WO2017086732A1 - 에어 포일 베어링 - Google Patents
에어 포일 베어링 Download PDFInfo
- Publication number
- WO2017086732A1 WO2017086732A1 PCT/KR2016/013329 KR2016013329W WO2017086732A1 WO 2017086732 A1 WO2017086732 A1 WO 2017086732A1 KR 2016013329 W KR2016013329 W KR 2016013329W WO 2017086732 A1 WO2017086732 A1 WO 2017086732A1
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- WO
- WIPO (PCT)
- Prior art keywords
- foil
- bump
- plate
- width
- air
- Prior art date
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/04—Shafts or bearings, or assemblies thereof
- F04D29/046—Bearings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
- F04D29/056—Bearings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C27/00—Elastic or yielding bearings or bearing supports, for exclusively rotary movement
- F16C27/02—Sliding-contact bearings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/06—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
Definitions
- the present invention relates to an air foil bearing, and more particularly to an air foil bearing with improved damping efficiency.
- a bearing is a mechanical element that secures the shaft in a fixed position and supports the shaft rotatably while supporting the weight of the shaft and the load on the shaft.
- Ball bearings and journal bearings support the shaft using an oil film
- foil bearings support the shaft by forming a high-pressure air layer between the top foil and the shaft.
- Air foil bearings support axial loads by introducing air, which is a viscous fluid between the rotor or the foil that contacts the disk when the rotor rotates at high speed, to create pressure.
- the air foil bearing is effective for supporting a rotating shaft rotating at high speed, it can be applied to a rotating shaft rotating at high speed in a rotary machine such as a turbo compressor, a turbo cooler, a turbo generator, and an air compressor.
- air foil bearings have a structure in which bump foils and top foils are disposed between a pair of disk-shaped plates. Since the load bearing capacity of the air foil bearing is determined by the total pressure of the air formed inside the bearing, it is necessary to increase the total pressure. However, the conventional air foil bearing does not have a structure that can increase the pressure of the air has a problem that it is difficult to improve the load bearing capacity.
- the air foil bearing of the present invention is an air foil bearing rotatably supporting a rotating shaft, wherein the air foil bearing has a disk-shaped plate and a plurality of bumps coupled on the plate. A foil and a top foil disposed on top of the bump foil, one end of which is coupled to the plate and the other end of which is free.
- the bump foil includes a plurality of single bumps arranged in a plurality of rows spaced apart from each other, and the stiffness of the single bump is gradually increased or equal to the outer diameter from the inner diameter side of the plate.
- each row of the single bump (A ⁇ D) is gradually increased toward the outer diameter of the plate, or the width (A ⁇ D) of the single bump is characterized in that a plurality of outer diameter side larger than the plurality of inner diameter side of the plate is formed It is done.
- the length of the bump acid L of the single bump is characterized in that it becomes larger toward the outer diameter side from the inner diameter side of the plate.
- the length of the arc of the single bump disposed on the inner and outer diameter side of the plate is characterized in that formed longer than the length of the arc of the single bump disposed on the inside.
- the bump foil includes first to fifth single bumps disposed to be inclined in a radial direction of the plate, wherein the first to fifth single bumps are spaced apart from each other in a first to fourth row, and the rigidity of the single bumps. Is gradually larger or the same from the inner diameter side of the plate toward the outer diameter.
- the widths A to D of the first to fourth rows of the single bumps are gradually increased toward the outer diameter of the plate.
- the widths C and D of the third and fourth rows of the single bumps may be larger than the widths A and B of the first and second rows of the plate.
- the length of the bump acid L of the single bump is characterized in that it becomes larger toward the outer diameter side from the inner diameter side of the plate.
- the length of the arcs of the first and fourth rows of the single bumps is longer than the length of the arcs of the second and third rows.
- the present invention also provides an air foil bearing rotatably supporting a rotating shaft, wherein the air foil bearing is disposed on a disk-shaped plate, a plurality of bump foils coupled to the plate, and an upper portion of the bump foil.
- a top foil having one end coupled to the plate and the other end free, the bump foil provides an air foil bearing comprising a first foil and a second foil disposed inside the first foil.
- the first foil and the second foil are spaced apart from each other with a slit interposed therebetween.
- the first foil is characterized in that it has a greater rigidity than the second foil.
- the first foil and the second foil is made of a different material.
- the first foil and the second foil is characterized in that made of the same material.
- the thickness of the first foil is characterized in that thicker than the thickness of the second foil.
- the bump width of the first foil is smaller than the bump width of the second foil.
- the second foil is formed with a slit bisecting the width inside, and the width of the slit between the first foil and the second foil is characterized in that corresponding to the slit width of the second foil.
- the second foil is formed with a slit bisecting a width inside, wherein the width of the slit between the first foil and the second foil is larger than the slit width of the second foil.
- the first foil and the second foil are provided in plural numbers, and the first foil and the second foil are disposed with second slits having different widths and shapes therebetween.
- the first slit between the first foil and the second foil is formed in the same width from one end to the other end.
- the second slit between the second foils is formed such that its width increases toward the opposite side of the trailing edge F from the trailing edge F connecting the first foil and the second foil at the rotor rotational side end thereof. It is characterized by that.
- the second slit between the second foils is characterized in that its width becomes stepwise larger toward the opposite side of the trailing edge (F).
- the second foil is characterized in that the width of the opposite end of the trailing edge F is smaller than the width of the trailing edge F side.
- the second foil includes at least one stepped portion that is bent in a step shape on one side facing each other, and a connection part extending along the rotor rotation direction to connect the stepped portion.
- the first foil is characterized in that the opposite end of the trailing edge F is spot welded.
- the bump height of the first foil is smaller than the bump height of the second foil.
- the distance D from the trailing edge F side end of the slit to the trailing edge F is less than or equal to twice the bump pitch C.
- the present invention provides an air foil bearing rotatably supporting a rotating shaft, wherein the air foil bearing includes a disc-shaped plate, a plurality of bump foils coupled to the plate, and an upper end of the bump foil. And a top foil coupled to the plate and free at the other end, wherein the bump foil includes first to fourth foils extending in a direction opposite to the rotor rotation direction.
- the first to fourth foils are characterized in that the ends corresponding to the rotor rotation direction are connected to one.
- the height of the first bump mountain A provided adjacent to the opposite end of the rotor rotation direction of each of the first to fourth foils and the other bump mountains adjacent to each other is different.
- the height of the first bump mountains A of the first to fourth foils is lower than the height of the other bump mountains adjacent to each other.
- the height of the first bump mountains A of the first to fourth foils is within 70% of the height of the other bump mountains adjacent to it.
- the top foil is characterized in that it has an inclined section (L1) is gradually spaced apart from the plate, and the planar section (L2) is evenly spaced apart from the plate.
- the first bump mountains A of the first to fourth foils may correspond to a position where the planar section L2 of the top foil starts.
- An end B adjacent the first bump acid A of the first and fourth foils is spot welded to the plate.
- Air foil bearing according to an embodiment of the present invention can adjust the stiffness of the bump by varying the width of the single bump, the height of the bearing because the height of the initial bump is all the same so that the wedge effect is implemented only when the load by the oil film There is an advantage to management.
- FIG. 1 is a cross-sectional view showing an example in which the air foil bearing of the present invention is installed
- FIG. 2 is a plan view showing an air foil bearing according to a first embodiment of the present invention
- FIG. 3 is a schematic diagram showing the bump foil according to FIG.
- FIG. 4 is a plan view showing an air foil bearing according to a second embodiment of the present invention.
- FIG. 5 is a plan view showing an air foil bearing according to a third embodiment of the present invention.
- 6 and 7 are a plan view showing a welded portion of the air foil bearing according to another embodiment
- FIG. 8 is a graph showing a pressure distribution according to the air foil bearing of FIG. 6,
- FIG. 9 is a plan view showing an air foil bearing according to a fourth embodiment of the present invention.
- FIG. 10 is a plan view and a side view of the air foil bearing according to the fifth embodiment of the present invention.
- FIG. 11 is a plan view illustrating an air foil bearing according to a sixth embodiment of the present invention.
- FIG. 1 is a cross-sectional view showing an example in which the air foil bearing of the present invention is installed.
- an air foil bearing according to an exemplary embodiment of the present invention is installed in a mechanical device having a rotating shaft rotating at high speed.
- the air foil bearing 700 is installed to support the rotating shaft 650 of the blower motor 600 mounted to the air compressor 10.
- the description is only one embodiment. Where the mechanism with rotary axis can be applied).
- the vehicle air compressor 10 may include a housing 100 forming an appearance, an impeller 400 coupled to the front of the housing 100 to compress air, an impeller receiving portion 200 accommodating the impeller 400, and It includes an impeller housing 300, a rear cover 500 coupled to the rear of the housing 100, and a blower motor 600 installed inside the housing 100 to drive the impeller 400 to rotate. .
- An air inlet 310 through which external air is introduced is formed at the front center of the impeller housing 300, and air outlets 330 are formed at both front sides.
- Impeller 400 is installed inside the impeller housing 300, the rotating shaft 650 of the blower motor 600 to be described later is coupled to the hollow penetrating the impeller 400. That is, the impeller 400 is supported by the rotation shaft 650. The air sucked through the air inlet 310 by the impeller 400 is compressed by the impeller 400 and discharged to the air outlet 330.
- the blower motor 600 is inserted into the motor housing 600a inserted inside the housing 100.
- the blower motor 600 is installed adjacent to the inner circumferential surface of the motor housing 600a and has a stator 630 having a hollow (not shown), a rotating shaft 650 installed through the hollow of the stator 630, and a rotating shaft ( Rotor 610 is coupled to the outer peripheral surface of the 650.
- the rotating shaft 650 is provided inside the housing 100 by a thrust bearing 700 and a journal bearing 750 installed at the rear of the impeller 400 in a state where one end is coupled to the hollow of the impeller 400. It is rotatably supported, and the rear end is also rotatably supported by the rear bearing 800.
- FIG. 2 is a plan view illustrating an air foil bearing according to a first exemplary embodiment of the present invention
- FIG. 3 is a schematic diagram illustrating a bump foil according to FIG. 2.
- a disk-shaped rotor disk (not shown) is formed on the front side of the rotating shaft 650, and the thrust bearing 700 is inserted adjacent to the front side and the rear side of the rotor disk (see FIG. 1).
- the thrust bearing 700 is an air foil bearing, and a plurality of fan-shaped bump foils are formed on a disc-shaped plate 702. 706 is seated and again covered with top foil 704.
- the center of the thrust bearing 700 is formed with a circular hole in which the rotation shaft 650 is inserted. With the rotating shaft 650 inserted into the hole of the thrust bearing 700, one surface of the bump foil 706 is adjacent to one surface of the rotor disk and the other surface is seated on the plate 702.
- the top foil 704 is formed with a free end, one end of which is fixed to the plate 702 and the other end of which is deformed apart from the plate 702.
- the bump foil 706 is formed in the shape of a fan plate and is in contact with the top foil 704 between the fixed end and the free end of the top foil 704. Top foil 704 and bump foil 706 are attached to plate 702 by welding.
- air which is a viscous fluid, flows between the air foils to form a pressure to support the load during rotation.
- the load bearing force is affected not only by the viscosity of the air but also by the stiffness of the bump foil 706.
- each single bump foil 706 is determined by the area of the bump projected on the plane, and the stiffness of the bump foil 706 goes from the inner diameter side to the outer diameter side of the plate 702 (1 to 4 rows). It is preferable to make them all uniform, or to become larger gradually. The reason for this is that the load is concentrated during rotation in the fourth row direction, so that the wear becomes more severe. Therefore, the rigidity in the fourth row direction is advantageous in terms of durability.
- the widths A to D of each row of the bump foil 706 are uniformly configured, and in this case, each single bump (means 1 to 5 in FIG. 3).
- the stiffness of each of 1 to 5 numbers sequentially becomes different.
- the rotational side stiffness in the rotational direction is lower than the inner diameter side, which is very disadvantageous for uniform stiffness distribution. Therefore, when the widths A to D of the single bumps are uniformly configured as in the related art, the rigidity of the bump foils 706 may not be configured to increase gradually toward the uniform or heavily loaded side.
- the diagonal length of the single bumps (1 to 5) (the part of the convex bump mountain when viewed from the side of the single bump, L) must be adjusted, and the diagonal length (L) is the single bump (1 to 5). It can be changed by adjusting the width (A ⁇ D) of each column of 5) (in this case, the bump mountain height of the single bump is all designed to be the same).
- a and B are the same if the width of each row of columns A to D of a single bump (1 to 5) is A, the width of two rows is B, the width of three columns is C, and the width of four columns is D.
- the length of the bump mountains L increases from one row to four columns, and the area of the single bumps also increases, thereby increasing the load bearing capacity.
- the wedge effect of preventing the leakage of air forming the oil film can be realized. .
- the air pocket P which traps air between the top foil 704 and the bump foil 706 by configuring the lengths of the single bumps 1 to 5 so that the second and third rows are indented into the first row and the fourth row. Area becomes large. Therefore, by the wedge effect (when the space in which the fluid is stored becomes wedge-shaped, the fluid is pulled by the viscosity of the fluid, pushed into the wedge-shaped gap, and the dynamic pressure (pressure) is generated, and the load is supported by this pressure). The loss of the oil film can be prevented. In addition, as the area of the air pocket P increases, the damping force is improved, so that the non-contact area of the top foil 704 is widened, thereby reducing the friction applied to the top foil 704.
- the wedge effect is implemented only when subjected to the load by the oil film, which is advantageous in managing the height of the thrust bearing 700.
- the stiffness also increases as the width of the single bumps increases. Therefore, the stiffness can be adjusted by varying the width of the single bump under the condition that the shape of the single bump is the same.
- Figure 5 is a plan view showing an air foil bearing according to a third embodiment of the present invention.
- the thrust bearing 700 is an air foil bearing, and a plurality of fan-shaped bump foils 706 are formed in a disc-shaped plate 702. Seated and covered with top foil 704 again.
- the center of the thrust bearing 700 is formed with a circular hole in which the rotation shaft 650 is inserted. With the rotary shaft 650 inserted into the hole of the thrust bearing 700, one surface of the bump foil 706 is adjacent the top foil 704 to one surface of the trust disk 652 and the other surface is seated on the plate 702. .
- the top foil 704 is formed with a free end, one end of which is fixed to the plate 702 and the other end of which is deformed apart from the plate 702.
- the fixed end of the top foil 704 is attached to the plate 702 by welding.
- the bump foil 706 is in the form of a flat plate and is in contact with the top foil 704 between the fixed end and the free end of the top foil 704.
- the bump foil 706 is composed of two foils, a foil having an approximately '-' shape forming a fan-shaped edge and a foil provided inside the '-' shaped foil.
- the bump foil 706 includes a connecting foil 706a constituting a fan-shaped radial edge, a first foil 706b constituting a fan-shaped outer diameter side edge, and a fan-shaped inner diameter edge 3rd foil 706d and 4th spaced apart between the 2nd foil 706c which comprises this, and each slit C1-C3 between the 1st foil 706b and the 2nd foil 706c. It consists of a foil 706e. In addition, the free ends of the third foil 706d and the fourth foil 706e are also spaced apart from the connecting foil 706a with the slit C4 interposed therebetween.
- An end portion of the third foil 706d is diagonally cut, and a diagonal cut is made correspondingly to the portion where the first foil 706b and the connecting foil 706a are diagonally cut.
- the diagonally cut portions are spaced apart from each other with the cutting slits 704a interposed therebetween.
- One end of the first to fourth foils 706b, 706c, 706d, and 706e is welded to the plate 702 (to be described later), and the other end extends along a circular arc direction.
- the lengths of the first to fourth foils 706b, 706c, 706d, and 706e become shorter from the first foil 706b to the fourth foil 706e.
- the third and fourth foils 706d and 706e are disposed on the side under less pressure generated during rotation, and thus, the first and second foils 706b and 2nd. It is preferable to be made of a material having a smaller rigidity than the foil 706c.
- the widths of the bumps constituting the third foil 706d and the fourth foil 706e are made wide so that the amount of deformation is reduced.
- the rigidity can be lowered than the first foil 706b and the second foil 706c.
- the aforementioned slit includes a first slit C1, a second slit C2, a third slit C3, and a fourth slit C4, wherein the first to third slits C1 to C3 are made of
- the first to fourth foils 706b, 706c, 706d, and 706e serve to maintain a minimum gap so as not to contact each other.
- the fourth slit C4 is connected to the foil 706a even when the bump acids of the third and fourth foils 706d and 706e are pressed when the bump foil 706 is deformed so that the third and fourth foils 706d and 706e are tensioned. It is desirable to have a gap that is not in contact with.
- the direction in which the fluid is introduced while the rotor is rotated is introduced in the axial direction and the rotor rotation direction, in which case the fluid introduced into the fourth slit C4 and the first to third slits C1 to C3 is simultaneously or When introduced randomly, it is possible to form a space that provides a stable movement of the fluid can improve the stable damping ability.
- All of the first to third slits C1 to C3 are formed in the circumferential direction of the plate 702, and the fourth slit C4 is formed in the radial direction to stably perform vibration damping according to inflow and outflow of fluid. can do.
- the thrust bearing 700 according to the third embodiment of the present invention is configured in the same manner as in the above-described second embodiment, and the interval between the first to third slits C1 to C3 is different. Can be set.
- the interval between the first to third slits C1 to C3 may be designed to be the same as the fourth slit C4.
- the width of the third foil 706d 'and the fourth foil 706e' is formed to be smaller than the width of the first foil 706b 'and the second foil 706c', which is the third foil. 706d 'and the fourth foil 706e' perform different damping from the first foil 706b 'and the second foil 706c', thereby stably supporting and dispersing the axial stress applied to the rotor. To prevent breakage.
- the thrust bearing 700 ' according to the third embodiment of the present invention has a different damping and load than the second embodiment described above. You have support.
- the damping amount is changed and the deformation amount of the third foil 706d 'and the fourth foil 706e' is larger than in the second embodiment, thereby minimizing stress concentration and load in the axial direction due to the inflow and movement of the fluid. can do.
- the vibration applied to the rotor is minimized, thereby improving the vibration damping efficiency in the axial direction.
- the vibration and shock transmitted to the compressor or air blower to improve the durability and vibration damping ability at the same time can be used stably in long-term use.
- 6 and 7 are plan views illustrating a welded portion of an air foil bearing according to another embodiment.
- the bump foils 706 and 706 are formed of approximately 'C' shaped first foils 706a and 706a constituting a fan-shaped edge and a first foil 706a.
- second foils 706b and 706b ' which are disposed inside the 706a' and are spaced apart from each other with the first foils 706a and 706a 'and the slits 706c and 706c' interposed therebetween.
- One end of the first foil 706a, 706a 'and the second foil 706b, 706b' may be welded to the plate 702, and the other end may be formed to extend in a circular arc direction (FIGS. 6 and 7).
- 4 and 5 have only the same reference numerals as those of the embodiments of FIGS. 4 and 5, and thus the detailed description of each configuration will be omitted.
- the welded portions (parts corresponding to 706f, 706f 'in Figs. 4 and 5) are disposed on the rotor rotational side.
- the welded portions are formed to be narrower in width than the first foils 706a and 706a 'and the second foils 706b and 706b' and are installed to maintain only a fixed state.
- the welded portion is not formed with an uneven portion such as bump acid, the welded portion is stably maintained without being damped in accordance with the inflow and discharge of the fluid.
- FIG. 8 is a graph illustrating a pressure distribution according to the air foil bearing of FIG. 6.
- the radial direction of the plate 702 (defining the center side of the plate at any point in FIG. 2 is defined as d1 and the outer diameter side as d2).
- the pressure of the bump foil 706 is called P1.
- P2 is the pressure of the bump foil 706 along the radial direction of the plate 702 when the first foil 706a and the second foil 706b are provided according to an embodiment of the present invention.
- pressure is concentrated between the radially inner (d1) and the outer (d2), whereas in the case of P2, the pressure is relatively evenly distributed between the radially inner (d1) and the outer (d2). Can be.
- the contact of the bump foil 706 and the top foil 704 of the portion may be increased, thereby increasing the wear of the top foil 704.
- the edges of the bump foil 706 close to the inner side d1 and the outer side d2 of the radial radius may have a low load bearing force and thus may not be sufficiently pressured.
- the load bearing force is improved, so that radially inner side d1 and outer side d2 also have sufficient pressure. You can get The pressure distribution P2 is thus evenly distributed without concentrating the pressure in one place.
- Air foil bearing according to an embodiment of the present invention having the configuration described above has the effect of improving the load bearing capacity and increase the damping effect by changing the shape and rigidity of the bump foil.
- the durability of the bearing is improved by improving the damping force.
- the air foil bearing according to the above embodiments by changing the shape of the bump foil and the shape of the slit it is possible to prevent the end of the bump foil to protrude sharply during deformation of the bump foil.
- the shapes of the bump foil and the slit are changed will be described in detail, and the shape may be applied to the above-described embodiments (a detailed description of the same configuration as the above-described embodiments will be omitted.
- the outer arc of the fan shape is defined as the outer diameter side and the inner arc as the inner diameter direction based on FIG. 9).
- FIG. 9 is a plan view illustrating an air foil bearing according to a fourth exemplary embodiment of the present invention.
- bump foils 706a ′′ and 706b ′′ are provided between the top foil 704 ′′ and the plate 702 ′′ of the air foil bearing.
- the bump foils 706a “and 706b” are the first foil 706a "disposed on the outer diameter and the inner diameter side of the top foil ⁇ based on the rotation direction of the rotor (arrow direction in Fig. 5) and the first foil 706a". ) Is composed of a second foil 706b "disposed in between (in this embodiment, the first foil is composed of two and the second foil is described as an example).
- the trailing edge F is a rotor. It is the portion connecting the first foil 706a "and the second foil 706b" at the end in the direction of rotation.
- the bump foils 706a “and 706b” are the widths (spacings) of the slits 706c “and 706d” and the bump widths B to B “of the bump foils 706a” and 706b “as in the above-described embodiment.
- the individual stiffness of each of the first foil 706a “and the second foil 706b” can be adjusted.
- the bump widths B to B "of the second foil 706b” are more specifically adjusted. By adjusting the stiffness can be adjusted.
- the bump foils 706a “and 706b” are divided into a plurality of slits 706c “and 706d", and the first slit between the first foil 706a “and the second foil 706b” 706c ′′ and the second slit 706d ′′ between the second foil 706b ′′ are different in shape.
- the second slit 706d "located between the two second foils 706b" differs in width from one end to the other end facing the trailing edge F (slit between the second slits also trailing). The opposite end of the edge is open).
- the second foil 706b is comprised of longer and shorter lengths corresponding to the rotor rotational direction than the other.
- the second slit 706d located between them is in the form of a stepped step, trailing edge
- the width of the second slit 706d “becomes narrower toward F. That is, the bump widths B to B" of the second foil 706b "may be configured differently for each section.
- the second long foil 706b ′′ having a relatively long length is formed with a first stepped portion 7060 at one end portion adjacent to the trailing edge F, and the trailing edge F at the first stepped portion 7060.
- the first connecting portion 7071 is formed to extend in the opposite direction to the C.
- a second step portion 7062 is formed again, and trailing from the second step portion 7082.
- the second connection portion 7063 extends toward the opposite end of the edge F. Since the stepped direction is toward the outer diameter side, the bump width B ′ of the first connection portion 7071 is the second connection portion 7063. Is greater than the bump width (B).
- the relatively short second foil 706b ′′ may be formed at a portion spaced apart from the trailing edge F by the first step portion 7060 on one side facing the long second foil 706b ′′.
- Three stepped portions 7065 may be provided. That is, the third connection portion 7094 is provided at the portion adjacent to the trailing edge F, and the fourth connection portion 7066 is provided at the opposite side of the trailing edge F, and the third step portion 7027 is disposed therebetween. ) Can be connected. At this time, since the stepped direction is toward the inner diameter side, the bump width B ′′ of the fourth connection portion 7066 is narrower than the bump width (not shown) of the third connection portion 7094.
- the bump width B of the second connector 7063 and the bump width B ′′ of the fourth connector 7066 may be the same or different according to design specifications.
- the stiffness of the trailing edge F region can have a higher stiffness than the center part E region.
- the stiffness of the trailing edge (F) region can be adjusted.
- the distance D from the ends of the slits 706c ′′, 706d ′′ to the trailing edge F is preferably designed to be less than or equal to twice the bump pitch C (D ⁇ 2C).
- the height of the bump mountain and the bump width may be changed to improve the load bearing force and the damping effect.
- a detailed structure will be described with reference to the drawings. (Bump foils of the present embodiment have only the same reference numerals as those of the fourth embodiment and have the same structure, and thus detailed description of the bump foils will be omitted).
- FIG. 10 is a plan view and a side view showing an air foil bearing according to a fifth embodiment of the present invention
- FIG. 11 is a plan view showing an air foil bearing according to a sixth embodiment of the present invention.
- the top foil 704 has a fixed end and a bump foil 706 is inserted between the plate 702 so that the other end of the top foil 704 is the free end of the top foil 704 with the plate 702. It is a structure that is spaced apart. Therefore, the top foil 704 is formed with an inclined section L1 in which the distance from the fixed end side toward the free end side gradually increases with the plate 702. When a predetermined position passes after the inclined section L1, a planar section L2 having a uniform interval between the top foil 704 and the plate 702 is formed.
- the portion where the planar section L2 is formed corresponds to the portion of the first leading edge A of the bump foil 706 based on the rotor rotation direction. That is, the first bump mountain portion A of the first to fourth foils 706a to 706d becomes the start position of the plane section L2.
- the highest point of the top foil 704 and the first bump mountain A by setting the height of the first bump mountain A of the first to fourth foils 706a to 706d lower than the adjacent bump mountain (second or more).
- a gap is formed in the liver, a thin oil film is first formed along the shape of the top foil 704 due to the film stiffness of the top foil 704 and the stiffness of the bump acid after the second.
- the load applied to the bump foil 706 is gradually increased to increase the pressure of the oil film.
- the lowered first bump mountain A contacts the top foil 704 and deforms to support the load (activation).
- the first bump acid A is positioned in the plane section L2 of the top foil 704 in order to be uniformly pressurized when the first bump acid A is activated. As the first bump mountain A supports the load, the planar section L2 increases so that the thrust bearing 700 has a higher load bearing capacity.
- the height of the first bump mountain A be configured to be up to 30% lower than the height of the other bump mountain. That is, the height of the first bump mountain A is formed to be within 70% of the height of the other bump mountain.
- the rotor 610 is excited while vibrating by an external force.
- the rotor 610 has a set gap (gap at the initial position) with the thrust bearing 700 at the initial position, but the set gap increases or decreases due to the excitation.
- the bump foil 706 is pressed and restored to repeat, and when the bump foil 706 is pressed and the maximum restored displacement, the bump foil 706 is pressed to approximately 30% of the bump acid of the bump foil 706. And restored (measurement of displacement of the rotor over time).
- the height of the first bump mountain (A) within 30% of the other bump mountain height, it is possible to properly support the load due to the pressure when a certain pressure or more is applied to the thrust bearing 700.
- the lengths of the second foil and the third foil may be changed.
- the non-welded end E of the second foil 706b 'and the third foil 706c' connects the welded end B of the first foil 706a 'and the fourth foil 706d'. It may have a form disposed on the same line as the virtual line.
- Air foil bearing according to an embodiment of the present invention having the configuration described above has the effect of improving the load bearing capacity and increase the damping effect by changing the shape and rigidity of the bump foil.
- the durability of the bearing is improved by improving the damping force.
- the present invention relates to an air foil bearing with improved damping efficiency.
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Abstract
Description
Claims (36)
- 회전축을 회전 가능하게 지지하는 에어 포일 베어링에 있어서,상기 에어 포일 베어링은, 원판형의 플레이트와, 상기 플레이트 상에 결합되는 복수의 범프 포일과, 상기 범프 포일의 상부에 배치되되 일단이 상기 플레이트에 결합되고 타단이 자유단인 탑 포일을 포함하는 에어 포일 베어링.
- 제1항에 있어서,상기 범프 포일은 서로 이격된 복수 개의 열로 배치된 복수의 단일 범프를 포함하며, 상기 단일 범프의 강성은 상기 플레이트의 내경 쪽에서 외경 쪽으로 갈수록 점차 커지거나 동일한 것을 특징으로 하는 에어 포일 베어링.
- 제2항에 있어서,상기 단일 범프의 각 열의 폭(A~D)은 상기 플레이트의 외경 쪽으로 갈수록 점차 커지거나, 상기 단일 범프의 폭(A~D)은 상기 플레이트의 내경 쪽 복수 개 보다 외경 쪽 복수 개가 크게 형성된 것을 특징으로 하는 에어 포일 베어링.
- 제1항에 있어서,상기 단일 범프의 범프 산(L)의 길이는 상기 플레이트의 내경 쪽에서 외경 쪽으로 갈수록 커지는 것을 특징으로 하는 에어 포일 베어링.
- 제2항 내지 제4항 중 어느 한 항에 있어서,상기 플레이트의 내경 및 외경 쪽에 배치된 상기 단일 범프의 호의 길이가 내측에 배치된 상기 단일 범프의 호의 길이보다 길게 형성된 것을 특징으로 하는 에어 포일 베어링.
- 제1항에 있어서,상기 범프 포일은 상기 플레이트의 반경 방향에 경사지게 배치되는 제1 내지 제5 단일 범프를 포함하고, 상기 제1 내지 제5 단일 범프는 제1 내지 제4 열을 이루며 서로 이격되며, 상기 단일 범프의 강성은 상기 플레이트의 내경 쪽에서 외경 쪽으로 갈수록 점차 커지거나 동일한 것을 특징으로 하는 에어 포일 베어링.
- 제6항에 있어서,상기 단일 범프의 상기 제1 내지 제4 열의 폭(A~D)은 상기 플레이트의 외경 쪽으로 갈수록 점차 커지는 것을 특징으로 하는 에어 포일 베어링.
- 제6항에 있어서,상기 단일 범프의 상기 제3 및 제4 열의 폭(C, D)은 상기 플레이트의 상기 제1 및 제2열의 폭(A, B) 보다 크게 형성된 것을 특징으로 하는 에어 포일 베어링.
- 제6항에 있어서,상기 단일 범프의 범프 산(L)의 길이는 상기 플레이트의 내경 쪽에서 외경 쪽으로 갈수록 커지는 것을 특징으로 하는 에어 포일 베어링.
- 제7항 내지 제9항 중 어느 한 항에 있어서,상기 단일 범프의 상기 제1 및 제4 열의 호의 길이가 상기 제2 및 제3열의 호의 길이보다 길게 형성된 것을 특징으로 하는 에어 포일 베어링.
- 회전축을 회전 가능하게 지지하는 에어 포일 베어링에 있어서,상기 에어 포일 베어링은, 원판형의 플레이트와, 상기 플레이트 상에 결합되는 복수의 범프 포일과, 상기 범프 포일의 상부에 배치되되 일단이 상기 플레이트에 결합되고 타단이 자유단인 탑 포일을 포함하며,상기 범프 포일은 제1 포일과, 상기 제1 포일의 내측에 배치되는 제2 포일을 포함하는 에어 포일 베어링.
- 제11항에 있어서,상기 제1 포일과 상기 제2 포일은 슬릿을 사이에 두고 상호 이격된 것을 특징으로 하는 에어 포일 베어링.
- 제12항에 있어서,상기 제1 포일은 상기 제2 포일 보다 큰 강성을 갖는 것을 특징으로 하는 에어 포일 베어링.
- 제13항에 있어서,상기 제1 포일과 상기 제2 포일은 서로 다른 재질로 만들어지는 것을 특징으로 하는 에어 포일 베어링.
- 제13항에 있어서,상기 제1 포일과 상기 제2 포일은 동일한 재질로 만들어지는 것을 특징으로 하는 에어 포일 베어링.
- 제15항에 있어서,상기 제1 포일의 두께는 상기 제2 포일의 두께보다 두꺼운 것을 특징으로 하는 에어 포일 베어링.
- 제15항에 있어서,상기 제1 포일의 범프 폭은 상기 제2 포일의 범프 폭 보다 작은 것을 특징으로 하는 에어 포일 베어링.
- 제12항에 있어서,상기 제2 포일은 내측에 폭을 이등분하는 슬릿이 형성되며, 상기 제1 포일 및 제2 포일 사이의 상기 슬릿의 폭은 상기 제2 포일의 상기 슬릿 폭에 대응하는 것을 특징으로 하는 에어 포일 베어링.
- 제12항에 있어서,상기 제2 포일은 내측에 폭을 이등분하는 슬릿이 형성되며, 상기 제1 포일 및 제2 포일 사이의 상기 슬릿의 폭은 상기 제2 포일의 상기 슬릿 폭 보다 큰 것을 특징으로 하는 에어 포일 베어링.
- 제11항에 있어서,상기 제1 포일 및 제2 포일은 복수 개로 구비되며, 상기 제1 포일 및 제2 포일은 서로 상이한 폭 및 형상을 갖는 제2 슬릿을 사이에 두고 배치되는 것을 특징으로 하는 에어 포일 베어링.
- 제20항에 있어서,상기 제1 포일과 제2 포일 사이의 제1 슬릿은 일단부에서 타단부까지 동일한 폭으로 형성되는 것을 특징으로 하는 에어 포일 베어링.
- 제21항에 있어서,상기 제2 포일 사이의 제2 슬릿은 로터 회전 방향 쪽 단부에서 상기 제1 포일 및 제2 포일을 연결하는 트레일링 에지(F) 쪽에서 상기 트레일링 에지(F)의 반대쪽으로 갈수록 그 폭이 커지는 형상인 것을 특징으로 하는 에어 포일 베어링.
- 제22항에 있어서,상기 제2 포일 사이의 제2 슬릿은 상기 트레일링 에지(F)의 반대쪽으로 갈수록 그 폭이 단차지게 커지는 것을 특징으로 하는 에어 포일 베어링.
- 제23항에 있어서,상기 제2 포일은 상기 트레일링 에지(F)의 반대쪽 단부의 폭이 상기 트레일링 에지(F)쪽 단부의 폭보다 작은 것을 특징으로 하는 에어 포일 베어링.
- 제24항에 있어서,상기 제2 포일은 서로 마주보는 일측에 계단형으로 꺾인 적어도 하나의 단차부와, 상기 로터 회전 방향을 따라 연장되어 상기 단차부를 연결하는 연결부를 포함하는 에어 포일 베어링.
- 제25항에 있어서,상기 제1 포일은 상기 트레일링 에지(F)의 반대쪽 단부가 스팟 용접(spot welding)되는 것을 특징으로 하는 에어 포일 베어링.
- 제26항에 있어서,상기 제1 포일의 범프 높이는 상기 제2 포일의 범프 높이보다 작은 것을 특징으로 하는 에어 포일 베어링.
- 제27항에 있어서,상기 슬릿의 상기 트레일링 에지(F) 쪽 단부에서 상기 트레일링 에지(F)까지의 거리(D)는 범프 피치(C)의 2배 값보다 작거나 같은 것을 특징으로 하는 에어 포일 베어링.
- 회전축을 회전 가능하게 지지하는 에어 포일 베어링에 있어서,상기 에어 포일 베어링은, 원판형의 플레이트와, 상기 플레이트 상에 결합되는 복수의 범프 포일과, 상기 범프 포일의 상부에 배치되되 일단이 상기 플레이트에 결합되고 타단이 자유단인 탑 포일을 포함하며,상기 범프 포일은 로터 회전방향의 반대 방향을 향해 연장 형성된 제1 포일 내지 제4 포일을 포함하는 에어 포일 베어링.
- 제29항에 있어서,상기 제1 포일 내지 제4 포일은 상기 로터 회전방향에 대응하는 단부가 하나로 연결된 것을 특징으로 하는 에어 포일 베어링.
- 제30항에 있어서,상기 각각의 제1 포일 내지 제4 포일의 상기 로터 회전방향의 반대 방향 쪽 단부에 인접하여 구비된 첫 번째 범프 산(A)과 이웃한 다른 범프 산의 높이가 상이한 것을 특징으로 하는 에어 포일 베어링.
- 제1항에 있어서,상기 제1 포일 내지 제4 포일의 상기 첫 번째 범프 산(A)의 높이는 상기 이웃한 다른 범프 산의 높이보다 낮은 것을 특징으로 하는 에어 포일 베어링.
- 제32항에 있어서,상기 제1 포일 내지 제4 포일의 상기 첫 번째 범프 산(A)의 높이는 상기 이웃한 다른 범프 산 높이의 70% 이내인 것을 특징으로 하는 에어 포일 베어링.
- 제33항에 있어서,상기 탑 포일은 상기 플레이트와 이격 간격이 점차 커지는 경사 구간(L1)과, 상기 플레이트와의 이격 간격이 균일한 평면 구간(L2)를 갖는 것을 특징으로 하는 에어 포일 베어링.
- 제34항에 있어서,상기 제1 포일 내지 제4 포일의 상기 첫 번째 범프 산(A)은 상기 탑 포일의 상기 평면 구간(L2)가 시작되는 위치에 대응하는 것을 특징으로 하는 에어 포일 베어링.
- 제33항에 있어서,상기 제1 포일 및 제4 포일의 상기 첫 번째 범프 산(A)에 인접한 단부(B)는 상기 플레이트에 스팟 용접(spot welding)되는 것을 특징으로 하는 에어 포일 베어링.
Priority Applications (3)
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US15/574,443 US10415634B2 (en) | 2015-11-18 | 2016-11-18 | Air foil bearing |
JP2017566656A JP6742349B2 (ja) | 2015-11-18 | 2016-11-18 | エアフォイルベアリング |
US16/548,348 US10941807B2 (en) | 2015-11-18 | 2019-08-22 | Air foil bearing |
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KR1020150161838A KR20170058077A (ko) | 2015-11-18 | 2015-11-18 | 에어 포일 베어링 |
KR10-2015-0161838 | 2015-11-18 | ||
KR20150166595 | 2015-11-26 | ||
KR10-2015-0166595 | 2015-11-26 | ||
KR10-2016-0034023 | 2016-03-22 | ||
KR1020160034023A KR102530819B1 (ko) | 2015-11-26 | 2016-03-22 | 에어 포일 베어링 |
KR1020160044117A KR102465360B1 (ko) | 2016-04-11 | 2016-04-11 | 에어 포일 베어링 |
KR10-2016-0044117 | 2016-04-11 |
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US15/574,443 A-371-Of-International US10415634B2 (en) | 2015-11-18 | 2016-11-18 | Air foil bearing |
US16/548,348 Continuation US10941807B2 (en) | 2015-11-18 | 2019-08-22 | Air foil bearing |
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WO2017086732A1 true WO2017086732A1 (ko) | 2017-05-26 |
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