WO2022179144A1 - 压缩机和空调 - Google Patents
压缩机和空调 Download PDFInfo
- Publication number
- WO2022179144A1 WO2022179144A1 PCT/CN2021/126093 CN2021126093W WO2022179144A1 WO 2022179144 A1 WO2022179144 A1 WO 2022179144A1 CN 2021126093 W CN2021126093 W CN 2021126093W WO 2022179144 A1 WO2022179144 A1 WO 2022179144A1
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- WO
- WIPO (PCT)
- Prior art keywords
- rotor
- rotating shaft
- face
- limiting
- main body
- Prior art date
Links
- 230000000670 limiting effect Effects 0.000 claims description 303
- 239000000463 material Substances 0.000 claims description 9
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 7
- 229910000906 Bronze Inorganic materials 0.000 claims description 6
- 239000010974 bronze Substances 0.000 claims description 6
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 claims description 6
- 230000002093 peripheral effect Effects 0.000 claims description 2
- 239000003921 oil Substances 0.000 description 32
- 238000010586 diagram Methods 0.000 description 12
- 238000000034 method Methods 0.000 description 8
- 238000009434 installation Methods 0.000 description 6
- 238000005057 refrigeration Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000002452 interceptive effect Effects 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 206010003497 Asphyxia Diseases 0.000 description 1
- 238000004378 air conditioning Methods 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 239000010726 refrigerant oil Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C18/082—Details specially related to intermeshing engagement type pumps
- F04C18/084—Toothed wheels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C18/12—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
- F04C18/14—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
- F04C18/16—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type
- F04C18/165—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type having more than two rotary pistons with parallel axes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C18/12—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
- F04C18/14—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
- F04C18/16—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0021—Systems for the equilibration of forces acting on the pump
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0042—Driving elements, brakes, couplings, transmissions specially adapted for pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/02—Lubrication; Lubricant separation
- F04C29/023—Lubricant distribution through a hollow driving shaft
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2230/00—Manufacture
- F04C2230/60—Assembly methods
- F04C2230/602—Gap; Clearance
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/20—Rotors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/30—Casings or housings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/50—Bearings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/60—Shafts
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2250/00—Geometry
- F04C2250/10—Geometry of the inlet or outlet
- F04C2250/101—Geometry of the inlet or outlet of the inlet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2250/00—Geometry
- F04C2250/10—Geometry of the inlet or outlet
- F04C2250/102—Geometry of the inlet or outlet of the outlet
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/04—Heavy metals
- F05C2201/0469—Other heavy metals
- F05C2201/0475—Copper or alloys thereof
- F05C2201/0478—Bronze (Cu/Sn alloy)
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/04—Heavy metals
- F05C2201/0469—Other heavy metals
- F05C2201/0493—Tin
Definitions
- the present disclosure relates to the technical field of compressors, and in particular, to a compressor and an air conditioner.
- a pair of parallel helical rotors are arranged in the compressor, and the pair of helical rotors and the inner wall of the casing form a space volume.
- the volume will increase and decrease periodically.
- the volume is periodically connected and closed with the suction port and the exhaust port, so that the whole process of suction, compression and exhaust can be completed.
- dual compressors are widely used in refrigeration and air conditioning in the medium cooling capacity range.
- the different pressures of the gas at the suction port and the exhaust port will cause the helical rotor to generate an axial force, and the axial force will cause the helical rotor to move in the axial direction of the helical rotor in the casing, causing the helical rotor to move in the axial direction.
- Adjacent end faces of the two oppositely arranged helical rotors collide together.
- a thrust bearing is usually added between the two helical rotors to prevent the adjacent end faces of the two helical rotors from colliding together.
- the additional thrust bearing will increase the number of parts of the compressor, resulting in The volume of the compressor increases.
- the present disclosure provides a compressor and an air conditioner that can maintain a gap between a first rotor and a second rotor without increasing the number of components of the compressor.
- the present disclosure provides a compressor comprising:
- a first rotor assembly the first rotor assembly including a first rotor and a second rotor coaxially arranged on the connecting assembly, the connecting assembly can carry the first rotor and the second rotor together around the the first shaft rotates;
- the connecting assembly is configured to limit the relative position of the first rotor and the second rotor so that there is a gap between the first rotor and the second rotor.
- an end face of the first rotor away from the second rotor and an end face of the housing close to the first rotor have a first axial gap
- the second rotor is at An end face away from the first rotor and an end face of the housing proximate the second rotor have a second axial gap
- the connection assembly is configured to limit the gap between the first rotor and the second rotor The gap is larger than the first axial gap, and the gap between the first rotor and the second rotor is larger than the second axial gap.
- the compressor further includes:
- the second rotor assembly includes a third rotor and a fourth rotor coaxially arranged on the second rotating shaft, the second rotating shaft is configured to drive the second rotor assembly along the The rotation direction of the first rotor assembly rotates in the opposite direction, the third rotor and the first rotor are in mesh with each other, and the fourth rotor and the second rotor are in mesh with each other.
- the end face of the third rotor close to the fourth rotor protrudes from the end face of the first rotor close to the second rotor, and the fourth rotor is close to the The end face of the third rotor protrudes from the end face of the second rotor close to the first rotor, so that the first rotor does not interfere with the fourth rotor and the second rotor does not interfere with the third rotor put one's oar in.
- the third rotor is engaged with adjacent end faces of the fourth rotor.
- the gap between the first rotor and the second rotor is L3, and the third rotor faces in the housing along the axial direction of the second shaft.
- the axial movement amount of moving in the direction close to the fourth rotor is D1
- the axial movement amount of the second rotor moving in the direction close to the first rotor is D2
- the fourth rotor is in the housing
- the axial movement amount of moving in the direction close to the third rotor along the axial direction of the second rotating shaft is D3
- the axial movement amount of the first rotor moving in the direction close to the second rotor is D4, so
- the second rotor assembly is configured to satisfy: L3 ⁇ D1+D2, and L3 ⁇ D3+D4.
- suction ports are provided at adjacent positions of the first rotor, the second rotor, the third rotor, and the fourth rotor, and the first rotor , A first exhaust port is arranged at the adjacent position of the third rotor and the casing, and a second row is arranged at the adjacent position of the second rotor, the fourth rotor and the casing breath.
- the helical direction of the first rotor is opposite to the helical direction of the second rotor, and the helical direction of the third rotor is opposite to the helical direction of the fourth rotor.
- the third rotor and the second rotating shaft are integrally formed, the fourth rotor has a shaft hole matched with the second rotating shaft, and the shaft hole is connected to the first rotating shaft.
- the second shaft adopts a tight fit.
- the compressor further includes a thrust bearing disposed on one side of the second rotating shaft and a motor disposed on the other side of the second rotating shaft, and the electric motor is configured to The second rotating shaft is driven to rotate, so that the second rotor assembly follows the second rotating shaft to rotate and drives the first rotor assembly and the connecting assembly to rotate around the first rotating shaft together.
- an end face of the third rotor away from the fourth rotor is away from the second rotor from the first rotor in a direction perpendicular to the axial direction of the second shaft.
- the end face of the rotor is flush; the end face of the fourth rotor away from the third rotor is flush with the end face of the second rotor away from the first rotor in the direction perpendicular to the axial direction of the second shaft .
- the connecting assembly includes a first limiting member and a second limiting member that are both sleeved on the first rotating shaft and can both rotate around the first rotating shaft,
- the first limiting member is configured to limit the position of the first rotor approaching the end face of the second rotor
- the second limiting member is configured to limit the second rotor approaching the position of the first rotor. position of the end face.
- an end surface of the first rotor close to the second rotor is provided with a first limiting groove along the axial direction of the first rotating shaft
- the first limiting member includes a first main body part and a first limiting part, the first main body part is sleeved on the first rotating shaft, the first limiting part is arranged around the periphery of the outer surface of the first main body part and the The first limiting portion is clamped in the first limiting slot; the end face of the second rotor close to the first rotor is provided with a second limiting slot along the axial direction of the first rotating shaft, and the The second limiting member includes a second main body portion and a second limiting portion, the second main body portion is sleeved on the first rotating shaft and is disposed adjacent to the first main body portion, and the second limiting portion surrounds The second limiting portion is arranged on the periphery of the outer surface of the second main body portion and the second limiting portion is clamped
- an end face of the first limiting portion close to the second limiting portion protrudes from a side of the first rotor close to an end face of the second rotor, and the The end face of the second limiting portion close to the first limiting portion protrudes from the side of the second rotor close to the end face of the first rotor.
- the end face of the first rotor close to the second rotor and the end face of the second rotor close to the first rotor in the axial direction of the first shaft The distance gradually increases from the axis of the first rotor assembly to the outer periphery of the first rotor assembly.
- the first limiting member includes a first main body portion and a first limiting portion, the first main body portion is sleeved on the first rotating shaft, and the first The limiting portion is arranged around the periphery of the outer surface of the first main body portion, and the side of the first limiting portion facing away from the second rotor is in contact with the end surface of the first rotor close to the second rotor;
- the second limiting member includes a second main body portion and a second limiting portion, the second main body portion is sleeved on the first rotating shaft and is disposed adjacent to the first main body portion, and the second main body portion is set adjacent to the first main body portion.
- the limiting portion is disposed around the periphery of the outer surface of the second main body portion, and a side of the second limiting portion facing away from the first rotor abuts the end surface of the second rotor close to the first rotor.
- the connecting assembly further includes a third limiting member and a fourth limiting member, and the third limiting member is configured to limit the first rotor to move away from the second The distance between the end face of the rotor and the casing, the fourth limiting member is configured to limit the distance between the end face of the second rotor away from the first rotor and the casing.
- the third limiting member includes a third main body portion and a third limiting portion, and the third main body portion is sleeved on the first rotating shaft and is connected to the first rotating shaft.
- a main body part is arranged adjacently, the third limiting part is arranged around the periphery of the outer surface of the third main body part, and the third limiting part abuts against the end surface of the first rotor facing away from the second rotor connected;
- the fourth limiting member includes a fourth main body portion and a fourth limiting portion, the fourth main body portion is sleeved on the first rotating shaft and is disposed adjacent to the second main body portion, the The fourth limiting portion is disposed around the periphery of the outer surface of the fourth main body portion, and the fourth limiting portion abuts on the end surface of the second rotor facing away from the first rotor.
- an end surface of the first rotor away from the second rotor is provided with a third limiting groove along the axial direction of the first rotating shaft
- the third limiting member includes A third main body part and a third limiting part, the third main body part is sleeved on the first rotating shaft and is disposed adjacent to the first main body part, and the third limiting part is arranged around the The peripheral edge of the outer surface of the third main body portion and the third limiting portion is clamped in the third limiting groove; the end face of the second rotor away from the first rotor is along the axial direction of the first rotating shaft
- a fourth limiting slot is opened in the direction
- the fourth limiting member includes a fourth main body part and a fourth limiting part, the fourth main body part is sleeved on the first rotating shaft and is connected with the second main body The fourth limiting portion is arranged around the periphery of the outer surface of the fourth main body portion, and the fourth limiting portion is clamped in the
- the material of the connection component includes tin bronze material.
- both the first rotating shaft and the connecting assembly are provided with an oil supply channel, and the oil supply channel located on the first rotating shaft and the oil supply channel located on the connecting component The oil flow passage is communicated.
- Embodiments of the present disclosure also provide an air conditioner including the compressor as described above.
- the embodiments of the present disclosure improve the connecting assembly connecting the first rotating shaft and the first rotor assembly, so that the connecting assembly can limit the relative position between the first rotor and the second rotor, and realize the first rotor without additional components.
- a gap is maintained between the first rotor and the second rotor, so as to ensure that the adjacent end faces of the first rotor and the second rotor do not collide with each other.
- FIG. 1 is a schematic cross-sectional view of a compressor provided in an embodiment of the application.
- FIG. 2 is a partial structural schematic diagram of the first rotating shaft, the first rotor assembly and the connecting assembly in the compressor shown in FIG. 1 .
- FIG. 3 is an enlarged structural schematic diagram of the first rotating shaft, the first rotor assembly and the part A of the connecting assembly shown in FIG. 2 .
- FIG. 4 is an enlarged structural schematic diagram of the first rotating shaft, the first rotor assembly and the B part of the connecting assembly shown in FIG. 2 .
- FIG. 5 is an enlarged structural schematic diagram of the first rotating shaft, the first rotor assembly and the C part of the connecting assembly shown in FIG. 2 .
- FIG. 6 is a schematic structural diagram of a first limiting member in the compressor shown in FIG. 1 .
- FIG. 7 is a schematic cross-sectional view of the first limiting member shown in FIG. 6 along the P-P direction.
- FIG. 8 is a perspective structural view of the first rotating shaft, the second rotating shaft, the first rotor assembly and the second rotor assembly in the compressor shown in FIG. 1 .
- FIG. 9 is a schematic diagram of a second structure of the first rotating shaft, the first rotor assembly and the connecting assembly shown in FIG. 2 .
- FIG. 10 is a schematic structural diagram of the first rotating shaft in the compressor shown in FIG. 1 .
- the first shaft 21.
- the second oil supply channel 211, The main oil supply channel; 212, The auxiliary oil supply channel;
- the first rotor assembly 41, the first rotor; 411, the first end face; 412, the second end face; 413, the first limit groove; 414, the first body; 415, the first spiral blade; Limit slot; 42, second rotor; 421, third end face; 422, fourth end face; 423, second limit slot; 424, second body part; 425, second helical blade; 426, fourth limit groove;
- 60 the second rotor assembly; 61, the third rotor; 611, the fifth end face; 612, the sixth end face; 613, the third helical blade; 62, the fourth rotor; 621, the seventh end face; 622, the eighth end face; 623, the fourth spiral blade;
- FIG. 1 is a first partial cross-sectional view of a compressor provided by an embodiment of the application.
- the compressor 200 shown in FIG. 1 may be a screw compressor, such as the compressor 200 being an opposed screw compressor. It should be noted that the compressor 200 shown in FIG. 1 is not limited to a screw compressor, for example, the compressor 200 may also be a scroll compressor.
- the compressor 200 may include a casing 10 , a first rotating shaft 20 , a connecting assembly 30 and a first rotor assembly 40 .
- the housing 10 may be used to accommodate a portion of the first rotating shaft 20 , the connecting assembly 30 and the first rotor assembly 40 .
- the first rotating shaft 20 may be installed in the casing 10 , for example, the first rotating shaft 20 may pass through the casing 10 , and both ends of the first rotating shaft 20 are exposed outside the casing 10 .
- the connecting assembly 30 can be sleeved on the first rotating shaft 20
- the first rotor assembly 40 can include a first rotor 41 and a second rotor 42
- the first rotor 41 and the second rotor 42 are coaxially arranged on the connecting shaft 20
- the connecting assembly 30 is configured to carry the first rotor 40 and the second rotor 42 to rotate together around the first shaft 20, and to limit the relative position between the first rotor 41 and the second rotor 42, so that the first rotor There is a gap between 41 and the second rotor 42 .
- the connecting components can be sliding bearings or rolling bearings.
- an additional spacer is usually provided between the two rotors of the first rotor assembly 40 to separate the two rotors and maintain the gap between the two rotors during the rotation process.
- additional spacers need to be added, thereby increasing the The number of parts of the compressor 200 is reduced.
- FIG. 2 is a schematic structural diagram of the first rotating shaft, the first rotor assembly and the connecting assembly in the compressor shown in FIG. 1
- FIG. 3 is the first rotating shaft, the first rotor assembly and the connecting assembly shown in FIG. 2 .
- FIG. 4 is an enlarged structural schematic view of the first shaft, the first rotor assembly and part B in the connecting assembly shown in FIG. 2
- FIG. 5 is the first rotating shaft and the first rotor shown in FIG. 2
- the first rotor 41 may include a first end face 411 and a second end face 412 that are opposite to each other, the first end face 411 is the end face of the first rotor 41 that is close to the second rotor 42 , and the second end face 412 is the end face of the first rotor 41 that is far away from the second rotor 42 .
- the end faces of the two rotors 42 may include a third end face 421 and a fourth end face 422 that are opposite to each other, the third end face 421 is the end face of the second rotor 42 close to the first rotor 41 , and the fourth end face 421 is the end face of the second rotor 42 that is far away from the first rotor 41 .
- An end face of the rotor 41 is the end face of the rotor 41 .
- the first end surface 411 and the third end surface 421 are adjacent and spaced apart, the second end surface 412 is adjacent to and spaced apart from one side of the housing 10 , and the fourth end surface 422 is opposite and spaced apart from the other surface of the housing 10 .
- the second end face 412 of the first rotor 41 and the end face of the casing 10 close to the first rotor 41 have a first axial gap L1
- the fourth end face 4 of the second rotor 42 and the end face of the casing 10 close to the second rotor 42 have a first axial gap L1.
- connection assembly 30 is configured to limit the relative positions of the first rotor 41 and the second rotor 42 so that there is a first end face 411 of the first rotor 41 and the third end face 421 of the second rotor 42 Three axial gaps L3.
- the connecting assembly 30 may include a first limiting member 31 and a second limiting member 32 , both of which are sleeved on the first limiting member 31 and the second limiting member 32 .
- the first rotor 41 On a rotating shaft 20 and rotatable around the first rotating shaft 20, the first rotor 41 is sleeved on the first limiting member 31 and is fixedly connected with the first limiting member 31, so that the first rotor 41 can follow the first limiting member
- the parts 31 rotate together around the first rotating shaft 20, wherein the first limiting part 31 is configured to limit the moving distance of the end face of the first rotor 41 close to the second rotor 42 moving toward the second rotor 42; the second rotor 42 is sleeved on the
- the second limiting member 32 is fixedly connected with the second limiting member 32 , so that the second rotor 42 can rotate around the first rotation shaft 20 along with the second limiting member 32 , wherein the second limiting member 32 is configured to limit The moving distance by which the end surface of the second rotor 42 close to the first rotor 41 moves toward the first rotor 41 .
- first limiting member 31 is configured to limit the position of the first end face 411 of the first rotor 41
- second limiting member 32 is configured to limit the position of the second end face 411 of the second rotor 42
- the first end surface 411 of the first rotor 41 and the third end surface 421 of the second rotor 42 have the third axial gap L3 in cooperation with the first stopper 31 and the second stopper 32 .
- FIG. 6 is a schematic structural diagram of the first limiting member in the compressor shown in FIG. 1
- the first limiting member 31 may include a first main body portion 311 and a first limiting portion 312.
- the first main body portion 311 is sleeved on the first rotating shaft 20.
- the first main body portion 311 may be provided with a first shaft hole 313.
- the first limiting member 31 is sleeved on the first rotating shaft 20 through the first shaft hole 313 .
- the first main body portion 311 may be a ring structure, and the first limiting portion 312 is disposed around the periphery of the outer surface of the first main body portion 311 .
- the first end surface 411 of the first rotor 41 may be provided with a first limiting slot 413 , and the notch of the first limiting slot 413 faces the second rotor 42 , or the first end surface 411 is opened along the axial direction of the first rotating shaft 20 .
- the first limiting portion 312 is clamped in the first limiting slot 413 , so that the first limiting portion 312 can limit the first rotor 41 through the first limiting slot 413 .
- the first limiting portion 312 is protrudingly disposed on the periphery of the outer surface of the first main body portion 311 , and when the first rotor 41 is sleeved on the first limiting member 31 , the first limiting portion of the first rotor 41 is The groove wall of the slot 413 is in contact with the first limiting portion 312 , and the first end surface 411 of the first rotor 41 cannot be relative to the first limiting member 31 under the restriction of the first limiting portion 312 of the first limiting member 31 . movement, so as to realize the restricting effect of the first limiting member 31 on the first end surface 411 of the first rotor 41 .
- the structure of the second limiting member 32 may be the same as that of the first limiting member 31 , for example, the second limiting member 32 may include a second main body portion 321 and a second limiting portion 322 , and the second main body portion 321 is sleeved On the first rotating shaft 20 , for example, the second main body portion 321 may be provided with a second shaft hole 323 , and the second limiting member 32 is sleeved on the first rotating shaft 20 through the second shaft hole 313 .
- the second main body portion 321 may be a ring structure, and the second limiting portion 322 is disposed around the periphery of the outer surface of the second main body portion 321 .
- the third end surface 421 of the second rotor 42 may be provided with a second limiting slot 423 , the notch of the second limiting slot 423 faces the first rotor 41 , or the third end surface 421 is opened along the axial direction of the first rotating shaft 20 There is the second limiting groove 423 .
- the second limiting portion 322 is clamped in the second limiting slot 423 , so that the second limiting portion 322 can limit the second rotor 42 through the second limiting slot 423 .
- the second limiting portion 322 is protrudingly disposed on the periphery of the outer surface of the second main body portion 321 , and when the second rotor 42 is sleeved on the second limiting member 32 , the second limiting portion of the second rotor 42 is The groove wall of the slot 423 is in contact with the second limiting portion 322 , and the second end surface 421 of the second rotor 42 cannot be relative to the second limiting member 32 under the restriction of the second limiting portion 322 of the second limiting member 32 . movement, so as to realize the limiting effect of the second limiting member 32 on the third end surface 421 of the second rotor 42 .
- the position of the first end surface 411 of the first rotor 41 is limited by the first limiting member 31
- the position of the third end surface 421 of the second rotor 42 is limited by the second limiting member 32 . , so that a third axial gap is maintained between the first end surface 411 of the first rotor 411 and the third end surface 421 of the second rotor 421 .
- FIG. 8 is a three-dimensional structural view of the first rotating shaft, the second rotating shaft, the first rotor assembly and the second rotor assembly in the compressor shown in FIG. 1 .
- the first rotor 41 includes a first body portion 414 . and a plurality of first helical vanes 415 disposed around the periphery of the outer surface of the first body portion 414 .
- the first end surface 411 of the first rotor 41 includes a first part located on the first body part 414 and a second part located on a first helical blade 415 close to the second rotor 42 , and the first limiting groove 413 is opened in the first part superior.
- the plurality of first helical blades 415 are sequentially arranged on the first body portion 414 from the first end face 411 to the second end face 412 on the first body portion 414 .
- the end surface and the end surface of the first body portion 414 close to the second rotor 42 are combined together to form the first end surface 411 .
- the first limiting groove 413 is formed on the end surface of the first body portion 414 .
- the second rotor 42 includes a second body portion 424 and a plurality of second helical vanes 425 disposed around the periphery of the outer surface of the second body portion 424 .
- the third end surface 421 of the second rotor 42 includes a third portion located on the second body portion 424 and a fourth portion located on a second helical blade 425 close to the first rotor 42 , and the second limiting groove 423 is opened in the first rotor 42 .
- the plurality of second helical blades 425 are sequentially arranged on the second body portion 424 from the third end face 421 to the fourth end face 422 on the second body portion 424 .
- the end face and the end face of the second body portion 424 close to the first rotor 42 are combined together to form a third end face 421 .
- the second limiting groove 423 is formed on the end surface of the second body portion 424 .
- the first limiting portion 312 may have a first side surface 3121 and a second side surface 3122 disposed opposite to each other, and the first side surface 3121 is the side of the first limiting portion 312 that is close to the second limiting portion 322 .
- the second side surface 3122 is the side of the first limiting portion 312 away from the second limiting portion 322 .
- the second limiting portion 322 may have a third side surface 3221 and a fourth side surface 3222 disposed opposite to each other, the third side surface 3221 is the side of the second limiting portion 322 that is close to the first limiting portion 312, and the fourth side surface 3222 is the first limiting portion 322.
- the first side surface 3121 is set to protrude from one side of the first end surface 411 of the first rotor 41
- the third side surface 3221 is set to protrude from one side of the third end surface 421 of the second rotor 42 .
- the positional relationship between the first limiting member 31 and the first rotor 41 and the positional relationship between the second limiting member 32 and the second rotor 42 are not limited to this.
- the first side surface 3121 is flush with the end surface of the other part of the first part except for the first limiting groove 413 in the direction perpendicular to the axial direction of the first rotating shaft 20 .
- the third side surface 3221 is flush with the end surface of the third part except the second limiting groove 423 in the direction perpendicular to the axial direction of the first rotating shaft 20 .
- the other parts of the first part except the first limiting groove 413 are in contact with other parts of the third part except the second limiting groove 423, and the second part and the fourth part are spaced apart from each other.
- a third axial gap L3 is formed between the second portion and the fourth portion.
- first limiting member 31 and the first rotor 41 and the second limiting member 32 and the second rotor 42 move together in the direction of approaching each other to the first limiting portion 312 of the first limiting member 31
- second limiting part 322 of the second limiting member 322 is in contact with each other, since the end face of the first part excluding the first limiting groove 413 and the first side surface 3121 of the first limiting part 312 are in contact with each other.
- the direction perpendicular to the axial direction of the first rotating shaft 20 is flush, and the end face of the third part except the other part where the second limiting groove 423 is provided is perpendicular to the third side surface 3221 of the second limiting part 322 .
- the axial direction of the first rotating shaft 20 is flush, so the end face of the first part excluding the other part with the first limiting groove 413 and the third part excluding the other part with the second limiting groove 423 The end leaves are abutted against each other.
- the embodiment of the present disclosure can reduce the occupation of the inner space of the housing 10 by the connection assembly 30 .
- the first part of the first rotor 41 is provided with a first limiting The larger the gap between the end face of the other part of the position slot 413 and the end face of the third part of the second rotor 42 except for the end face of the other part of the second position limit slot 423, the larger the overall length of the first rotor assembly 40, Therefore, the occupied volume of the inner space of the housing 10 by the first rotor assembly 40 is larger.
- the end face of the first part excluding the first limiting groove 413 and the first side surface 3121 of the first limiting portion 312 are arranged in a direction perpendicular to the axial direction of the first rotating shaft 20 as Flush
- the end face of the third part except the other part with the second limiting groove 423 and the third side surface 3221 of the second limiting part 322 are arranged in a direction perpendicular to the axial direction of the first rotating shaft 20 to be Flush, so that the first side surface 3121 of the first limiting member 31 abuts the third side surface 3221 of the second limiting member 32 to minimize the overall length of the first rotor assembly 40, thereby reducing the
- the first rotor assembly 40 occupies the inner space of the housing 10 .
- the end face of the first body portion 414 and the end face of the second body portion 424 abut each other, and the end face of the first first helical blade 415 and the end face of the first second helical blade 425 are spaced apart from each other so as to be in the second part
- a third axial gap L3 is formed between the first rotor 41 and the fourth part.
- the embodiment of the present disclosure can make the first rotor 41
- the first helical vane 415 and the second helical vane 425 of the second rotor 42 do not interfere with each other, and the length of the first rotor assembly 40 in the housing 10 due to the provision of the third axial gap L3 can be reduced.
- FIG. 9 is a schematic diagram of the second structure of the first rotating shaft, the first rotor assembly and the connecting assembly shown in FIG. 2 .
- the first rotor 41 is not provided with the first limiting slot 413
- the second rotor 42 is not provided with the second limiting slot 423 .
- a limiting slot may also be provided for the first rotor 41, and the first rotor 41 is clamped with the first limiting member 31 through the limiting slot; the third end face 421 of the second rotor 42 directly abuts against the second limiting portion 322 in the second limiting member 32 .
- the second rotor 42 is provided with a limiting slot, and the second rotor 42 is clamped with the second limiting member 32 through the limiting slot; the first end surface 411 of the first rotor 41 is directly connected to the first limiting member 31 The bit portion 312 abuts.
- first limiting member 31 and the second limiting member 32 are separately formed into two parts. In other embodiments, the first limiting member 31 and the second limiting member 32 may also be integrally formed as two parts. a part.
- the connecting assembly 30 , the first rotor 41 and the second rotor 42 can be rotated together in the casing 10 around the first rotating shaft 20 , because during the rotation, the two sides of the first rotor 41 and the second rotor The pressures on both sides of the 42 are different, resulting in an axial force along the axial direction of the first rotating shaft 20 . If the axial movement of the first rotor 41 and the second rotor 42 is too large, the first rotor 41 and the second rotor 42 may interfere with each other.
- the embodiment of the present disclosure restricts the first rotor 41 and the second rotor 42 through the connecting assembly 30, so that the gap between the first rotor 41 and the second rotor 42 is larger than that of the first rotor assembly 40 (including the first rotor 41 and the second rotor 42).
- the axial movement amount of the first rotor 41 and the second rotor 42) moving in the axial direction of the first rotating shaft so as to avoid the occurrence of the above problems.
- the third axial gap L3 is set to be larger than the first axial gap L1 and larger than the second axial gap L2, that is, L3>L1 and L3 is larger than L2.
- the first axial gap L1 is the gap between the second end face 412 of the first rotor 41 and the end face adjacent to the first rotor 41 in the housing 10 in the axial direction of the first rotating shaft 20;
- the second The axial gap L2 is a gap between the fourth end face 422 of the second rotor 42 and the end face adjacent to the second rotor 42 in the housing 10 in the axial direction of the first rotating shaft 20 .
- connection assembly 300 of the embodiment of the present disclosure may further include a third limiting member 33 and a fourth limiting member 34 , and the third limiting member 33 is configured to limit the first rotor The distance between the second end surface 412 of the first rotor 41 and the housing 10 so that the second end surface 412 of the first rotor 41 and the housing 10 have a first axial gap L1; the fourth limiting member 34 is configured to limit the second rotor 42 The distance between the fourth end face 422 of the second rotor 42 and the casing 10 is such that the fourth end face 422 of the second rotor 42 and the casing 10 have a second axial gap L2.
- the third limiting member 33 may include a third main body portion 331 and a third limiting portion 332.
- the third main body portion 331 is sleeved on the first rotating shaft 20 and is disposed adjacent to the first main body portion 311.
- the position portion 332 is provided around the periphery of the outer surface of the third main body portion 331 .
- the third limiting portion 331 may have a fifth side surface 3311 and a sixth side surface 3312 .
- the fifth side surface 3311 is the side of the third limiting portion 331 facing away from the housing 10
- the sixth side surface 3312 is the side of the third limiting portion 331 that is close to the housing 10 .
- the fourth limiting member 34 may include a fourth main body portion 341 and a fourth limiting portion 342.
- the fourth main body portion 341 is sleeved on the first rotating shaft 20 and is disposed adjacent to the second main body portion 321.
- the fourth limiting portion 342 is provided around the periphery of the outer surface of the fourth main body portion 341 .
- the fourth limiting portion 341 may have a seventh side surface 3421 and an eighth side surface 3422 .
- the seventh side surface 3421 is the side of the fourth limiting portion 341 that faces away from the housing 10
- the eighth side surface 3422 is the side of the fourth limiting portion 341 that is close to the housing 10 .
- the fourth limiting portion 341 is in contact with the second end surface 412 of the first rotor 41 .
- the structures of the third limiting member 33 and the fourth limiting member 34 may be the same as the structures of the first limiting member 31 shown in FIG. 6 .
- the second end surface 412 of the first rotor 41 and the fourth end surface 422 of the second rotor 42 may also have limit slots, which are respectively clamped to the third limit member 33 and the fourth limit member 34 through the limit slots.
- the second end surface 421 of the first rotor 41 may be provided with a third limiting slot 416 , and the notch of the third limiting slot 416 faces the casing 10 , or the second end surface 421 is along the first rotating shaft 20 .
- the third limiting groove 416 is opened in the axial direction of the .
- the third limiting portion 331 is clamped in the third limiting slot 416 , so that the third limiting portion 331 can limit the second end surface 412 of the first rotor 41 through the third limiting slot 416 .
- the third limiting portion 331 is protrudingly disposed on the periphery of the outer surface of the third main body portion 331 , the first rotor 41 is sleeved on the first limiting member 31 and the third limiting member 33 at the same time, and the A limiting member 31 is used to limit the first end surface 411 of the first rotor 41, and the third limiting member 33 is used to limit the second end surface 412 of the first rotor 42.
- the positioning member 33 When the first rotor 41 is sleeved to the third limit When the positioning member 33 is on, the groove wall of the third limiting groove 416 of the first rotor 41 is in contact with the third limiting portion 331 , and the second end surface 412 of the first rotor 41 is on the third limiting portion of the third limiting member 33 . Under the restriction of the position portion 331 , it cannot move relative to the third position-limiting member 33 , so that the third position-limiting member 33 restricts the second end surface 412 of the first rotor 41 .
- the fourth end surface 422 of the second rotor 42 may be provided with a fourth limiting slot 426 , and the notch of the fourth limiting slot 426 faces the housing 10 , or the fourth end surface 422 is along the first rotating shaft 20 .
- the fourth limiting groove 426 is opened in the axial direction of the .
- the fourth limiting portion 342 is clamped in the fourth limiting slot 426 , so that the fourth limiting slot 426 can limit the fourth limiting slot 426 of the second rotor 42 through the fourth limiting slot 426 .
- the fourth limiting portion 342 is protruded from the periphery of the outer surface of the fourth main body portion 341 , the second rotor 41 is sleeved on the second limiting member 32 and the fourth limiting member 34 at the same time, and the first The second limiting member 32 is used for limiting the third end surface 421 of the second rotor 42, and the fourth limiting member 34 is used for limiting the fourth end surface 422 of the second rotor 42.
- the position of the second end surface 412 of the first rotor 41 is restricted by the third limiting member 33 , so that there is a first axial gap between the second end surface 412 of the first rotor 41 and the casing 10 .
- L1 and the position of the fourth end surface 422 of the second rotor 42 is limited by the fourth limiting member 34 , so that there is a second axial gap L2 between the fourth end surface 422 of the second rotor 42 and the housing 10 .
- the connecting component 30 may include a tin bronze material, that is, the connecting component 30 may be made of a tin bronze material, and the tin bronze material is a bronze material with tin as the main alloying element, which contains tin The amount is generally between 3 and 14%.
- the material has the characteristics of corrosion resistance and wear resistance, and has good mechanical properties and technological properties, and can improve the wear resistance of the connecting component 30 .
- an oil supply channel may be provided on both the first rotating shaft 20 and the connecting assembly 30,
- the oil supply component located outside the housing 10 supplies refrigeration oil or other oil to the oil supply channel for lubrication and cooling, reducing friction between the connecting assembly 30 and the first rotor assembly 40 and ensuring reliable operation of the compressor 200 .
- FIG. 10 is a schematic structural diagram of the first rotating shaft in the compressor shown in FIG. 1 .
- the connecting assembly 30 is provided with a plurality of first oil supply passages 35, and one limiter may be provided with one or more first oil supply passages 36 (for example, the first limiter 31, the second limiter 32, the third limiter Both the limiting member 33 and the fourth limiting member 34 are provided with a first oil supply passage 35), and the first shaft 20 is provided with an oil supply main passage 211 along the axial direction of the first shaft 20, and along the direction perpendicular to the first shaft
- a plurality of auxiliary oil supply channels 212 communicated with the main oil supply channel 211 are provided in the second direction of the axial direction of
- the second oil supply passage 21 communicates with the plurality of first oil supply passages 35 through the plurality of auxiliary oil supply passages 212 .
- the refrigeration oil or other oil can be input into the main oil supply channel 211 of the first rotating shaft 20 through the oil supply component located in the housing 10, and the main oil supply channel 211 can pass the refrigeration oil or other oil through a plurality of
- the auxiliary oil supply channel 212 flows between the first rotating shaft 20 and the connecting assembly 30 to lubricate and cool the contact surface of the first rotating shaft 20 and the connecting assembly 30 .
- Refrigerant oil or other oil may flow between the connecting assembly 20 and the first rotor assembly 40 through the plurality of first oil supply passages 35 to lubricate or cool the connecting assembly 20 and the first rotor assembly 40 .
- the compressor 200 in the embodiment of the present disclosure may further include a second rotating shaft 50 and a second rotor assembly 60 , the second rotating shaft 50 is installed in the casing 10 , and the second rotating shaft 50 is located in the second rotating shaft 50 .
- the axial direction of the rotating shaft 50 is arranged in parallel with the first rotating shaft 20 .
- the second rotor assembly 60 may include a third rotor 61 and a fourth rotor 62 coaxially disposed on the second rotating shaft 50 , and the second rotating shaft 50 is configured to drive the second rotor assembly 60 along the distance between the first rotor assembly 40 and the second rotating shaft 50 .
- the third rotor 61 meshes with the first rotor 41
- the fourth rotor 62 meshes with the second rotor 42 .
- the first rotor assembly 20 can be a female rotor assembly
- the second rotor assembly 60 can be a male rotor assembly
- the second rotor assembly 60 serving as a male rotor assembly is an active rotor assembly
- Assembly 40 may be a driven rotor assembly.
- the second shaft 50 can be connected with a driving component such as a motor
- the first rotating shaft 50 can be driven to rotate by the driving component
- the first rotating shaft 50 drives the second rotor assembly 60 to rotate together when rotating
- the second rotor assembly 60 rotates
- the first rotor assembly 40 is driven to rotate around the first rotating shaft 20 .
- the first rotor assembly 40 and the second rotor assembly 60 will move axially under the action of the axial force.
- the two rotors of the first rotor assembly 40 and the two rotors of the second rotor assembly 60 are dislocated and meshed, and the two rotors of the first rotor assembly 40 and the two rotors of the second rotor assembly 60 interfere with each other, thereby causing the four rotors to be scratched. Even hanged situations occurred.
- the end face of the third rotor 61 close to the fourth rotor 62 protrudes from the end face of the first rotor 41 close to the second rotor 42
- the end face of the fourth rotor 62 close to the third rotor 61 protrudes from the end face of the first rotor 41 close to the second rotor 42
- the second rotor 42 is close to the end face of the first rotor 41 .
- the embodiment of the present disclosure can ensure that the first rotor 41 and the fourth rotor 62 do not interfere and the second rotor 31 and the third rotor 61 do not interfere.
- the third rotor 61 may have a fifth end face 611 and a sixth end face 612 arranged opposite to each other, the fifth end face 611 is a side close to the fourth rotor 62 , and the sixth end face 612 is a side away from the fourth rotor 62 , wherein the fifth end face 611 of the third rotor 61 is higher than the first end face 411 of the first rotor 41 in the axial direction of the second rotating shaft 50 , which can ensure that a part of the third rotor 61 is always located between the first rotor 41 and the second rotor 42 in the gap between.
- the fourth rotor 62 may have a seventh end face 621 and an eighth end face 622 arranged opposite to each other, the seventh end face 621 is a face close to the third rotor 61, and the eighth end face 622 is a face away from the third rotor 61, wherein the fourth rotor
- the seventh end surface 621 of the 62 is higher than the third end surface 421 of the second rotor 42 in the axial direction of the second rotating shaft 50 , which can ensure that a part of the fourth rotor 62 is always located in the gap between the first rotor 41 and the second rotor 42 Inside.
- a part of the third rotor 61 located in the first rotor 41 and the second rotor 42 can limit the seventh end face 621 of the fourth rotor 62 , so that the The seventh end surface 621 of the fourth rotor 62 and the first end surface 411 of the first rotor 41 always have a gap without interfering with each other;
- a part ie, the part higher than the third end surface 421 of the second rotor 31
- the three end faces 421 always have gaps without interfering with each other.
- the first rotor assembly 40 is limited by the connecting assembly 30, so that a third axial gap L3 is maintained between the first rotor 41 and the second rotor 42 in the first rotor assembly 40, and this
- the adjacent end faces of the third rotor 61 and the fourth rotor 62 of the second rotor assembly 60 are higher than the adjacent end faces of the first rotor 41 and the second rotor 42, respectively, thereby ensuring that the first rotor assembly 40 and the In the second rotor assembly 60, the two pairs of rotors located at the diagonal positions do not interfere with each other, so as to avoid the occurrence of scratches and strangulation of the rotors.
- the fifth end face 611 of the third rotor 61 is engaged with the seventh end face 621 of the fourth rotor 62 , that is, the adjacent end faces of the third rotor 61 and the fourth rotor 62 are engaged.
- the three rotors 61 and the fourth rotor 62 are arranged to be spaced apart from each other, and the embodiment of the present disclosure can reduce the overall length of the second rotor assembly 60 , thereby reducing the occupation of the inner space of the housing 10 by the second rotor assembly 60 .
- the third rotor 61 and the fourth rotor 62 are also possible to be spaced apart from each other, as long as it is ensured that the adjacent end faces of the third rotor 61 and the fourth rotor 62 are both located at the first rotor 41 and the fourth rotor 62 .
- the effect of ensuring that the two pairs of rotors located at the diagonal positions do not interfere with each other can also be achieved.
- the distance between the fifth end surface 611 of the third rotor 61 in the axial direction of the second rotating shaft 50 and the first end surface 411 of the first rotor 41 is d1 , and d1 may be 0.2mm, 0.3mm, 0.4mm or other smaller value.
- the distance between the seventh end surface 621 of the fourth rotor 62 and the third end surface 421 of the second rotor 42 in the axial direction of the second rotating shaft 50 is d2, and d2 may be 0.2 mm, 0.3 mm, 0.4 mm or other relatively small distances. small value.
- the second rotating shaft 50 and the second rotor assembly 60 will move in the axial direction of the second rotating shaft 50 under the influence of the axial force exerted thereon.
- the amount of movement is D1
- the amount of axial movement of the second rotor 42 in the direction close to the first rotor 41 is D2
- the fourth rotor 62 in the housing 10 in the axial direction of the second shaft 50 is close to the third rotor 61
- the axial movement amount of the first rotor 41 moving in the direction close to the second rotor 42 is D4
- the second rotor assembly 60 must satisfy: L3>D1+D2, and L3>D3 +D4, so as to ensure that the fifth end face 611 of the third rotor 61 does not interfere with the third end face 612 of the second rotor 42 and the seventh end face 621 of the fourth rotor 62 does not interfere with the first end face 621 of the first rotor 41
- the end face 411 interferes.
- the first rotor assembly 40 can move axially and the second rotor assembly 60 can move axially, when the two pairs of rotors located at the diagonal positions move axially toward each other
- the two pairs of rotors located in the diagonal position can always have a gap or the gap is just zero, so that the two pairs of rotors located in the diagonal position can always have a gap.
- the rotors do not interfere with each other.
- the housing 10 also has an accommodating space communicating with the housing 10 for accommodating the first rotating shaft 20 , the connecting assembly 30 , the first rotor assembly 40 , the second rotating shaft 50 and the second rotor assembly 60 .
- the suction port 11, the first exhaust port 12 and the second exhaust port 13, the suction port 11 is used to transmit the gas outside the casing 10 to the casing when the first rotor assembly 40 and the second rotor assembly 60 are engaged and rotated
- the accommodating space in the casing 10, the first exhaust port 12 and the second exhaust port 13 are used to compress the gas in the accommodating space of the casing 10 to the casing when the first rotor assembly 40 and the second rotor assembly 60 are engaged and rotated. body 10.
- the suction port 11 is located at adjacent positions of the first rotor 41 , the second rotor 42 , the third rotor 61 and the fourth rotor 62 , the first end face of the first rotor 41 , the third end face of the second rotor 42 , The fifth end face 611 of the third rotor 61 and the fourth rotor 621 are both suction end faces adjacent to the suction port 11 .
- the first exhaust port 12 is located at the adjacent positions of the first rotor 41 , the third rotor 61 and the casing 10 .
- the exhaust end face adjacent to the exhaust port 12; the second exhaust port 13 is located at the adjacent position of the second rotor 42, the fourth rotor 62 and the housing 10, the fourth end face 422 of the second rotor 42, the fourth rotor
- the eighth end surface 622 of 62 is the exhaust end surface adjacent to the second exhaust port 13 .
- the intake port 11 is located in the middle of the housing 10 along the axial direction of the first rotating shaft 30
- the first exhaust port 12 and the second exhaust port 13 are located along the axial direction of the first rotating shaft 20 . both ends of the housing 10.
- the helical direction of the first rotor 41 and the helical direction of the second rotor 42 are arranged in opposite directions, so that when the first rotor assembly 40 and the second rotor assembly 60 rotate in mesh with each other, the first rotor 41
- the opposite axial force is generated between the first rotor 41 and the second rotor 42
- the opposite axial flow is generated between the first rotor 41 and the second rotor 42 . Due to the symmetry of the axial force, the opposite axial forces generated between the first rotor 41 and the second rotor 42 can almost cancel each other out.
- the first rotor 41 may have a plurality of first helical blades 415
- the second rotor 42 may have a plurality of second helical blades 425
- the number of the first helical blades 415 is the same as that of the second helical blades 415.
- the number of the helical blades 425 is the same, and the helical direction of the first helical blade 415 and the helical direction of the second helical blade 425 can be set in opposite directions, for example, one can be configured as left-handed, and the other can be configured as right-handed, so as to realize the first
- the spiral directions of the first rotor 41 and the second rotor 42 are opposite.
- the helical direction of the third rotor 61 and the helical direction of the fourth rotor 62 are also configured to be opposite directions, so that when the first rotor assembly 40 and the second rotor assembly 60 rotate in mesh with each other, the third rotor 61
- the opposite axial force is generated between the fourth rotor 62 and the fourth rotor 62
- the opposite axial flow is generated between the third rotor 62 and the second rotor 42 . Due to the symmetry of the axial force, the opposite axial forces generated between the first rotor 41 and the second rotor 42 can almost cancel each other out.
- the third rotor 61 may have a plurality of third helical blades 613
- the fourth rotor 62 may have a plurality of fourth helical blades 623
- the number of the fourth helical blades 623 is the same as the number of the third helical blades 613 .
- the third rotor 61 may be integrally formed with the second rotating shaft 50, and the fourth rotor 62 may be directly sleeved on the second rotating shaft 50 and fixedly connected to the second rotating shaft 50.
- the fourth rotor 62 may have a The shaft hole 624 of the second rotating shaft 50 is matched with the shaft hole 624 and the second rotating shaft 50 in a tight fit so that the fourth rotor 63 is sleeved and connected to the second rotating shaft 50 .
- both the third rotor 61 and the fourth rotor 62 may be integrally formed with the second rotating shaft 50 , or the third rotor 61 and the fourth rotor 62 may be sleeved on the second rotating shaft 520 .
- the compressor 200 of the embodiment of the present disclosure further includes a thrust bearing 70 , the thrust bearing 70 is arranged on one side of the second rotating shaft 50 , and the third rotor 61 is connected to the first rotor 61 through the thrust bearing 70 .
- the remaining small amount of axial force between the four rotors 62 is balanced out, so that the forces of the third rotor 61 and the fourth rotor 62 are balanced.
- the compressor 200 further includes a drive motor 80, and the drive motor 80 is disposed on the other side of the second shaft 50.
- the second shaft 50 may have a first end portion 51 and a second end portion 52 disposed opposite to each other, and a thrust bearing 70 It is sleeved on the first end portion 51, and the second end portion 52 is drivingly connected with the driving motor 80.
- the driving motor 80 is configured to drive the second rotating shaft 50 to rotate to drive the second rotor assembly 60 to rotate, and drive the first rotor assembly 40. It rotates around the first rotating shaft 20 together with the connecting assembly 30 .
- the end face of the third rotor 61 away from the fourth rotor 62 is flush with the end face of the first rotor 41 away from the second rotor 42 in the direction perpendicular to the axial direction of the second rotating shaft 50 ; the fourth rotor 62 The end face away from the third rotor 61 is flush with the end face of the second rotor 42 away from the first rotor 41 in the direction perpendicular to the axial direction of the second rotating shaft 50 .
- the sixth end face 621 of the third rotor 61 is flush with the second end face 412 of the first rotor 41 in the first direction, that is, the exhaust end face of the third rotor 61 is flush with the first rotor
- the exhaust end face of the 41 is flush.
- the eighth end surface 62 of the fourth rotor 62 is flush with the fourth end surface 422 of the second rotor 42 in the first direction, and the exhaust end surface of the fourth rotor 62 is flush with the exhaust end surface of the second rotor 41 .
- the housing 10 may include a casing 14 , a first bearing seat 15 , and a second bearing seat 1 .
- the first bearing seat 15 is arranged on the side of the exhaust end face of the first rotor 41 and the third rotor 61 , or a part of the first bearing seat 15 is arranged on the side of the second end face 412 of the first rotor 41 .
- a part of the bearing housing 15 is provided on the sixth end face 412 side of the third rotor 42 .
- the first bearing seat 15 is also located between the first rotor 41 and the driving assembly 80 .
- the first bearing seat 15 is used to carry the first end 51 of the second rotating shaft 50 and the end of the first rotating shaft 20 close to the first rotor 41 . .
- the second bearing seat 16 is provided on the side of the exhaust end face of the second rotor 42 and the fourth rotor 62, or a part of the second bearing seat 16 is provided on the side of the fourth end face 422 of the second rotor 42.
- the first bearing seat A part of 15 is provided on the eighth end surface 622 side of the fourth rotor 62 .
- the second bearing seat 13 is used to carry the second end 52 of the second rotating shaft 30 and the end of the second rotating shaft 20 close to the third rotor 42 .
- the compressor 200 may further include a first radial bearing 91 and a second radial bearing 92, the first radial bearing 91 is sleeved on the first end 51 of the second rotating shaft 50, and the outer surface of the first radial bearing 91 Fitted with the first bearing seat 15 .
- the first bearing seat 15 may be provided with an installation groove, and the first radial bearing 91 is installed in the installation groove and abuts with the groove wall of the installation groove.
- the second radial bearing 92 is sleeved on the second end 52 of the second rotating shaft 50, and the second radial bearing 92 is located on the side of the thrust bearing 70 close to the third rotor 42.
- the outer surface of the thrust bearing 70 and The outer surfaces of the second radial bearings 92 are all abutted with the second bearing seat 16 .
- the second bearing seat 16 may also be provided with an installation groove, and both the thrust bearing 70 and the second radial bearing 92 are installed in the installation groove and are in contact with the groove wall of the installation groove.
- the second radial bearing 92 and the first radial bearing 12 are used for cooperating to balance the radial force of the second rotating shaft 50 .
- both ends of the first rotating shaft 30 may be respectively fixed on the first bearing seat 15 and the second bearing seat 13 .
- the third limiting member 33 and the fourth limiting member 34 in the embodiment of the present disclosure can limit the exhaust end face of the first rotor 41 so that there is a gap between the first rotor 41 and the first bearing seat 15 , and the second rotor 42 and the second bearing seat 14 have a gap, which can ensure that the exhaust end face of the first rotor 41 does not collide with the end face of the first bearing seat 15, and that the exhaust end face of the second rotor 42 does not collide with the end face of the second bearing seat 13 , or the exhaust end faces of the two groups of yin and yang rotors are separated from the end faces of the bearing housing.
- the compressor 200 in one or more of the above embodiments may be applied to an air conditioner.
- Embodiments of the present disclosure also provide an air conditioner including the compressor 200 as defined in combination with one or more of the above embodiments.
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Abstract
Description
Claims (23)
- 一种压缩机(200),包括:壳体(10);第一转轴(20),安装于所述壳体(10)内;连接组件(30),套设于所述第一转轴(20)上;以及第一转子组件(40),所述第一转子组件(40)包括同轴设置于所述连接组件(30)上的第一转子(41)和第二转子(42),所述连接组件(30)可承载所述第一转子(41)和所述第二转子(42)一起围绕所述第一转轴(20)旋转;其中,所述连接组件(30)还被配置为限制所述第一转子(41)和所述第二转子(42)的相对位置,以使得所述第一转子(41)和所述第二转子(42)之间具有间隙。
- 根据权利要求1所述的压缩机(200),其中所述第一转子(41)远离所述第二转子(42)的端面与所述壳体(10)靠近所述第一转子(41)的端面具有第一轴向间隙,所述第二转子(42)在远离所述第一转子(41)的端面与所述壳体(10)靠近所述第二转子(42)的端面具有第二轴向间隙,所述连接组件(30)被配置为限制所述第一转子(41)和所述第二转子(42)之间的间隙大于所述第一轴向间隙,以及所述第一转子(41)和所述第二转子(42)之间的间隙大于所述第二轴向间隙。
- 根据权利要求1或2所述的压缩机(200),还包括:第二转轴(50),安装于所述壳体(10)内;和第二转子组件(60),所述第二转子组件(60)包括同轴设置于所述第二转轴(50)上的第三转子(61)和第四转子(62),所述第二转轴(50)被配置为带动所述第二转子组件(60)沿与所述第一转子组件(40)的转动方向相反的方向转动,所述第三转子(61)与所述第一转子(41)相互啮合,所述第四转子(62)与所述第二转子(42)相互啮合。
- 根据权利要求3所述的压缩机(200),其中所述第三转子(61)靠近所述第四转子(62)的端面凸出于所述第一转子(41)靠近所述第二转子(42)的端面,且所述第四转子(62)靠近所述第三转子(61)的端面凸出于所述第二转子(42)靠近所述第一转子(41)的端面,以使得所述第一转子(41)与所述第四转子(62)不干涉以及所述第二转子(42)与所述第三转子(61)不干涉。
- 根据权利要求3或4所述的压缩机(200),其中所述第三转子(61)与所述第四转子(62)的相邻端面相接合。
- 根据权利要求3至5任一所述的压缩机(200),其中所述第三转子(61)靠近所述第四转子(62)的端面在所述第二转轴(50)的轴向方向上与所述第一转子(41)靠近所述第二转子(42)的端面之间的距离为d1,所述第四转子(62)靠近所述第三转子(61)的端面在所述第二转轴(50)的轴向方向上与所述第二转子(42)靠近所述第一转子(41)的端面之间的距离为d2,所述第二转子组件(60)被配置为满足:d2=d1。
- 根据权利要求3至6任一所述的压缩机(200),其中所述第一转子(41)和所述第二转子(42)之间的间隙为L3,所述第三转子(61)在所述壳体(10)内沿所述第二转轴(50)的轴向方向朝靠近所述第四转子(62)的方向移动的轴向移动量为D1,所述第二转子(42)朝靠近所述第一转子(41)的方向移动的轴向移动量为D2,所述第四转子(62)在所述壳体(10)内沿所述第二转轴(50)的轴向方向朝靠近第三转子(61)的方向移动的轴向移动量为D3,所述第一转子(41)朝靠近所述第二转子(42)的方向移动的轴向移动量为D4,所述第二转子组件(60)被配置为满足:L3≥D1+D2,且L3≥D3+D4。
- 根据权利要求3至7任一所述的压缩机(200),其中所述第一转子(41)、所述第二转子(42)、所述第三转子(61)和所述第四转子(62)的相邻位置处设置有吸气口(11),所述第一转子(41)、所述第三转子(61)和所述壳体(10)的相邻位置处设置有第一排气口(12),所述第二转子(42)、所述第四转子(62)和所述壳体(10)的相邻位置处设置有第二排气口(13)。
- 根据权利要求3至8任一所述的压缩机(200),其中所述第一转子(41)的螺旋方向与第二转子(42)的螺旋方向相反,所述第三转子(61)的螺旋方向与所述第四转子(62)的螺旋方向相反。
- 根据权利要求3至9任一所述的压缩机(200),其中所述第三转子(61)与所述第二转轴(50)一体成型,所述第四转子(62)具有与所述第二转轴(50)配合的轴孔,所述轴孔与所述第二转轴(50)采用紧配合。
- 根据权利要求3至10任一所述的压缩机(200),还包括设置在所述第二转轴(50)一侧的止推轴承(70)和设置在所述第二转轴(50)另一侧的电机(80),所述电机(80)被配置为驱动所述第二转轴(50)转动,以使得所述第二转子组件(60)跟随所述第二转轴(50)转动并带动所述第一转子组件(40)和所述连接组件(30)一起围绕所述第一转轴(20)转动。
- 根据权利要求3至11任一的压缩机(200),其中所述第三转子(61)远离所述第四转子(62)的端面在垂直于所述第二转轴(50)的轴向方向的方向上与所述第一转子 (41)远离所述第二转子(42)的端面齐平;所述第四转子(62)远离所述第三转子(61)的端面在垂直于所述第二转轴(50)的轴向方向的方向上与所述第二转子(42)远离所述第一转子(41)的端面齐平。
- 根据权利要求1至12任一项所述的压缩机(200),其中所述连接组件(30)包括均套设在所述第一转轴(20)上且均可围绕所述第一转轴(20)转动的第一限位件(31)和第二限位件(32),所述第一限位件(31)被配置为限制所述第一转子(41)靠近所述第二转子(42)的端面的位置,所述第二限位件(32)被配置为限制所述第二转子(42)靠近所述第一转子(41)的端面的位置。
- 根据权利要求13所述的压缩机(200),其中所述第一转子(41)靠近所述第二转子(42)的端面沿所述第一转轴(20)的轴向方向开设有第一限位槽(413),所述第一限位件(31)包括第一主体部(311)和第一限位部(312),所述第一主体部(311)套设在所述第一转轴(20)上,所述第一限位部(312)围绕设置在所述第一主体部(311)的外表面周缘且所述第一限位部(312)卡设在所述第一限位槽(413)内;所述第二转子(42)靠近所述第一转子(41)的端面沿所述第一转轴(20)的轴向方向开设有第二限位槽(423),所述第二限位件(32)包括第二主体部(321)和第二限位部(322),所述第二主体部(321)套设在第一转轴(20)上且与所述第一主体部(311)相邻设置,所述第二限位部(322)围绕设置在所述第二主体部(321)的外表面周缘且所述第二限位部(322)卡设在所述第二限位槽(423)内。
- 根据权利要求14所述的压缩机(200),其中所述第一限位部(312)靠近所述第二限位部(322)的端面凸出在所述第一转子(41)靠近所述第二转子(42)的端面的一侧,且所述第二限位部(322)靠近所述第一限位部(312)的端面凸出在所述第二转子(42)靠近所述第一转子(41)的端面的一侧。
- 根据权利要求1至15任一所述的压缩机(200),其中所述第一转子(41)靠近所述第二转子(42)的端面与所述第二转子(42)靠近所述第一转子(41)的端面在所述第一转轴(20)的轴向方向上的距离自所述第一转子组件(40)的轴线至所述第一转子组件(40)的外周缘逐渐增加。
- 根据权利要求13至16任一所述的压缩机(200),其中所述第一限位件(31)包括第一主体部(311)和第一限位部(312),所述第一主体部(311)套设在所述第一转轴(20)上,所述第一限位部(312)环绕设置在所述第一主体部(311)的外表面周缘,所述第一限位部(312)中背离所述第二转子(42)的一面与所述第一转子(41)靠近所 述第二转子(42)的端面抵接;所述第二限位件(32)包括第二主体部(321)和第二限位部(322),所述第二主体部(321)套设在所述第一转轴(20)上且与所述第一主体部(311)相邻设置,所述第二限位部(322)环绕设置在所述第二主体部(321)的外表面周缘,所述第二限位部(322)中背离所述第一转子(41)的一面与所述第二转子(42)靠近所述第一转子(41)的端面抵接。
- 根据权利要求13至17任一所述的压缩机(200),其中所述连接组件(30)还包括第三限位件(33)和第四限位件(34),所述第三限位件(33)被配置为限制所述第一转子(41)远离所述第二转子(42)的端面与所述壳体(10)之间的距离,所述第四限位件(34)被配置为限制所述第二转子(42)远离所述第一转子(41)的端面与所述壳体(10)之间的距离。
- 根据权利要求18所述的压缩机(200),其中所述第三限位件(33)包括第三主体部(331)和第三限位部(332),所述第三主体部(331)套设在所述第一转轴(20)上且与所述第一主体部(311)相邻设置,所述第三限位部(332)围绕设置在所述第三主体部(331)的外表面周缘,所述第三限位部(332)与所述第一转子(41)背离所述第二转子(42)的端面抵接;所述第四限位件(34)包括第四主体部(341)和第四限位部(342),所述第四主体部(341)套设在所述第一转轴(20)上且与所述第二主体部(321)相邻设置,所述第四限位部(342)围绕设置在所述第四主体部(341)的外表面周缘,所述第四限位部(342)与所述第二转子(42)背离所述第一转子(41)的端面抵接。
- 根据权利要求18或19所述的压缩机(200),其中所述第一转子(41)远离所述第二转子(42)的端面沿所述第一转轴(20)的轴向方向开设有第三限位槽(416),所述第三限位件(33)包括第三主体部(331)和第三限位部(332),所述第三主体部(331)套设在所述第一转轴(20)上且与所述第一主体部(311)相邻设置,所述第三限位部(332)围绕设置在所述第三主体部(331)的外表面周缘且所述第三限位部(332)卡设在所述第三限位槽(416)内;所述第二转子(42)远离所述第一转子(41)的端面沿所述第一转轴(20)的轴向方向开设有第四限位槽(426),所述第四限位件(34)包括第四主体部(341)和第四限位部(342),所述第四主体部(341)套设在所述第一转轴(20)上且与所述第二主体部(321)相邻设置,所述第四限位部(342)围绕设置在所述第四主体部(341)的外表面周缘且所 述第四限位部(342)卡设在所述第四限位槽(426)内。
- 根据权利要求1至20任一项所述的压缩机(200),其中所述连接组件(30)的材料包括锡青铜材料。
- 根据权利要求1至21任一项所述的压缩机(200),其中所述第一转轴(20)和所述连接组件(30)均设置有供油流道,位于所述第一转轴(20)上的供油流道(211,212)与位于所述连接组件(30)上的供油流道(35)连通。
- 一种空调,包括如权利要求1至22任一项所述的压缩机(200)。
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JP2023531658A JP2024507620A (ja) | 2021-02-26 | 2021-10-25 | 圧縮機及び空調装置 |
US18/267,875 US20240035471A1 (en) | 2021-02-26 | 2021-10-25 | Compressor and Air Conditioner |
KR1020237017746A KR20230147031A (ko) | 2021-02-26 | 2021-10-25 | 압축기 및 공조기 |
EP21927568.2A EP4234935A1 (en) | 2021-02-26 | 2021-10-25 | Compressor and air conditioner |
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CN202110219948.6A CN112780554A (zh) | 2021-02-26 | 2021-02-26 | 压缩机和空调 |
CN202110219948.6 | 2021-02-26 |
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EP (1) | EP4234935A1 (zh) |
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CN112780555A (zh) * | 2021-02-26 | 2021-05-11 | 珠海格力电器股份有限公司 | 转子组件、压缩机及空调 |
CN112780560A (zh) * | 2021-02-26 | 2021-05-11 | 珠海格力电器股份有限公司 | 一种转子组件、压缩机及空调机 |
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CN111247343A (zh) * | 2017-10-24 | 2020-06-05 | 开利公司 | 用于压缩机的润滑剂供应通道 |
CN109751240A (zh) * | 2017-11-02 | 2019-05-14 | 开利公司 | 具有非干扰系统的对置式螺杆压缩机 |
CN111043033A (zh) * | 2020-01-06 | 2020-04-21 | 珠海格力电器股份有限公司 | 螺杆压缩机和空调 |
CN112780554A (zh) * | 2021-02-26 | 2021-05-11 | 珠海格力电器股份有限公司 | 压缩机和空调 |
CN112780556A (zh) * | 2021-02-26 | 2021-05-11 | 珠海格力电器股份有限公司 | 压缩机及空调 |
CN112796999A (zh) * | 2021-02-26 | 2021-05-14 | 珠海格力电器股份有限公司 | 压缩机以及空调 |
CN215256792U (zh) * | 2021-02-26 | 2021-12-21 | 珠海格力电器股份有限公司 | 压缩机和空调 |
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JP2024507620A (ja) | 2024-02-21 |
KR20230147031A (ko) | 2023-10-20 |
CN112780554A (zh) | 2021-05-11 |
US20240035471A1 (en) | 2024-02-01 |
EP4234935A1 (en) | 2023-08-30 |
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