizing nozzle and the backflow gas. The backflow gas flows coaxially and in the opposite direction to the aerosol plume formed by the nozzle so that the backflow gas suppresses and dilutes the plume. In the desired use, the high pressure gas is heated to 150 degrees. This temperature is adjusted using a thermocouple in the compressed gas stream upstream from the heater using the associated PID controller. This heated compressed gas is delivered to the flow conditioner manifold via a quick disconnect. One stream travels through a small orifice to the backflow tube. The small orifice diameter defines the gas flow rate in the backflow tube. This flow rate is typically about the same or slightly higher than the gas flow rate through the nozzle. The other flow proceeds to the annulus surrounding the cylindrical container in the flow conditioner. The nozzle holder port is aligned with this annulus, so that gas flows through the nozzle holder input port , through the two conductive channels, to the small pressure equalization chamber and to the nozzle. The fluid is delivered to the nozzle via the central channel. The external pump provides a fluid flow rate of 0.1 to 5 ml / min, depending on the application. Aerosols are generated by the interaction of compressed gas and fluid. The aerosol generated in this way is suppressed by the jet of gas from the backflow tube. Warm dilution gas from the flow conditioner enhances liquid evaporation and carries the particles through the evaporation chamber towards the aerosol concentrator. Infrared illumination is provided by an infrared lamp and a corresponding reflector on the opposite side of the chamber increases the evaporation of liquid from the particles. The particles are concentrated by passing through a virtual impactor and delivered to the output via the output cone. The output flow is slightly positive and is moderated by a device or person connected to the output.

Alternatively, if a sufficient supply of high pressure is possible, the compressed gas enters the external quick disconnect fitting and is split into two streams using a T-shaped fitting. One goes to the high pressure regulator and the other goes to the low pressure regulator. Rather than valves, the adjuster is used to control gas flow and pressure from the downstream to these two adjusters. This structure allows for excellent control of these various flows and pressures while minimizing changes in these flows and pressures due to upstream compressed gas pressure fluctuations or adjustments by other regulators. . In this preferred embodiment, the upstream pressure is typically 30 to 100 pounds per square inch. This does not exclude the use of higher or lower pressures. The low pressure regulator controls the downstream flow rate from 100 to 300 liters / minute.

  In order to achieve this optimum performance, the dilution and compressed gases are delivered to the nozzle and backflow tube, dried and heated. Such devices are designed for respiratory delivery of pharmacologically active aerosols and must be used immediately within one minute of switching on. Therefore, the temperature of the heated gas must rise to the operating temperature within 1 minute. This requires a heater that presents a high energy transfer from the heater to the gas passing through it with low temperature inertia. Especially in the case of dilution gas, the heater must exhibit a minimum resistance to gas flow. This facilitates the use of a small gas blower. Low gas flow resistance heaters minimize the required gas mover size and pressure head. In this disclosure, large slit width radial slits are described for minimizing termination efficiency and providing a clear path to the exhaust gas outlet. The use of multiple slit lengths has two purposes: (a) minimizing the total cumulative length of the slit to minimize pressure loss across the concentrator, and (b) relatively uniform at the outlet of the evaporation chamber. A concentric and relatively uniform concentrator crossing is achieved.

  These and other advantages of one or more aspects of the present invention will be apparent from the following description and accompanying drawings.

(Detailed description of the drawings)
Referring to FIG. 1 for purposes of illustrating an aerosol generator, the following assembly groups are: (a) a dilution gas drying chamber, blower and heater, (b) a compressed gas heater, (c) a flow conditioner manifold, and (D) Backflow tube is revealed.

<Input gas adjustment>
Low pressure gas for diluting and evaporating the liquid aerosol travels through the flow components. The gas dryer chamber 1002 includes a desiccant 1003 such as, but not limited to, an aluminum oxide pallet. The gas dryer chamber 1002 is connected to a gas filter 1021 and an attachment 1022 for a small blower 1001 or equivalent gas mover. The blower is connected to the dilution flow heater 1004 via the flow rate measuring device 1023. The flow metering device may be an anemometer, a hot wire velocimeter, a mass flow meter or other low resistance device. The heater 1004 is provided in a heat resistant cylinder (outer diameter 1.0 inch, inner diameter 0.75 inch) 1005. In the preferred construction, the cylinder is made of ceramic. The fast heating infrared light bulb 1006 is arranged at the center in the tube. In the preferred construction, the fast heating infrared bulb 1006 has a tapered end to reduce gas flow resistance. The heat resistant cylinder 1005 fits within the right angle lumen fitting 1007. The other opening of the mounting part 1007 has a tapered container (not shown). This allows for easy placement of similar tapered female fittings (not shown) of the flow conditioner manifold 1020. In the preferred construction, the port and container taper is the standard 22 mm of the respiratory taper. There is an iron constantan thermocouple (not shown) that is placed in the gas flow in the lumen of the right angle channel of the fitting 1007. This thermocouple is connected to a temperature adjusting device 1008. In the preferred structure, the temperature adjusting device is a PID that controls the power supply to the infrared bulb 1006. The high pressure gas, which generates a fluid aerosol at the nozzle 1101 with the nozzle 1024 and provides a coaxial backflow through the backflow tube 1102 to constrain the aerosol plume, constitutes the flow element. The compressed gas enters the attachment 1019 and is warmed in the heater 1011. In the preferred construction, the heater comprises a ceramic tube 1009 having an outer diameter of 0.75 inches and an inner diameter of 0.56 inches in which the infrared bulb 1010 is disposed. The iron constantan thermocouple is located downstream of the heater 1011 at the outlet gas flow (not shown) or other convenient location of the female portion of the quick disconnect 1032. This thermocouple is connected to a temperature adjusting device 1012 such as a PID controller. This quick disconnect is connected to a right angle mounting component 1013 via a Teflon (registered trademark) tube 1031. For illustration purposes, the tube 1060 is inserted into the inlet (see FIG. 4C) of the flow conditioner manifold 1020 to show the connectivity of the compressed gas flow. Other structures that achieve the desired function are possible.

<Input gas adjustment>
The dilution gas up to 300 liters is supplied by a small blower 1001 or an equivalent gas mover. If the relatively humid room gas is higher than the desired aerosolized volume of the fluid to be dried, this diluent gas may pass through a gas dryer chamber 1002 containing a desiccant 1003. This dry gas passes through the filter 1021 for protecting the blower from fraying (due to the desiccant dust) and moves to the blower 1001 via the mounting part 1022. This dry gas is pushed by the blower 1001 through the flow meter or flow measurement device 1023 to the dilution flow heater 1004. The gas is heated in the heater 1004 while passing between the infrared light bulb 1006 and the inner wall of the heat-resistant cylinder 1005 formed of a ceramic tube. The temperature of the gas exiting the tube is measured with an iron constantan thermocouple (not shown) placed directly in the gas stream, and the gas is a temperature, such as a PID controller that moderates the power supply to the heater bulb 1006. A moderation device 1008 is used to maintain the desired temperature, typically 35-45 ° C. Similarly, the compressed gas used in the nozzle and the backflow gas passes through the heater 1011. This gas is heated while passing between the infrared heater 1010 and the wall of the ceramic tube 1009. The temperature of the gas exiting the tube is measured with an iron constantan thermocouple (not shown) and maintained at a desired temperature, typically 100-140 ° C., using a second PID controller 1012. This PID controller adjusts the electric power in the infrared light bulb 1010.

In other desirable configurations of the invention, the compressed gas may be used as a diluent gas source. In this case, the pressure adjuster replaces the dilution gas blower 1001. Compressed or other gases are generally removed, if not all, of the water vapor. In this case, the input high pressure fitting is connected to two gas pressure regulators (not shown) via a high pressure tube and a T-shaped part. One adjuster controls the gas flow rate towards the compressed gas heater 1011, and the other controls the gas flow rate now located between the adjuster and diluted flow gas heater 1004 via the flow measurement device 1023.

<Replaceable nozzle holder and nozzle>
A schematic showing the desired structural features of the nozzle holder is shown in FIGS. 2A-2C. The nozzle holder is constituted by an aerosol generating nozzle 1024 mounted in a mounting part 2112 on the neck 2003 at the end of the barrel 2001. The constriction from the barrel to the neck 2003 allows the gas to go to a streamline along the neck adjacent to the nozzle. This minimizes particle deposition on the front face of the nozzle via vortices caused by large flow surfaces near the nozzle. Figure 2 nozzle 1024 B is the two channels ending in one or more ports 2008, in turn, a small pressure equalization chamber 2105 connected proximate. A tube 2104 proximate to the nozzle and coaxial with the nozzle orifice is connected to the other channels 2103 and 2007 , fluid port 2005. The other end of the barrel is a knob 2006 with several circumferential grooves that allow easy insertion and removal of the nozzle holder into a container (see 4030 in FIGS. 4A and 4C) in the flow conditioner manifold 1020. It is. A fluid port 2005 at the opposite end of the nozzle allows an attachment a fluid line (not shown). In the preferred construction, this is a Luer connector. The port 2008 in the barrel 2001 matches the compressed gas supply groove in the flow conditioner manifold 1020 (see 4071 in FIG. 4C). According to the present invention, these nozzle holders must be inserted into the flow conditioner. This feature essentially eliminates the indiscriminate use of this nozzle holder by the patient. This protects the patient and helps ensure proper delivery of the cartridge contents.

In the preferred nozzle holder structure of FIGS. 2A, 2B, 2C and 2D, the nozzle 1024 requires both high pressure gas and high pressure fluid for sufficient aerosol generation. The fluid port 2005 is connected to the channel 2103 and the tube 2104 via the channel 2007. In the preferred construction, the tube 2104 has an inner diameter of 0.03 inches and a port 2110 located at a diameter of 1-2 from a 0.014 inch diameter orifice in the nozzle 1024. These dimensions do not exclude other diameters and distances, but are functional examples. The nozzle 1024 includes a mounting component 2112 to ensure that the orifice and tube 2104 are exactly coaxial. This structure provides an example. Similar structures may be achieved with other structures. The compressed gas intake port 2008 is on the side of the barrel 2001 of the nozzle holder. Port 2008 is connected to one or more channels 2101 and pressure equalization chamber 2105. This chamber 2105 extends into the nozzle body to facilitate a uniform gas flow at the nozzle from around tube 2104 to the orifice. A liquid aerosol plume 2106 is formed at the outlet of the nozzle 1024. Knob 2006 functions as a stop in flow conditioner manifold 1020 to limit the distance of barrel 2001 inserted into container 4030 of FIGS. 4A and 4C. A circumferential groove on the knob 2006 facilitates insertion and removal of the nozzle holder from the flow conditioner barrel. In this nozzle holder configuration, fluid is supplied by an external pump (not shown) via the nozzle holder fluid port 2005. The fluid flow flows along the center of the nozzle barrel 2001 via the channel 2007 and the central channel 2103 . Tube 2104 carries this fluid to its port 2110. Compressed gas enters through port 2008 on one of the sides of barrel 2001. This compressed gas enters channel 2101 on one of the sides of channel 2103. These external channels carry the compressed gas to the pressure equalization chamber 2105. The compressed gas in the chamber 2105 flows through the center of the orifice of the nozzle 1024 and along the tube 2104 containing the fluid for the fluid to flow without contacting the orifice. The aerosol is generated by concentrating the fluid flow through the nozzle 1024. A liquid aerosol plume 2106 is formed downstream of the orifice.

In another desirable structure of FIG. 2D, instead of the knob 2006 and fluid port 2005 shown in FIGS. 2A, 2B and 2C, a cylindrical cartridge 2020 is incorporated into the nozzle holder. The aerosolized fluid is stored in a chamber 2021 in the cartridge 2020. The chamber 2021 of this cartridge has a piston 2022 that is translated downward within the chamber. This chamber is connected to channel 2103. The piston 2202 may be pushed down with the attached plunger 2023, i.e., used multiple times or may be pushed down using a rod that is not attached to the piston, such as a single use nozzle system. The plunger or rod may be pushed down by a servo motor or other means. A plurality of circumferential grooves around the cartridge 2020 facilitates insertion and removal of the cartridge-nozzle holder from and into the container 4030 of the flow conditioner manifold 1020 (see FIGS. 4A and 4C).

<Another nozzle holder and nozzle>
3A, 3B, 3C, 3E, 3F show a nozzle and a nozzle holder that uses a high pressure gas in the middle of a low pressure fluid stream. This second nozzle and nozzle holder is used as an example of the breadth of utility of the construction of the container 4030 (see FIG. 4) within the flow conditioner manifold 1020 for a combined nozzle with completely different operational functionality. The essence of the structure and aerosol generation is different at all, this alternative nozzle holder has an external features and common functionality. These nozzles are both single path nozzles, i.e. all of the liquid is aerosolized during the passage of the nozzle. No fluid is recirculated. However, both nozzles share the property that aerosol is generated through shear forces between liquid and gas. In either case, the aerosol is generated through the shearing of the liquid on the solid. This reduces the possibility of high shear forces due to shear degradation of large molecules dissolved or suspended in the fluid being aerosolized.

In this other desirable structure, the nozzle holder and nozzle are shown in FIGS. 3A, 3B, 3C, 3D, 3E and 3F. As already mentioned, this structure makes it possible to generate aerosols using compressed gas passing through the central channel along with the low pressure fluid flow towards the periphery of the compressed gas nozzle. A fluid port 2005 (see FIG. 3C) is at the end of the nozzle holder. In the preferred structure of the present invention, fluid port 2005 is a luer fitting. This fluid port 2005 is connected to one or more channels 3203 (see FIG. 3C) via a channel 2007 and a small dispensing container 3208 and thus an annular cavity 3206 surrounding the base 3204 of the nozzle body 3300 (see FIG. 3A). Connected to. In this case, the nozzle is composed of two elements, a nozzle body 3300 and a nozzle annulus 3205. Nozzle body 3300 is located within the neck 3220 of the nozzle barrel 3001 (see FIG. 3C) having a base 3204 of the nozzle the body that is sealed to the barrel of the nozzle holder. Annular cavity 3206 (see FIG. 3B) includes recesses 3216 in top 3211 and annulus over top 3211 through grooves, for example grooves 3210 (see FIG. 3A) and 3212 in top 3211 of nozzle body 3300. 3205 is connected to a small container 3213 (see FIG. 3B). The container 3213 is adjacent to the annular cavity 3230 between the stem 3214 and the annulus 3205 on the nozzle body 3300. The annulus 3205 is positioned at the end of the neck 3220 of the nozzle barrel 3001 (see FIGS. 3C and 3D) such that the central hole 3233 of the annulus 3205 is concentrically positioned around the nozzle stem 3214 (see FIG. 3B). . The distance between the nozzle stem and the annulus is small enough so that the surface tension is greater than the gravity-dominated fluid movement. The difference in diameter between the internal annulus diameter and the external stem diameter is 0.006 to 0.8 mm, and as a result, the annular gap width is 0.003 to 0.4 mm. The other nozzle size is 0.05 to 1 mm, but the stem 3214, 1.75 mm in the desired structure, but may vary from 0.5 mm to 3 mm, is the orifice 3209, the diameter of about 0. 5 mm. The orifice exits at the tip of a hollow cone 3240 in the nozzle stem 3214. The edge 3215 of the cone 3240 is either at the same height as the external surface of the annulus 3205 or protrudes slightly from this surface, possibly up to 1 mm. The nozzle body 3300 is comprised of a machined ceramic or other material that is wetted by an aerosolized solution or suspension. For aqueous based solutions, the nozzle should have a high surface energy to improve wettability. This may be achieved by using hydrophilic drugs or other means. The outer surface of the annulus 3205 is covered with a hydrophilic agent to prevent diffusion of aqueous fluid across the annulus. Barrel 3001 Nozuruhoru Da has one or more ports 2008 which are connected to the channel 3202 (see FIG. 3D) through the channel 3201. Channel 3202 is proximate to a similar diameter channel 3234 in nozzle body 3300. This is close to the orifice scan 3 209. In a preferred construction, the nozzle barrel 3001 and knob 3301 (see FIG. 3F) are made of polysulfone or Ultem®, although other materials may be used.

<Generation of aerosol by nozzle holder and nozzle shown in FIGS. 3A-F>
In the preferred structure of the nozzle holder shown in FIGS. 3A, 3B, 3C, 3D, 3E and 3F, aerosol is generated by supplying compressed gas to the channel orifice 3209 in the nozzle. The fluid to be aerosolized is supplied to the external surface of the nozzle through the annular cavity 3206, the container 3213 and the annular cavity 3230 at low pressure and by capillary force from the cone 3240 toward the orifice 3209. The fluid to be aerosolized is supplied to the fluid port 2005 by an external pump (not shown). Fluid is poured into the fluid port 2005 and the channel 3203, it is supplied to the annular cavity 3206 surrounding the base 3204 of the orifice the body. This fluid is distributed to the small container 3213 through each of the plurality of grooves 3210 on the side surface of the top 3211 of the nozzle and the plurality of grooves 3212. To ensure that the fluid is uniform in the cavity 3230 surrounding the central nozzle stem 3214, the top tip is recessed. The fluid flows uniformly through cavities 3230 between the stem the annulus to the nozzle edge 3215. In a desired configuration, the nozzle stem 3214 may protrude about 0 to 0.050 inches through the annulus. Fluid flows beyond this edge 3215 to form a thin film on the inner surface of cone 3240 in nozzle stem 3214. The compressed gas enters the side of the nozzle barrel 3001 via the port 2008. The gas flows to the channel 3234 along the axis of the nozzle body 330 via the central coaxial channel 3202. The compressed gas then passes through the orifice 3209. Aerosolization occurs at the point of contact formed by the interaction of the fluid flowing into the cone and the gas jet around the orifice 3209 at the tip of the cone 3240. In this way, large shear stresses between the solid surface and the fluid are avoided. An aerosol plume is generated having a particle free center. The negative pressure in the cone is caused by a gas jet that helps to form a thin fluid film on the inner surface of the cone. For optimal function, the cone tip should be defined in a solid angle range of about 45 degrees, preferably 15 to 80 degrees. However, other angles of 10 to 80 degrees are possible. Note that all surfaces through which fluid made to flow pass or exceed should have high surface energy, i.e. should be wetted by the fluid. The fluid flows beyond the edge of the cone due to capillary forces. These forces increase as the fluid flows toward the tip of the cone. As already mentioned, the maintenance of this thin fluid layer is also assisted by the negative pressure generated by the jet of gas exiting the orifice 3209. For optimal function, it is important that the surface of the nozzle body, including the top and nozzle stem, and the inner surface of the annulus, have a high surface energy that is easily wetted by the aqueous substrate fluid. On the other hand, the tip surface of the annulus 3205 has a hydrophobic coating to prevent fluid flow beyond the annulus. The distance between the nozzle stem and the annulus is sufficiently small, for example, .about.0.17 mm, so that the surface tension is greater than the gravity controlled fluid movement. If the nozzle stem has a high surface energy, the fluid forms a meniscus between the edge 3215 of the cone 3240 on the nozzle stem 3214 and the annulus.

<Positioning of the nozzle holder for insertion into the flow conditioner>
The positioning of the nozzle holder for insertion into the flow conditioner is shown in FIGS. 4A, 4B and 4C. The nozzle holder is aligned with the central on-axis container 4030 in the flow conditioner manifold 1020 (see FIGS. 4A and 4C). The nozzle holder barrel 2001 or 3001 is inserted into this container 4030 of the flow conditioner 1020. When the nozzle holder is fully inserted, the port 2008 for compressed gas used for aerosolization will align with a circular groove 4071 in the flow conditioner 1020. An O-ring 4033 is present on each side of the groove to prevent compressed gas leakage from the groove 4071. The compressed gas enters a circular groove 4071 through a channel 4036 that is in turn connected to a compressed gas input 4028. In the middle of the manifold is a column 4040. This column 4040 facilitates the inclusion of a container 4030 with a 4: 1 width ratio. This ensures proper positioning of the nozzle barrel 2001 or 3001 and its correct coaxial alignment. This is important when the aerosol plume needs to be precisely aligned with the backflow gas axis for efficient performance.

<Flow conditioner structure>
An exploded view and a cross-sectional view showing the individual elements including the flow conditioner acting on the diluent gas flow profile are shown in FIGS. 5A, 5B, 5C, 5D, 5E and 5F. In FIG. 5A, an adjacent evaporation chamber 5100 is also displayed. To refer to the rapid evaporation of liquid aerosol in an enclosed space, the aerosol plume formed by any one of the nozzles described is rapidly dispersed and diluted while sufficient thermal energy is supplied to the evaporating liquid. Need to be done. The flow conditioner must provide a uniform flow of gas through the evaporation chamber 5100 when a minimal pressure drop occurs again. This is made more difficult by the presence of the aerosol plume 2106 (see FIG. 5A) and the jet of gas 5120 (see FIG. 5D) from the backflow tube 1102. As already mentioned, this needs to be achieved with a minimum pressure drop across the flow conditioner to minimize the required fan power and size. Small flow conditioners that are less expensive to manufacture and are easily assembled and disassembled for cleaning make the final product more commercially attractive. The flow partitioner is configured to reduce the radial velocity of incoming dilution gas and distribute the gas so that the gas is at a substantially uniform velocity at the outlet of the evaporation chamber. These flow conditioner elements are configured to be easily assembled and dismantled while all functionality is maintained.

An exploded view of the elements used to convert the relatively fast dilute gas stream entering port 5122 (see FIG. 5B) into a relatively uniform slow gas stream at the outlet of the evaporation chamber 5100 is shown in detail in FIG. 5C. Has been. Cross sections of the assembled parts are included in FIGS. 5A and 5B, along with a front view of the flow conditioner showing the location of the port 5122 for diluent gas and the port 4028 for compressed gas. The flow conditioner consists of four main elements: a manifold 1020, two flow partitioners 5102 and 5103, and a backflow tube 1102. As shown in FIGS. 4A and 4C, the manifold 1020, an input port 4028 for compression gas, diluted gas input port 5122 for scan, the container 4030 nozzle holder is inserted therein, a central stabilizing post 4040 , A container for the backflow container 4041, and two concentric steps 4011 and 4021, and a step 4013 on the end of the column 4040. These stages facilitate stable localization of the two flow partitioners 5103 and 5102 (see FIG. 5C). Of course, these two flow partitioners 5103 and 5102 may be manufactured integrally as one piece. The flow conditioner manifold 1020 is made of Ultem or other high temperature non-conductive material with good dimensional stability, as found in the two flow partitioners 5102 and 5103. During normal work and operation, the flow partitioner is still effective, as shown in FIG. They are easily removed or replaced. This functionality is achieved through a special structure that features the substantial description. An input port 5122 of the flow conditioner for dilution gas is made into 22mm standard respiratory male taper. This port fits the corresponding female taper (not shown) in the fitting 1007 (see FIG. 1). For this reason, the flow conditioner is held in position by gravity.

A port 4028 for compressed gas is located in the flow conditioner manifold 1020. The compressed gas flowing through this port is divided into two. One flow is directed in the central container 4030 through the channel 4036 to the annular groove 4071. An O-ring 4033 is in the groove on one side of the annular groove 4071 in the central coaxial container 4030. The flow divider is also connected to a flow restriction orifice 5024 , which in turn is connected to a backflow tube 1102 via a backflow vessel 4041.

The backflow tube 1102 has a 180 degree curve 5016 that reverses the direction of gas flow and directs it to the approaching aerosol plume 2106 generated by the nozzle 1024. The reverse flow is the side that interacts with the groove 5031 in the flow conditioner column 4040 when inserted into the flow conditioner so that the reverse flow tube is exactly coaxial with the nozzle 1024 when the reverse flow tube is installed. Has a small plate 5029 attached to it. In the preferred construction, the backflow tube consists of 12 gauge stainless steel tubing. In the preferred construction, the back tube outlet is 2 inches from nozzle 1024. This is an example rather than excluding the tube diameter of the backflow distance and other combinations of nozzles.

The two flow partitioners 5102 and 5103 are designed to reduce the radial velocity of the incoming dilution gas and to distribute a substantially uniform velocity gas at the outlet of the evaporation chamber 5100. These elements of the flow conditioner are configured for easy assembly and disassembly while maintaining all functionality. These two flow partitioners 5102 and 5103 divide the manifold 1020 chamber into two pressure / flow equalization chambers 5021 and 5222. The diameter of the flow partitioner 5102 is slightly larger than the circumference of the flow partitioner 5103. The flow partitioner 5103 has a “chimney” 5134 with a hole 5009 located in the periphery. The upper end of the chimney has a circumferential protrusion 5007 that provides a stabilizing means for the second flow conditioner. The flow partitioner 5103 is located in the flow conditioner manifold chamber so that it is located in the circumferential step 4012 inside the flow conditioner and the circumferential step 4013 in the central post 4040 of the manifold 1020. Inserted into. The flow partitioner 5102 is inserted into the chamber of the flow manifold 1020 such that the flow partitioner is located at a stage 4011 in the manifold.

Of note, there are four contact surfaces between the flow conditioner manifold 1020 and the first flow partitioner 5103 (see FIGS. 4C and 5A). These surfaces provide a stable position of the flow partitioner within the housing. Again, these multiple surface contacts facilitate the placement of this second flow partitioner and are suitable to prevent it from falling or moving during normal operation and operation of the device. Fix in position. Through the use of such a plurality of stages, the gas stream, flow partitioner and than "leakage" which via the connection area between the manifold 1020, through a hole 501 3及 beauty slots 5012, flow partitioner 5102 and 5103 ( It is also important to be directed to FIG. In this way, flow is controlled by the size of the flow channel rather than leakage. The use of O-rings is avoided. The use of such a large O-ring would make it very difficult for the patient or end user to assemble the part. This minimizes aerosol deposition on the flow partitioner. The flow partitioner 5102 has a central hole 5014 through which the nozzle neck 2003 protrudes. It has a generally circular hole 5015 that facilitates insertion of the backflow tube 1102. A central portion 5017 of the flow partitioner 5102 is raised. This facilitates the inclusion of circumferential grooves 5018. This groove allows the user to grip the outside of the flow partitioner with their fingers for easy removal and easy insertion from the flow conditioner manifold 1020. The raised center of the flow conditioner has a recessed surface to reduce aerosol deposition on its surface.

Flow conditioners manifold, play an important various functions for he wanted the operation of the device. These are: (a) the exact placement of the nozzle holder on the central axis of the manifold container, (b) the injection port 2008 on the barrel 2001 of the nozzle holder (see FIG. 2B), and the backflow tube 1102 (see FIG. 4C). And (c) inhalation and redistribution of diluent gas to achieve a substantially uniform gas flow rate at the outlet of the evaporation chamber 5100 (see FIG. 5A).

<Division of compressed gas>
In Figure 5A, the compressed gas is quick and disconnect fitting 5019 through the Teflon tube 1031 through a right angle fitting 1013 on the manifold 1020 of the flow conditioners, connected thereto can be seen. For simple and practical use of the device, there is a flow conditioners manifold on only one connector 4028 for compression gas. The compressed gas stream is divided using a flow divider located inside the flow conditioner manifold. One flow is directed through channel 4036 to an annular groove and to an annular groove 4071 in the central vessel that supplies compressed gas to the nozzle holder. O-rings 4033 in the plurality of grooves on one side of the annular groove 4071 in the central container 4030 seal against compressed gas leakage. The other flow passes through a flow restriction orifice 5024 that restricts the flow rate of the backflow gas to be equal to or slightly greater than the volumetric flow rate entering the aerosolization nozzle 1024. The liquid aerosol plume 2106 is constrained by the coaxial backflow jet of gas 5120 from the port 5026 of the backflow tube 1102 so that the stagnation point 5300 is in the middle of the nozzle and backflow port 5026 (see FIG. 5A).

<Execution of function by dilution gas flow conditioner>
The input gas flow from the input port 5122 (see FIG. 5B) is directed circumferentially and is in the pressure equalization chamber 5021 around the central column 4040 (see FIG. 4C) of the first stage of the flow conditioner. This first stage is a low gas flow resistance hollow “donut”. The rotational speed of the gas is attenuated while moving vertically through slots 5012 (see FIG. 5C) located around the plurality of melons 5042 on the flow partitioner 5103. These slots form a gas flow path with a resistance higher than the resistance of the channel forming the first donut-shaped pressure equalization chamber 5021. Gas enters the second stage of the flow conditioner through these slots 5012 and enters the second donut-shaped pressure equalization chamber 5022 with low flow resistance. From this channel, there are two paths: (a) through a hole 5009 around a “chimney” 5008 and further substantially through a hole 5223 in the central portion of the second flow partitioner, (b) a second flow partitioner. 5102 through a concentric hole 5013 in the outer region. The location and size of these holes (or slits) achieve a uniform flow profile on the virtual impactor face plate while minimizing aerosol deposition on the walls of the second flow partitioner 5102 and evaporation chamber 5100. To do. Part of the gas flow towards the center of the evaporation chamber is moderated by the size of the hole 5009 in this “chimney”.

<Evaporation chamber>
The features of the evaporation chamber 5100 seen in FIG. 5A are shown in FIGS. 6A, 6B, 6C and 6D. The evaporation chamber 5100 fits between the flow conditioner manifold 1020 and the aerosol concentrator 6100. The preferred structure of the evaporation chamber is transparent to infrared radiation and consists of a tube with an outer diameter of 2.75 inches, an inner diameter of 2.56 inches, and a length of 6 inches. Other similar dimensions are possible. In the desired structure, the tube may be made of quartz or borosilicate glass. This tube is inserted into the opening at the end of the flow conditioner manifold 1020 until it is adjacent to the flow partitioner 5102 (see FIG. 5A). The manifold opening and tube dimensions are such that the friction fits sufficiently (a) to support the tube and (b) to prevent substantial gas leakage from the interior of the chamber to the atmosphere. It is a thing. The other end of the evaporation chamber is inserted into a circumferential groove 6055 (see FIGS. 6A and 7C) on the acceleration plate 6110 (see FIG. 6A) of the virtual impactor type aerosol concentrator 6100. Again, this is a friction fit. Alternatively, the edge seal or tapered end of the chamber 5100 and the corresponding female taper on the manifold 1020 and the concentrator acceleration plate 6110 may be connected to the evaporation chamber 5100 and the flow conditioner manifold or aerosol concentrator 6100. It can be used to eliminate gas leaks.

  A 125 W rapid heating infrared lamp 6001 is adjacent to the evaporation chamber on one side of the evaporation chamber. The desired parabolic infrared reflector 6002 is placed behind the bulb so that the bulb is centered in the focal plane of the reflector. In addition, the infrared reflector 6003 on the opposite side of the evaporation chamber again increases the infrared irradiation flux within the evaporation chamber. In the preferred construction, these infrared reflectors are made of polished aluminum. The infrared reflective material 6003 may be composed of a gold coating on the evaporation tube. The reflective material 6002 may be replaced with a gold coating on the infrared lamp 6001. In order to increase the rate of evaporation, the aerosol passing through the evaporation chamber 5100 is heated with infrared radiation. Heat transfer by convection is proportional to the temperature gradient. However, heat transfer by radiant heat is proportional to the fourth force of temperature differentiation. Water has a strong absorption band in the infrared region. For this reason, the quick response infrared lamp 6001 is disposed downstream of the evaporation chamber 5100. The infrared reflector 6002 increases the infrared irradiation flux in the chamber 5100. A quartz or borosilicate glass evaporation chamber that is transparent to infrared radiation allows infrared radiation to enter the chamber 5100. This infrared radiation is absorbed by the water in the aerosol particles. This energy is delivered as latent heat of steam. A second infrared reflector 6003 disposed on the opposite side of the evaporation chamber increases the transfer of infrared energy to aqueous aerosol particles passing through the evaporation chamber 5100.

<Backflow tube>
The evaporation chamber 5100 also includes a backflow tube 1102 (see FIGS. 1 and 5A). The backflow tube is in a backflow vessel 4041 (see FIGS. 4C and 5A) with a small plate 5029 (see FIG. 5C) attached to the backflow tube placed in the slot 5031 of the column 4040 (see FIG. 4C) of the manifold 1020. Be placed. Housing the gas from the flow divider 5052, the tube (see FIG. 5A) has a 180-degree curve following the short straight portions. The curvature of this curve, small when the plate 5029 (see FIG. 5C) is correctly inserted into the slot 5031 of the manifold, so that port 5026 of the backflow tube is orifice or exactly the coaxial center of the chamber and aerosol nozzle 1024 Is something.

The compressed gas from the flow divider 5052 exits the backflow port 5026 through the backflow tube. The jet of gas so generated is coaxial except in the opposite direction of the aerosol plume. The short straight section of the backflow tube 1102 ensures a symmetrical jet of backflow gas. Flow rate of the gas jet, aerosol plume 2106 is such suppressed in the middle of the port 5026 of Nozzle 1 024 and the backflow tube 1102.

<Aerosol concentrator>
Virtual impactors, shown in detail in FIGS. 7A, 7B, 7C, 7D, 7E and 7F, are used to concentrate the output aerosol from the evaporation chamber 5100. As shown in FIG. 7C, the borosilicate / quartz tube of the evaporation chamber 5100 constitutes a snug fit to the circumferential groove 6055 in the acceleration plate 6110 of the aerosol concentrator 6100. Returning to FIG. 7A, the virtual impactor consists of an acceleration plate 6110 that includes a long acceleration slit nozzle 7002, an intermediate slit nozzle 7102 and a short acceleration slit nozzle 7202, and intermediate 7103 and short 7203 auxiliary deceleration slit nozzles. The exhaust gas cowling 7021 and the exhaust port 7022 (FIGS. 7D and 7E) are attached to the deceleration plate 7120. Plume 7004, deceleration plate 7120, and exhaust gas cowling 7021 formed by acceleration plate 6110 diverge from the gap between the edges of acceleration nozzles 7002, 7102, 7202 and the receiving slits of deceleration nozzles 7003, 7103, 7203. Provide a low resistance flow path for gas. The acceleration plate 6110 fits within the virtual impactor deceleration plate 7120 such that the long 7002, intermediate 7102 and short 7202 acceleration nozzles are exactly aligned with the long 7003, intermediate 7103 and short 7203 deceleration nozzles, respectively. There is a small gap 7300 between the orifices of these acceleration nozzles and auxiliary deceleration nozzles. The slit of the acceleration nozzle is 1.1 mm wide. The receiving slit is 1.4 mm wide and is arranged to be an intermediate gap 7300 between a plurality of acceleration nozzles, and the deceleration nozzle is 1.3 mm. These are descriptions as practical solutions and are not intended to exclude other similar dimensions. A filter (not shown) may be attached to the exhaust port 7022 to prevent particles suspended and carried in the exhaust gas from entering the atmosphere.

  While a virtual impactor aerosol concentrator has been described so far, this concentrator has clearly new features that make the present invention ideally suited to its proposed function. The concentrator was optimized to deliver a large mass fraction of breathable aerosol generated by nozzle 1024 (see FIG. 1) to the output. For this reason, the concentrator is optimized to work best in the breathable range, ie, aerodynamic diameter of 1 to 5 microns. Thus, for the purposes of the present invention, the output aerosol is considered to consist of particles larger than an aerodynamic diameter of 0.5 micrometers. For this reason, the virtual impactor should concentrate as many particles as possible with an aerodynamic diameter of 5 micrometers or less. This introduces several new structural features that are included to remove exhaust gas from the gap between the nozzle and receiving slit, along with the requirement for a minimum pressure drop across the concentrator and the absence of negative gas pressure. Requested.

  1.16 acceleration slit nozzles 7002, 7102 and 7202 are arranged in the radial direction as shown in FIG. 7A. This structure allows the exhaust gas to exit the concentrator with minimal interaction with the aerosol jet passing between the acceleration nozzles 7002, 7102 and 7202 and the deceleration nozzles 7003, 7103 and 7203 in the radial direction. chosen. The shorter slit nozzles 7102 and 7202 were designed to keep the flow across the evaporation chamber and concentrator as uniform as possible. This structure further minimizes the total accumulated length of the accelerating and decelerating nozzle slits. The total cumulative length of the accelerating nozzle is preferably 18 cm, but other cumulative lengths from 10 to 25 cm are possible.

  2. The tapered surface of the input of the acceleration nozzle minimizes the pressure difference required to accelerate the aerosol to the nozzle velocity while minimizing aerosol deposition on the surface of the accelerator plate 6110 of the concentrator 6100. In addition, a parabolic contour 7008 (see FIG. 7C) is designed.

  3. Similarly, the output cones of the deceleration nozzles 7003, 7103, and 7203 are parabolically sculpted to reduce the resistance through the concentrator and minimize aerosol turbulence at the concentrator output. And has a contour 7009 (see FIG. 7C).

  4). In addition, the downstream surfaces of the acceleration nozzles 7002, 7102 and 7202 and the upstream surfaces of the deceleration nozzles 7003, 7103 and 7203 are engraved to make the exhaust gas resistance between these nozzles lower. The engraved shape is not provided with engraved acceleration and deceleration channels, i.e. through these channels towards the cowling and finally leaving the system via the discharge port 7022 (see Fig. 7E). For flowing, low particle density, divided discharge volume flow, leave a wide radial channel, leaving at least 1 cm gap between the acceleration and deceleration plates at those locations. Again, this allows the exhaust volume flow to be removed with minimal perturbation of the aerosol jet. These upstream and downstream surface profiles, designed to minimize both flat surfaces and steep acute angles, are essential to the overall performance of the concentrator. Of note, the downstream profile of the deceleration nozzle has been shown to significantly increase the efficiency of the concentrator compared to a slit in a flat virtual impactor plate.

  5. In order to facilitate accurate alignment between the acceleration nozzles 7002, 7102 and 7202 and the deceleration nozzles 7003, 7103 and 7203, a location cylinder 7010 (see FIG. 7A) and a close fitting male cylinder 7011 are: Ensures coaxial alignment of the concentrator jet plate and the receiving plate. This ensures that the jet slit, along with the male fitting 7115 and the close fitting female cross formed in the container 7013, is precisely aligned with the receiving slit of the deceleration nozzle.

  6). The acceleration plate 6110 and the deceleration plate 7120 can be easily separated by using a centrally located helicoil 7014 and screw 7015 (see FIG. 7F). This facilitates various assembly and disassembly and cleaning of the aerosol deposited on the inner surface of the plate.

  7). The cavity 7016 downstream of the concentrator (see FIG. 7C) is configured to attenuate turbulence from the receiving slit and reduce unwanted aerosol deposition on the output cone.

8). The cowling 7021 (see FIG. 7E) has a sculpted outlet channel 7106 and a drain port 7022 having a standard 22 mm taper to facilitate connection of a disposable filter (not shown).

  At the output of the evaporation chamber 5100, the aerosol is concentrated using a virtual impactor, shown in FIGS. 7A, 7B, 7C, 7D, 7E and 7F. The aerosol from the evaporation chamber 5100 is accelerated as it passes through the acceleration nozzles 7002, 7102 and 7202. In this case, flow resistance is minimized through the use of long 7002, intermediate 7102 and short 7202 slit nozzle structures. If the aerosol particles have a much higher momentum than the suspended gas and water vapor molecules, the particles will enter deceleration nozzles 7003, 7103 and 7203 across gap 7300. The aerosol flow rate at the output of the concentrator is typically only 1/5 to 1/10 of the input flow rate. The gas flow rate difference between the input gas flow rate and the output gas flow rate is discharged to the plume 7004 through the gap 7300 (see FIG. 7C) between the slits. The concentrated aerosol at the output is passed through an aerodynamically designed output cone 7006 for delivery to the patient or for other desired purposes.

  In the preferred construction, there is a 1-2 cm wide flange 7030 on the output outer wall of the concentrator cavity 7016. This facilitates the placement of an output cone 7006 having an internal diameter that fits in the inlet and stage 7031 so that there is no flow conditioner. The cone output has a standard 22 mm respirator taper 7032 (see FIG. 7F) to facilitate connection to a suction tube or filter (not shown).

The flow resistance of the dilution heater was found to be 0.12, 0.3 and 0.5 inches H ₂ O at 100, 150 and 200 liters / minute, respectively. The flow resistance of the flow conditioner was defined to be 1 inch H ₂ O at 150 liters / minute and 1.8 inch H ₂ O at 200 liters / minute. The aerosol concentrator flow resistance was defined to be less than 1 mm H ₂ O at all tested input flow rates of 300 liters / minute or less when the concentrator output flow rate was 40 liters / minute. The pressure in the evaporation chamber is 0.3, 0.8 at chamber flow rates of 100, 150, 200, 250 and 300 liters / min, respectively, when the concentrator output flow rate is 40 liters / min. 1.4, 2.2 and 2.7 inches H ₂ O.

  A solution of 16% bovine serum albumin was supplied to the nozzle using an infusion pump and aerosolized at 1 ml / min. The nozzle pressure was 20-24 pounds per square inch and the dilution gas flow rate was 200 liters / minute. The resulting dry aerosol downstream from the concentrator was measured at 40 liters / minute for 2 minutes. The mass collected was determined gravimetrically. Typically, 180-210 mg was collected. For this reason, the output of the device is about 100 mg / min.

  The overall efficiency of device throughput was found to be 64%. The efficiency of the concentrator alone was found to be 85%.

  Red food dye number 4 (0.2%) was added as a tracer of a 16% albumin solution. Under similar conditions, albumin aerosol was extracted at 30 liters / min with a Marble-Miller cascade impactor. Each stage of the impactor was washed three times with water and the relative mass of each stage was determined spectrophotometrically at 508 nanometers. Cumulative mass was plotted on log probability paper. The mass median diameter was found to be 3.4 μm. It was found that 85% of the collected aerosol was inhalable, the sum of all stages below 5 microns. To determine, porcine trypsin was aerosolized and collected when the aerosolized protein was degraded by passing through a nebulizer. This trypsin solution was placed in a confluent cell culture. The cells appeared to be detached from the substrate. There was no difference between similar enrichment results of non-aerosolized trypsin.

  To evaluate the sharpness and surface properties of the generated albumin particles, the particles at the output were collected on a 12 mm diameter Millipore filter. This filter was placed in the middle of a larger filter with similar flow characteristics. This filter was mounted on an electron microscope stud and stored upright in a desiccator. Each sample was sputtered with palladium gold and a random image was recorded on the SEM at a magnification of 1500. The albumin particles were found to be smooth surface spheres.

  The embodiments described in the specification of the present disclosure provide a practical miniature portable device for the generation of inhalable particles dry concentrated from an aqueous solution or suspension. The present disclosure describes the generation, i.e., diluting, heating, and quickly evaporating aqueous aerosols in a small, practical medical device, then concentrating the resulting particles and complying with the full range of standard inhalation flow rates Provides a means to deliver them at a flow rate.

  Where i. Enables improved functionality, ii. Facilitate practical use of embodiments, iii. The inclusion of many beneficial features in embodiments having medical benefits is described.

In other advantages, embodiments of the present invention achieve the following:
(A) Local radiant heat is supplied at the maximum infrared absorption wavelength of water to newly formed aqueous aerosol particles from a source directly adjacent to the evaporation chamber.
(B) Allows the device to utilize different nozzle holders configured to be easily replaceable. These nozzle holders allow compressed gas to be routed to one of the central orifice or the periphery of the central fluid stem. The nozzle holder is adjusted towards the flow conditioner and may or may not include a compressible fluid container.
(C) Provide a means for heated high-speed gas reverse flow in one direction and uniform low-speed flow in the opposite direction while there is a perturbation due to the aerosol plume and the reverse flow gas. This is achieved with a minimum pressure drop using a two stage flow conditioner.
(D) Slit concentrators of various lengths having a 1.1 mm wide radial input slit and a 1.4 mm wide output slit, with input and output cones that are parabolically contoured on both upstream and downstream surfaces. Is used to efficiently concentrate inhalable aerosols with minimal pressure loss between the input and exhaust gases.
(E) Minimize aerosol deposition due to turbulence at the output of the concentrator by including cavities that can attenuate these vortices.
(F) Provides an efficient means of delivering concentrated aerosol at the output by utilizing an internal parabolic shaped output cone.
(G) Remove large diameter high pressure bonds so that the device is easily assembled and disassembled for cleaning.
(H) A small blower that provides dilution gas is used to reduce the resistance of the gas flow in order to enable the construction of a small device.
(I) inclusion of at least two, preferably three or four mutually orthogonal surfaces, to maintain gas and / or aerosol between the various elements of the device while maintaining a structurally sound connection between the elements; Minimize leakage.
(J) exactly coaxial with the aerosol plume, facilitating the supply of a detachable backflow gas in the opposite direction to the aerosol plume, and the backflow tube was plugged into the flow conditioner.
(K) Supply heated compressed gas to both the nozzle and the backflow tube with minimal heat loss by including a flow divider and flow control orifice in the flow conditioner.
(L) Facilitating accurate assembly and disassembly of the concentrator plate by having male cylindrical protrusions and crosses raised in the center of the concentrator and female irregularities showing relative relationships.
(M) Use cowling and filter ports to prevent aerosol particles in the exhaust gas stream from polluting the atmosphere.
(N) Supply concentrated aerosol with a slight positive pressure as a pressure aid for patients with sufficient inspiratory pressure generation and flow problems that contribute to other dry powder inhalations.
(O) Generate, dry and concentrate a nearly sterile aerosol using the sterilizable elements of the embodiments, along with the positive pressure in the device.

  In the following, embodiments of the present invention are summarized.

<Generation of aerosol>
The liquid to be aerosolized is supplied into a fluid port 2005 in the nozzle holder and guided to the nozzle 1024 through the channel. The compressed gas requires that the liquid to be aerosolized be supplied to the fitting 1019. It passes through a heater 1011 where it is warmed to the required temperature. This temperature is measured by a thermocouple, and the heater is adjusted by a PID controller. This heated gas is divided into two streams. One flow is directed to the backflow tube 1102 through the flow restriction orifice 5024. The remaining flow proceeds into the annular groove 4071 from which it enters the barrel port 2008 and toward the nozzle 1024. The interaction between the aerosolized liquid and the high pressure gas at the nozzle causes the generation of a liquid aerosol plume 2106. The warm gas in the backflow tube is directed into the aerosol plume, but in the opposite direction with respect to the plume. This gas flow suppresses the middle aerosol plume between the nozzle and the end of the backflow tube. Injection of this heated gas into the aerosol plume facilitates rapid evaporation of the liquid solvent.

As shown in FIG. 1, the aerosol processing system warms the pressure gas supplied to the counter-flow gas stream 5120 (see FIG. 5A) to generate two gas heaters, aerosol, and to suppress the aerosol plume 2106. One gas heater 1011 and the other gas heater 1004 that warms the gas for diluting the aerosol are included. These warm gas streams are distributed to function in the flow conditioner, respectively. Flow Within conditioner manifold 1020 (FIG. 5A), a warm gas compressed, the two elements, the one hand, through the barrel 2001 of Nozuruhoru Da, in order to generate an aerosol, is sent to the tip of the nozzle, reflux The gas flow 5120 is divided into the other to form a coaxial flow but opposite direction to the nozzle plume 2106. When the aerosol through the evaporation chamber 5100, evaporation of the aerosol, by using in conjunction with anti Ysaÿe 6002 and 6003 that are associated radiant heater 6001 is increased. The aerosol is accelerated through nozzles 7002, 7102 and 7202 in the acceleration plate (see FIG. 7A) of the low resistance virtual impactor. Particles having a much higher momentum than gas molecules cross the gap, pass through the slits of the deceleration nozzles 7003, 7103 and 7203 in the deceleration plate 7120 and travel into the output collection cone. When the aerosol flow rate at the output of the virtual impactor is lower than the flow rate at the time of entering the virtual impactor, the residual gas is discharged between the acceleration plate 6110 and the deceleration plate 7120. Most of the particles contain the output aerosol as a result of passing through the slits in the deceleration plate 7120. A diagram of the gas input and regulation elements of the present invention is depicted in FIG. An optional gas dryer chamber 1002 is provided for use when needed. The desiccant chamber is filled with desiccant 1003. The small blower 1001 is connected to the dilution gas heater 1004 via the flow rate measuring device 1023. The heater 1004 is connected to a port 4028 on the flow conditioner manifold 1020 via a right angle fitting 1013. A thermocouple (not shown) is placed in the lumen of this right angle fitting. Flow conditioner, gas has been separated by flow partitioner 5103 with slots 5012 to allow passage from one chamber 5021 to the other chamber 5022 has a chamber 5021 and 5022 of two donut-shaped. The second stage of the flow conditioner is connected to the evaporation chamber 5100 through holes 5013 and 5223 in the second flow partitioner 5102. The evaporation chamber 5100 is disposed between the flow conditioner manifold 1020 and the aerosol concentrator 6100 . The aerosol concentrator has radially arranged acceleration nozzles 7002, 7102, 7202 that are also connected to an exhaust plume 7004. The deceleration nozzles 7003, 7103, and 7203 are arranged close to the acceleration nozzles 7002, 7102, and 7202, respectively. The downstream ends of these deceleration nozzles are adjacent to a turbulent damping cavity 7016 and an aerosol collection and cone 7006. This collection cone is connected to an output device or a person (not shown) inhaling the desired output flow.

The compressed gas is supplied to the mounting part 1019. This attachment component is connected to the compressed gas heater 1011. This is connected to the input port 4028 of the flow conditioner manifold 1020. This port 4028 is connected to a flow divider. One side of the divider is connected to the backflow tube 1102 via a flow restriction orifice 5024. The other side surface of this divider is connected to an annular groove 4071. This annular groove is aligned with the nozzle holder port 2008. These ports are connected to nozzles 1024 via channels. In the preferred construction, fluid port 2005 is a luer fitting. The fluid port 2005 is connected to the nozzle 1024 via a channel. The present invention includes a new easily replaceable integrated nozzle holder and nozzle. Barrel 2001,3001 of the nozzle holder is inserted into the container 4030 of cylindrical along the central axis of the flow conditioners manifold 1020. Notably, the circumferential groove 4071 of the manifold is adjacent to the port 2008 of the barrel 2001,3001 on Nozuruhoru da.

A gas that is diluted and aids in the evaporation of the liquid aerosol is supplied by a small blower 1001. The flow rate of this gas is measured as it passes through the flow measurement device 1023. This gas is heated when passing through the heater 1004. This high speed warm gas proceeds to port 5122 via attachment 1007. This gas stream is converted to a relatively uniform velocity stream as it passes through pressure equalization chambers 5021, 5222 and flow partitioners 5103, 5102. This fast dilution gas is relatively uniform when the output aerosol velocity enters the acceleration plate 6110 of the virtual impactor described in FIGS. 7A, 7B, 7C, 7D, 7E, 7F (see FIG. 6A). Is converted by this very low resistance flow conditioner to provide a uniform gas flow to the evaporation chamber 5100.

  As the aerosol flows through the evaporation chamber, it is mixed and further evaporated by the diluent gas. This evaporation is increased by infrared irradiation from the infrared lamp 6001. The solid phase aerosol enters the acceleration nozzles 7002, 7102, 7202 to form an aerosol jet. Most of the aerosol in these jets enters the deceleration nozzles 7003, 7103, 7203 and is transmitted to the output cone 7006. Most of the gas (which has a much smaller momentum than particles) is exhausted through the exhaust plume 7004.

  In order to facilitate rapid drying of the aqueous aerosol in an enclosed space, the aerosol plume from the compressed gas-powder nozzle is desirably suppressed and mixed with a diluent gas. This dilution gas should be warmed. US Patent Application 200701445 teaches the use of a coaxial counter-current jet to suppress the aerosol plume. However, there was neither a jet gas nor a backflow gas heated to 100 ° C. or higher. This hot gas provides the latent heat of evaporation which facilitates very rapid evaporation of the aerosol droplets. Despite the high input gas temperature, the temperature in the plume is generally below 30 ° C. The particles are cooled by the latent heat of evaporation. For this reason, this hot gas supply does not result in any denaturation of the protein as the aerosol is generated.

<Horizontal system>
The virtual impactor concentrator described in US Patent Application 200701445 has a cutoff of 2.5 micrometers. Prior art systems have eliminated the need to collect and resuspend the dry powder mixture, i.e. time consuming and potentially wasteful procedures. However, liquid-dry powder aerosol generators have used up to 300 liters of diluent gas at relatively high pressure (20-50 pounds per square inch). This requires a 5 horsepower compressor and a pressurized gas tank. Utilizing such large and expensive compressors and / or large pressurized gas tanks makes prior art devices impractical for home use.

  Several new features of the system of the present invention are a flow conditioner, a virtual impactor, and a replaceable cartridge / nozzle. In addition, further progress has been achieved by reducing the pressure loss through the gas heater and internal connections.

This facilitates the generation, dilution, evaporation and concentration of protein aerosols of less than 1 density that deliver a highly concentrated aerosol of particles for delivery to the airways of about 1 micrometer. This is a small device, whose dilution gas can be from the dilution gas blower downstream of the device with a pressure loss at a total volume flow of only 1-3 inches H ₂ O. This requires a substantial reduction in the characteristic pressure loss within the prior system US Patent Application Publication No. 200701445.

Claims (17)

  A nozzle for generating an aerosol from a fluid and a gas,
  A cone having an edge extending from a cone apex in a gas flow direction toward a cone base provided on the cone, at which the aerosolization circumference between the orifice and the cone A cone having at least one wet cone-shaped gas outlet channel connected to a nozzle gas supply channel forming an aerosolizing perimeter;
  At the cone base connected to the nozzle fluid supply channel, at least one annular fluid outlet port surrounding the edge, so that the fluid to be aerosol is generated by capillary forces and by a jet of gas exiting the orifice Negative pressure flows from the nozzle fluid supply channel, and the fluid flows from the annular fluid outlet port beyond the edge of the cone toward the apex of the cone which is aerosolized at the aerosolization circumference.
  A nozzle comprising:   A cylindrical stem having an outer stem wall having a stem outer diameter;
  An annulus having an annulus hole wall having an annulus inner diameter slightly larger than the stem outer diameter;
  Further comprising
  The cylindrical stem extends through the annulus hole and includes the wet cone-shaped gas outlet channel;
  The annular fluid outlet port is formed by an annular gap between the annulus hole wall and the outer stem wall.
  The nozzle according to claim 1.   The diameter difference between the annulus inner diameter and the stem outer diameter is 0.006 to 0.8 mm, and as a result, the annular gap width is 0.003 to 0.4 mm. The nozzle described.   The nozzle of claim 2, wherein the annulus has a front surface extending substantially perpendicular to the annular fluid outlet port.   The nozzle according to claim 4, wherein the stem protrudes beyond the front surface of the annulus by 0 to 1 mm.   The nozzle according to claim 4, wherein the front surface of the annulus is hydrophobic, but the outer stem wall is easily wetted by the fluid.   The diameter of the cone base of the wet cone-shaped gas outlet channel is substantially equal to the overall diameter of the outer stem, so that the stem of the cone base of the wet cone-shaped gas outlet channel ends. The nozzle according to claim 2, wherein the annular edge is a sharp annular lip.   The nozzle according to claim 1, wherein the wet cone-shaped gas outlet channel has an angle range of 15 to 80 degrees.   The nozzle according to claim 8, wherein the cone base has a diameter of 1 to 2 mm.   The nozzle according to claim 1, wherein the nozzle gas supply channel has a diameter of 0.005 mm to 1 mm.   A nozzle holder comprising a first end associated with a nozzle holder fluid injection port and a second end including the nozzle of claim 1,
  A barrel having an inner cylindrical barrel hole and an inner cylindrical barrel diameter;
  A nozzle body having a stem and a cylindrical top having an outer cylindrical top surface that fits snugly into a cylindrical barrel hole wall;
  With
  The cylindrical top has a plurality of circumferentially arranged grooves connected to the annular fluid outlet port.
  A nozzle holder characterized by that.   The nozzle body comprises a cylindrical nozzle body base having an outer cylindrical nozzle body base surface having an outer nozzle body base diameter,
  An annular fluid supply channel is formed between the outer cylindrical nozzle body base surface and the cylindrical barrel hole wall.
  The nozzle holder according to claim 11.   13. The barrel according to claim 12, wherein the barrel comprises a radial gas supply channel connected to the nozzle gas supply channel and supplying gas to a central gas supply channel having a diameter several times larger than the nozzle gas supply channel. Nozzle holder.   The nozzle holder is designed as a disposable part having a knob that is in close proximity to the first end of the nozzle holder and has a knob for inserting or removing the nozzle holder into an aerosol generator container. Item 12. A nozzle holder according to Item 11.   15. A nozzle holder according to claim 14, wherein the barrel has an outer cylindrical surface configured to fit snugly with an aerosol generator container.   The nozzle holder of claim 15, wherein the nozzle holder fluid injection port is a luer fitting configured to receive a disposable fluid cartridge.   The nozzle holder according to claim 16, wherein the nozzle holder and the fluid cartridge are preassembled as a single-use unit.

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