[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

WO2016077045A1 - Pressure modulated cryoablation system and related methods - Google Patents

Pressure modulated cryoablation system and related methods Download PDF

Info

Publication number
WO2016077045A1
WO2016077045A1 PCT/US2015/056780 US2015056780W WO2016077045A1 WO 2016077045 A1 WO2016077045 A1 WO 2016077045A1 US 2015056780 W US2015056780 W US 2015056780W WO 2016077045 A1 WO2016077045 A1 WO 2016077045A1
Authority
WO
WIPO (PCT)
Prior art keywords
pressure
fluid
catheter
tissue
cryogen
Prior art date
Application number
PCT/US2015/056780
Other languages
French (fr)
Inventor
Alexei Babkin
Original Assignee
Adagio Medical, Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Adagio Medical, Inc. filed Critical Adagio Medical, Inc.
Priority to AU2015347201A priority Critical patent/AU2015347201B2/en
Priority to CA2965314A priority patent/CA2965314C/en
Priority to CN201580061386.XA priority patent/CN107205766B/en
Priority to JP2017525853A priority patent/JP6607938B2/en
Priority to EP15858716.2A priority patent/EP3217903A4/en
Priority to BR112017009586-6A priority patent/BR112017009586B1/en
Priority to KR1020177012980A priority patent/KR101994471B1/en
Publication of WO2016077045A1 publication Critical patent/WO2016077045A1/en
Priority to IL251824A priority patent/IL251824B/en

Links

Classifications

    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B18/00Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body
    • A61B18/02Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body by cooling, e.g. cryogenic techniques
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B18/00Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body
    • A61B2018/00005Cooling or heating of the probe or tissue immediately surrounding the probe
    • A61B2018/00041Heating, e.g. defrosting
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B18/00Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body
    • A61B2018/00315Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body for treatment of particular body parts
    • A61B2018/00345Vascular system
    • A61B2018/00404Blood vessels other than those in or around the heart
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B18/00Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body
    • A61B2018/00571Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body for achieving a particular surgical effect
    • A61B2018/00577Ablation
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B18/00Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body
    • A61B18/02Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body by cooling, e.g. cryogenic techniques
    • A61B2018/0212Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body by cooling, e.g. cryogenic techniques using an instrument inserted into a body lumen, e.g. catheter
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B18/00Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body
    • A61B18/02Surgical instruments, devices or methods for transferring non-mechanical forms of energy to or from the body by cooling, e.g. cryogenic techniques
    • A61B2018/0231Characteristics of handpieces or probes
    • A61B2018/0262Characteristics of handpieces or probes using a circulating cryogenic fluid

Definitions

  • This invention relates to cryosurgery and more particularly to cryoablation catheters comprising a fluid operating near its critical point.
  • the pressure is modulated based on the temperature of the catheter.
  • the pressure is reduced.
  • FIG. 1 illustrates a typical cryogen phase diagram
  • FIG. 2 is a schematic illustration of a cryogenic cooling system
  • FIG. 4 provides a flow diagram that summarizes aspects of the cooling method of FIG. 2;
  • FIG.10A is a perspective view of a cryoablation catheter
  • FIG. 10B is a view taken along line 10B-10B of FIG. 10A;
  • the reduced pressure p is fixed at a constant value of approximately one, and hence at a fixed physical pressure near the critical pressure, while the reduced temperature t varies with the heat load applied to the device. If the reduced pressure p is a constant set by the engineering of the system, then the reduced molar volume v is an exact function of the reduced temperature t.
  • the operating pressure p may be adjusted so that over the course of variations in the temperature t of the device, v is maintained below some maximum value at which the vapor lock condition will result. It is generally desirable to maintain p at the lowest value at which this is true since boosting the pressure to achieve higher values of p may involve use of a more complex and more expensive compressor, resulting in more expensive procurement and maintenance of the entire apparatus support system and lower overall cooling efficiency.
  • heat exchange may be performed with a cryogen that is at a pressure that differs from ambient pressure, such as by providing the cryogen at lower pressure to create a colder ambient.
  • Step 510 recites to generate cryogen at or near critical pressure
  • Step 520 recites to lower the cryogen temperature. Step 520 may also be carried out, for example, as described above with reference to FIGS. 2-3
  • Step 522 recites to determine whether the catheter temperature is below a threshold value. Temperature measurement may be performed using thermocouples placed on the end of the treatment section, or within the transport channels or otherwise along the flow path so as to measure temperature of the apparatus itself, the cryogen, and/or the tissue. Indeed a plurality of temperature sensors may be placed throughout the tip, treatment section, the inlet flowpath, the return flowpath, and preferably, in direct contact with the cryogen to obtain an accurate measurement of real time temperature, temperature change over time, and temperature difference of the incoming cryogen versus the outgoing cryogen.
  • the pressure is decreased to a pre-set value as indicated by step 524.
  • the pressure is substantially reduced from the first relatively high (near critical) pressure to a second lower pressure once the apparatus tip or tissue reaches a target temperature.
  • the catheter freezing element or tissue temperature is lowered to a target cold temperature (for example, -100 degrees C)
  • a target cold temperature for example, -100 degrees C
  • the chilled tissue does not act as a heat sink (and warm) the flowing cryogen in the same way that the tissue initially acted as a heat sink to warm the cryogen.
  • the cryogen shall not have a tendency to transform from a liquid phase to vapor phase within the apparatus.
  • the cryogen is anticipated to remain as a liquid, and the gas molar volume does not increase during the flow cycle. Consequently, the em bodiment described in FIG.
  • FIGS. 6-8 are schematic diagrams illustrating various cryoablation systems having pressure modulation or adjustment components.
  • a cryoablation system 600 comprises a first cryogen flow path including a high pressure cryogen supply or generator 610, a cooling means 620, a cryoablation catheter 630, and a high pressure check valve 640.
  • Check valve 640 may operate to open at pressures ranging from, e.g., 400 to 480 psi.
  • the first flow path transports the cryogen for a first or initial phase to the treatment section of the catheter preferably under a near critical pressure. Vapor lock is avoided.
  • pressure regulator 750 is activated to cause a reduction in the pressure to a second low pressure P t . Consequently, a low pressure cryogen is transported through the cryoablation catheter 730 for treating an adjacent tissue. Vapor lock is avoided despite the reduction in pressure to a pressure substantially below near critical pressure because the instrument end section, and surrounding tissue is cold, and does not cause the cryogen fluid to change phase despite the decrease in pressure.
  • FIG. 8 illustrates another cryoablation system 800 capable of modulating the pressure.
  • Cryoablation system 800 comprises a cryogen supply 810, one way valve 812, a cooling means 820, a cryoablation catheter 830, and a check valve 840.
  • the system shown in FIG. 8 includes a piston 850 downstream of the one way valve 812.
  • the piston is activated to increase the pressure of the cryogen downstream of the one way valve 812 to a high pressure at or above near critical pressure.
  • piston is a fast activating member which can increase pressure instantaneously and maintain the desired high pressure for a selected time period.
  • the pressure P may be increased to near critical pressure P c periodically as shown in plot 9B.
  • the pressure time curve may be defined as a waveform having an amplitude and frequency.
  • the instrument and tissue decrease in temperature towards a lower steady state lethal target temperature.
  • Time period (t t ) is representative of a second treatment phase during which the instrument ablation is maintained at the low pressure P t .
  • the pressure may be decreased at a continuous rate as shown in Figure 9D.
  • FIG. 9D illustrates a straight profile, the profile may be curved or otherwise ramped towards the low treatment pressure Pt.
  • valves 814 and 862 are opened. Consequently, a low pressure cryogen is transported through the cryoablation catheter 830 for treating an adjacent tissue. Vapor lock is avoided despite the reduction in pressure to a pressure substantially below near critical pressure because the instrument end section, and surrounding tissue is cold, and does not cause the cryogen fluid to change phase despite the decrease in pressure.
  • system components including without limitation the piston, valves, pumps, switches, and regulators
  • the system components may be activated manually or in other embodiments via a controller.
  • a workstation or console as shown in FIG. 11 and described in the corresponding text may be provided to allow an operator to conveniently operate the cryoablation instrument.
  • the cryoablation apparatus of the present invention may have a wide variety of configurations.
  • one embodiment of the present invention is a flexible catheter 400 as shown in FIG. 10A.
  • the catheter 400 includes a proximally disposed housing or connector 410 adapted to fluidly connect to a fluid source (not shown).
  • a plurality of fluid transfer tubes 420 are shown extending from the connector 410. These tubes include a set of inlet fluid transfer tubes 422 for receiving the inlet flow from the connector and a set of outlet fluid transfer tubes 424 for discharging the outlet flow to the connector 410.
  • each of the fluid transfer tubes 422,424 is formed of material that maintains flexibility in a full range of temperatures from -200° C to am bient temperature.
  • each fluid transfer tube has an inside diameter in a range of between about 0.10 mm and 1.0 mm (preferably between about 0.20 mm and 0.50 mm).
  • Each fluid transfer tube may have a wall thickness in a range of between about 0.01 mm and 0.30 mm (preferably between about 0.02 mm and 0.10 mm).
  • An end cap 440 is positioned at the ends of the fluid transfer tubes 422, 424 to provide fluid transfer from the inlet fluid transfer tubes 422 to the outlet fluid transfer tubes 424.
  • the endcap is shown having an atraumatic tip.
  • the endcap 440 may be any suita ble element for providing fluid transfer from the inlet fluid transfer tubes 422 to the outlet fluid transfer tubes 424.
  • endcap 440 may define an internal chamber, cavity, or passage serving to fluidly connect tubes 422,424.
  • An outer sheath 430 is also shown in FIG. 10B surrounding the tube bundle 420.
  • the outer sheath serves to hold the tubes in a tubular arrangement, and protect the construct from being penetrated or disrupted by foreign objects and obstacles.
  • a temperature sensor 432 is shown on the surface of the distal section.
  • Temperature sensor may be a thermocouple to sense a temperature corresponding to the adjacent tissue, and sends the signal back through a wire in the tube bundle to the console for processing. Temperature sensor may be placed elsewhere along the shaft or within one or more of the fluid transport tubes to determine a temperature difference between inflow and outflow.
  • the fluid transfer tubes 420 are formed of annealed stainless steel or a polymer such as polyimide. In such configurations, the material may maintain flexibility at near critical temperature. In other embodiments, the transfer tube is shape- forming, deflectable, or steerable to make continuous firm contact with various anatomies. Other suitable device designs including deflectable designs are described in international patent application PCT/US2015/024778, filed April 7, 2015, entitled Endovascular Near Critical Fluid Based Cryoablation Catheter Having Plurality of Preformed Treatment Shapes.
  • the fluid transfer tubes are formed of a circular array, wherein the set of inlet fluid transfer tubes comprises at least one inlet fluid transfer tube defining a central region of a circle and wherein the set of outlet fluid transfer tubes comprises a plurality of outlet fluid transfer tubes spaced about the central region in a circular pattern.
  • the fluid transfer tubes 422,424 fall within this class of embodiments.
  • the cryogen fluid arrives at the catheter through a supply line from a suitable cryogen source at a temperature close to -200°C.
  • the cryogen is circulated through the multi-tubular freezing zone provided by the exposed fluid transfer tubes, and returns to the connector.
  • the nitrogen flow does not form gaseous bubbles inside the small diameter tubes under any heat load, so as to not create a vapor lock that limits the flow and the cooling power.
  • the vapor lock is eliminated as the distinction between the liquid and gaseous phases disappears.
  • a multi-tubular design may be preferably to a single tube design because the additional tubes can provide a substantial increase in the heat exchange area between the cryogen and tissue.
  • cryo instruments can increase the contact area several times over previous designs having similarly sized diameters with single shafts.
  • the invention is not intended to be limited to a single or multi-tube design except where specifically recited in the appended claims.
  • FIG. 11 illustrates a cryoablation system 950 having a cart or console 960 and a cryoablation catheter 900 detachably connected to the console via a flexible elongate tube 910.
  • the cryoablation catheter 900 which shall be described in more detail below in connection with FIG. 12, contains one or more fluid transport tubes to remove heat from the tissue.
  • the console 960 may include or house a variety of components (not shown) such as, for example, a generator, controller, tank, valve, pump, etc.
  • a computer 970 and display 980 are shown in FIG. 11 positioned on top of cart for convenient user operation.
  • Computer may include a controller, timer, or communicate with an external controller to drive components of the cryoablation systems such as a pump, valve or generator.
  • Input devices such as a mouse 972 and a keyboard 974 may be provided to allow the user to input data and control the cryoablation devices.
  • computer 970 is configured or programmed to control cryogen flowrate, pressure, and temperatures as described herein.
  • Target values and real time measurement may be sent to, and shown, on the display 980.
  • FIG. 12 shows an enlarged view of distal section of cryoablation apparatus 900.
  • the distal section 900 is similar in designs described above except that treatment region 914 includes a flexible protective cover 924.
  • the cover serves to contain leaks of the cryogen in the event one of the fluid transport tubes is breached. Although a leak is not expected or anticipated in any of the fluid delivery transport tubes, the protective cover provides an extra or redundant barrier that the cryogen would have to penetrate in order to escape the catheter during a procedure.
  • the protective cover may be formed of metal.
  • a thermally conducting liquid may be disposed within spaces or gaps between the transport tubes and the inner surface of the cover to enhance the device's thermal cooling efficiency during treatment.
  • the thermally conductive liquid is water.
  • Cover 924 is shown being tubular or cylindrically shaped and terminates at distal tip 912.
  • the cooling region 914 contains a plurality of fluid delivery and fluid return tubes to transport a cooling fluid through the treatment region 914 causing heat to be transferred/removed from the target tissue.
  • the fluid is transported through the tube bundle under physical conditions near the fluid's critical point in the phase diagram for a first time period, and then the pressure is reduced for a second time period as described herein.
  • the cover serves to, amongst other things, contain the cooling fluid and prevent it from escaping from the catheter in the event a leak forms in one of the delivery tubes.
  • FIG. 11-12 Although a cover is shown in Figures 11-12, the invention is not intended to be so limited except as where recited in the claims.
  • the apparatus may be provided with or without a protective cover and used to cool a target tissue.
  • Candidate tumors to be ablated with cryoenergy include target tissues and tumors in the thorax, and upper and lower Gl.
  • the devices described herein may also be applied to destroy or reduce target tissues in the head and neck.
  • An exemplary cardiovascular application is endovascular-based cardiac ablation to create elongate continuous lesions.
  • creating elongate continuous lesions in certain locations of the heart can serve to treat various conditions such as, for example, atrial fibrillation. See, for example, Patent Application No. 61/981,110, filed April 17, 2014, entitled Endovascular Near Critical Fluid Based Cryoablation Catheter Having Plurality of Preformed Treatment Shapes.
  • Methods and systems described herein serve to create lesions having a length ranging from 1-15 cm, or 2-10 cm., and more prefera bly between 5-8 cm.
  • the lesions are preferably continuous and linear, not a series of spots such as in some prior art point- ablation techniques.
  • cryoenergy and heat transfer may be focused on the endocardium, creating a lesion completely through the endocardium (a transmural lesion).
  • catheters achieve cooling power without vapor lock by modulating the pressure of the cooling fluid.
  • the cooling fluid is preferably transported near its critical point in the phase diagram for at least a portion of the time of energy activation, and then optionally reduced to a lower pressure.
  • a cardiac ablation catheter in accordance with the principals of the present invention can be placed in direct contact along the internal lining of the left atrium, thereby avoiding most of the massive heat-sink of flowing blood inside the heart as the ablation proceeds outward.
  • catheter configurations may include substantial bends, or loops which provide both the circumferential, as well as linear, ablations.
  • the catheters described herein may be manipulated to form ring-shaped lesions near or around the pulmonary vessel entries, for example.

Landscapes

  • Health & Medical Sciences (AREA)
  • Surgery (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Nuclear Medicine, Radiotherapy & Molecular Imaging (AREA)
  • Medical Informatics (AREA)
  • Engineering & Computer Science (AREA)
  • Biomedical Technology (AREA)
  • Heart & Thoracic Surgery (AREA)
  • Otolaryngology (AREA)
  • Molecular Biology (AREA)
  • Animal Behavior & Ethology (AREA)
  • General Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Veterinary Medicine (AREA)
  • Thermotherapy And Cooling Therapy Devices (AREA)
  • Surgical Instruments (AREA)

Abstract

A near critical fluid based cryoablation system comprises a cryoablation catheter for creating a lesion in tissue. A cryogenic fluid is transported under pressure through the catheter. A controller adjusts the pressure from a relatively high (e.g., near critical) pressure to a substantially lower pressure based on a condition during the catheter activation. In one configuration, the pressure is modulated based on the temperature of the catheter. When the temperature of the catheter reaches a target temperature, the pressure is reduced.

Description

NON-PROVISIONAL PATENT APPLICATION FOR
PRESSURE MODULATED CRYOABLATION SYSTEM AND RELATED METHODS
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] This International PCT patent application claims the benefit of US Provisional Patent Application No. 62/079,299, filed on November 13, 2014.
BACKGROUND OF TH E INVENTION
[0002] 1. Field of the Invention
[0003] This invention relates to cryosurgery and more particularly to cryoablation catheters comprising a fluid operating near its critical point.
[0004] 2. Description of the Related Art
[0005] Cryoablation is a surgical technique for ablating tissue by cooling or freezing the tissue to a lethal degree. Cryoablation has the benefit of minimizing permanent collateral tissue damage and has applicability to a wide range of therapies including the treatment of cancer and heart disease.
[0006] A shortcoming with certain cryosurgical systems, however, arises from the process of evaporation. The process of evaporation of a liquefied gas results in enormous expansion as the liquid converts to a gas; the volume expansion is on the order of a factor of 200. In a small-diameter system, this degree of expansion consistently results in a phenomenon known in the art as "vapor lock." The phenomenon is exemplified by the flow of a cryogen in a thin-diameter tube. The formation of a relatively massive volume of expanding gas impedes the forward flow of the liquid cryogen through the tubes.
[0007] Traditional techniques that have been used to avoid vapor lock have included restrictions on the diameter of the tube, requiring that it be sufficiently large to
accommodate the evaporative effects that lead to vapor lock. Other complex cryo- apparatus and tubing configurations have been used to "vent" N2 gas as it is formed along transport tubing. These designs also contributed to limiting the cost efficacy and tube diameter. [0008] There is accordingly a need for improved methods and systems for providing minimally invasive, safe and efficient cryogenic cooling of tissues.
SUMMARY OF THE INVENTION
[0009] An endovascular near critical fluid based cryoablation system for creating a lesion in tissue comprises a near critical fluid pressure source or generator; a near critical fluid cooler for cooling the near critical fluid; a near critical fluid based cryoablation catheter in fluid communication with the generator; and a controller operable to control the cooling power delivered from a distal treatment section of the catheter to the tissue to cool the tissue. The controller adjusts the pressure from a relatively high (for example, near critical) pressure to a substantially lower pressure based on a condition during the catheter activation.
[0010] In embodiments, the pressure is modulated based on the temperature of the catheter. When the temperature of the catheter reaches a target temperature, the pressure is reduced.
[0011] The description, objects and advantages of the present invention will become apparent from the detailed description to follow, together with the accompanying drawings.
BRIEF DESCRIPTION OF TH E DRAWINGS
[0012] FIG. 1 illustrates a typical cryogen phase diagram;
[0013] FIG. 2 is a schematic illustration of a cryogenic cooling system;
[0014] FIG. 3 is a cryogen phase diagram corresponding to the system shown in FIG. 2;
[0015] FIG. 4 provides a flow diagram that summarizes aspects of the cooling method of FIG. 2;
[0016] FIG. 5 is a flow diagram that summarizes aspects of another cooling method;
[0017] FIG. 6 is a schematic illustration of a cryogenic cooling system comprising a second flow path;
[0018] FIG. 7 is a schematic illustration of a cryogenic cooling system comprising a pressure regulator;
[0019] FIG. 8 is a schematic illustration of a cryogenic cooling system comprising a piston or diaphragm; [0020] FIGS. 9A-9D are pressure time curves corresponding to various pressure modulated cryogenic cooling systems;
[0021] FIG.10A is a perspective view of a cryoablation catheter;
[0022] FIG. 10B is a view taken along line 10B-10B of FIG. 10A;
[0023] FIG. 11 is an illustration of a cryoa blation system including a cryoa blation catheter; and
[0024] FIG. 12 is an enlarged perspective view of a distal section of the cryoa blation catheter shown in FIG. 11.
DETAI LED DESCRI PTION OF TH E I NVENTION
[0025] Before the present invention is described in detail, it is to be understood that this invention is not limited to particular variations set forth herein as various changes or modifications may be made to the invention described and equivalents may be su bstituted without departing from the spirit and scope of the invention. As will be apparent to those of skill in the art upon reading this disclosure, each of the individual embodiments described and illustrated herein has discrete components and features which may be readily separated from or combined with the features of any of the other several em bodiments without departing from the scope or spirit of the present invention. I n addition, many modifications may be made to adapt a particular situation, material, composition of matter, process, process act(s) or step(s) to the objective(s), spirit or scope of the present invention. All such modifications are intended to be within the scope of the claims made herein.
[0026] Methods recited herein may be carried out in any order of the recited events which is logically possible, as well as the recited order of events. Furthermore, where a range of values is provided, it is understood that every intervening value, between the upper and lower limit of that range and any other stated or intervening value in that stated range is encompassed within the invention. Also, it is contemplated that any optional feature of the inventive variations described may be set forth and claimed independently, or in com bination with any one or more of the features described herein.
[0027] All existing subject matter mentioned herein (e.g., pu blications, patents, patent applications and hardware) is incorporated by reference herein in its entirety except insofar as the su bject matter may conflict with that of the present invention (in which case what is present herein shall prevail). [0028] Embodiments of the invention make use of thermodynamic processes using cryogens that provide cooling without encountering the phenomenon of vapor lock.
[0029] CRYOGEN PHASE DIAGRAM AND N EAR CRITICAL POINT
[0030] This application uses phase diagrams to illustrate and compare various thermodynamic processes. An example phase diagram is shown in FIG. 1. The axes of the diagram correspond to pressure P and temperature T, and includes a phase line 102 that delineates the locus of all (P, T) points where liquid and gas coexist. For (P, T) values to the left of the phase line 102, the cryogen is in a liquid state, generally achieved with higher pressures and lower temperatures, while (P, T) values to the right of the phase line 102 define regions where the cryogen is in a gaseous state, generally achieved with lower pressures and higher temperatures. The phase line 102 ends abruptly in a single point known as the critical point 104. In the case of nitrogen N2, the critical point is at Pc=3.396 MPa and Tc=-147.15°C.
[0031] When a fluid has both liquid and gas phases present during a gradual increase in pressure, the system moves up along the liquid-gas phase line 102. In the case of N 2, the liquid at low pressures is up to two hundred times more dense than the gas phase. A continual increase in pressure causes the density of the liquid to decrease and the density of the gas phase to increase, until they are equal only at the critical point 104. The distinction between liquid and gas disappears at the critical point 104. The blockage of forward flow by gas expanding ahead of the liquid cryogen is thus avoided by conditions surrounding the critical point, defined herein as "near-critical conditions." Factors that allow greater departure from the critical point while maintaining a functional flow include greater speed of cryogen flow, larger diameter of the flow lumen and lower heat load upon the thermal exchanger, or cryo treatment region tip.
[0032] As the critical point is approached from below, the vapor phase density increases and the liquid phase density decreases until right at the critical point, where the densities of these two phases are exactly equal. Above the critical point, the distinction of liquid and vapor phases vanishes, leaving only a single, supercritical phase. All gases obey quite well the following van der Waals equation of state:
[0033] (p + 3/v2)(3v-l) = 8t [Eq. 1]
[0034] where p = P/Pc, v= V/Vc, and t=T/Tc, and Pc, Vc, and Tc are the critical pressure, critical molar volume, and the critical temperature respectively. [0035] The variables v, p, and t are often referred to as the "reduced molar volume," the "reduced pressure," and the "reduced temperature," respectively. Hence, any two substances with the same values of p, v, and t are in the same thermodynamic state of fluid near its critical point. Eq. 1 is thus referred to as embodying the "Law of Corresponding States." This is described more fully in H. E. Stanley, Introduction to Phase Transitions and Critical Phenomena (Oxford Science Publications, 1971), the entire disclosure of which is incorporated herein by reference for all purposes.
[0036] In embodiments of the invention, the reduced pressure p is fixed at a constant value of approximately one, and hence at a fixed physical pressure near the critical pressure, while the reduced temperature t varies with the heat load applied to the device. If the reduced pressure p is a constant set by the engineering of the system, then the reduced molar volume v is an exact function of the reduced temperature t.
[0037] In other embodiments of the invention, the operating pressure p may be adjusted so that over the course of variations in the temperature t of the device, v is maintained below some maximum value at which the vapor lock condition will result. It is generally desirable to maintain p at the lowest value at which this is true since boosting the pressure to achieve higher values of p may involve use of a more complex and more expensive compressor, resulting in more expensive procurement and maintenance of the entire apparatus support system and lower overall cooling efficiency.
[0038] The conditions that need to be placed on v depend in a complex and non-analytic way on the volume flow rate dV/dt, the heat capacity of the liquid and vapor phases, and the transport properties such as the thermal conductivity, viscosity, etc., in both the liquid and the vapor. This exact relationship is not derived here in closed form algebraically, but may be determined numerically by integrating the model equations that describe mass and heat transport within the device. Conceptually, vapor lock occurs when the rate of heating of the needle (or other device structure for transporting the cryogen and cooling the tissue) produces the vapor phase. The cooling power of this vapor phase, which is proportional to the flow rate of the vapor times its heat capacity divided by its molar volume, is not able to keep up with the rate of heating to the needle. When this occurs, more and more of the vapor phase is formed in order to absorb the excess heat through the conversion of the liquid phase to vapor in the cryogen flow. This creates a runaway condition where the liquid converts into vapor phase to fill the needle, and effectively all cryogen flow stops due to the large pressure that results in this vapor phase as the heat flow into the needle increases its temperature and pressure rapidly. This condition is called "vapor lock."
[0039] In accordance with one embodiment of the present invention, the liquid and vapor phases are substantially identical in their molar volume. The cooling power is at the critical point, and the cooling system avoids vapor lock. Additionally, at conditions slightly below the critical point, the apparatus may avoid vapor lock as well.
[0040] CRYOABLATION SYSTEMS
[0041] FIG. 2 provides a schematic illustration of a structural arrangement for a cryogenic system in one embodiment, and FIG. 3 provides a phase diagram that illustrates a thermodynamic path taken by the cryogen when the system of FIG. 2 is operated. The circled numerical identifiers in the two figures correspond so that a physical position is indicated in FIG. 2 where operating points identified along the thermodynamic path are achieved. The following description thus sometimes makes simultaneous reference to both the structural drawing of FIG. 2 and to the phase diagram of FIG. 3 in describing physical and thermodynamic aspects of the cooling flow.
[0042] For purposes of illustration, both FIGS. 2 and 3 make specific reference to a nitrogen cryogen, but this is not intended to be limiting. The invention may more generally be used with any suitable cryogen such as, for example, argon, neon, helium, hydrogen, and oxygen.
[0043] In FIG. 3, the liquid-gas phase line is identified with reference label 256 and the thermodynamic path followed by the cryogen is identified with reference label 258.
[0044] A cryogenic generator 246 is used to supply the cryogen at a pressure that exceeds the critical-point pressure Pc for the cryogen at its outlet, referenced in FIGS. 2 and 3 by label ©. The cooling cycle may generally begin at any point in the phase diagram having a pressure above or slightly below Pc, although it is advantageous for the pressure to be near the critical-point pressure Pc. The cooling efficiency of the process described herein is generally greater when the initial pressure is near the critical-point pressure Pc so that at higher pressures there may be increased energy requirements to achieve the desired flow. Thus, embodiments may sometimes incorporate various higher upper boundary pressure but generally begin near the critical point, such as between 0.8 and 1.2 times Pc, and in one embodiment at about 0.85 times Pc. [0045] As used herein, the term "near critical" is meant to refer to near the liquid-vapor critical point. Use of this term is equivalent to "near a critical point" and it is the region where the liquid-vapor system is adequately close to the critical point, where the dynamic viscosity of the fluid is close to that of a normal gas and much less than that of the liquid; yet, at the same time its density is close to that of a normal liquid state. The thermal capacity of the near critical fluid is even greater than that of its liquid phase. The combination of gas-like viscosity, liquid-like density and very large thermal capacity makes it a very efficient cooling agent. Reference to a near critical point refers to the region where the liquid-vapor system is adequately close to the critical point so that the fluctuations of the liquid and vapor phases are large enough to create a large enhancement of the heat capacity over its background value. The near critical temperature is a temperature within ±10% of the critical point temperature. The near critical pressure is between 0.8 and 1.2 times the critical point pressure.
[0046] Referring again to FIG. 2, the cryogen is flowed through a tube, at least part of which is surrounded by a reservoir 240 of the cryogen in a liquid state, reducing its temperature without substantially changing its pressure. In FIG. 2, reservoir is shown as liquid N 2, with a heat exchanger 242 provided within the reservoir 240 to extract heat from the flowing cryogen. Outside the reservoir 240, thermal insulation may be provided around the tube to prevent unwanted warming of the cryogen as it is flowed from the cryogen generator 246. At point ©, after being cooled by being brought into thermal contact with the liquid cryogen, the cryogen has a lower temperature but is at substantially the initial pressure. In some instances, there may be a pressure change, as is indicated in FIG. 3 in the form of a slight pressure decrease, provided that the pressure does not drop substantially below the critical-point pressure Pc, i.e. does not drop below the determined minimum pressure. In the example shown in FIG. 3, the temperature drop as a result of flowing through the liquid cryogen is about 50° C.
[0047] The cryogen is then provided to a device for use in cryogenic applications. In the exemplary embodiment shown in FIG. 2, the cryogen is provided to an inlet 236 of a catheter 224, such as may be used in medical cryogenic endovascular applications, but this is not a requirement.
[0048] Indeed, the form of the medical device may vary widely and include without limitation: instruments, appliances, catheters, devices, tools, apparatus', and probes regardless of whether such probe is short and rigid, or long and flexible, and regardless of whether it is intended for open, minimal, non-invasive, manual or robotic surgeries.
[0049] In embodiments, the cryogen may be introduced through a proximal portion of a catheter, continue along a flexible intermediate section of the catheter, and into the distal treatment section of the catheter. As the cryogen is transported through the catheter, and across the cryoablation treatment region 228, between la bels © and © in FIGS. 2 and 3, there may be a slight change in pressure and/or temperature of the cryogen as it moves through the interface with the device, e.g. cryoablation region 228 in FIG. 2. Such changes may typically show a slight increase in temperature and a slight decrease in pressure.
Provided the cryogen pressure remains above the determined minimum pressure (and associated conditions), slight increases in temperature do not significantly affect performance because the cryogen simply moves back towards the critical point without encountering the liquid-gas phase line 256, thereby avoiding vapor lock.
[0050] Thermal insulation along the shaft of the cryotherapy catheter (or apparatus, appliance, needle, probe, etc.) and along the support system that delivers near-critical freeze capability to these needles may use a vacuum.
[0051] Flow of the cryogen from the cryogen generator 246 through the catheter 224 or other device may be controlled in the illustrated embodiment with an assembly that includes a check valve 216, a flow impedance, and/or a flow controller. The catheter 224 itself may comprise a vacuum insulation 232 (e.g., a cover or jacket) along its length and may have a cold cryoablation region 228 that is used for the cryogenic applications. Unlike a Joule-Thomson probe, where the pressure of the working cryogen changes significantly at the probe tip, these embodiments of the invention provide relatively little change in pressure throughout the apparatus. Thus, at point ©, the temperature of the cryogen has increased approximately to ambient temperature, but the pressure remains elevated. By maintaining the pressure above or near the critical-point pressure Pc as the cryogen is transported through the catheter, the liquid-gas phase line 256 and vapor lock are avoided.
[0052] The cryogen pressure returns to ambient pressure at point ©. The cryogen may then be vented through vent 204 at substantially ambient conditions.
[0053] Examples of near critical fluid cryoablation systems, their components, and various arrangements are described in U.S. patent application Ser. No. 10/757,768 which issued as U.S. Pat. No. 7,410,484, on Aug. 12, 2008 entitled "CRYOTH ERAPY PROBE", filed Jan. 14, 2004 by Peter J. Littrup et al.; U.S. patent application Ser. No. 10/757,769 which issued as U.S. Pat. No. 7,083,612 on Aug. 1, 2006, entitled "CRYOTH ERAPY SYSTEM", filed Jan. 14, 2004 by Peter J. Littrup et al.; U.S. patent application Ser. No. 10/952,531 which issued as U.S. Pat. No. 7,273,479 on Sep. 25, 2007 entitled "METHODS AN D SYSTEMS FOR CRYOGEN IC COOLING" filed Sep. 27, 2004 by Peter J. Littrup et al. and U.S. Pat. No.
8,387,402 to Littrup et al., all of which are incorporated herein by reference, in their entireties, for all purposes.
[0054] A method for cooling a target tissue in which the cryogen follows a
thermodynamic path similar to that shown in FIG. 3 is illustrated with the flow diagram of FIG. 4. At block 310, the cryogen is generated with a pressure that exceeds the critical-point pressure and is near the critical-point temperature. The temperature of the generated cryogen is lowered at block 314 through heat exchange with a substance having a lower temperature. In some instances, this may conveniently be performed by using heat exchange with an ambient-pressure liquid state of the cryogen, although the heat exchange may be performed under other conditions in different embodiments. For instance, a different cryogen might be used in some embodiments, such as by providing heat exchange with liquid nitrogen when the working fluid is argon. Also, in other alternative
embodiments, heat exchange may be performed with a cryogen that is at a pressure that differs from ambient pressure, such as by providing the cryogen at lower pressure to create a colder ambient.
[0055] The further cooled cryogen is provided at block 318 to a cryogenic-application device, which may be used for a cooling application at block 322. The cooling application may comprise chilling and/or freezing, depending on whether an object is frozen with the cooling application. The temperature of the cryogen is increased as a result of the cryogen application, and the heated cryogen is flowed to a control console at block 326. While there may be some variation, the cryogen pressure is generally maintained greater than the critical-point pressure throughout blocks 310-326; the principal change in thermodynamic properties of the cryogen at these stages is its temperature. At block 330, the pressure of the heated cryogen is then allowed to drop to ambient pressure so that the cryogen may be vented, or recycled, at block 334. In other embodiments, the remaining pressurized cryogen at block 326 may also return along a path to block 310 to recycle rather than vent the cryogen at ambient pressure. [0056] PRESSURE MODULATION
[0057] FIG. 5 is a flow diagram 500 illustrating another embodiment of the invention.
[0058] Step 510 recites to generate cryogen at or near critical pressure and
temperature. Step 510 may be carried out, for example, as described above with reference to FIGS. 2-3.
[0059] Step 520 recites to lower the cryogen temperature. Step 520 may also be carried out, for example, as described above with reference to FIGS. 2-3
[0060] Step 522 recites to determine whether the catheter temperature is below a threshold value. Temperature measurement may be performed using thermocouples placed on the end of the treatment section, or within the transport channels or otherwise along the flow path so as to measure temperature of the apparatus itself, the cryogen, and/or the tissue. Indeed a plurality of temperature sensors may be placed throughout the tip, treatment section, the inlet flowpath, the return flowpath, and preferably, in direct contact with the cryogen to obtain an accurate measurement of real time temperature, temperature change over time, and temperature difference of the incoming cryogen versus the outgoing cryogen.
[0061] If the temperature is not below a threshold value, the pressure is not reduced.
[0062] If the temperature is below a threshold value, then the pressure is decreased to a pre-set value as indicated by step 524. In embodiments, after the cryo apparatus treatment section is placed adjacent the target tissue to be cooled, and the temperature is confirmed to be below a threshold value, the pressure is substantially reduced from the first relatively high (near critical) pressure to a second lower pressure once the apparatus tip or tissue reaches a target temperature.
[0063] Subsequent to determining whether the temperature is below a pre-set value and whether to reduce the pressure, step 530 recites to provide cryogen to a catheter. Step 530 may also be carried out, for example, as described above with reference to FIGS. 2-3.
[0064] Without being bound by theory, once the catheter freezing element or tissue temperature is lowered to a target cold temperature (for example, -100 degrees C), the above mentioned problem associated with vapor lock is minimized because the tissue surrounding the apparatus' treatment section is lowered (namely, frozen). The chilled tissue does not act as a heat sink (and warm) the flowing cryogen in the same way that the tissue initially acted as a heat sink to warm the cryogen. The cryogen shall not have a tendency to transform from a liquid phase to vapor phase within the apparatus. The cryogen is anticipated to remain as a liquid, and the gas molar volume does not increase during the flow cycle. Consequently, the em bodiment described in FIG. 5 provides an initial (or first) high pressure phase of cryogen operation, and a second low-pressure treatment phase. Exemplary pressures during the low pressure treatment phase range from 200 to 0 psi and temperatures in the range of -50 to -150 degrees C. Additionally, the time period for the initial high pressure and lower treatment phases range from 10 seconds to 1 minute, and 30 seconds to 4 minutes respectively.
[0065] A wide variety of systems may be employed to modulate the pressure between the high (near critical) pressure to a relatively low pressure. FIGS. 6-8 are schematic diagrams illustrating various cryoablation systems having pressure modulation or adjustment components.
[0066] With reference to FIG. 6, for example, a cryoablation system 600 comprises a first cryogen flow path including a high pressure cryogen supply or generator 610, a cooling means 620, a cryoablation catheter 630, and a high pressure check valve 640. Check valve 640 may operate to open at pressures ranging from, e.g., 400 to 480 psi. The first flow path transports the cryogen for a first or initial phase to the treatment section of the catheter preferably under a near critical pressure. Vapor lock is avoided.
[0067] After an initial phase, or at which point in time the measured temperature reaches a threshold temperature indicating that the adjacent tissue is substantially cooled, and that the risk of vapor lock is minimized, valve 660 is opened. The cryogen flows to low pressure valve 662, which opens at a second substantially lower pressure than check valve 640. The second low pressure valve may be programmed to open at a pressure ranging from 300 to 0 psi, and more preferably less than or equal to 200 psi. The cryogen may then be further processed, or released to the environment.
[0068] The valves described herein may be operated manually or, in embodiments, by using more sophisticated equipment such as a controller. The controller would operate to send signals to the valves and other system components to perform a cryoablation treatment.
[0069] The pressure modulated system described herein has both practical and safety advantages over a steady state near critical based cryoablation system. Lower pressure cryogen is easier to work with because there is less energy required to reach the operating pressure, the risk of a leak is less likely at low pressure, the consequences or damage arising from leaks is less with use of a cryogen under a lower pressure. In particular, a leak of a low pressure cryogen would have less impact on equipment, patient safety, and the operator than a leak of high pressure cryogen. Additionally, a low pressure cryogen may be vented directly to the atmosphere.
[0070] FIG. 7 illustrates another cryoablation system 700 capable of modulating the pressure. Similar to the system described above, cryoablation system 700 comprises a high pressure cryogen supply or generator 710, a cooling means 720, a cryoablation catheter 730, and a first check valve 740. A first flow path transports the cryogen for a first or initial phase to the treatment section of the catheter preferably under a near critical pressure. Vapor lock is avoided.
[0071] With reference to FIG. 9A, after the initial time period t,, pressure regulator 750 is activated to cause a reduction in the pressure to a second low pressure Pt. Consequently, a low pressure cryogen is transported through the cryoablation catheter 730 for treating an adjacent tissue. Vapor lock is avoided despite the reduction in pressure to a pressure substantially below near critical pressure because the instrument end section, and surrounding tissue is cold, and does not cause the cryogen fluid to change phase despite the decrease in pressure.
[0072] The pressure regulator and valves may be operated manually or, more preferably, using more sophisticated equipment such as a controller which sends signals to the valves and other system components to perform a cryoablation treatment as described herein.
[0073] FIG. 8 illustrates another cryoablation system 800 capable of modulating the pressure. Cryoablation system 800 comprises a cryogen supply 810, one way valve 812, a cooling means 820, a cryoablation catheter 830, and a check valve 840.
[0074] Additionally, the system shown in FIG. 8 includes a piston 850 downstream of the one way valve 812. The piston is activated to increase the pressure of the cryogen downstream of the one way valve 812 to a high pressure at or above near critical pressure. Preferably piston is a fast activating member which can increase pressure instantaneously and maintain the desired high pressure for a selected time period. For example, the pressure P may be increased to near critical pressure Pc periodically as shown in plot 9B. As such, the pressure time curve may be defined as a waveform having an amplitude and frequency. The instrument and tissue decrease in temperature towards a lower steady state lethal target temperature. Time period (tt) is representative of a second treatment phase during which the instrument ablation is maintained at the low pressure Pt.
[0075] Alternatively, the pressure may be modulated in steps as shown in FIG. 9C. The steps may decrease in equal increments, or non-linearly.
[0076] Still in another embodiment, the pressure may be decreased at a continuous rate as shown in Figure 9D. Although FIG. 9D illustrates a straight profile, the profile may be curved or otherwise ramped towards the low treatment pressure Pt.
[0077] With reference again to FIG. 8. after the initial phase, piston 850 is deactivated, and valves 814 and 862 are opened. Consequently, a low pressure cryogen is transported through the cryoablation catheter 830 for treating an adjacent tissue. Vapor lock is avoided despite the reduction in pressure to a pressure substantially below near critical pressure because the instrument end section, and surrounding tissue is cold, and does not cause the cryogen fluid to change phase despite the decrease in pressure.
[0078] As described further herein, the system components (including without limitation the piston, valves, pumps, switches, and regulators) may be activated manually or in other embodiments via a controller. A workstation or console as shown in FIG. 11 and described in the corresponding text may be provided to allow an operator to conveniently operate the cryoablation instrument.
[0079] CRYOABLATION CATH ETER
[0080] The cryoablation apparatus of the present invention may have a wide variety of configurations. For example, one embodiment of the present invention is a flexible catheter 400 as shown in FIG. 10A. The catheter 400 includes a proximally disposed housing or connector 410 adapted to fluidly connect to a fluid source (not shown).
[0081] A plurality of fluid transfer tubes 420 are shown extending from the connector 410. These tubes include a set of inlet fluid transfer tubes 422 for receiving the inlet flow from the connector and a set of outlet fluid transfer tubes 424 for discharging the outlet flow to the connector 410. In embodiments each of the fluid transfer tubes 422,424 is formed of material that maintains flexibility in a full range of temperatures from -200° C to am bient temperature. In embodiments, each fluid transfer tube has an inside diameter in a range of between about 0.10 mm and 1.0 mm (preferably between about 0.20 mm and 0.50 mm). Each fluid transfer tube may have a wall thickness in a range of between about 0.01 mm and 0.30 mm (preferably between about 0.02 mm and 0.10 mm).
[0082] An end cap 440 is positioned at the ends of the fluid transfer tubes 422, 424 to provide fluid transfer from the inlet fluid transfer tubes 422 to the outlet fluid transfer tubes 424. The endcap is shown having an atraumatic tip. The endcap 440 may be any suita ble element for providing fluid transfer from the inlet fluid transfer tubes 422 to the outlet fluid transfer tubes 424. For example, endcap 440 may define an internal chamber, cavity, or passage serving to fluidly connect tubes 422,424.
[0083] An outer sheath 430 is also shown in FIG. 10B surrounding the tube bundle 420. The outer sheath serves to hold the tubes in a tubular arrangement, and protect the construct from being penetrated or disrupted by foreign objects and obstacles.
[0084] A temperature sensor 432 is shown on the surface of the distal section.
Temperature sensor may be a thermocouple to sense a temperature corresponding to the adjacent tissue, and sends the signal back through a wire in the tube bundle to the console for processing. Temperature sensor may be placed elsewhere along the shaft or within one or more of the fluid transport tubes to determine a temperature difference between inflow and outflow.
[0085] In embodiments, the fluid transfer tubes 420 are formed of annealed stainless steel or a polymer such as polyimide. In such configurations, the material may maintain flexibility at near critical temperature. In other embodiments, the transfer tube is shape- forming, deflectable, or steerable to make continuous firm contact with various anatomies. Other suitable device designs including deflectable designs are described in international patent application PCT/US2015/024778, filed April 7, 2015, entitled Endovascular Near Critical Fluid Based Cryoablation Catheter Having Plurality of Preformed Treatment Shapes.
[0086] There are many configurations for tube arrangements. In embodiments the fluid transfer tubes are formed of a circular array, wherein the set of inlet fluid transfer tubes comprises at least one inlet fluid transfer tube defining a central region of a circle and wherein the set of outlet fluid transfer tubes comprises a plurality of outlet fluid transfer tubes spaced about the central region in a circular pattern. In the configuration shown in FIG. 10B, the fluid transfer tubes 422,424 fall within this class of embodiments.
[0087] During operation, the cryogen fluid arrives at the catheter through a supply line from a suitable cryogen source at a temperature close to -200°C. The cryogen is circulated through the multi-tubular freezing zone provided by the exposed fluid transfer tubes, and returns to the connector.
[0088] In embodiments, the nitrogen flow does not form gaseous bubbles inside the small diameter tubes under any heat load, so as to not create a vapor lock that limits the flow and the cooling power. By operating at the near critical condition for at least an initial period of energy application, the vapor lock is eliminated as the distinction between the liquid and gaseous phases disappears.
[0089] A multi-tubular design may be preferably to a single tube design because the additional tubes can provide a substantial increase in the heat exchange area between the cryogen and tissue. Depending on the number of tubes used, cryo instruments can increase the contact area several times over previous designs having similarly sized diameters with single shafts. However, the invention is not intended to be limited to a single or multi-tube design except where specifically recited in the appended claims.
[0090] CRYOABLATION CONSOLE
[0091] FIG. 11 illustrates a cryoablation system 950 having a cart or console 960 and a cryoablation catheter 900 detachably connected to the console via a flexible elongate tube 910. The cryoablation catheter 900, which shall be described in more detail below in connection with FIG. 12, contains one or more fluid transport tubes to remove heat from the tissue.
[0092] The console 960 may include or house a variety of components (not shown) such as, for example, a generator, controller, tank, valve, pump, etc. A computer 970 and display 980 are shown in FIG. 11 positioned on top of cart for convenient user operation. Computer may include a controller, timer, or communicate with an external controller to drive components of the cryoablation systems such as a pump, valve or generator. Input devices such as a mouse 972 and a keyboard 974 may be provided to allow the user to input data and control the cryoablation devices.
[0093] In embodiments computer 970 is configured or programmed to control cryogen flowrate, pressure, and temperatures as described herein. Target values and real time measurement may be sent to, and shown, on the display 980.
[0094] FIG. 12 shows an enlarged view of distal section of cryoablation apparatus 900. The distal section 900 is similar in designs described above except that treatment region 914 includes a flexible protective cover 924. The cover serves to contain leaks of the cryogen in the event one of the fluid transport tubes is breached. Although a leak is not expected or anticipated in any of the fluid delivery transport tubes, the protective cover provides an extra or redundant barrier that the cryogen would have to penetrate in order to escape the catheter during a procedure. In embodiments the protective cover may be formed of metal.
[0095] Additionally, a thermally conducting liquid may be disposed within spaces or gaps between the transport tubes and the inner surface of the cover to enhance the device's thermal cooling efficiency during treatment. In embodiments the thermally conductive liquid is water.
[0096] Cover 924 is shown being tubular or cylindrically shaped and terminates at distal tip 912. As described herein, the cooling region 914 contains a plurality of fluid delivery and fluid return tubes to transport a cooling fluid through the treatment region 914 causing heat to be transferred/removed from the target tissue. In em bodiments, the fluid is transported through the tube bundle under physical conditions near the fluid's critical point in the phase diagram for a first time period, and then the pressure is reduced for a second time period as described herein. The cover serves to, amongst other things, contain the cooling fluid and prevent it from escaping from the catheter in the event a leak forms in one of the delivery tubes.
[0097] Although a cover is shown in Figures 11-12, the invention is not intended to be so limited except as where recited in the claims. The apparatus may be provided with or without a protective cover and used to cool a target tissue.
[0098] APPLICATIONS
[0099] The systems and methods described herein may be used in a wide variety of medical applications including, for example, oncology and cardiovascular applications.
Candidate tumors to be ablated with cryoenergy include target tissues and tumors in the thorax, and upper and lower Gl. The devices described herein may also be applied to destroy or reduce target tissues in the head and neck.
[00100] An exemplary cardiovascular application is endovascular-based cardiac ablation to create elongate continuous lesions. As described herein, creating elongate continuous lesions in certain locations of the heart can serve to treat various conditions such as, for example, atrial fibrillation. See, for example, Patent Application No. 61/981,110, filed April 17, 2014, entitled Endovascular Near Critical Fluid Based Cryoablation Catheter Having Plurality of Preformed Treatment Shapes. [00101] Methods and systems described herein serve to create lesions having a length ranging from 1-15 cm, or 2-10 cm., and more prefera bly between 5-8 cm. The lesions are preferably continuous and linear, not a series of spots such as in some prior art point- ablation techniques. In accordance with the designs described above, the cryoenergy and heat transfer may be focused on the endocardium, creating a lesion completely through the endocardium (a transmural lesion). Additionally, in embodiments, catheters achieve cooling power without vapor lock by modulating the pressure of the cooling fluid. The cooling fluid is preferably transported near its critical point in the phase diagram for at least a portion of the time of energy activation, and then optionally reduced to a lower pressure.
[00102] A cardiac ablation catheter in accordance with the principals of the present invention can be placed in direct contact along the internal lining of the left atrium, thereby avoiding most of the massive heat-sink of flowing blood inside the heart as the ablation proceeds outward.
[00103] Additionally, catheter configurations may include substantial bends, or loops which provide both the circumferential, as well as linear, ablations. The catheters described herein may be manipulated to form ring-shaped lesions near or around the pulmonary vessel entries, for example.
[00104] Many modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.

Claims

CLAI MS We claim:
1. A near critical fluid based cryoa blation method for creating a lesion in tissue, the method comprising:
providing a cryotherapy catheter, the cryotherapy catheter comprising a flexible shaft, a distal section, and an active freeze region in the distal section;
advancing the distal section of the catheter into a patient's vasculature such that the active freeze region is adjacent the tissue to be cooled;
circulating a cryogenic fluid through the cryotherapy catheter for a first time period under physical conditions near a critical point of a liquid-vapor system for the cryogenic fluid, wherein the critical point defines a point in a phase diagram of the liquid-vapor system where molar volumes are su bstantially equivalent for liquid and gas, and whereby vapor lock associated with cooling of the cryotherapy catheter is avoided during the first time period; and
circulating the cryogenic fluid through the cryotherapy catheter at a low pressure PL for a second time period su bsequent to the first time period, wherein the PL is su bstantially less than a critical pressure Pc of the cryogenic fluid, and whereby vapor lock associated with cooling of the cryotherapy catheter is avoided during the second time period.
2. The method of claim 1, wherein the cryogenic fluid is nitrogen.
3. The method of claim 1, wherein the PL is less than 200 psi.
4. The method of claim 1, wherein the first period continues until a threshold
temperature is reached.
5. The method of claim 4, wherein the threshold temperature is -100 °C or less.
6. The method of claim 4, wherein the step of circulating the cryogenic fluid for a
second time period corresponds to a tissue treatment period effective to freeze a target volume of the tissue.
7. The method of claim 6, wherein the second time period ranges from 10 seconds to 2 minutes.
8. The method of claim 6, wherein the first time period ranges from 10 seconds to 1 minute.
9. The method of claim 1, wherein the physical conditions comprise pressure and the pressure is held substantially constant during the first time period.
10. The method of claim 1, wherein the physical conditions comprise pressure and the pressure is varied during the first time period.
11. The method of claim 1, wherein the physical conditions comprise pressure and the pressure is adjusted by actuating a low pressure valve, thereby switching a fluid path from a high pressure path to a low pressure path, serving to decrease the pressure of the fluid being transported through the distal treatment section of the catheter from the first fluid pressure to the second fluid pressure
12. The method of claim 1, wherein the physical conditions comprise pressure and the pressure is adjusted with a regulator.
13. The method of claim 1, wherein the physical conditions comprise pressure and the pressure is adjusted with a piston or diaphragm.
14. The method of claim 1, wherein the freeze region has a length ranging from 1-8 cm, and the steps of circulating the cryogenic fluid operate collectively to create an elongate lengthwise-continuous lesion in the tissue.
15. The method of claim 14, wherein the tissue is cardiac tissue and the lesion extends through a full thickness of heart wall.
16. A near critical fluid based cryoablation method for creating a lesion in tissue
comprising:
inserting a treatment region of a cryoablation catheter adjacent a target tissue to be cooled;
transporting a cryogenic fluid through the treatment region of the cryoablation catheter for an initial phase under a first pressure, said first pressure being at or above near critical pressure of the fluid; and
adjusting the first pressure to a second pressure lower than the first pressure for a treatment phase, whereby the target tissue is cooled to create the lesion as the cryogenic fluid is transported through the treatment region.
17. The method of claim 16, wherein the adjusting step is based on measuring a
temperature.
18. The method of claim 17, wherein the step of measuring is performed by measuring the temperature of the cryogenic fluid returning from the treatment region of the catheter.
19. The method of claim 16, wherein the step of adjusting is performed by switching from a first fluid path to a second fluid path.
20. The method of claim 19, wherein the switching step is performed by opening a valve downstream of the catheter.
21. An endovascular near critical fluid based cryoablation system for creating a lesion in tissue, the system comprising:
a first cryogenic fluid source comprising a fluid;
a cryogenic fluid cooler for cooling the fluid;
a cryoablation catheter comprising a distal treatment section, and a fluid path in fluid communication with the fluid source wherein the fluid is transported along the fluid path under pressure, and wherein the fluid comprises a molar volume of gas and a molar volume of liquid; and
a controller operable to control cooling power delivered from the distal treatment section to create the lesion, wherein the controller modulates the pressure from a first fluid pressure to a second fluid pressure less than the first fluid pressure, and wherein the first fluid pressure is at a near critical pressure of the fluid such that the molar volume of gas and the molar volume of liquid are substantially equivalent, and
wherein modulating the pressure from the first fluid pressure to the second fluid pressure is carried out without increasing the molar volume of gas in the fluid, thereby avoiding vapor lock associated with cooling the catheter.
22. The system of claim 21, wherein the distal section of the catheter further comprises a temperature sensor.
23. The system of claim 22, wherein the controller modulates the pressure based on a measured temperature from the temperature sensor.
24. The system of claim 23, wherein the controller operates to change the first fluid pressure to the second fluid pressure when the measured temperature reaches -100 °C or less.
25. The system of claim 21, further comprising a high pressure valve and a low pressure valve, and wherein the controller operates to switch the fluid path from the high pressure valve to the low pressure valve, serving to decrease the pressure of the fluid being transported through the distal treatment section of the catheter from the first fluid pressure to the second fluid pressure.
26. The system of claim 21, further comprising a pressure regulator in fluid
communication with the first fluid source, and wherein the controller operates to control the pressure regulator to adjust the pressure from the first fluid pressure to the second fluid pressure.
27. The system of claim 21, further comprising a piston in fluid communication with the first fluid source, and wherein the controller operates to control the piston to adjust the pressure from the first fluid pressure to the second fluid pressure.
28. The system of claim 21, further comprising a heat element in communication with the first fluid source, and for increasing the pressure of the fluid in the first fluid source to the first pressure.
29. The system of claim 21, further comprising a timer, wherein the controller is
operable to modulate the pressure based on information arising from the timer.
30. The system of claim 21, wherein the distal treatment section of the catheter
comprises an elongate shape ranging from 3 to 10 cm.
31. The system of claim 30, wherein the distal treatment section is deflectable.
32. The system of claim 21, wherein the fluid is cooled to a temperature near the critical temperature of the fluid.
33. The system of claim 21, wherein the fluid is Nitrogen.
34. The system of claim 21, wherein the second fluid pressure is less than or equal to 200 psi.
35. The system of claim 21, wherein the second pressure is less than or equal to am bient pressure.
PCT/US2015/056780 2014-11-13 2015-10-21 Pressure modulated cryoablation system and related methods WO2016077045A1 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
AU2015347201A AU2015347201B2 (en) 2014-11-13 2015-10-21 Pressure modulated cryoablation system and related methods
CA2965314A CA2965314C (en) 2014-11-13 2015-10-21 Pressure modulated cryoablation system and related methods
CN201580061386.XA CN107205766B (en) 2014-11-13 2015-10-21 Pressure regulated cryoablation system and related methods
JP2017525853A JP6607938B2 (en) 2014-11-13 2015-10-21 Pressure-regulated refrigeration ablation system and related method
EP15858716.2A EP3217903A4 (en) 2014-11-13 2015-10-21 Pressure modulated cryoablation system and related methods
BR112017009586-6A BR112017009586B1 (en) 2014-11-13 2015-10-21 CRYOABLATION SYSTEM
KR1020177012980A KR101994471B1 (en) 2014-11-13 2015-10-21 Pressure modulated cryoablation system and related methods
IL251824A IL251824B (en) 2014-11-13 2017-04-20 Pressure modulated cryoablation system and related methods

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201462079299P 2014-11-13 2014-11-13
US62/079,299 2014-11-13

Publications (1)

Publication Number Publication Date
WO2016077045A1 true WO2016077045A1 (en) 2016-05-19

Family

ID=55954846

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2015/056780 WO2016077045A1 (en) 2014-11-13 2015-10-21 Pressure modulated cryoablation system and related methods

Country Status (10)

Country Link
US (1) US10543032B2 (en)
EP (1) EP3217903A4 (en)
JP (1) JP6607938B2 (en)
KR (1) KR101994471B1 (en)
CN (1) CN107205766B (en)
AU (1) AU2015347201B2 (en)
BR (1) BR112017009586B1 (en)
CA (1) CA2965314C (en)
IL (1) IL251824B (en)
WO (1) WO2016077045A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019207426A1 (en) * 2018-04-27 2019-10-31 Biocompatibles Uk Limited Cryosurgical system with pressure regulation

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109846543B (en) 2013-09-24 2021-09-21 艾达吉欧医疗公司 Cryoablation catheter based on intravascular near-critical fluid and related methods
KR101905830B1 (en) 2016-11-15 2018-10-08 울산과학기술원 Cryoanesthesia device, method for controlling cryoanesthesia device and temperature controller of coolant in cryoanesthesia device
KR20180131356A (en) 2017-05-30 2018-12-10 주식회사 리센스메디컬 Medical cooling apparatus
WO2018221848A1 (en) 2017-05-30 2018-12-06 주식회사 리센스메디컬 Medical cooling device
US11564725B2 (en) 2017-09-05 2023-01-31 Adagio Medical, Inc. Ablation catheter having a shape memory stylet
KR102517065B1 (en) 2017-12-29 2023-04-03 주식회사 리센스메디컬 Cooling generator
AU2019206388B2 (en) 2018-01-10 2021-10-14 Adagio Medical, Inc. Cryoablation element with conductive liner
KR102145098B1 (en) * 2018-04-27 2020-08-18 울산과학기술원 Medical cooling device
EP4353285A3 (en) 2018-04-27 2024-04-24 Recensmedical, Inc. Cooling apparatus and cooling method
CN112955099B (en) 2018-07-27 2024-04-26 雷森斯医疗有限公司 Medical cooling device and cooling method using same
US11666479B2 (en) 2018-08-19 2023-06-06 Recensmedical, Inc. Device for cooling anesthesia by chilled fluidic cooling medium
USD921211S1 (en) 2019-06-21 2021-06-01 Recensmedical, Inc. Medical cooling device
USD921911S1 (en) 2019-06-21 2021-06-08 Recensmedical, Inc. Medical cooling device
US11963708B2 (en) * 2019-12-27 2024-04-23 Lifetech Scientific (Shenzhen) Co., Ltd. Left atrial appendage occluder and occlusion system
US11633224B2 (en) 2020-02-10 2023-04-25 Icecure Medical Ltd. Cryogen pump
US11278341B2 (en) 2020-07-14 2022-03-22 Recensmedical, Inc. Method of safely using controlled cooling systems and devices
USD968627S1 (en) 2020-08-07 2022-11-01 Recensmedical, Inc. Medical cooling device
USD968626S1 (en) 2020-08-07 2022-11-01 Recensmedical, Inc. Medical cooling device
USD977633S1 (en) 2020-08-07 2023-02-07 Recensmedical, Inc. Cradle for a medical cooling device
CN113197660B (en) * 2021-05-12 2022-12-09 上海导向医疗系统有限公司 Control method and system of single-channel cryoablation device and cryoablation system
US20240268877A1 (en) * 2021-06-07 2024-08-15 Ágil Therapeutics, Inc. Cryogenic catheter probe, system, and method for selective ablation of mucosa and submucosa of the gastrointestinal tract
CN113476134B (en) * 2021-06-30 2022-06-24 海杰亚(北京)医疗器械有限公司 Method and device for adjusting pressure in working medium storage tank
CN113616313B (en) * 2021-08-12 2022-07-26 上海导向医疗系统有限公司 Multi-channel cryoablation system and control method
CN117243689B (en) * 2023-09-15 2024-04-19 南京康友医疗科技有限公司 Microwave ablation system for preventing tissue carbonization

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050198972A1 (en) * 2004-03-10 2005-09-15 Lentz David J. Pressure-temperature control for a cryoablation catheter system
WO2006137887A2 (en) * 2004-09-27 2006-12-28 Cryodynamics, Llc. Methods and systems for cryogenic cooling
US8080005B1 (en) * 2010-06-10 2011-12-20 Icecure Medical Ltd. Closed loop cryosurgical pressure and flow regulated system
US20120053575A1 (en) * 2008-04-24 2012-03-01 Cryomedix, LLC. Method and System for Cryoablation Treatment
US20120059364A1 (en) 2009-11-02 2012-03-08 Baust John M Cryogenic Medical System
US20120209257A1 (en) * 2009-07-28 2012-08-16 Neuwave Medical, Inc. Energy delivery systems and uses thereof
US20130204241A1 (en) * 2012-02-07 2013-08-08 Cpsi Holdings Llc Dual thermal ablation device and method of use

Family Cites Families (192)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3062017A (en) 1959-09-30 1962-11-06 Air Reduction Oxygen dispensing
US3942010A (en) 1966-05-09 1976-03-02 The United States Of America As Represented By The Secretary Of The Navy Joule-Thomson cryostat cooled infrared cell having a built-in thermostat sensing element
US3613689A (en) 1970-01-13 1971-10-19 Frigitronics Of Conn Inc Cryosurgical apparatus
GB1422535A (en) 1972-06-16 1976-01-28 Spembly Ltd Cryogenic apparatus
US3889680A (en) 1974-02-07 1975-06-17 Armao T A Cryoadhesion preventing cryosurgical instruments
US3993123A (en) 1975-10-28 1976-11-23 International Business Machines Corporation Gas encapsulated cooling module
US4034251A (en) 1976-02-23 1977-07-05 North American Philips Corporation Transmission x-ray tube
US4167771A (en) 1977-06-16 1979-09-11 International Business Machines Corporation Thermal interface adapter for a conduction cooling module
JPS5496985A (en) 1978-01-18 1979-07-31 Toshiba Corp X-ray tube
JPS5539104A (en) 1978-09-12 1980-03-18 Toshiba Corp X-ray generator
US4226281A (en) 1979-06-11 1980-10-07 International Business Machines Corporation Thermal conduction module
CA1129015A (en) 1980-06-11 1982-08-03 Timofei S. Gudkin Thermoelectric cryoprobe
JPS5814499A (en) 1981-07-20 1983-01-27 Toshiba Corp X-ray generator
US4548045A (en) 1984-03-30 1985-10-22 General Foods Corporation Method for continuously producing pop-shaped frozen confections
US4843446A (en) 1986-02-27 1989-06-27 Hitachi, Ltd. Superconducting photodetector
US4838041A (en) 1987-02-05 1989-06-13 Gte Laboratories Incorporated Expansion/evaporation cooling system for microelectronic devices
US4802475A (en) 1987-06-22 1989-02-07 Weshahy Ahmed H A G Methods and apparatus of applying intra-lesional cryotherapy
US5147355A (en) 1988-09-23 1992-09-15 Brigham And Womens Hospital Cryoablation catheter and method of performing cryoablation
US4982080A (en) 1988-11-03 1991-01-01 Santa Barbara Research Center Radiation detecting array including unit cells with periodic output signals each within a unique frequency band
US5108390A (en) 1988-11-14 1992-04-28 Frigitronics, Inc. Flexible cryoprobe
US4960134A (en) 1988-11-18 1990-10-02 Webster Wilton W Jr Steerable catheter
CA2027550C (en) 1989-02-16 1995-12-26 Janusz B. Pawliszyn Apparatus and method for delivering supercritical fluid
US4945562A (en) 1989-04-24 1990-07-31 General Electric Company X-ray target cooling
US4946460A (en) 1989-04-26 1990-08-07 Cryo Instruments, Inc. Apparatus for cryosurgery
US5012505A (en) 1989-05-19 1991-04-30 Picker International, Inc. Fluidic slip ring for CT scanners
US5037395A (en) 1989-06-02 1991-08-06 Denco, Inc. Catheter for suppressing tunnel infection
DE69009109T2 (en) 1989-07-05 1994-09-15 Canon Kk Device and method for measuring light.
US5211646A (en) 1990-03-09 1993-05-18 Alperovich Boris I Cryogenic scalpel
US5147538A (en) 1990-04-19 1992-09-15 Electric Power Research Institute, Inc. Field-portable apparatus and method for analytical supercritical fluid extraction of sorbent materials
ZA917281B (en) 1990-09-26 1992-08-26 Cryomedical Sciences Inc Cryosurgical instrument and system and method of cryosurgery
US5212626A (en) 1990-11-09 1993-05-18 International Business Machines Corporation Electronic packaging and cooling system using superconductors for power distribution
JPH04196395A (en) 1990-11-28 1992-07-16 Hitachi Ltd Electronic computer and cooling device thereof
US5173606A (en) 1991-09-03 1992-12-22 United Technologies Corporation Superconductor electromagnetic radiation detector
US5254116A (en) 1991-09-06 1993-10-19 Cryomedical Sciences, Inc. Cryosurgical instrument with vent holes and method using same
US5520682A (en) 1991-09-06 1996-05-28 Cryomedical Sciences, Inc. Cryosurgical instrument with vent means and method using same
US5214925A (en) 1991-09-30 1993-06-01 Union Carbide Chemicals & Plastics Technology Corporation Use of liquified compressed gases as a refrigerant to suppress cavitation and compressibility when pumping liquified compressed gases
GB9123415D0 (en) 1991-11-05 1991-12-18 Clarke Brian K R Cryosurgical apparatus
US5531742A (en) 1992-01-15 1996-07-02 Barken; Israel Apparatus and method for computer controlled cryosurgery
US5274237A (en) 1992-04-02 1993-12-28 North American Philips Corporation Deicing device for cryogenically cooled radiation detector
US5275595A (en) 1992-07-06 1994-01-04 Dobak Iii John D Cryosurgical instrument
DE4227213C2 (en) 1992-08-17 1995-08-31 Kloeckner Moeller Gmbh Switch lock for a circuit breaker
US5324286A (en) 1993-01-21 1994-06-28 Arthur A. Fowle, Inc. Entrained cryogenic droplet transfer method and cryosurgical instrument
IL104506A (en) 1993-01-25 1997-11-20 Israel State Fast changing heating- cooling device and method, particularly for cryogenic and/or surgical use
US6161543A (en) 1993-02-22 2000-12-19 Epicor, Inc. Methods of epicardial ablation for creating a lesion around the pulmonary veins
US5433717A (en) 1993-03-23 1995-07-18 The Regents Of The University Of California Magnetic resonance imaging assisted cryosurgery
US5405533A (en) 1993-04-07 1995-04-11 General Atomics Heat transfer via dense gas in a fluid circulation system
JP3898754B2 (en) 1993-07-01 2007-03-28 ボストン サイエンティフィック リミテッド Imaging, potential detection and ablation catheters
US5400602A (en) 1993-07-08 1995-03-28 Cryomedical Sciences, Inc. Cryogenic transport hose
US5494039A (en) 1993-07-16 1996-02-27 Cryomedical Sciences, Inc. Biopsy needle insertion guide and method of use in prostate cryosurgery
US5417072A (en) 1993-11-08 1995-05-23 Trw Inc. Controlling the temperature in a cryogenic vessel
GB2283678B (en) 1993-11-09 1998-06-03 Spembly Medical Ltd Cryosurgical catheter probe
JP3528931B2 (en) 1993-11-17 2004-05-24 株式会社前川製作所 Liquid refrigerant supply / discharge method and apparatus
IL110176A (en) 1994-06-30 1999-12-31 Israel State Multiprobe surgical cryogenic apparatus
US5452582A (en) 1994-07-06 1995-09-26 Apd Cryogenics, Inc. Cryo-probe
US5471844A (en) 1994-11-18 1995-12-05 The United States Of America As Represented By The Secretary Of The Air Force High dissipation packaging for cryogenic integrated circuits
US5573532A (en) 1995-01-13 1996-11-12 Cryomedical Sciences, Inc. Cryogenic surgical instrument and method of manufacturing the same
US5661980A (en) 1995-06-06 1997-09-02 Hughes Missile Systems Company Thermally stabilized dewar assembly, and its preparation
US5741248A (en) 1995-06-07 1998-04-21 Temple University-Of The Commonwealth System Of Higher Education Fluorochemical liquid augmented cryosurgery
US5924975A (en) 1995-08-30 1999-07-20 International Business Machines Corporation Linear pump
US5901783A (en) 1995-10-12 1999-05-11 Croyogen, Inc. Cryogenic heat exchanger
US5733280A (en) 1995-11-15 1998-03-31 Avitall; Boaz Cryogenic epicardial mapping and ablation
US5997781A (en) 1996-04-04 1999-12-07 Mitsui Chemicals, Inc. Injection-expansion molded, thermoplastic resin product and production process thereof
US5716353A (en) 1996-05-03 1998-02-10 Urds, Corp. Cryosurgical instrument
US6039730A (en) 1996-06-24 2000-03-21 Allegheny-Singer Research Institute Method and apparatus for cryosurgery
US5800487A (en) 1996-07-23 1998-09-01 Endocare, Inc. Cryoprobe
US5899897A (en) 1996-09-26 1999-05-04 Allegheny-Singer Research Institute Method and apparatus for heating during cryosurgery
US6719755B2 (en) 1996-10-22 2004-04-13 Epicor Medical, Inc. Methods and devices for ablation
ES2176704T3 (en) 1996-11-01 2002-12-01 Bp Oil Int TEST DEVICE AND METHOD OF USE.
US6048329A (en) 1996-12-19 2000-04-11 Ep Technologies, Inc. Catheter distal assembly with pull wires
US5910104A (en) 1996-12-26 1999-06-08 Cryogen, Inc. Cryosurgical probe with disposable sheath
US5816052A (en) 1997-02-24 1998-10-06 Noran Instruments, Inc. Method and apparatus for mechanically cooling energy dispersive X-ray spectrometers
US5899898A (en) 1997-02-27 1999-05-04 Cryocath Technologies Inc. Cryosurgical linear ablation
US5868735A (en) 1997-03-06 1999-02-09 Scimed Life Systems, Inc. Cryoplasty device and method
US7220257B1 (en) 2000-07-25 2007-05-22 Scimed Life Systems, Inc. Cryotreatment device and method
US5757885A (en) 1997-04-18 1998-05-26 Siemens Medical Systems, Inc. Rotary target driven by cooling fluid flow for medical linac and intense beam linac
JP3398300B2 (en) 1997-05-28 2003-04-21 京セラ株式会社 Electronic equipment
US6171277B1 (en) 1997-12-01 2001-01-09 Cordis Webster, Inc. Bi-directional control handle for steerable catheter
US5971979A (en) 1997-12-02 1999-10-26 Odyssey Technologies, Inc. Method for cryogenic inhibition of hyperplasia
US5885276A (en) 1997-12-02 1999-03-23 Galil Medical Ltd. Method and device for transmyocardial cryo revascularization
US6190378B1 (en) 1997-12-05 2001-02-20 Massachusetts Institute Of Technology Cryosurgical instrument and related techniques
US5978697A (en) 1998-01-05 1999-11-02 Galil Medical Ltd. System and method for MRI-guided cryosurgery
US5916212A (en) 1998-01-23 1999-06-29 Cryomedical Sciences, Inc. Hand held cyrosurgical probe system
US6096068A (en) 1998-01-23 2000-08-01 Innercool Therapies, Inc. Selective organ cooling catheter and method of using the same
US6051019A (en) 1998-01-23 2000-04-18 Del Mar Medical Technologies, Inc. Selective organ hypothermia method and apparatus
US6378525B1 (en) 1998-01-29 2002-04-30 American Medical Systems, Inc. Combined cryotherapy and hyperthermia method for the treatment of airway obstruction or prostrate enlargement
US5947960A (en) 1998-02-26 1999-09-07 Brymill Corporation Venting cryosurgical instrument
US6602276B2 (en) 1998-03-31 2003-08-05 Innercool Therapies, Inc. Method and device for performing cooling- or cryo-therapies for, e.g., angioplasty with reduced restenosis or pulmonary vein cell necrosis to inhibit atrial fibrillation
US6142991A (en) 1998-03-31 2000-11-07 Galil Medical, Ltd. High resolution cryosurgical method and apparatus
US6251105B1 (en) 1998-03-31 2001-06-26 Endocare, Inc. Cryoprobe system
US6106518A (en) 1998-04-09 2000-08-22 Cryocath Technologies, Inc. Variable geometry tip for a cryosurgical ablation device
US6368304B1 (en) 1999-02-19 2002-04-09 Alsius Corporation Central venous catheter with heat exchange membrane
US6520933B1 (en) 1998-04-21 2003-02-18 Alsius Corporation Central venous line cooling catheter having a spiral-shaped heat exchange member
US6338727B1 (en) 1998-08-13 2002-01-15 Alsius Corporation Indwelling heat exchange catheter and method of using same
US6241722B1 (en) 1998-06-17 2001-06-05 Cryogen, Inc. Cryogenic device, system and method of using same
US6198974B1 (en) 1998-08-14 2001-03-06 Cordis Webster, Inc. Bi-directional steerable catheter
WO2000020795A2 (en) 1998-09-14 2000-04-13 Massachusetts Institute Of Technology Superconducting apparatuses and cooling methods
US6217518B1 (en) 1998-10-01 2001-04-17 Situs Corporation Medical instrument sheath comprising a flexible ultrasound transducer
US6190382B1 (en) 1998-12-14 2001-02-20 Medwaves, Inc. Radio-frequency based catheter system for ablation of body tissues
US6451011B2 (en) 1999-01-19 2002-09-17 Hosheng Tu Medical device having temperature sensing and ablation capabilities
US6592577B2 (en) 1999-01-25 2003-07-15 Cryocath Technologies Inc. Cooling system
US6554797B1 (en) 1999-02-19 2003-04-29 Alsius Corporation Method and system for patient temperature management and central venous access
US6648879B2 (en) 1999-02-24 2003-11-18 Cryovascular Systems, Inc. Safety cryotherapy catheter
US6432102B2 (en) 1999-03-15 2002-08-13 Cryovascular Systems, Inc. Cryosurgical fluid supply
US6347675B1 (en) 1999-03-15 2002-02-19 Tempress Technologies, Inc. Coiled tubing drilling with supercritical carbon dioxide
US6440126B1 (en) 1999-04-21 2002-08-27 Cryocath Technologies Cryoblation catheter handle
US6179831B1 (en) 1999-04-29 2001-01-30 Galil Medical Ltd. Method of cryoablating benign prostate hyperplasia
US6139544A (en) 1999-05-26 2000-10-31 Endocare, Inc. Computer guided cryosurgery
US6471694B1 (en) 2000-08-09 2002-10-29 Cryogen, Inc. Control system for cryosurgery
US6237355B1 (en) 1999-06-25 2001-05-29 Cryogen, Inc. Precooled cryogenic ablation system
US6270493B1 (en) 1999-07-19 2001-08-07 Cryocath Technologies, Inc. Cryoablation structure
US6263046B1 (en) 1999-08-04 2001-07-17 General Electric Company Heat pipe assisted cooling of x-ray windows in x-ray tubes
US6575966B2 (en) 1999-08-23 2003-06-10 Cryocath Technologies Inc. Endovascular cryotreatment catheter
US7527622B2 (en) 1999-08-23 2009-05-05 Cryocath Technologies Inc. Endovascular cryotreatment catheter
US6307916B1 (en) 1999-09-14 2001-10-23 General Electric Company Heat pipe assisted cooling of rotating anode x-ray tubes
US6530420B1 (en) 1999-09-17 2003-03-11 Sanyo Electric Co., Ltd. Heat carrier
US6235018B1 (en) 1999-10-29 2001-05-22 Cryoflex, Inc. Method and apparatus for monitoring cryosurgical operations
DE19956491C2 (en) 1999-11-24 2001-09-27 Siemens Ag X-ray tube with forced-cooled anode
JP2001174085A (en) 1999-12-16 2001-06-29 Nec Corp Electronic equipment
US6324852B1 (en) 2000-01-24 2001-12-04 Praxair Technology, Inc. Method of using high pressure LN2 for cooling reactors
SE519802C2 (en) 2001-02-09 2003-04-08 Wallsten Medical Sa Balloon catheter for application of pressure and heat
US6537271B1 (en) 2000-07-06 2003-03-25 Cryogen, Inc. Balloon cryogenic catheter
US6812464B1 (en) 2000-07-28 2004-11-02 Credence Systems Corporation Superconducting single photon detector
US6905492B2 (en) 2000-07-31 2005-06-14 Galil Medical Ltd. Planning and facilitation systems and methods for cryosurgery
US6486078B1 (en) 2000-08-22 2002-11-26 Advanced Micro Devices, Inc. Super critical drying of low k materials
US6551309B1 (en) 2000-09-14 2003-04-22 Cryoflex, Inc. Dual action cryoprobe and methods of using the same
AU2001289914A1 (en) 2000-09-25 2002-04-02 Sensovation Ag Image sensor device, apparatus and method for optical measurements
US6527765B2 (en) 2000-10-06 2003-03-04 Charles D. Kelman Cryogenic surgical system and method of use in removal of tissue
US6685720B1 (en) 2000-10-16 2004-02-03 Interventional Technologies Catheter having improved shaped retention
US6706037B2 (en) 2000-10-24 2004-03-16 Galil Medical Ltd. Multiple cryoprobe apparatus and method
US6432174B1 (en) 2000-11-13 2002-08-13 Westinghouse Savannah River Induced natural convection thermal cycling device
US6477231B2 (en) 2000-12-29 2002-11-05 General Electric Company Thermal energy transfer device and x-ray tubes and x-ray systems incorporating same
US6377659B1 (en) 2000-12-29 2002-04-23 Ge Medical Systems Global Technology Company, Llc X-ray tubes and x-ray systems having a thermal gradient device
US20020087152A1 (en) 2001-01-04 2002-07-04 Endocare, Inc. Systems and methods for delivering a probe into tissue
US20020151331A1 (en) 2001-04-02 2002-10-17 Amr Abdelmonem Cryo-cooled front-end system with multiple outputs
ATE489047T1 (en) 2001-05-31 2010-12-15 Endocare Inc CRYOGENE SYSTEM
US7192426B2 (en) * 2001-05-31 2007-03-20 Endocare, Inc. Cryogenic system
US6622507B2 (en) 2001-07-26 2003-09-23 International Business Machines Corporation Electromechanical device and a process of preparing same
US6572610B2 (en) 2001-08-21 2003-06-03 Cryogen, Inc. Cryogenic catheter with deflectable tip
US6767346B2 (en) 2001-09-20 2004-07-27 Endocare, Inc. Cryosurgical probe with bellows shaft
US6936045B2 (en) 2001-09-20 2005-08-30 Endocare, Inc. Malleable cryosurgical probe
US6628002B2 (en) 2001-10-02 2003-09-30 Margolin Development Heat transfer system with supracritical fluid
US20030088240A1 (en) 2001-11-02 2003-05-08 Vahid Saadat Methods and apparatus for cryo-therapy
US6781060B2 (en) 2002-07-26 2004-08-24 X-Ray Optical Systems Incorporated Electrical connector, a cable sleeve, and a method for fabricating an electrical connection
CA2467338A1 (en) 2001-12-19 2003-07-03 Conversion Gas Imports, L.L.C. Method and apparatus for warming and storage of cold fluids
US6737225B2 (en) 2001-12-28 2004-05-18 Texas Instruments Incorporated Method of undercutting micro-mechanical device with super-critical carbon dioxide
US6679315B2 (en) 2002-01-14 2004-01-20 Marconi Communications, Inc. Small scale chip cooler assembly
US6848458B1 (en) 2002-02-05 2005-02-01 Novellus Systems, Inc. Apparatus and methods for processing semiconductor substrates using supercritical fluids
US6989009B2 (en) 2002-04-19 2006-01-24 Scimed Life Systems, Inc. Cryo balloon
US7004937B2 (en) 2002-07-31 2006-02-28 Cryocor, Inc. Wire reinforced articulation segment
US6893433B2 (en) 2002-12-11 2005-05-17 Cryocor, Inc. System and method for performing a single step cryoablation
US7195625B2 (en) 2002-12-11 2007-03-27 Cryocor, Inc. Catheter system for performing a single step cryoablation
US20040118144A1 (en) 2002-12-20 2004-06-24 Hsu John S. Hermetic inverter/converter chamber with multiple pressure and cooling zones
US7083612B2 (en) 2003-01-15 2006-08-01 Cryodynamics, Llc Cryotherapy system
US7410484B2 (en) 2003-01-15 2008-08-12 Cryodynamics, Llc Cryotherapy probe
ES2442445T3 (en) * 2003-01-15 2014-02-11 Cryodynamics, Llc. Cryotherapy system
US6941953B2 (en) 2003-02-20 2005-09-13 Medwaves, Inc. Preformed catheter set for use with a linear ablation system to produce ablation lines in the left and right atrium for treatment of atrial fibrillation
AU2003901345A0 (en) 2003-03-21 2003-04-03 Ventracor Limited Improved cannula
US7220252B2 (en) 2003-07-18 2007-05-22 Polyzen, Inc. Inflatable dual balloon catheter
US20050027289A1 (en) 2003-07-31 2005-02-03 Thomas Castellano Cryoablation systems and methods
US8579892B2 (en) * 2003-10-07 2013-11-12 Tsunami Medtech, Llc Medical system and method of use
US7291142B2 (en) 2004-05-10 2007-11-06 Boston Scientific Scimed, Inc. Low temperature lesion formation apparatus, systems and methods
JP4593968B2 (en) 2004-05-14 2010-12-08 キヤノン株式会社 Position and orientation measurement method and apparatus
US7740627B2 (en) 2005-04-29 2010-06-22 Medtronic Cryocath Lp Surgical method and apparatus for treating atrial fibrillation
US7794455B2 (en) 2005-04-29 2010-09-14 Medtronic Cryocath Lp Wide area ablation of myocardial tissue
US8992515B2 (en) 2005-05-13 2015-03-31 Medtronic Cryocath Lp Coolant injection tube
US7842031B2 (en) 2005-11-18 2010-11-30 Medtronic Cryocath Lp Bioimpedance measurement system and method
US8641704B2 (en) 2007-05-11 2014-02-04 Medtronic Ablation Frontiers Llc Ablation therapy system and method for treating continuous atrial fibrillation
US20080312644A1 (en) 2007-06-14 2008-12-18 Boston Scientific Scimed, Inc. Cryogenic balloon ablation instruments and systems
EP2211743B1 (en) 2007-11-21 2017-08-02 Adagio Medical, Inc. Flexible multi-tubular cryoprobe
EP2211745B1 (en) 2007-11-21 2017-07-19 Endocare, Inc. Expandable multi-tubular cryoprobe
US8945106B2 (en) 2008-07-03 2015-02-03 Steve Arless Tip design for cryogenic probe with inner coil injection tube
US8475441B2 (en) 2008-12-23 2013-07-02 Cryomedix, Llc Isotherm-based tissue ablation control system
CA2756263A1 (en) * 2009-04-06 2010-10-14 Cryomedix Llc Single phase liquid refrigerant cryoablation system with multitubular distal section and related method
US8888768B2 (en) 2009-04-30 2014-11-18 Cryomedix, Llc Cryoablation system having docking station for charging cryogen containers and related method
US8298219B2 (en) 2009-09-02 2012-10-30 Medtronic Cryocath Lp Cryotreatment device using a supercritical gas
US9089314B2 (en) 2010-01-27 2015-07-28 Medtronic Cryocath Lp Partially compliant balloon device
CN103118613A (en) 2010-08-26 2013-05-22 克莱米迪克斯有限责任公司 Cryoablation balloon catheter and related method
US9095320B2 (en) 2010-09-27 2015-08-04 CyroMedix, LLC Cryo-induced renal neuromodulation devices and methods
CA2816072A1 (en) 2010-10-27 2012-05-03 Cryomedix, Llc Cryoablation apparatus with enhanced heat exchange area and related method
US20120109118A1 (en) 2010-10-29 2012-05-03 Medtronic Ablation Frontiers Llc Cryogenic-radiofrequency ablation system
WO2013013099A1 (en) 2011-07-19 2013-01-24 Adagio Medical, Inc. Methods and devices for the treatment of atrial fibrillation
WO2013013098A1 (en) 2011-07-19 2013-01-24 Adagio Medical, Inc. System and method for creation of cox maze lesions
US9283110B2 (en) 2011-09-20 2016-03-15 Zoll Circulation, Inc. Patient temperature control catheter with outer sleeve cooled by inner sleeve
CN102488550B (en) * 2011-11-29 2013-04-17 浙江大学 Low-temperature therapeutic apparatus for tumour
US10595937B2 (en) 2011-12-29 2020-03-24 St. Jude Medical, Atrial Fibrillation Division, Inc. System for optimized coupling of ablation catheters to body tissues and evaluation of lesions formed by the catheters
US9345528B2 (en) 2012-01-27 2016-05-24 Medtronic Cryocath Lp Large area cryoablation catheter with multi-geometry tip ECG/CRYO mapping capabilities
WO2013181660A1 (en) 2012-06-01 2013-12-05 Cibiem, Inc. Methods and devices for cryogenic carotid body ablation
CN103027742B (en) * 2012-12-31 2015-02-11 中国科学技术大学 Nuclear magnetic resonance compatible cold-thermal therapy system
US11026737B2 (en) * 2013-03-15 2021-06-08 Endocare, Inc. Cryogenic system and methods
US10492842B2 (en) 2014-03-07 2019-12-03 Medtronic Ardian Luxembourg S.A.R.L. Monitoring and controlling internally administered cryotherapy
CN103829999A (en) * 2014-03-12 2014-06-04 童师颖 Liquid nitrogen air minimally invasive cold knife cold and heat source system
EP3131487A4 (en) 2014-04-17 2017-12-13 Adagio Medical, Inc. Endovascular near critical fluid based cryoablation catheter having plurality of preformed treatment shapes

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050198972A1 (en) * 2004-03-10 2005-09-15 Lentz David J. Pressure-temperature control for a cryoablation catheter system
WO2006137887A2 (en) * 2004-09-27 2006-12-28 Cryodynamics, Llc. Methods and systems for cryogenic cooling
US20120053575A1 (en) * 2008-04-24 2012-03-01 Cryomedix, LLC. Method and System for Cryoablation Treatment
US20120209257A1 (en) * 2009-07-28 2012-08-16 Neuwave Medical, Inc. Energy delivery systems and uses thereof
US20120059364A1 (en) 2009-11-02 2012-03-08 Baust John M Cryogenic Medical System
US8080005B1 (en) * 2010-06-10 2011-12-20 Icecure Medical Ltd. Closed loop cryosurgical pressure and flow regulated system
US20130204241A1 (en) * 2012-02-07 2013-08-08 Cpsi Holdings Llc Dual thermal ablation device and method of use

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP3217903A4

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019207426A1 (en) * 2018-04-27 2019-10-31 Biocompatibles Uk Limited Cryosurgical system with pressure regulation
US11266458B2 (en) 2018-04-27 2022-03-08 Boston Scientific Scimed, Inc. Cryosurgical system with pressure regulation
US11813012B2 (en) 2018-04-27 2023-11-14 Boston Scientific Scimed, Inc. Cryosurgical system with pressure regulation

Also Published As

Publication number Publication date
IL251824A0 (en) 2017-06-29
EP3217903A1 (en) 2017-09-20
BR112017009586A2 (en) 2018-04-03
IL251824B (en) 2021-01-31
CA2965314A1 (en) 2016-05-19
US20160135864A1 (en) 2016-05-19
JP2017534396A (en) 2017-11-24
US10543032B2 (en) 2020-01-28
KR101994471B1 (en) 2019-06-28
AU2015347201A1 (en) 2017-06-29
KR20170089842A (en) 2017-08-04
CN107205766A (en) 2017-09-26
CA2965314C (en) 2021-07-06
JP6607938B2 (en) 2019-11-20
BR112017009586B1 (en) 2022-09-20
EP3217903A4 (en) 2018-05-30
AU2015347201B2 (en) 2018-05-10
CN107205766B (en) 2020-04-14

Similar Documents

Publication Publication Date Title
AU2015347201B2 (en) Pressure modulated cryoablation system and related methods
AU2019253840B2 (en) Endovascular near critical fluid based cryoablation catheter and related methods
US8298219B2 (en) Cryotreatment device using a supercritical gas
US7442190B2 (en) Contact assessment of balloon catheters
US10617459B2 (en) Endovascular near critical fluid based cryoablation catheter having plurality of preformed treatment shapes
US20100256621A1 (en) Single phase liquid refrigerant cryoablation system with multitubular distal section and related method
US20160249970A1 (en) Endovascular near critical fluid based cryoablation catheter having superelastic treatment section

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 15858716

Country of ref document: EP

Kind code of ref document: A1

ENP Entry into the national phase

Ref document number: 2965314

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 251824

Country of ref document: IL

REEP Request for entry into the european phase

Ref document number: 2015858716

Country of ref document: EP

ENP Entry into the national phase

Ref document number: 20177012980

Country of ref document: KR

Kind code of ref document: A

Ref document number: 2017525853

Country of ref document: JP

Kind code of ref document: A

NENP Non-entry into the national phase

Ref country code: DE

REG Reference to national code

Ref country code: BR

Ref legal event code: B01A

Ref document number: 112017009586

Country of ref document: BR

ENP Entry into the national phase

Ref document number: 2015347201

Country of ref document: AU

Date of ref document: 20151021

Kind code of ref document: A

ENP Entry into the national phase

Ref document number: 112017009586

Country of ref document: BR

Kind code of ref document: A2

Effective date: 20170505