WO2023189092A1 - フォイル軸受及び流体機械 - Google Patents
フォイル軸受及び流体機械 Download PDFInfo
- Publication number
- WO2023189092A1 WO2023189092A1 PCT/JP2023/007034 JP2023007034W WO2023189092A1 WO 2023189092 A1 WO2023189092 A1 WO 2023189092A1 JP 2023007034 W JP2023007034 W JP 2023007034W WO 2023189092 A1 WO2023189092 A1 WO 2023189092A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- foil
- bearing
- impeller
- rotating body
- bump
- Prior art date
Links
- 239000011888 foil Substances 0.000 title claims abstract description 395
- 239000012530 fluid Substances 0.000 title claims description 39
- 230000002093 peripheral effect Effects 0.000 claims description 39
- 238000003780 insertion Methods 0.000 claims description 21
- 230000037431 insertion Effects 0.000 claims description 21
- 239000000463 material Substances 0.000 claims description 11
- 238000006073 displacement reaction Methods 0.000 description 32
- 239000000446 fuel Substances 0.000 description 22
- 238000013459 approach Methods 0.000 description 9
- 239000007789 gas Substances 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 230000000694 effects Effects 0.000 description 5
- 230000006866 deterioration Effects 0.000 description 4
- 230000005489 elastic deformation Effects 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 239000003507 refrigerant Substances 0.000 description 3
- 239000010935 stainless steel Substances 0.000 description 3
- 229910001220 stainless steel Inorganic materials 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000005284 excitation Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000002441 reversible effect Effects 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- NBVXSUQYWXRMNV-UHFFFAOYSA-N fluoromethane Chemical compound FC NBVXSUQYWXRMNV-UHFFFAOYSA-N 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
Classifications
-
- 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
-
- 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
- F04D17/12—Multi-stage pumps
- F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
-
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
-
- 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
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- 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
- F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
- F16C17/024—Sliding-contact bearings for exclusively rotary movement for radial load only with flexible leaves to create hydrodynamic wedge, e.g. radial foil bearings
-
- 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
- F16C17/042—Sliding-contact bearings for exclusively rotary movement for axial load only with flexible leaves to create hydrodynamic wedge, e.g. axial foil bearings
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/50—Bearings
-
- 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
- F16C2360/00—Engines or pumps
- F16C2360/23—Gas turbine engines
-
- 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
- F16C2360/00—Engines or pumps
- F16C2360/23—Gas turbine engines
- F16C2360/24—Turbochargers
Definitions
- the present disclosure relates to foil bearings and fluid machines.
- a typical foil bearing rotatably supports a rotating body.
- Foil bearings include a top foil, a bump foil, and a housing.
- the housing has an insertion hole into which the rotating body is inserted.
- the top foil has a bearing surface facing the rotating body.
- a bump foil is disposed between the top foil and the housing.
- the bump foil includes a plurality of peaks that contact the outer peripheral surface of the top foil and a plurality of troughs that contact the inner peripheral surface of the housing. The peaks and valleys are alternately arranged along the rotation direction of the rotating body.
- the rotating body When the rotational speed of the rotating body reaches the floating rotational speed, the rotating body floats relative to the foil bearing due to the dynamic pressure of the air film generated between the rotating body and the bearing surface. Thereby, the foil bearing supports the rotating body without contacting the rotating body.
- the rotating body may come too close to the bearing surface, which may cause an excessive load to act on the top foil.
- the portion of the top foil that has received an excessive load is displaced closer to the housing, so that the plurality of peaks of the bump foil are pushed by the top foil.
- the bump foil deforms so that the plurality of peaks approach the housing. If the bump foil is damaged due to such deformation of the bump foil, the bearing performance of the foil bearing may deteriorate. In a fluid machine equipped with a foil bearing, if the above-mentioned deterioration in bearing performance due to the foil bearing occurs, the reliability of the fluid machine will decrease. Therefore, it is necessary to suppress such damage to the bump foil.
- Patent Document 1 discloses a foil bearing that includes, in addition to the bump foil, a convex portion that projects from the inner surface of the housing toward the top foil.
- a foil bearing includes a housing having an insertion hole through which a rotating body is inserted, a cylindrical top foil having a bearing surface facing the rotating body, and a space between the top foil and the housing.
- a thin plate-like bump foil disposed in the top foil, the bump foil having a plurality of peaks contacting the outer peripheral surface of the top foil and a plurality of troughs contacting the inner peripheral surface of the housing; troughs are arranged alternately along the rotational direction of the rotating body, and the plurality of peaks and the plurality of troughs extend in the rotational direction to elastically support the top foil.
- the bump foil when the load that the bearing surface receives from the rotating body is less than or equal to a threshold value, the bump foil has gaps between the plurality of peaks and the housing, and the bump foil has gaps between the plurality of peaks and the plurality of valleys.
- the bump foil is configured to support the top foil with a gap between the bump foil and the top foil, and when the load that the bearing surface receives from the rotating body exceeds the threshold value, the bump foil portions also contact the inner circumferential surface of the housing, the plurality of valley portions also contact the outer circumferential surface of the top foil to support the top foil, and the top foil and the bump foil are locally plane. It is configured to function as a bearing to support the rotating body.
- contact includes not only static contact but also dynamic contact.
- the outer circumferential surface of the top foil and the plurality of peaks may be in contact with each other before the rotating body rotates.
- the outer circumferential surface of the top foil and the plurality of peaks may not be in contact with each other before the rotating body rotates, and as the rotating body rotates, the plurality of peaks may approach and touch the outer circumferential surface of the top foil.
- the inner circumferential surface of the housing and the plurality of valleys may be in contact with each other before the rotating body rotates.
- the inner circumferential surface of the housing and the plurality of valleys are not in contact with each other before the rotating body rotates, and as the rotating body rotates, the plurality of valleys approach and touch the inner circumferential surface of the housing. Good too.
- a fluid machine includes the rotating body, an impeller configured to compress fluid by rotating integrally with the rotating body, and an impeller in which the rotating body and the impeller are housed.
- the impeller housing includes a housing and the foil bearing, and the impeller housing includes a shroud surface that covers the outer periphery of the impeller, and even if the top foil and the bump foil locally become plain bearings, the impeller and the foil bearing The tip clearance with the shroud surface is greater than zero.
- a fluid machine includes the rotating body, an impeller configured to compress fluid by rotating integrally with the rotating body, and an impeller in which the rotating body and the impeller are housed.
- the impeller housing includes a housing and the foil bearing, and the impeller housing includes a shroud surface that covers the outer periphery of the impeller, and the bumps on the peak portion in a state where no load from the rotating body acts on the bearing surface.
- the distance in the radial direction of the rotating body between the outer peripheral surface of the foil and the inner peripheral surface of the housing is H1, and the minimum value of the gap between the impeller and the shroud surface in the radial direction is less than H1. big.
- FIG. 15 is a perspective view showing the first foil bearing in a second state of the modification of FIG. 14;
- the fluid machine 10 includes a rotating shaft 40 that is a rotating body, a first impeller 34, and a second impeller 35.
- the fluid machine 10 includes a housing 11.
- the fluid machine 10 includes a first foil bearing 20 and a second foil bearing 22.
- the fluid machine 10 includes an electric motor 39.
- the fluid machine 10 of the first embodiment is mounted on a vehicle.
- the fluid machine 10 can be used, for example, as a centrifugal compressor that compresses air, which is a fluid containing oxygen, that is supplied to the fuel cell of a fuel cell vehicle, or as a centrifugal compressor that compresses refrigerant in a vehicle-mounted refrigeration circuit. can.
- the housing 11 is made of metal. Examples of the material for the housing 11 include aluminum.
- the housing 11 includes a motor housing member 12 , a first impeller housing member 13 , a second impeller housing member 14 , a first plate 15 , a second plate 16 , and a third plate 17 .
- the fluid machine 10 includes the first impeller housing member 13 and the second impeller housing member 14.
- the housing 11 includes a bearing housing member 71 (FIG. 2), which will be described later.
- the motor housing member 12 has a cylindrical peripheral wall 12a and a flat end wall 12b located at a first end of the peripheral wall 12a.
- the second end of the peripheral wall 12a is an open end.
- the first plate 15 closes off the second end of the motor housing member 12 .
- a motor chamber 51 is defined by the inner surface of the motor housing member 12 and the first plate 15 .
- An electric motor 39 is housed within the motor chamber 51 .
- the first plate 15 has a first bearing holding portion 18.
- the first bearing holding portion 18 has a cylindrical shape.
- a recess 15c is opened in an end surface 15b of the first plate 15 on the side opposite to the motor housing member 12.
- the inside of the first bearing holding portion 18 and the inside of the recess 15c communicate with each other via an opening in the bottom surface 15d of the recess 15c.
- the axis of the recess 15c and the axis of the first bearing holding part 18 are aligned.
- a side surface 15e of the recess 15c connects the end surface 15b and the bottom surface 15d.
- the end wall 12b of the motor housing member 12 has a second bearing holding portion 19.
- the second bearing holding portion 19 has a cylindrical shape.
- the second bearing holding portion 19 has an open end wall 12b on both end surfaces.
- the axial center of the second bearing holder 19 coincides with the axial center of the first bearing holder 18.
- the second plate 16 is connected to the first plate 15.
- the second plate 16 extends along the first plate 15.
- the second plate 16 has a first shaft insertion hole 16a in the center.
- the first shaft insertion hole 16a passes through the second plate 16.
- the first shaft insertion hole 16a communicates with the recess 15c.
- the axis of the first shaft insertion hole 16a coincides with the axis of the recess 15c.
- a thrust bearing housing chamber 52 is defined by the inner surface of the first plate 15 that defines the recess 15c and the second plate 16.
- the first impeller housing member 13 is cylindrical and has an inlet 13a that is a circular hole through which air, which is an example of working fluid, is sucked.
- the first impeller housing member 13 is connected to the second plate 16.
- the axis of the suction port 13a coincides with the axis of the first shaft insertion hole 16a of the second plate 16.
- the suction port 13a opens at an end surface of the first impeller housing member 13 on the opposite side to the second plate 16.
- a first impeller chamber 13b, a discharge chamber 13c, and a first diffuser flow path 13d are defined between the first impeller housing member 13 and the second plate 16.
- the first impeller chamber 13b communicates with the suction port 13a.
- the discharge chamber 13c extends around the axis of the suction port 13a around the first impeller chamber 13b.
- the first diffuser flow path 13d communicates the first impeller chamber 13b and the discharge chamber 13c.
- the first impeller chamber 13b communicates with the first shaft insertion hole 16a of the second plate 16.
- the first impeller housing member 13 includes a first shroud surface 53a.
- the first shroud surface 53a cooperates with the second plate 16 to define a first impeller chamber 13b.
- the first shroud surface 53a has a truncated conical shape.
- the third plate 17 is connected to the end wall 12b of the motor housing member 12.
- the third plate 17 has a second shaft insertion hole 17a in the center.
- the second shaft insertion hole 17a communicates with the inside of the second bearing holding portion 19.
- the axial center of the second shaft insertion hole 17a coincides with the axial center of the second bearing holding part 19.
- the second impeller housing member 14 is cylindrical and has a discharge port 14a that is a circular hole through which air is sucked.
- the second impeller housing member 14 is connected to an end surface of the third plate 17 on the opposite side to the motor housing member 12 .
- the axial center of the discharge port 14a coincides with the axial center of the second shaft insertion hole 17a of the third plate 17.
- the discharge port 14a opens at an end surface of the second impeller housing member 14 on the opposite side to the third plate 17.
- a second impeller chamber 14b, a suction chamber 14c, and a second diffuser flow path 14d are defined between the second impeller housing member 14 and the third plate 17.
- the second impeller chamber 14b communicates with the discharge port 14a.
- the suction chamber 14c extends around the axis of the discharge port 14a around the second impeller chamber 14b.
- the second diffuser flow path 14d communicates the second impeller chamber 14b and the suction chamber 14c.
- the second impeller chamber 14b communicates with the second shaft insertion hole 17a.
- the second impeller housing member 14 includes a second shroud surface 53b.
- the second shroud surface 53b cooperates with the third plate 17 to define a second impeller chamber 14b.
- the second shroud surface 53b has a truncated conical shape.
- a rotating shaft 40 which is a rotating body, is housed within the housing 11.
- the rotating shaft 40 is rotated by the electric motor 39.
- a portion of the rotating shaft 40 is located in the first impeller chamber 13b and the second impeller chamber 14b. Thereby, the rotating shaft 40 is accommodated in the first impeller housing member 13 and the second impeller housing member 14.
- the second impeller chambers 14b are arranged in this order along the rotating shaft 40.
- the axis SL of the rotating shaft 40 is aligned with the central axis of each of the first bearing holding part 18, the second bearing holding part 19, the first shaft insertion hole 16a, the second shaft insertion hole 17a, the suction port 13a, and the discharge port 14a. Match.
- the "axial direction of the rotating shaft 40" which is the direction along the axis SL of the rotating shaft 40, may be referred to as the "thrust direction”.
- the "radial direction of the rotating shaft 40” may be referred to as the "radial direction”.
- the axial direction of the rotating shaft 40 may be indicated by the symbol X.
- the radial direction of the rotating shaft 40 may be indicated by the symbol Y.
- the radial direction Y corresponds to the radial direction of the rotating body.
- the rotating shaft 40 includes a disk-shaped support plate 33.
- the support plate 33 protrudes from the outer peripheral surface of the rotating shaft 40.
- the support plate 33 is press-fitted onto the outer peripheral surface of the rotating shaft 40.
- the support plate 33 rotates integrally with the rotating shaft 40.
- the support plate 33 is arranged in the thrust bearing housing chamber 52.
- the support plate 33 is supported by a thrust bearing 80.
- the thrust bearing 80 has bearing parts arranged between the first plate 15 and the support plate 33 and between the second plate 16 and the support plate 33, respectively.
- the thrust bearing 80 rotatably supports the support plate 33 without contacting the support plate 33. Therefore, the thrust bearing 80 is an air dynamic pressure bearing that rotatably supports the rotating shaft 40 in the thrust direction.
- the first impeller 34 is made of metal. Examples of the material for the first impeller 34 include aluminum.
- the first impeller 34 is connected to the first end 30a of the rotating shaft 40.
- the first impeller 34 is an impeller that rotates integrally with the rotating shaft 40.
- the first impeller 34 is housed in the first impeller chamber 13b. That is, the first impeller 34 is housed in the first impeller housing member 13 .
- the first impeller 34 has a truncated conical shape.
- the diameter of the first impeller 34 gradually decreases from the first back surface 34a of the first impeller 34 toward the first end surface 34b of the first impeller 34.
- the first back surface 34a faces the second plate 16 in the axial direction X.
- a first shroud surface 53a extends along the outer periphery of the first impeller 34 from the first back surface 34a to the first tip surface 34b. Thereby, the first shroud surface 53a covers the outer periphery of the first impeller 34.
- the first impeller 34 rotates integrally with the rotating shaft 40 to compress air, which is a fluid.
- the second impeller 35 is made of metal. Examples of the material for the second impeller 35 include aluminum.
- the second impeller 35 is connected to the second end 30b of the rotating shaft 40.
- the second impeller 35 is an impeller that rotates integrally with the rotating shaft 40.
- the second impeller 35 is housed in the second impeller chamber 14b. That is, the second impeller 35 is housed in the second impeller housing member 14 .
- the second impeller 35 has a truncated conical shape.
- the diameter of the second impeller 35 gradually decreases from the second back surface 35a of the second impeller 35 toward the second tip surface 35b of the second impeller 35.
- the second back surface 35a faces the third plate 17 in the axial direction X.
- a second shroud surface 53b extends along the outer periphery of the second impeller 35 from the second back surface 35a to the second tip surface 35b. Thereby, the second shroud surface 53b covers the outer periphery of the second impeller 35.
- the second impeller 35 rotates integrally with the rotating shaft 40 to compress air, which is a fluid.
- the first impeller 34 and the first shroud surface 53a are separated by a first tip clearance 55.
- the first tip clearance 55 is a gap extending from the first tip surface 34b of the first impeller 34 to the first back surface 34a between the outer periphery of the first impeller 34 and the first shroud surface 53a.
- the dimension of the first tip clearance 55 in the radial direction Y is referred to as a first clearance dimension C1.
- the first clearance dimension C1 is the dimension of the gap between the first impeller 34 and the first shroud surface 53a in the radial direction Y.
- the first clearance dimension C1 may be the same or different from the first tip surface 34b of the first impeller 34 to the first back surface 34a.
- the first clearance dimension C1 may become smaller as it approaches the first back surface 34a from the first tip surface 34b.
- the size of the first clearance dimension C1 is illustrated in an exaggerated manner compared to the actual size.
- ⁇ Second tip clearance 56> The second impeller 35 and the second shroud surface 53b are separated by a second tip clearance 56.
- the second tip clearance 56 is a gap extending from the second tip surface 35b of the second impeller 35 to the second back surface 35a between the outer periphery of the second impeller 35 and the second shroud surface 53b.
- the dimension of the second tip clearance 56 in the radial direction Y is referred to as a second clearance dimension C2.
- the second clearance dimension C2 is the dimension of the gap between the second impeller 35 and the second shroud surface 53b in the radial direction Y.
- the second clearance dimension C2 may be the same dimension or different dimensions from the second tip surface 35b of the second impeller 35 to the second back surface 35a.
- the second clearance dimension C2 may become smaller as the distance from the second tip surface 35b approaches the second back surface 35a.
- the size of the second clearance dimension C2 is illustrated in an exaggerated manner compared to the actual size.
- the second clearance dimension C2 is the same size as the first clearance dimension C1.
- the electric motor 39 is arranged between the first impeller 34 and the second impeller 35 in the axial direction X.
- the electric motor 39 is housed in a motor chamber 51.
- the electric motor 39 includes a stator 42 and a rotor 41.
- the stator 42 includes a cylindrical stator core 43 and a coil 44 wound around the stator core 43.
- the stator core 43 is fixed to the inner surface of the peripheral wall 12a of the motor housing member 12.
- the rotor 41 is arranged inside the stator core 43 in the motor chamber 51.
- the rotor 41 rotates integrally with the rotating shaft 40.
- the rotor 41 includes a rotor core 41a fixed to the rotating shaft 40, and a plurality of permanent magnets (not shown) provided on the rotor core 41a.
- the rotor 41 rotates by supplying electric power controlled by an inverter device (not shown) to the coil 44 .
- the rotating shaft 40 rotates integrally with the rotor 41.
- a vehicle on which the fluid machine 10 is mounted includes a fuel cell system 1.
- the fuel cell system 1 includes a fuel cell stack 99 that is an on-vehicle fuel cell, a fluid machine 10, a supply flow path LA, and a discharge flow path LB.
- Fuel cell stack 99 includes a plurality of battery cells.
- the supply flow path LA connects the discharge chamber 13c and the fuel cell stack 99.
- the discharge flow path LB connects the fuel cell stack 99 and the suction chamber 14c.
- the air passing through the fuel cell stack 99 is discharged to the discharge flow path LB as exhaust gas from the fuel cell stack 99.
- Exhaust gas from the fuel cell stack 99 is sucked into the suction chamber 14c via the discharge flow path LB.
- the exhaust gas from the fuel cell stack 99 sucked into the suction chamber 14c is discharged into the second impeller chamber 14b through the second diffuser flow path 14d.
- the second impeller 35 is rotated by exhaust gas from the fuel cell stack 99 discharged into the second impeller chamber 14b.
- the rotating shaft 40 is rotated not only by the drive of the electric motor 39 but also by the rotation of the second impeller 35 which is rotated by the exhaust gas from the fuel cell stack 99.
- the rotation of the second impeller 35 due to exhaust gas from the fuel cell stack 99 assists the rotation of the rotating shaft 40 .
- the exhaust gas from the fuel cell stack 99 discharged into the suction chamber 14c is discharged to the outside from the discharge port 14a.
- the first foil bearing 20 is held by the first bearing holding section 18 .
- the second foil bearing 22 is held by a second bearing holding section 19. Therefore, the first foil bearing 20 and the second foil bearing 22 are arranged within the housing 11.
- the first foil bearing 20 and the second foil bearing 22 are both examples of foil bearings according to the present disclosure.
- the first foil bearing 20 and the second foil bearing 22 rotatably support the rotating shaft 40.
- the first foil bearing 20 and the second foil bearing 22 support the rotating shaft 40 while being in contact with the rotating shaft 40 until the rotational speed of the rotating shaft 40 reaches the floating rotational speed.
- the floating rotational speed is the rotational speed of the rotating shaft 40 when the rotating shaft 40 floats relative to the first foil bearing 20 and the second foil bearing 22.
- dynamic pressure is generated between the rotating shaft 40 and the first foil bearing 20 and between the rotating shaft 40 and the second foil bearing 22.
- the rotating shaft 40 floats relative to the first foil bearing 20 and the second foil bearing 22 due to the generated dynamic pressure.
- the first foil bearing 20 and the second foil bearing 22 rotatably support the rotating shaft 40 without contacting the rotating shaft 40. Therefore, the first foil bearing 20 and the second foil bearing 22 rotatably support the rotating shaft 40 in the radial direction.
- the shape of the second foil bearing 22 is the same as the shape of the first foil bearing 20. Therefore, detailed explanation of the same configuration as the first foil bearing 20 among the configurations of the second foil bearing 22 will be omitted below.
- the first foil bearing 20 includes a bearing housing member 71, a top foil 72, and a bump foil 73. Since the housing 11 includes the bearing housing member 71, it can also be said that the first foil bearing 20 includes the housing 11.
- the bearing housing member 71 has a cylindrical shape.
- the axis of the bearing housing member 71 coincides with the axis SL of the rotating shaft 40. Therefore, the axial direction X is also the axial direction of the bearing housing member 71.
- the radial direction Y is also the radial direction of the bearing housing member 71.
- the bearing housing member 71 is formed with an insertion hole 71h through which the rotating shaft 40 is inserted.
- the insertion hole 71h is a through hole that penetrates the bearing housing member 71 in the axial direction X.
- the bearing housing member 71 in the first foil bearing 20 is held by the first bearing holding part 18.
- the bearing housing member 71 in the first foil bearing 20 is separate from the first bearing holding part 18.
- the bearing housing member 71 of the second foil bearing 22 is held by the second bearing holding part 19.
- the bearing housing member 71 in the second foil bearing 22 is separate from the second bearing holding part 19.
- the top foil 72 is cylindrical.
- the top foil 72 has a substantially cylindrical shape.
- Top foil 72 is located inside bearing housing member 71 .
- the top foil 72 extends in the circumferential direction of the bearing housing member 71 inside the bearing housing member 71 .
- the circumferential direction of the bearing housing member 71 may be simply referred to as the "circumferential direction.”
- the top foil 72 has a thin plate shape.
- the top foil 72 is formed from a flexible metal plate material such as stainless steel. More specifically, the top foil 72 is obtained by curving this metal plate material into a cylindrical shape such that the longitudinal direction is along the circumferential direction and the lateral direction is along the axial direction X.
- top foil 72 in the circumferential direction is fixed to the bearing housing member 71 by welding or interference fit, and the other end is not fixed to the bearing housing member 71.
- the end of the top foil 72 fixed to the bearing housing member 71 in this manner is referred to as a first fixed end 72a
- first free end 72b is the end of the top foil 72 that is not fixed to the bearing housing member 71.
- the first fixed end portion 72a is bent toward the outside of the top foil 72 in the radial direction Y.
- the first free end portion 72b is spaced apart from the base end portion of the first fixed end portion 72a in the circumferential direction. Therefore, the top foil 72 is an open ring (non-annular) with a portion of the closed ring cut out.
- Open ring refers to a generally looped shape with a gap, such as a C-shape.
- the top foil 72 is arranged outside the rotating shaft 40 in the radial direction Y. Top foil 72 faces rotation axis 40 .
- the top foil 72 has a bearing surface 72s.
- the inner surface of the top foil 72 constitutes a bearing surface 72s facing the rotating shaft 40.
- the top foil 72 rotatably supports the rotating shaft 40 in a non-contact manner when the rotating shaft 40 rotates.
- the bump foil 73 has a generally cylindrical shape.
- the bump foil 73 is arranged between the top foil 72 and the bearing housing member 71 in the radial direction Y.
- the bump foil 73 has a thin plate shape.
- the bump foil 73 is formed from a flexible metal plate material such as stainless steel. More specifically, the bump foil 73 is obtained by curving this metal plate material into a cylindrical shape such that the longitudinal direction is along the circumferential direction and the lateral direction is along the axial direction X.
- the thickness of the bump foil 73 is indicated by h1.
- the thickness h1 may be approximately the same as the thickness of the top foil 72.
- One end of the bump foil 73 in the circumferential direction is fixed to the bearing housing member 71 by welding or interference fitting, and the other end is not fixed to the bearing housing member 71.
- the end of the bump foil 73 fixed to the bearing housing member 71 in this manner is referred to as a second fixed end 73a
- the end of the bump foil 73 that is not fixed to the bearing housing member 71 is referred to as a second free end 73b.
- the second fixed end portion 73a is bent toward the outside of the bump foil 73 in the radial direction Y.
- the second free end portion 73b is spaced apart from the base end portion of the second fixed end portion 73a in the circumferential direction. Therefore, the bump foil 73 is an open ring with a portion of the closed ring cut out. Bump foil 73 elastically supports top foil 72.
- the bump foil 73 includes a plurality of peaks 81 and a plurality of troughs 82.
- the plurality of peaks 81 contact the outer peripheral surface 72f of the top foil 72.
- the plurality of troughs 82 contact the inner circumferential surface 71g of the bearing housing member 71.
- the peak portions 81 and the valley portions 82 are alternately arranged along the rotation direction D of the rotation shaft 40.
- the trough portion 82 protrudes in a direction away from the outer circumferential surface 72f of the top foil 72 and is curved in an arc so as to bulge toward the inner circumferential surface 71g of the bearing housing member 71.
- Each peak portion 81 protrudes from the end portion 82c of the adjacent valley portion 82 toward the outer circumferential surface 72f of the top foil 72 in the rotation direction D of the rotation shaft 40, and also bulges toward the top foil 72. curved in an arc.
- the end portion 82c of the valley portion 82 is a boundary portion between the peak portion 81 and the valley portion 82 in the bump foil 73.
- the bump foil 73 elastically supports the top foil 72 by having a plurality of peaks 81 and a plurality of troughs 82 extending in the rotation direction D of the rotation shaft 40 .
- the bump foil 73 includes a plurality of divided bodies 73c divided in the rotation direction D of the rotating shaft 40.
- the bump foil 73 includes three divided bodies 73c. All the divided bodies 73c included in the bump foil 73 are hereinafter also referred to as a plurality of divided bodies 73c.
- the dimensions of the plurality of divided bodies 73c in the rotation direction D of the rotating shaft 40 may be substantially the same, or may be partially or entirely different.
- the plurality of divided bodies 73c may have the same number of peaks 81, or some or all of them may have different numbers of peaks 81.
- the plurality of divided bodies 73c may have the same number of valleys 82, or some or all of them may have different numbers of valleys 82.
- Each divided body 73c has a fixed end 73d fixed to the bearing housing member 71 and a free end 73e not fixed to the bearing housing member 71 in the rotation direction D of the rotating shaft 40.
- the fixed end 73d of one divided body 73c is the second fixed end 73a
- the free end 73e of the other divided body 73c is the second free end 73b.
- an end in the rotation direction D of the rotating shaft 40 is a fixed end 73d.
- the end opposite to the fixed end 73d is a free end 73e.
- the fixed end 73d of one divided body 73c and the free end 73e of the other divided body 73c are adjacent to each other.
- a fixed end 73d and a free end 73e extend in the axial direction X between one end and the other end of the divided body 73c in the axial direction X.
- each divided body 73c is arranged so that a gap 83 is formed between the adjacent fixed end 73d and free end 73e regardless of the extension.
- ⁇ No load state SN> Next, the first foil bearing 20 in a state where no load is applied to the bearing surface 72s from the rotating shaft 40 will be described with reference to FIG. 3.
- the state in which no load is applied from the rotating shaft 40 to the bearing surface 72s refers to a state in which the rotating shaft 40 is not rotating and the bearing surface 72s is in contact with the rotating shaft 40 over the entire circumference.
- the state in which no load is applied from the rotating shaft 40 to the bearing surface 72s will hereinafter be referred to as a no-load state SN.
- each of the peaks 81 of the bump foil 73 locally contacts the outer circumferential surface 72f of the top foil 72.
- the tip portion of the peak portion 81 in the direction of protrusion toward the top foil 72 contacts the outer circumferential surface 72f of the top foil 72.
- each of the valleys 82 of the bump foil 73 locally contacts the inner circumferential surface 71g of the bearing housing 71.
- the tip portion of the valley portion 82 in the direction of protrusion toward the bearing housing member 71 contacts the inner peripheral surface 71g of the bearing housing member 71.
- the distance in the radial direction Y between the outer circumferential surface 73f of the bump foil 73 and the inner circumferential surface 71g of the bearing housing member 71 at the peak portion 81 is defined as a first distance H1.
- the first distance H1 is smaller than the first clearance dimension C1, which is the dimension of the first tip clearance 55 in the radial direction Y, and the second clearance dimension C2, which is the dimension of the second tip clearance 56 in the radial direction Y. That is, the minimum value of the first clearance dimension C1, which is the dimension of the gap between the first impeller 34 and the first shroud surface 53a in the radial direction Y, is larger than the first distance H1.
- the distance between the adjacent peaks 81 and troughs 82 in the rotation direction D of the rotating shaft 40 is the second distance L1.
- the second distance L1 is the distance in the rotation direction D between the tip of the peak 81 in the protruding direction and the tip of the valley 82 in the protrusion direction, of the peaks 81 and troughs 82 that are adjacent to each other in the rotation direction D.
- the thickness h1 of the bump foil 73, the first distance H1, and the second distance L1 have a relationship of L1 2 /600h1>H1.
- the no-load state SN is different from a state in which the rotating shaft 40 is simply not rotating.
- the rotating shaft 40 contacts a portion or the entire bearing surface 72s of the top foil 72 in the rotation direction D of the rotating shaft 40.
- a load is applied from the rotating shaft 40 to the bearing surface 72s in the portion of the top foil 72 that is in contact with the rotating shaft 40.
- first state S1 Next, the first state S1 will be explained with reference to FIGS. 4 and 5.
- the rotating shaft 40 In the first state S1, the rotating shaft 40 is floating above the bearing surface 72s. This state of the first foil bearing 20 is referred to as a first state S1.
- the load that the bearing surface 72s receives from the rotating shaft 40 is equal to or less than the threshold value P.
- the top foil 72 is elastically deformed outward in the radial direction Y as the rotating shaft 40 rotates. As a result, an air film is formed between the rotating shaft 40 and the top foil 72, thereby generating dynamic pressure.
- the first foil bearing 20 rotatably supports the rotating shaft 40 in a state where the rotating shaft 40 is not in contact with the top foil 72 .
- the peak portion 81 of the bump foil 73 that is in contact with the outer peripheral surface 72f of the top foil 72 is pressed by the top foil 72.
- the bump foil 73 is elastically deformed outward in the radial direction Y together with the top foil 72.
- the top foil 72 is thus elastically supported by the bump foil 73.
- the peaks 81 and troughs 82 are elastically deformed.
- a load is applied evenly from the rotating shaft 40 to the entire bearing surface 72s via the air film. Therefore, all the peaks 81 and troughs 82 are uniformly elastically deformed.
- each of the peaks 81 of the bump foil 73 locally contacts the outer peripheral surface 72f of the top foil 72. Due to the elastic deformation of the peak portion 81, a wider area of the peak portion 81 in the circumferential direction contacts the top foil 72 in the first state S1 compared to the no-load state SN.
- each of the valleys 82 of the bump foil 73 locally contacts the inner surface of the bearing housing member 71. Due to the elastic deformation of the trough portion 82, a wider area of the trough portion 82 in the circumferential direction contacts the bearing housing member 71 in the first state S1 than in the no-load state SN.
- the peak portion 81 has a gap G1 between it and the bearing housing member 71.
- the valley portion 82 has a gap G2 between it and the top foil 72.
- the bump foil 73 supports the top foil 72 with such gaps G1 and G2.
- the dimension of the gap 83 along the circumferential direction is the gap dimension A.
- the first state S1 there is a gap 83 between the adjacent fixed end 73d and free end 73e.
- the two adjacent divided bodies 73c are separated from each other in the rotation direction D of the rotation shaft 40.
- the peaks 81 and troughs 82 elastically deform, the divided body 73c deforms so that the adjacent fixed end 73d and free end 73e approach each other. Therefore, the gap dimension A in the first state S1 is smaller than in the no-load state SN.
- the second state S2 will be explained with reference to FIGS. 6 and 7.
- the rotating shaft 40 is closer to a part of the bearing surface 72s in the circumferential direction than in the first state S1.
- This state of the first foil bearing 20 is referred to as a second state S2.
- the cause of the rotating shaft 40 coming closer to the bearing surface 72s than in the first state S1 is eccentricity of the rotating shaft 40, for example, a case where the rotating shaft 40 shifts in the radial direction Y. Further, the diameter of the rotating shaft 40 may increase due to thermal expansion of the rotating shaft 40.
- the load that the bearing surface 72s receives from the rotating shaft 40 exceeds the threshold P.
- a portion of the top foil 72 in the circumferential direction is the first displacement portion 72p.
- a portion of the bump foil 73 located on the outer side in the radial direction Y than the first displacement portion 72p is the second displacement portion 73p.
- the first displacement portion 72p in the second state S2 corresponds to a portion where the rotating shaft 40 is closer to the bearing surface 72s than in the first state S1.
- the entirety of one divided body 73c is illustrated as the second displacement portion 73p.
- a portion of the top foil 72 located on the inner side in the radial direction Y than one divided body 73c, which is the second displacement portion 73p, is illustrated as the first displacement portion 72p.
- the second state S2 can also be said to be the state of the first foil bearing 20 when the first displacement portion 72p is displaced outward in the radial direction Y from the position in the first state S1.
- the plurality of divided bodies 73c deform so that the adjacent fixed ends 73d and free ends 73e approach each other. Therefore, the divided body 73c including the second displacement portion 73p in the second state S2 is displaced more in the rotation direction D of the rotating shaft 40 than in the first state S1.
- the divided body 73c including the second displacement portion 73p and the divided body 73c adjacent to this divided body 73c in the rotation direction D of the rotating shaft 40 do not overlap. That is, the gap dimension A in the first state S1 is set to be equal to or larger than the amount of displacement in the rotational direction D of the rotating shaft 40 of the divided body 73c including the second displacement portion 73p in the second state S2.
- the peak portion 81 abuts not only the outer circumferential surface 72f of the top foil 72 but also the inner circumferential surface 71g of the bearing housing member 71.
- the valley portion 82 abuts not only the inner peripheral surface 71g of the bearing housing member 71 but also the outer peripheral surface 72f of the top foil 72.
- the bump foil 73 supports the top foil 72 by the contact between the peaks 81 and the valleys 82 .
- the second displacement portion 73p which is a part of the bump foil 73, extends along the outer peripheral surface 72f of the top foil 72 and the inner peripheral surface 71g of the bearing housing member 71.
- the top foil 72 and the bump foil 73 locally serve as a plain bearing 85 to support the rotating shaft 40.
- the top foil 72 and bump foil 73 locally serve as a plain bearing 85, the first tip clearance 55 between the first impeller 34 and the first shroud surface 53a is larger than zero. Even when the top foil 72 and the bump foil 73 locally form a plain bearing 85, the second tip clearance 56 between the second impeller 35 and the second shroud surface 53b is larger than zero.
- the first model 100 is obtained by extracting one pitch of the bump foil 73.
- the first model 100 has a first convex portion 102 curved in an arc shape so as to bulge from both ends. Both ends of the first model 100 correspond to the troughs 82.
- the first convex portion 102 corresponds to the peak portion 81.
- the second model 200 is a model in which one pitch of the bump foil 73 is modeled into a beam fixed at both ends.
- the second model 200 which is a beam model, is a flat plate extending between one end and the other end.
- the bump pitch is "2L1” and the bump plate thickness is "h”.
- the applied load is “F”
- the bearing width is “b”
- the stress is “ ⁇ ”
- the amount of deformation is “ ⁇ ”
- the Young's modulus is "E.”
- the bearing width b is the length of the bump foil 73 in the axial direction X. Note that the bump pitch "2L1” corresponds to the number obtained by multiplying the second distance L1 by 2.
- the bump plate thickness "h” corresponds to the thickness h1.
- the typical bump foil 73 is made of alloy steel or stainless steel, it generally has a Young's modulus E of about 200 [GPa] and a yield strength ⁇ max of about 1000 [MPa]. By substituting these values into (Equation 3), the following (Equation 4) can be derived.
- the deformation amount ⁇ is equal to or less than “L1 2 /600h” and the deformation amount ⁇ is in the elastic region, and the deformation amount ⁇ larger than that is the plastic region. That is, "L1 2 /600h” is the maximum displacement amount in the elastic region.
- the first distance H1 which is the height of the bump foil 73, to a value that satisfies "L1 2 /600h>H1"
- the bump foil 73 can be used in an elastic range.
- the values of the first distance H1, the second distance L1, and the thickness h1 of the bump foil 73 are set in advance so as to satisfy the relationship "L1 2 /600h1>H1".
- the bump foil 73 can be elastically deformed while the displacement amount of the bump foil 73 in the radial direction Y is equal to or less than the first distance H1. Since the bump foil 73 after deformation is not plastically deformed, it can return to the shape of the bump foil 73 in the no-load state SN or the first state S1. Therefore, the bump foil 73 has reversibility.
- the peaks 81 and the troughs 82 exceed the material's proof stress limit after the threshold P is exceeded, that is, after the support mode of the top foil 72 by the first foil bearing 20 shifts from the first state S1 to the second state S2. It is set to not. If the load that the bearing surface 72s receives from the rotating shaft 40 exceeds the threshold P and then returns to below the threshold P, the manner in which the top foil 72 is supported by the first foil bearing 20 shifts from the second state S2 to the first state S1. It turns out.
- the bump foil 73 moves its peak portion 81 away from the inner circumferential surface 71g of the bearing housing member 71 due to its own elastic force, and the trough portion 82 moves away from the top foil 72. spaced apart from the outer circumferential surface 72f.
- the top foil 72 may enter the second state S2 in which it is displaced outward in the radial direction Y from the first state S1.
- each peak portion 81 of the bump foil 73 that is in contact with the outer peripheral surface 72f of the top foil 72 may be excessively pressed by the top foil 72.
- the second displacement portion 73p in the second state S2 has a larger contact range with the top foil 72 and the bearing housing member 71 in the rotation direction D of the rotating shaft 40 than in the first state S1.
- the second displacement portion 73p in the second state S2 extends along the outer peripheral surface 72f of the top foil 72 and the inner peripheral surface 71g of the bearing housing member 71.
- the top foil 72 and the bump foil 73 mutually extend in the rotation direction D of the rotation shaft 40, forming a plain bearing shape. Therefore, the first foil bearing 20 in the second state S2 can support the rotating shaft 40 by dynamic pressure because the top foil 72 and the bump foil 73 locally become the plain bearing 85.
- the bump foil 73 has the peak portion 81 also in contact with the inner circumferential surface 71g of the bearing housing member 71, and the valley portion 82 at the top.
- the top foil 72 is supported by also coming into contact with the outer peripheral surface 72f of the foil 72.
- the top foil 72 and the bump foil 73 locally become a plain bearing 85, so that the first foil bearing 20 and the second foil bearing 22 rotate.
- the shaft 40 can be supported by dynamic pressure. Therefore, even under a situation where an excessive load acts on the top foil 72, it is possible to suppress the bearing performance of the first foil bearing 20 and the second foil bearing 22 from deteriorating.
- Each divided body 73c has a fixed end 73d fixed to the bearing housing member 71 and a free end 73e not fixed to the bearing housing member 71 in the rotation direction D of the rotating shaft 40. .
- Each divided body 73c is arranged so that there is a gap 83 between the adjacent fixed end 73d and free end 73e regardless of the extension. Therefore, even if the bump foil 73 extends in the rotation direction D of the rotation shaft 40, the adjacent divided bodies 73c do not overlap with each other. Therefore, the displacement of the bump foil 73 in the rotational direction D of the rotating shaft 40 is not hindered, so that the top foil 72 can be suitably elastically supported by the bump foil 73.
- the peaks 81 and the valleys 82 are formed so that the proof stress limit of the material is not exceeded after the threshold P is exceeded. Therefore, even after the load that the bearing surface 72s receives from the rotating shaft 40 exceeds the threshold P, deformation of the bump foil 73 that would deteriorate the bearing performance of the first foil bearing 20 and the second foil bearing 22 can be suppressed.
- the maximum displacement amount of the bump foil 73 in the radial direction Y is the displacement amount when the bump foil 73 is along the inner peripheral surface 71g of the bearing housing member 71, and is the first distance H1.
- the bump foil 73 can be elastically deformed. Since the bump foil 73 after deformation is not plastically deformed, it can return to the shape of the bump foil 73 when the load that the bearing surface 72s receives from the rotating shaft 40 is equal to or less than the threshold value P. Therefore, since the reversible bump foil 73 can be employed, deterioration in the bearing performance of the first foil bearing 20 and the second foil bearing 22 can be further suppressed.
- the resonance frequency of the first foil bearing 20 and the second foil bearing 22 will increase.
- the excitation force (unbalanced force of the rotating shaft 40) increases in proportion to the square of the rotational speed. Therefore, the rotating shaft 40 passes through the resonance points of the first foil bearing 20 and the second foil bearing 22 at a high rotation speed with a large excitation force, and vibration of the rotating shaft 40 occurs.
- deformation of the bump foil 73 that would degrade the bearing performance of the first foil bearing 20 and the second foil bearing 22 can be suppressed without increasing the rigidity of the bump foil 73. Therefore, the occurrence of problems that occur when increasing the rigidity of the bump foil 73 as described above can be suppressed.
- each divided body 73c is arranged such that a gap 83 is formed between the adjacent fixed end 73d and free end 73e regardless of the extension.
- the gap 83 is formed even when the top foil 72 is supported by the first foil bearing 20 and the second foil bearing 22 in any of the no-load state SN, the first state S1, and the second state S2. be done.
- each divided body 73c extends in the axial direction X between one end and the other end of the divided body 73c in the axial direction X, similarly to the first embodiment.
- the free end 73e has a shape that is shifted from both ends of the divided body 73c in the axial direction X toward the rotational direction D of the rotating shaft 40 as it approaches the intermediate portion. Due to the shapes of the fixed end 73d and the free end 73e, the gap 83 forms a herringbone-shaped groove 86.
- the bump foil 73 when transitioning from the no-load state SN to the first state S1, the bump foil 73 deforms similarly to the first embodiment.
- the second distance L1, the thickness h1, and the first distance H1 are L1 2 /600h1> The relationship is H1.
- the second displacement portion 73p in the second state S2 extends along the outer peripheral surface 72f of the top foil 72 and the inner peripheral surface 71g of the bearing housing member 71. .
- the top foil 72 and the bump foil 73 locally become a plain bearing 85, so that the rotating shaft 40 can be supported by dynamic pressure.
- a herringbone-shaped groove 86 is formed by the gap 83 of the bump foil 73.
- the first foil bearing 20 and the second foil bearing 22 support the rotating shaft 40 by locally becoming a herringbone bearing 87.
- the second displacement portion 73p in the second state S2 extends along the outer peripheral surface 72f of the top foil 72 and the inner peripheral surface 71g of the bearing housing member 71.
- the first foil bearing 20 in the second state S2 can support the rotating shaft 40 by dynamic pressure because the top foil 72 and the bump foil 73 locally become a plain bearing 85.
- a load acts on the first displacement portion 72p in the second state S2 from the rotating shaft 40 via the air film.
- a portion of the top foil 72 located inside the gap 83 in the radial direction Y is curved so as to be pressed toward the gap 83.
- the first foil bearing 20 becomes a herringbone bearing in the first displacement portion 72p. This also allows the first foil bearing 20 in the second state S2 to support the rotating shaft 40 by dynamic pressure.
- the gap 83 is a herringbone-shaped groove 86.
- the first foil bearing 20 and the second foil bearing 22 support the rotating shaft 40 by locally becoming a herringbone bearing 87. Therefore, when the load that the bearing surface 72s receives from the rotating shaft 40 exceeds the threshold P, the portion of the top foil 72 located inside the gap 83 between the adjacent fixed end 73d and free end 73e in the radial direction Y It curves so as to be pressed toward 83. Thereby, the first foil bearing 20 and the second foil bearing 22 can support the rotating shaft 40 by locally becoming a herringbone bearing 87. Therefore, it is possible to further suppress deterioration in the bearing performance of the first foil bearing 20 and the second foil bearing 22.
- the fixed end 73d is shifted in the rotational direction D of the rotating shaft 40 as it approaches the middle part from both ends of the divided body 73c in the axial direction X. It may also have a different shape. That is, the fixed end 73d may have a shape along the free end 73e.
- the minimum value of the first clearance dimension C1 and the minimum value of the second clearance dimension C2 may be the same as the first distance H1, or may be smaller than the first distance H1. If the top foil 72 and bump foil 73 locally form a plain bearing 85, the first tip clearance 55 and the second tip clearance 56 may be zero.
- the proof stress limit of the material may be exceeded.
- the second distance L1, the thickness h1, and the first distance H1 do not need to satisfy "L1 2 /600h1>H1".
- the bump foil 73 does not need to be deformed due to the elastic force of the bump foil 73.
- the peak portion 81 remains in contact with the inner circumferential surface 71g of the bearing housing member 71 even when the second state S2 shifts to the first state S1.
- the valley portion 82 remains in contact with the outer circumferential surface 72f of the top foil 72 even when transitioning from the second state S2 to the first state S1.
- the gap 83 between the adjacent fixed end 73d and free end 73e may disappear due to expansion.
- the fixed end 73d and the free end 73e of the two adjacent divided bodies 73c may be in contact with each other.
- the bump foil 73 may be comprised of a single member that is continuous over the entire circumference.
- the bearing housing member 71 may be omitted from the first foil bearing 20 and the second foil bearing 22. In this case, for example, by integrating the bearing housing member 71 into the first bearing holding part 18 and the second bearing holding part 19, the bearing housing member 71 can be omitted from the first foil bearing 20 and the second foil bearing 22. Good too. Bump foil 73 and top foil 72 may be fixed to housing 11 by welding or interference fitting.
- the fluid machine 10 does not need to include the second impeller 35, for example.
- the fluid compressed by the first impeller 34 and the second impeller 35 is not limited to air.
- the fluid may be, for example, a refrigerant or a fluorocarbon atmosphere in which a gas state and a liquid state are mixed. Therefore, the fluid to be compressed by the fluid machine 10 is arbitrary.
- the fluid machine 10 may be used in an air conditioner.
- the fluid machine 10 in this case may compress refrigerant.
- the fluid machine 10 may be mounted on any vehicle, without being limited to a vehicle.
- D...Rotation direction G1, G2...Gap, h1...Thickness, P...Threshold value, Y...Radial direction, 10...Fluid machine, 11...Housing, 40...Rotating shaft, 71...Bearing housing member, 71g...Inner peripheral surface, 71h...Insertion hole, 72...Top foil, 72f...Outer peripheral surface (of top foil), 72s...Bearing surface, 73...Bump foil, 73c...Divided body, 73d...Fixed end, 73e...Free end, 73f...Bump foil Outer peripheral surface, 81...crest, 82...trough, 83...gap, 85...plain bearing, 86...groove, 87...herringbone bearing.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Support Of The Bearing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
以下、フォイル軸受及び流体機械を具体化した第1実施形態を図1~図9にしたがって説明する。以下では、説明の都合上、流体機械についての説明をした後にフォイル軸受の説明をする。
図1に示すように、流体機械10は、回転体である回転軸40と、第1インペラ34と、第2インペラ35と、を備えている。流体機械10は、ハウジング11を備える。流体機械10は、第1フォイル軸受20と、第2フォイル軸受22と、を備えている。流体機械10は電動モータ39を備えている。第1実施形態の流体機械10は、車両に搭載されている。流体機械10は、例えば、燃料電池車の燃料電池に供給される酸素を含む流体である空気を圧縮する遠心圧縮機、又は、車載の冷凍回路の冷媒を圧縮する遠心圧縮機として使用することができる。
回転体である回転軸40は、ハウジング11内に収容されている。回転軸40は、電動モータ39によって回転される。回転軸40の一部は、第1インペラ室13b及び第2インペラ室14bに位置する。これにより、回転軸40は、第1インペラハウジング部材13及び第2インペラハウジング部材14に収容されている。
第1インペラ34は金属製である。第1インペラ34の材料としては、例えばアルミニウムが挙げられる。第1インペラ34は、回転軸40の第1端部30aに連結されている。第1インペラ34は、回転軸40と一体的に回転する羽根車である。第1インペラ34は、第1インペラ室13bに収容されている。すなわち、第1インペラハウジング部材13には、第1インペラ34が収容されている。
第2インペラ35は金属製である。第2インペラ35の材料としては、例えばアルミニウムが挙げられる。第2インペラ35は、回転軸40の第2端部30bに連結されている。第2インペラ35は、回転軸40と一体的に回転する羽根車である。第2インペラ35は、第2インペラ室14bに収容されている。すなわち、第2インペラハウジング部材14には、第2インペラ35が収容されている。
第1インペラ34と第1シュラウド面53aとは、第1チップクリアランス55によって離間されている。第1チップクリアランス55は、第1インペラ34の外周と第1シュラウド面53aとの間において、第1インペラ34の第1先端面34bから第1背面34aにかけて延びる隙間である。
第2インペラ35と第2シュラウド面53bとは、第2チップクリアランス56によって離間されている。第2チップクリアランス56は、第2インペラ35の外周と第2シュラウド面53bとの間において、第2インペラ35の第2先端面35bから第2背面35aにかけて延びる隙間である。
電動モータ39は、軸線方向Xにおいて、第1インペラ34と第2インペラ35との間に配置されている。電動モータ39はモータ室51に収容されている。電動モータ39は、ステータ42及びロータ41を備えている。ステータ42は、円筒状のステータコア43と、ステータコア43に巻回されるコイル44と、を有している。ステータコア43は、モータハウジング部材12の周壁12aの内面に固定されている。
流体機械10が搭載される車両は、燃料電池システム1を備える。燃料電池システム1は、車載用燃料電池である燃料電池スタック99と、流体機械10と、供給流路LAと、吐出流路LBと、を備えている。燃料電池スタック99は、複数の電池セルを含む。供給流路LAは、吐出室13cと、燃料電池スタック99と、を接続する。吐出流路LBは、燃料電池スタック99と、吸入室14cと、を接続する。
第1フォイル軸受20は、第1軸受保持部18によって保持されている。第2フォイル軸受22は、第2軸受保持部19によって保持されている。したがって、第1フォイル軸受20及び第2フォイル軸受22は、ハウジング11内に配置されている。第1フォイル軸受20及び第2フォイル軸受22は、共に、本開示に係るフォイル軸受の例である。第1フォイル軸受20及び第2フォイル軸受22は、回転軸40を回転可能に支持している。
軸受ハウジング部材71は、円筒状である。軸受ハウジング部材71の軸線は回転軸40の軸線SLと一致している。そのため、軸線方向Xは軸受ハウジング部材71の軸線方向でもある。径方向Yは、軸受ハウジング部材71の径方向でもある。軸受ハウジング部材71には、回転軸40が挿通される挿通孔71hが形成されている。挿通孔71hは、軸線方向Xにおいて軸受ハウジング部材71を貫通する貫通孔である。
図2及び図3に示すように、トップフォイル72は筒状である。トップフォイル72は、略円筒状である。トップフォイル72は、軸受ハウジング部材71の内部に位置する。トップフォイル72は、軸受ハウジング部材71の内部において軸受ハウジング部材71の周方向に延びている。以下、軸受ハウジング部材71の周方向を単に「周方向」ということがある。トップフォイル72は薄板状である。詳細には、トップフォイル72は、例えばステンレス鋼などの可撓性を有する金属板材から形成される。より詳細には、この金属板材を、長手方向が周方向に沿い、かつ短手方向が軸線方向Xに沿うように、筒状に湾曲させることによりトップフォイル72が得られる。
バンプフォイル73は、全体として円筒状である。バンプフォイル73は、径方向Yにおけるトップフォイル72と軸受ハウジング部材71との間に配置される。バンプフォイル73は薄板状である。詳細には、バンプフォイル73は、例えばステンレス鋼などの可撓性を有する金属板材から形成される。より詳細には、この金属板材を、長手方向が周方向に沿い、かつ短手方向が軸線方向Xに沿うように、筒状に湾曲させることによりバンプフォイル73が得られる。バンプフォイル73の厚みをh1で示す。厚みh1は、トップフォイル72の厚みと略同じであってもよい。
次に、回転軸40から軸受面72sに荷重が作用しない状態での第1フォイル軸受20について、図3を参照して説明する。回転軸40から軸受面72sに荷重が作用しない状態とは、回転軸40が回転しておらず、かつ軸受面72sが全周に亘って回転軸40に接触している状態のことをいう。こうした回転軸40から軸受面72sに荷重が作用しない状態のことを、以下では無荷重状態SNという。
次に、第1状態S1について、図4及び図5を参照して説明する。第1状態S1において、回転する回転軸40は軸受面72sから浮上している。このような第1フォイル軸受20の状態を第1状態S1という。第1状態S1において、軸受面72sが回転軸40から受ける荷重は、閾値P以下になっている。
次に、第2状態S2について、図6及び図7を参照して説明する。第2状態S2において、回転軸40は、第1状態S1よりも軸受面72sの周方向における一部に近づいている。こうした第1フォイル軸受20の状態を第2状態S2という。第1状態S1よりも回転軸40が軸受面72sに近づく要因としては、回転軸40の偏心、例えば、回転軸40が径方向Yにずれる場合が挙げられる。また、回転軸40の熱膨張によって回転軸40の径が大きくなることもある。第2状態S2において、軸受面72sが回転軸40から受ける荷重は閾値Pを超える。
図8及び図9に示すように、第1モデル100及び第2モデル200を使って、弾性変形範囲内のバンプフォイル73の変形量δについて検討する。第1モデル100は、バンプフォイル73の1ピッチ分を取り出したものである。第1モデル100は、両端部から膨出するように弧状に湾曲した第1凸部102を有する。第1モデル100の両端部が谷部82に相当する。第1凸部102が山部81に相当する。第2モデル200は、バンプフォイル73の1ピッチ分を両端固定の梁へモデル化したものである。梁モデルである第2モデル200は、一端と他端との間で延びる平坦な平板材である。第2モデル200の両端部が固定されている。これらモデルにおいて、バンプピッチを「2L1」とし、バンプ板厚を「h」とする。これらモデルにおいて、作用する荷重を「F」とし、軸受幅を「b」とし、応力を「σ」とし、変形量を「δ」とし、ヤング率を「E」とする。軸受幅bとは、バンプフォイル73の軸線方向Xの長さである。なお、バンプピッチ「2L1」は、第2距離L1に2を乗算した数に相当する。バンプ板厚「h」は、厚みh1に相当する。
次に、第1実施形態の作用について説明する。
例えば、回転軸40の振動や回転軸40の熱膨張に伴って、トップフォイル72が第1状態S1よりも径方向Y外側に変位する第2状態S2となることがある。この場合、トップフォイル72の外周面72fに接触しているバンプフォイル73の各山部81がトップフォイル72によって過剰に押圧されることがある。
上記第1実施形態によれば、以下の効果を得ることができる。
(1-1)軸受面72sが回転軸40から受ける荷重が閾値Pを超える場合、バンプフォイル73は、山部81が軸受ハウジング部材71の内周面71gにも当接し、谷部82がトップフォイル72の外周面72fにも当接してトップフォイル72を支持する。これにより、第1フォイル軸受20及び第2フォイル軸受22の軸受性能が低下するようなバンプフォイル73の変形を抑制できる。軸受面72sが回転軸40から受ける荷重が閾値Pを超える場合、トップフォイル72とバンプフォイル73とが局所的にプレーン軸受85となることにより、第1フォイル軸受20及び第2フォイル軸受22は回転軸40を動圧によって支持できる。したがって、トップフォイル72に過剰な荷重が作用する状況下でも、第1フォイル軸受20及び第2フォイル軸受22の軸受性能が低下することを抑制できる。
以下、第2実施形態に係るフォイル軸受及び流体機械を図10~図13にしたがって説明する。第2実施形態におけるフォイル軸受の形状が、第1実施形態と異なっている。以下では、第1実施形態との相違点を中心に説明する。第1実施形態と同様の構成については適宜説明を省略する。
図10~図12に示すように、各々の分割体73cは、伸長に関わらず隣り合う固定端73dと自由端73eとの間に間隙83が形成されるように配置されている。間隙83は、第1フォイル軸受20及び第2フォイル軸受22によるトップフォイル72の支持態様が、無荷重状態SN、第1状態S1、及び第2状態S2のいずれであるときにも間隙83は形成される。
図10及び図11に示すように、軸受面72sが回転軸40から受ける荷重が閾値Pを超える場合、山部81が軸受ハウジング部材71の内周面71gにも当接し、谷部82がトップフォイル72の外周面72fにも当接する。こうして山部81及び谷部82が当接した状態で、バンプフォイル73はトップフォイル72を支持する。
次に、第2実施形態の作用について説明する。
第1実施形態と同様に、第2状態S2における第2変位部73pは、トップフォイル72の外周面72f及び軸受ハウジング部材71の内周面71gに沿って延びている。第2状態S2での第1フォイル軸受20は、トップフォイル72とバンプフォイル73とが局所的にプレーン軸受85になることにより、回転軸40を動圧によって支持できる。
上記第2実施形態によれば、第1実施形態での効果に加えて、以下の効果を得ることができる。
なお、上記の各実施形態は、以下のように変更して実施することができる。上記の各実施形態及び以下の変更例は、技術的に矛盾しない範囲で互いに組み合わせて実施することができる。
○ トップフォイル72とバンプフォイル73とが局所的にプレーン軸受85となる場合、第1チップクリアランス55及び第2チップクリアランス56は、0であってもよい。
○ 第2距離L1、厚みh1、及び第1距離H1は、「L12/600h1>H1」を満たさなくてもよい。
○ 第1フォイル軸受20及び第2フォイル軸受22から軸受ハウジング部材71を省略してもよい。この場合、例えば、第1軸受保持部18及び第2軸受保持部19に軸受ハウジング部材71を一体化させることにより、第1フォイル軸受20及び第2フォイル軸受22から軸受ハウジング部材71を省略させてもよい。ハウジング11にバンプフォイル73とトップフォイル72とが、溶接又は締り嵌めによって固定されてもよい。
○ 第1インペラ34及び第2インペラ35が圧縮する流体は、空気に限らない。流体としては、例えば、冷媒や、ガス状態と液状態とが混在したフロン雰囲気でもよい。したがって、流体機械10が圧縮対象とする流体は任意である。例えば、流体機械10は空調装置に用いられていてもよい。この場合の流体機械10は、冷媒を圧縮対象としてもよい。流体機械10の搭載対象は、車両に限られず任意である。
Claims (8)
- 回転体が挿通される挿通孔を有するハウジングと、
前記回転体に対向する軸受面を有する筒状のトップフォイルと、
前記トップフォイルと前記ハウジングとの間に配置される薄板状のバンプフォイルであって、前記トップフォイルの外周面に接触する複数の山部と前記ハウジングの内周面に接触する複数の谷部とを有し、前記山部と前記谷部とが前記回転体の回転方向に沿って交互に配置され、前記複数の山部及び前記複数の谷部が前記回転方向に伸長することで前記トップフォイルを弾性的に支持するように構成される、バンプフォイルと、
を備え、
前記軸受面が前記回転体から受ける荷重が閾値以下の場合、前記バンプフォイルは、前記複数の山部が前記ハウジングとの間に隙間を有し、前記複数の谷部が前記トップフォイルとの間に隙間を有して前記トップフォイルを支持するように構成され、
前記軸受面が前記回転体から受ける荷重が前記閾値を超える場合、前記バンプフォイルは、前記複数の山部が前記ハウジングの内周面にも当接し、前記複数の谷部が前記トップフォイルの外周面にも当接して前記トップフォイルを支持し、前記トップフォイルと前記バンプフォイルとが局所的にプレーン軸受となって前記回転体を支持するように構成される、
フォイル軸受。 - 前記軸受面が前記回転体から受ける荷重が前記閾値を超えた後に前記閾値以下に戻る場合、前記バンプフォイルは、自身の弾性力により、前記複数の山部が前記ハウジングの内周面から離間し、前記複数の谷部が前記トップフォイルの外周面から離間するように構成される、
請求項1に記載のフォイル軸受。 - 前記バンプフォイルは、前記回転方向において分割された複数の分割体を含み、
前記各分割体は、前記回転方向において、前記ハウジングに固定される固定端と、前記ハウジングに固定されていない自由端と、を有し、
前記回転方向に並ぶ2つの分割体は、一方の分割体の固定端が他方の分割体の自由端と隣合っており、かつ、互いに隣合う前記固定端と前記自由端との間に、前記2つの分割体の伸長に関わらず、間隙が形成されるように配置されている、
請求項1又は請求項2に記載のフォイル軸受。 - 前記間隙は、へリングボーン形状の溝であり、
前記軸受面が前記回転体から受ける荷重が前記閾値を超える場合、前記複数の山部が前記ハウジングの内周面にも当接し、前記複数の谷部が前記トップフォイルの外周面にも当接して前記トップフォイルを支持し、局所的にヘリングボーン軸受となって前記回転体を支持するように構成される、
請求項3に記載のフォイル軸受。 - 前記複数の山部及び前記複数の谷部は、前記閾値を超えた後に、材料の耐力限界を超えないように形成されている、
請求項1~請求項4のうちいずれか一項に記載のフォイル軸受。 - 前記軸受面に前記回転体からの荷重が作用しない状態で、前記回転方向における隣り合う前記山部と前記谷部の距離がL1であり、前記バンプフォイルの厚みがh1であり、前記回転体の径方向における前記山部における前記バンプフォイルの外周面と前記ハウジングの内周面との間の距離が1である場合に、L12/600h1>H1である、
請求項1~請求項5のうちいずれか一項に記載のフォイル軸受。 - 前記回転体と、
前記回転体と一体的に回転することによって流体を圧縮するように構成されるインペラと、
前記回転体及び前記インペラが収容されたインペラハウジングと、
請求項1~請求項6のうちいずれか一項に記載のフォイル軸受と、を備え、
前記インペラハウジングは、前記インペラの外周を覆うシュラウド面を備え、
前記トップフォイルと前記バンプフォイルとが局所的にプレーン軸受となる場合でも、前記インペラと前記シュラウド面との間のチップクリアランスは、0よりも大きい、
流体機械。 - 前記回転体と、
前記回転体と一体的に回転することによって流体を圧縮するように構成されるインペラと、
前記回転体及び前記インペラが収容されたインペラハウジングと、
請求項1~請求項6のうちいずれか一項に記載のフォイル軸受と、を備え、
前記インペラハウジングは、前記インペラの外周を覆うシュラウド面を備え、
前記軸受面に前記回転体からの荷重が作用しない状態での、前記山部における前記バンプフォイルの外周面と前記ハウジングの内周面との間の前記回転体の径方向における距離がH1であり、前記径方向における前記インペラと前記シュラウド面との間の隙間の最小値がH1よりも大きい、
流体機械。
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202380030556.2A CN118871686A (zh) | 2022-03-31 | 2023-02-27 | 箔片轴承及流体机械 |
KR1020247035534A KR20240162152A (ko) | 2022-03-31 | 2023-02-27 | 포일 베어링 및 유체 기계 |
DE112023001720.4T DE112023001720T5 (de) | 2022-03-31 | 2023-02-27 | Folienlager und Strömungsmaschine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2022060597A JP7619317B2 (ja) | 2022-03-31 | 2022-03-31 | フォイル軸受及び流体機械 |
JP2022-060597 | 2022-03-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2023189092A1 true WO2023189092A1 (ja) | 2023-10-05 |
Family
ID=88200595
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2023/007034 WO2023189092A1 (ja) | 2022-03-31 | 2023-02-27 | フォイル軸受及び流体機械 |
Country Status (5)
Country | Link |
---|---|
JP (1) | JP7619317B2 (ja) |
KR (1) | KR20240162152A (ja) |
CN (1) | CN118871686A (ja) |
DE (1) | DE112023001720T5 (ja) |
WO (1) | WO2023189092A1 (ja) |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060018574A1 (en) * | 2004-07-20 | 2006-01-26 | Honeywell International Inc., | Hydrodynamic journal bearing |
JP2012241775A (ja) * | 2011-05-18 | 2012-12-10 | Ihi Corp | ラジアルフォイル軸受 |
JP2013501902A (ja) * | 2009-08-31 | 2013-01-17 | ニューロス カンパニー リミテッド | ジャーナルフォイルエアベアリング |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP7027968B2 (ja) | 2018-03-07 | 2022-03-02 | 株式会社Ihi | ラジアルフォイル軸受 |
-
2022
- 2022-03-31 JP JP2022060597A patent/JP7619317B2/ja active Active
-
2023
- 2023-02-27 KR KR1020247035534A patent/KR20240162152A/ko active Pending
- 2023-02-27 WO PCT/JP2023/007034 patent/WO2023189092A1/ja active Application Filing
- 2023-02-27 DE DE112023001720.4T patent/DE112023001720T5/de active Pending
- 2023-02-27 CN CN202380030556.2A patent/CN118871686A/zh active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060018574A1 (en) * | 2004-07-20 | 2006-01-26 | Honeywell International Inc., | Hydrodynamic journal bearing |
JP2013501902A (ja) * | 2009-08-31 | 2013-01-17 | ニューロス カンパニー リミテッド | ジャーナルフォイルエアベアリング |
JP2012241775A (ja) * | 2011-05-18 | 2012-12-10 | Ihi Corp | ラジアルフォイル軸受 |
Also Published As
Publication number | Publication date |
---|---|
JP2023151147A (ja) | 2023-10-16 |
DE112023001720T5 (de) | 2025-01-16 |
JP7619317B2 (ja) | 2025-01-22 |
CN118871686A (zh) | 2024-10-29 |
KR20240162152A (ko) | 2024-11-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR100573384B1 (ko) | 래디알 포일 베어링 | |
US20190170190A1 (en) | Air bearing and rotor system | |
US20070069597A1 (en) | Fuel-cell compressed-air supplying device | |
JP6113444B2 (ja) | フォイル軸受 | |
JP2012500953A (ja) | スラストフォイル軸受 | |
CN109812493A (zh) | 空气箔片径向轴承 | |
JP2008517238A (ja) | 多孔性フォイルを有するエアーフォイルベアリング | |
JP2008232289A (ja) | 軸受装置及び軸受装置を備えた回転駆動装置 | |
KR102442191B1 (ko) | 에어포일 베어링 및 이를 포함하는 공기압축기 | |
JP5840423B2 (ja) | フォイル軸受 | |
JP2013053645A (ja) | スラストフォイル軸受 | |
JP6104596B2 (ja) | フォイル軸受 | |
JP6305749B2 (ja) | フォイル軸受と、これを有するフォイル軸受ユニット及びターボ機械 | |
WO2023189092A1 (ja) | フォイル軸受及び流体機械 | |
US12345271B2 (en) | Foil bearing assembly including perforated inner foil assembly and compressor including same | |
WO2009054560A1 (en) | Bearing seal for gas turbine | |
JP6144222B2 (ja) | フォイル軸受 | |
JP2018168829A (ja) | 遠心圧縮機 | |
JPS6165908A (ja) | 動圧形スラスト軸受 | |
US20240183287A1 (en) | Turbomachine | |
JP6219489B2 (ja) | フォイル軸受 | |
KR101070888B1 (ko) | 에어 포일 베어링 | |
WO2024225180A1 (ja) | 遠心圧縮機 | |
JP2023046778A (ja) | フォイル軸受 | |
KR100479607B1 (ko) | 포일 저널 베어링 |
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: 23779122 Country of ref document: EP Kind code of ref document: A1 |
|
WWE | Wipo information: entry into national phase |
Ref document number: 18850889 Country of ref document: US Ref document number: 202380030556.2 Country of ref document: CN |
|
ENP | Entry into the national phase |
Ref document number: 20247035534 Country of ref document: KR Kind code of ref document: A |
|
WWE | Wipo information: entry into national phase |
Ref document number: 1020247035534 Country of ref document: KR |
|
WWE | Wipo information: entry into national phase |
Ref document number: 112023001720 Country of ref document: DE |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 23779122 Country of ref document: EP Kind code of ref document: A1 |