WO2014134961A1 - Scroll component and scroll compressor - Google Patents

Scroll component and scroll compressor Download PDF

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Publication number
WO2014134961A1
WO2014134961A1 PCT/CN2013/090720 CN2013090720W WO2014134961A1 WO 2014134961 A1 WO2014134961 A1 WO 2014134961A1 CN 2013090720 W CN2013090720 W CN 2013090720W WO 2014134961 A1 WO2014134961 A1 WO 2014134961A1
Authority
WO
WIPO (PCT)
Prior art keywords
scroll
component
scroll member
blade
step portion
Prior art date
Application number
PCT/CN2013/090720
Other languages
French (fr)
Chinese (zh)
Inventor
孙庆丰
Original Assignee
艾默生环境优化技术(苏州)有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from CN 201320097796 external-priority patent/CN203114634U/en
Priority claimed from CN201310068431.7A external-priority patent/CN104033386B/en
Application filed by 艾默生环境优化技术(苏州)有限公司 filed Critical 艾默生环境优化技术(苏州)有限公司
Publication of WO2014134961A1 publication Critical patent/WO2014134961A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F04C18/0207Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
    • F04C18/0215Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form where only one member is moving
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F04C18/0207Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
    • F04C18/0246Details concerning the involute wraps or their base, e.g. geometry
    • F04C18/0269Details concerning the involute wraps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C23/00Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
    • F04C23/008Hermetic pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C28/00Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
    • F04C28/28Safety arrangements; Monitoring

Definitions

  • the present invention relates to a scroll member and a scroll compressor including the scroll member. Background technique
  • Scroll compressors typically include a fixed scroll component and an orbiting scroll component.
  • the fixed scroll member and the movable scroll member respectively include an end plate and a substantially spiral scroll blade disposed on the end plate.
  • the scroll vanes of the fixed scroll member and the scroll vanes of the orbiting scroll member are engaged with each other to form a series of compression chambers whose volume gradually decreases from the radially outer side to the radially inner side, thereby realizing compression of the fluid.
  • the lateral seal between the scroll vanes of the fixed scroll member and the scroll vanes of the orbiting scroll member is achieved by the centrifugal force of the orbiting scroll member.
  • the orbiting scroll member is driven to rotate relative to the fixed scroll member (ie, the central axis of the orbiting scroll member is rotated about the central axis of the scroll member, but The scroll member itself does not rotate about its central axis, so that the scroll blades of the orbiting scroll member abut against the scroll blades of the fixed scroll member under the centrifugal force, thereby achieving a seal between the two .
  • the scroll blades of the orbiting scroll member or the fixed scroll member may be broken due to excessive centrifugal force. Therefore, there is a need for a scroll member that is more durable and a scroll compressor. Summary of the invention
  • a scroll member for a scroll compressor comprising: an end plate; and a spiral wrap blade formed on the end plate, the wrap blade being on the shaft Included in the direction of a proximal end adjacent the end plate and a distal end remote from the end plate, the scroll blade including an inner end near the substantially central position of the end plate and adjacent in the circumferential direction An outer end portion of the outer peripheral side of the end plate, and the scroll blade includes a radially inner side surface facing a center position of the end plate and a radially outer side surface facing an outer peripheral side of the end plate, wherein At least one of the radially inner side surface and the radially outer side surface is formed with a protrusion adapted to contact the scroll blade of the mating other scroll member, the position of the protrusion portion in the axial direction It is designed such that the distal end of the scroll blade does not come into contact with the scroll blades of the other scroll member during operation of the scroll compressor.
  • FIG. 1 is a longitudinal cross-sectional view of a conventional scroll compressor
  • 3 is a perspective view showing an orbiting scroll member according to an embodiment of the present invention
  • FIG. 4 is a view showing an embodiment of the present invention.
  • FIG. 5A is a partially cutaway perspective view showing a movable scroll member according to an embodiment of the present invention
  • FIG. 5B is a partially enlarged view of a portion B of FIG. 5A
  • FIG. 7 is a schematic view showing a compression state of an orbiting scroll member and a fixed scroll member according to an embodiment of the present invention;
  • FIG. 8 is a schematic view showing a compression process of an orbiting scroll member and a fixed scroll member according to an embodiment of the present invention
  • 9 is a perspective view showing a movable scroll member according to a modification of the embodiment of the present invention
  • FIG. 10 is a perspective view showing an orbiting scroll member according to another modification of the embodiment of the present invention
  • FIG. Is a perspective view showing a fixed scroll member according to still another modification of the embodiment of the present invention.
  • a conventional scroll compressor 100 generally includes a housing 110, a top cover 112 disposed at the end of the housing 110, a bottom cover 114 disposed at the other end of the housing 110, and a top cover 112 and
  • the partitions 116 between the housings 110 partition the internal space of the compressor into a high pressure side and a low pressure side.
  • a high pressure side is formed between the partition 116 and the top cover 112
  • a low pressure side is formed between the partition 116, the casing 110 and the bottom cover 114.
  • An intake joint 118 for sucking a fluid is provided on the low pressure side, and an exhaust joint 119 for discharging the compressed fluid is provided on the high pressure side.
  • a motor 120 composed of a stator 122 and a rotor 124 is disposed in the housing 110.
  • a drive shaft 130 is provided in the rotor 124 to drive a compression mechanism composed of the fixed scroll member 150 and the movable scroll member 160.
  • the movable scroll member 160 includes an end plate 164, a hub portion 162 formed on one side of the end plate, and a spiral blade 166 formed on the other side of the end plate.
  • the fixed scroll member 150 includes an end plate 154, a spiral blade 156 formed on one side of the end plate, and an exhaust port 152 formed at a substantially central position of the end plate.
  • a series of compression chambers C1, C2, and C3 whose volume gradually decreases from the radially outer side to the radially inner side are formed.
  • the radially outermost compression chamber C1 is at the suction pressure
  • the radially innermost compression chamber C3 is at the exhaust pressure.
  • the intermediate compression chamber C2 is between the suction pressure and the discharge pressure, and is also referred to as a medium pressure chamber.
  • One side of the movable scroll member 160 is supported by an upper portion of the main bearing housing 140 (which constitutes a thrust member), and one end of the drive shaft 130 is supported by a main bearing 144 provided in the main bearing housing 140.
  • One end of the drive shaft 130 is provided with an eccentric crank pin 132, and the eccentric crank pin 132 and the movement
  • An unloading bushing 142 is disposed between the hub portions 162 of the scroll member 160.
  • the above translational rotation is achieved by the cross slip ring 190 disposed between the fixed scroll member 150 and the movable scroll member 160.
  • the fluid compressed by the fixed scroll member 150 and the orbiting scroll member 160 is discharged to the high pressure side through the exhaust port 152.
  • a check valve or exhaust valve 170 is provided at the exhaust port 152.
  • an effective seal must be provided between the fixed scroll member 150 and the orbiting scroll member 160.
  • the distal end portion of the scroll blade 156 of the fixed scroll member 150 and the end plate 164 of the orbiting scroll member 160 and the distal end portion of the scroll blade 166 of the orbiting scroll member 160 and the fixed scroll member 150 An axial seal is required between the end plates 154.
  • a back pressure chamber 158 is provided on the opposite side of the end plate 154 of the fixed scroll member 150 from the scroll vanes 156.
  • a seal assembly 180 is disposed in the back pressure chamber 158, and the axial displacement of the seal assembly 180 is limited by the diaphragm 116.
  • the back pressure chamber 158 is in fluid communication with the intermediate pressure chamber C2 through an axially extending through bore (not shown) formed in the end plate 154 to form a force that urges the fixed scroll member 150 toward the orbiting scroll member 160. Since one side of the orbiting scroll member 160 is supported by the upper portion of the main bearing housing 140, the fixed scroll member 150 and the orbiting scroll member 160 can be effectively pressed together by the pressure in the back pressure chamber 158. When the pressure in each compression chamber exceeds a set value, the resultant force generated by the pressure in these compression chambers will exceed the downward pressure provided in the back pressure chamber 158 to cause the fixed scroll member 150 to move upward.
  • the fluid in the compression chamber will pass through the gap between the distal end portion of the scroll vane 156 of the fixed scroll member 150 and the end plate 164 of the orbiting scroll member 160 and the scroll vane 166 of the orbiting scroll member 160.
  • the gap between the distal end portion and the end plate 154 of the fixed scroll member 150 leaks to the low pressure side to effect unloading, thereby providing axial flexibility to the scroll compressor.
  • a radial seal is also required between the side surface of the scroll vane 156 of the fixed scroll member 150 and the side surface of the scroll vane 166 of the orbiting scroll member 160.
  • This radial sealing between the two is typically achieved by the centrifugal force of the orbiting scroll member 160 during operation and the driving force provided by the drive shaft 130.
  • the orbiting scroll member 160 will rotate in translation with respect to the fixed scroll member 150, so that the orbiting scroll member 160 will generate centrifugal force.
  • the eccentric crank pin 132 of the drive shaft 130 also generates a drive that facilitates radial sealing of the fixed scroll member and the orbiting scroll member during rotation. Force component.
  • the scroll vanes 166 of the orbiting scroll member 160 abut against the scroll vanes 156 of the fixed scroll member 150 by means of the above-described centrifugal force and driving force components, thereby achieving radial sealing therebetween.
  • the scroll vanes 156 and the scroll vanes 166 can be temporarily radially They are separated from each other to allow foreign matter to pass, thus preventing the scroll blades 156 or 166 from being damaged.
  • This ability to be radially separated provides radial flexibility to the scroll compressor, increasing compressor reliability.
  • the scroll blades of the orbiting scroll member or the fixed scroll member may be broken due to excessive centrifugal force and driving force. More specifically, as shown in FIG.
  • the orbiting scroll member 60 includes an end plate 64 and a spiral wrap blade 66 formed on the end plate 64.
  • the orbiting scroll member 60 may also include a hub portion 62 formed on the other side of the end plate 64 to receive the eccentric crank pin 132 and the unloading bushing 142 of the drive shaft 130.
  • the scroll blade 66 includes a proximal end portion 66A proximate the end plate 64 and a distal end portion 66B distal from the end plate 64 in an axial direction (ie, a direction parallel to the axis of rotation of the orbiting scroll member 60).
  • the scroll blade 66 includes an inner end portion 66C near a substantially central position of the end plate and an outer end portion 66D near the outer peripheral side of the end plate in the circumferential direction (more precisely, the extending direction of the spiral of the scroll blade 66) .
  • the scroll blade 66 further includes a radially inner side surface 66E facing the center position of the end plate and a radially outer side surface 66F facing the outer peripheral side of the end plate.
  • the radially inner side surface 66E and the radially outer side The side faces 66F are formed with protrusions 70 adapted to contact the matching scroll members 56 of the other scroll member, such as the fixed scroll member 50, the positions of the protrusions 70 in the axial direction are designed such that the scrolls The distal end portion 66B of the vane 66 does not contact the scroll vanes 56 of the fixed scroll member 50 during operation of the scroll compressor.
  • the projection 70 is spaced apart from the distal end portion 66B of the scroll vane 66 by a predetermined distance so that the projection 70 can come into contact with the scroll vane 56 of the fixed scroll member during operation of the scroll reducer .
  • the distance between the projection 70 and the end plate 64 is smaller than the distance between the distal end portion 66B and the end plate 64, in the case of the same centrifugal force, due to the force arm (from the contact point to the end plate) The distance is reduced, so that the bending moment at the proximal end portion 66A of the scroll blade 66 can also be reduced, thereby making it possible to reduce the possibility of the vortex blade breaking.
  • the projection 70 forms a step 80 on the radially inner side 66E and the radially outer side 66F. That is, the projections 70 are formed in the range from the proximal end portion 66A to the step portion 80 on the radially inner side surface 66E and the radially outer side surface 66F. More specifically, the thickness of the scroll blade 66 in the radial direction of the first portion 66-1 of the step portion 80 near the proximal end portion 66A side is larger than the near distal end portion 66B of the scroll blade 66 at the step portion 80.
  • the thickness of the second portion 66-2 of the side is in the radial direction, whereby a step portion 80 is formed between the first portion 66-1 having a larger thickness and the second portion 66-2 having a smaller thickness.
  • the longitudinal sections of the first portion 66-1 and the second portion 66-2 in a plane parallel to the axial direction are both rectangular, as shown in Figs. 5A and 5B.
  • the thickness T of the step portion 80 in the radial direction may be designed such that the end portion 66B of the scroll blade 66 does not contact the vortex of the fixed scroll member 50 under the action of temperature and gas force during operation of the scroll compressor. Blade 56.
  • the thickness T of the step portion 80 in the radial direction may be between 0.01 mm and 0.1 mm.
  • the seal between the second portion 66-2 of the scroll blade 66 of the orbiting scroll member 60 and the scroll blade 56 of the fixed scroll member 50 can be achieved, for example, by a lubricant therebetween, thus the two scroll blades 56 and The compression chamber between 66 can still effectively maintain a seal.
  • the extending range of the step portion 80 shown by a thick black solid line in FIG. 8) in the circumferential direction of the scroll blade 66 (the direction in which the spiral extends) may be designed as follows.
  • the step portion 80 may be designed in a portion of the scroll blade 66 that is relatively easily broken.
  • the step portion 80 can be disposed at least radially in outermost contact of the scroll vanes 66 of the driven scroll member 60 with the scroll vanes 56 of the other scroll member (i.e., the fixed scroll member 50).
  • the point P1 extends inwardly within a range of 360 degrees in the circumferential direction. That is, the step portion 80 The extent in the circumferential direction extends from the outermost contact point P1 to the point P2.
  • the spiral of the scroll blade 66 extends at an angle of approximately 720 degrees, then the point P1 to The angle between points P2 is greater than or equal to 360 degrees.
  • the radial direction of the portion of the scroll blade 66 of the orbiting scroll member 60 where the step portion 80 is not formed i.e., the portion near the center of the orbiting scroll member 60, or in other words, the portion extending inward from the point P2
  • the thickness may be designed to be the same as the thickness in the radial direction of the first portion 66-1. That is, the portion of the scroll blade 66 where the step portion 80 is not formed is also formed thicker, thereby making it less likely to be broken.
  • Figure 7 shows the relative position between the orbiting scroll member 60 and the fixed scroll member 50 during operation.
  • the position of the fixed scroll member 50 remains unchanged, and the orbiting scroll member 60 is rotated relative to the fixed scroll member 50 as indicated by the arrow in Fig. 7.
  • the outermost compression chamber C 1 is in an inhaled state.
  • the outermost compression chamber C1 is still in the inhalation state and is about to close.
  • the outermost compression chamber C 1 has been closed.
  • the height H of the step portion 80 may be between 40% and 60% of the height h (see Fig. 2) of the scroll vanes 66 of the orbiting scroll member 60 in the axial direction. More preferably, the height H of the step portion 80 may be approximately 50% of the height h of the scroll blade 66. As shown in FIG.
  • the height H of the step portion 80 is designed to be 50% of the height h of the scroll blade 66
  • the bending moment M2 at the proximal end portion 66A of the scroll blade 66 is only the existing design without the step portion 80.
  • the bending moment M1 (see Fig. 2) at the proximal end portion of the scroll blade is 50%, whereby the scroll blade 66 according to the embodiment of the present invention is less likely to be broken under the same high rotation speed condition.
  • the height H of the step portion 80 is generally designed to be in the vortex
  • the height of the rotor blade 66 is between 10% and 90%.
  • the orbiting scroll member 60 of the above configuration may be manufactured by, for example, a die casting process, or may be formed by milling, for example, by using an existing orbiting scroll member, and thus the production of the orbiting scroll member constructed in accordance with the present invention The process is still relatively simple and the manufacturing is lower.
  • the bending moment at the proximal end portion of the scroll blade can be effectively reduced, thereby effectively reducing the possibility of the vortex blade rupture, thereby improving the vortex The durability of the rotating parts.
  • the gap between the second portion of the scroll blade having a small thickness of the orbiting scroll member and the scroll blade of the fixed scroll member can be effectively sealed by the lubricant, the compression efficiency of the compressor is not Will decrease.
  • the thickness of the portion of the scroll blade 66 of the orbiting scroll member 60 where the step portion is not formed is designed to have a relatively large thickness.
  • the thickness of the first portion 66-1 in the radial direction is the same, but the thickness of the portion of the scroll blade 66 of the orbiting scroll member 60 in which the step portion is not formed may be the thickness of the second portion having a relatively small thickness.
  • the thickness of the 66-2 in the radial direction is the same.
  • the step portion 90 is provided at least at the radially outermost side of the scroll blade 66 of the driven scroll member 60 and the scroll blade 56 of the other scroll member 50.
  • the contact point P1 extends inwardly in the circumferential direction by 360 degrees, but in the symmetrical design of the scroll member shown in FIG. 9, the step portion 80 may be provided at least at the scroll blade 66 of the driven scroll member 60.
  • the outer end portion 66D extends inwardly within a range of 360 degrees in the circumferential direction.
  • the thickness of the portion of the scroll blade 66 of the movable scroll member 60 in which the step portion is not formed may be designed to have the same thickness as the radial direction of the first portion 66-1, or It may be designed to be the same thickness as the radial direction of the second portion 66-2.
  • the step portion 80 may be disposed within the range from the outer end portion 66D of the scroll blade 66 of the driven scroll member 60 to the inner end portion 66C, as shown in FIG.
  • the projection 70 formed with the step portion 80 is formed in the radial direction of the scroll blade 66, and the surface 66 is formed on the radially outer side surface 66F, but is formed on the step side surface 66F.
  • the protrusion 70 in which the step portion 80 is formed is formed on the orbiting scroll member 60, but the protrusion portion 70 in which the step portion 80 is formed may also form a fixed scroll member. 50, as shown in Figure 11.
  • the fixed scroll member 50 may include an end plate 54 and a spiral wrap vane 56 formed on the end plate 54.
  • the scroll vanes 56 include a proximal end portion 56A proximate the end plate 54 and a distal end portion 56B distal from the end plate 54 in an axial direction (ie, a direction parallel to the central axis of the fixed scroll member 50).
  • the scroll blade 56 includes an inner end portion 56C near a substantially central position of the end plate and an outer end portion 56D near the outer peripheral side of the end plate in the circumferential direction (more precisely, the extending direction of the spiral of the scroll blade 56) .
  • the scroll blade 56 further includes a radially inner side surface 56E facing the center position of the end plate and a radially outer side surface 56F facing the outer peripheral side of the end plate.
  • both the radially inner side surface 56E and the radially outer side surface 56F are formed with projections 70 adapted to contact the corresponding scroll member of the other scroll member, such as the orbiting scroll member 60.
  • the projection 70 forms a step portion 80 on the radially inner side surface 56E and the radially outer side surface 56F.
  • Parameters such as the thickness, height, and circumferential extent of the step portion 80, as well as other variations, can be determined with reference to the configuration and variations of the orbiting scroll member 60 described above.
  • the protrusion 70 is configured in the form of a step portion 80, but the protrusion 70 may be configured in other forms, for example, the protrusion 70 may be configured to be formed on the radially inner side surface 66E of the scroll blade 66. And/or a raised portion on the radially outer side 66F.
  • the ridge portion may be provided at least in a range extending 360 degrees inward from the radially outermost contact point of the scroll blade of the scroll member and the scroll blade of the other scroll member in the circumferential direction. .
  • the ridge height of the ridge may be between 0.01 mm and 0.1 mm.
  • the height of the ridge portion in the axial direction from the end plate may be between 10% and 90% of the height in the axial direction of the scroll blade of the scroll member.
  • a scroll member for a scroll compressor comprising: an end plate; and a spiral wrap blade formed on the end plate, the wrap blade
  • the axial direction includes a proximal end portion adjacent the end plate and a distal end portion remote from the end plate, the scroll blade including an inner end portion in a circumferential direction near a substantially central position of the end plate and An outer end portion on an outer peripheral side of the end plate, and the scroll blade includes a radially inner side surface facing a center position of the end plate and a radially outer side surface facing an outer peripheral side of the end plate, wherein At least one of the radially inner side surface and the radially outer side surface may be formed with a protrusion adapted to contact a corresponding scroll blade of another scroll member, the protrusion being axially oriented The position is such that the distal end of the scroll vane does not contact the scroll vanes of the other scroll member during operation of the scroll compressor.
  • the protrusion may be configured to be on the radially inner side and/or Or a step portion is formed on the radially outer side surface.
  • the thickness of the scroll blade of the scroll member in the radial direction of the first portion of the step portion near the proximal end portion may be larger than the vortex of the scroll member
  • the thickness of the spiral blade in the radial direction of the second portion of the step portion near the distal end portion may be larger than the vortex of the scroll member
  • the step portion may be provided at least in a circumferential direction from a radially outermost contact point of the scroll blade of the scroll member and the scroll blade of the other scroll member The inside extends within a range of 360 degrees.
  • the thickness of the portion of the scroll blade of the scroll member where the step portion is not formed may be the same as the thickness of the first portion in the radial direction.
  • the thickness of the portion of the scroll blade of the scroll member where the step portion is not formed may be the same as the thickness of the second portion in the radial direction.
  • the step portion may be provided at least in a range extending 360 degrees inward from the outer end portion of the scroll blade of the scroll member in the circumferential direction.
  • the thickness of the portion of the scroll blade of the scroll member where the step portion is not formed may be the same as the thickness of the first portion in the radial direction.
  • the thickness of the portion of the scroll blade of the scroll member where the step portion is not formed may be the same as the thickness of the second portion in the radial direction.
  • the step portion may be provided in a range from an outer end portion of the scroll blade of the scroll member to the inner end portion.
  • the thickness of the step portion in the radial direction may be
  • the height of the step portion from the axial direction of the end plate may be between 10% and 90% of the height of the scroll blade in the axial direction of the scroll member .
  • the height of the step portion may be between 40% and 60% of the height of the scroll blade of the scroll member.
  • the height of the step portion may be the scroll member 50% of the height of the vortex blade.
  • the longitudinal section of the first portion and the second portion in a plane parallel to the axial direction may be both rectangular.
  • the protrusion portion may be formed on both the radially inner side surface and the radially outer side surface.
  • the scroll member may be a movable scroll member, and the other scroll member may be a fixed scroll member.
  • the scroll member is a fixed scroll member, and the other scroll member is a movable scroll member.
  • the scroll member may be an asymmetrically designed scroll member.
  • the scroll member may be a vortex member of a symmetrical design.
  • the protrusion may be formed as a ridge on the radially inner side surface and/or the radially outer side surface.
  • the ridge portion may be disposed at least in a circumferential direction from a radially outermost contact point of the scroll blade of the scroll member and the scroll blade of the other scroll member The direction extends inward by 360 degrees.
  • the ridge height of the ridge portion may be between 0.01 mm and 0.1 mm.
  • the height of the ridge portion from the axial direction of the end plate may be 10% to 90% of the height of the scroll blade in the axial direction of the scroll member. between.
  • a scroll compressor comprising the above scroll member.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Abstract

Disclosed is a scroll component (60,50) for a scroll compressor, the scroll component comprising: an end plate (64,54); and a helical scroll blade (66,56) formed on the end plate, wherein the scroll blade comprises a near end part and a distant end part in an axial direction, and comprises an inner end part and an outer end part in a circumferential direction, and also comprises a radial inner side face (66E, 56E) and a radial outer side face (66F, 56F), and wherein a protruding part (70) which is suitable for contact with a scroll blade (56,66) of another matching scroll component (50,60) is formed on at least one of the radial inner side face and the radial outer side face. Further disclosed is a scroll compressor comprising the scroll component. This scroll component can effectively reduce the possibility that the scroll blade ruptures, thereby increasing the durability of the scroll component.

Description

涡旋部件和涡旋压缩机 相关申请的交叉引用 本申请要求于 2013 年 3 月 4 日提交中国专利局的、 申请号为 201310068431.7、 发明名称为 "涡旋部件和涡旋压缩机" 以及于 2013年 3 月 4日提交中国专利局的、 申请号为 201320097796.8、 发明名称为 "涡旋 部件和涡旋压缩机" 的中国专利申请的优先权, 上述专利申请的全部内容 通过参引结合在本申请中。 技术领域  WIRELESS COMPONENTS AND VORTEX COMPRESSOR CROSS-REFERENCE TO RELATED APPLICATIONS [0001] This application claims to be assigned to the Chinese Patent Office on March 4, 2013, with the application number 201310068431.7, the invention titled "Vortex Parts and Scroll Compressors" and in 2013 Priority of Chinese Patent Application No. 201320097796.8, entitled "Vortex Parts and Scroll Compressors", filed on March 4, the entire contents of which is hereby incorporated by reference. in. Technical field
本发明涉及一种涡旋部件以及一种包括该涡旋部件的涡旋压缩机。 背景技术  The present invention relates to a scroll member and a scroll compressor including the scroll member. Background technique
本部分的内容仅提供了与本公开相关的背景信息, 其可能并不构成 现有技术。 涡旋压缩机通常包括定涡旋部件和动涡旋部件。 定涡旋部件和动涡 旋部件分别包括端板和设置在端板上的大致螺旋状的涡旋叶片。定涡旋 部件的涡旋叶片和动涡旋部件的涡旋叶片彼此接合以在其间形成一系 列体积从径向外侧向径向内侧逐渐变小的压缩腔, 以此实现流体的压 缩。 通常, 定涡旋部件的涡旋叶片和动涡旋部件的涡旋叶片之间的侧向 密封通过动涡旋部件的离心力来实现。 换言之, 在涡旋压缩机的运转过 程中, 动涡旋部件被驱动而相对于定涡旋部件平动转动(即, 动涡旋部 件的中心轴线绕定涡旋部件的中心轴线旋转,但是动涡旋部件本身不会 绕自身的中心轴线旋转), 从而动涡旋部件的涡旋叶片在离心力的作用 下贴靠在定涡旋部件的涡旋叶片上, 由此在二者之间实现密封。 然而, 在涡旋压缩机高速旋转的状态下,动涡旋部件或定涡旋部件的涡旋叶片 有可能由于受到过大的离心力而破裂。 因此, 需要一种耐久性更好的涡旋部件以及涡旋压缩机。 发明内容 The content of this section merely provides background information related to the present disclosure, which may not constitute prior art. Scroll compressors typically include a fixed scroll component and an orbiting scroll component. The fixed scroll member and the movable scroll member respectively include an end plate and a substantially spiral scroll blade disposed on the end plate. The scroll vanes of the fixed scroll member and the scroll vanes of the orbiting scroll member are engaged with each other to form a series of compression chambers whose volume gradually decreases from the radially outer side to the radially inner side, thereby realizing compression of the fluid. Generally, the lateral seal between the scroll vanes of the fixed scroll member and the scroll vanes of the orbiting scroll member is achieved by the centrifugal force of the orbiting scroll member. In other words, during operation of the scroll compressor, the orbiting scroll member is driven to rotate relative to the fixed scroll member (ie, the central axis of the orbiting scroll member is rotated about the central axis of the scroll member, but The scroll member itself does not rotate about its central axis, so that the scroll blades of the orbiting scroll member abut against the scroll blades of the fixed scroll member under the centrifugal force, thereby achieving a seal between the two . However, in a state where the scroll compressor is rotated at a high speed, the scroll blades of the orbiting scroll member or the fixed scroll member may be broken due to excessive centrifugal force. Therefore, there is a need for a scroll member that is more durable and a scroll compressor. Summary of the invention
根据本发明的一个方面, 提供了一种用于涡旋压缩机的涡旋部件, 包括: 端板; 以及形成在所述端板上的螺旋状的涡旋叶片, 所述涡旋叶片 在轴向方向上包括靠近所述端板的近端部和远离所述端板的远端部, 所述 涡旋叶片在周向方向上包括靠近所述端板的大致中心位置的内端部和靠 近所述端板的外周侧的外端部, 并且所述涡旋叶片包括面向所述端板的中 心位置的径向内侧面和面向所述端板的外周侧的径向外侧面, 其中在所述 径向内侧面和所述径向外侧面中的至少一者上形成有适于与相配的另一 涡旋部件的涡旋叶片接触的突起部, 所述突出部在轴向方向上的位置设计 成使得所述涡旋叶片的远端部在所述涡旋压缩机运转过程中不会与所述 另一涡旋部件的涡旋叶片接触。 根据本发明的另一个方面, 提供了一种包括上述涡旋部件的涡旋压 缩机。 附图说明  According to an aspect of the invention, a scroll member for a scroll compressor is provided, comprising: an end plate; and a spiral wrap blade formed on the end plate, the wrap blade being on the shaft Included in the direction of a proximal end adjacent the end plate and a distal end remote from the end plate, the scroll blade including an inner end near the substantially central position of the end plate and adjacent in the circumferential direction An outer end portion of the outer peripheral side of the end plate, and the scroll blade includes a radially inner side surface facing a center position of the end plate and a radially outer side surface facing an outer peripheral side of the end plate, wherein At least one of the radially inner side surface and the radially outer side surface is formed with a protrusion adapted to contact the scroll blade of the mating other scroll member, the position of the protrusion portion in the axial direction It is designed such that the distal end of the scroll blade does not come into contact with the scroll blades of the other scroll member during operation of the scroll compressor. According to another aspect of the present invention, a scroll compressor including the above scroll member is provided. DRAWINGS
通过以下参照附图的描述, 本发明的一个或几个实施方式的特征和 优点将变得更加容易理解, 其中: 图 1是常规的涡旋压缩机的纵剖视图; 图 2是图 1中的动涡旋部件和定涡旋部件的局部放大图; 图 3是示出了根据本发明一种实施方式的动涡旋部件的立体图; 图 4是示出了根据本发明一种实施方式的定涡旋部件的立体图; 图 5A是示出了根据本发明一种实施方式的动涡旋部件的局部剖切 的立体图, 图 5B是图 5A中 B部分的局部放大图; 图 6示出了根据本发明一种实施方式的动涡旋部件的受力状态图; 图 7示出了根据本发明一种实施方式的动涡旋部件和定涡旋部件的 压缩过程的示意图; 图 8是根据本发明一种实施方式的动涡旋部件的突起部 (台阶部) 的延伸范围的示意图; 图 9是示出了根据本发明实施方式的一种变型的动涡旋部件的立体 图; 图 10是示出了根据本发明实施方式的另一种变型的动涡旋部件的 立体图; 以及 图 11 是示出了根据本发明实施方式的又一种变型的定涡旋部件的 立体图。 具体实施方式 BRIEF DESCRIPTION OF THE DRAWINGS Features and advantages of one or more embodiments of the present invention will be more readily understood from the following description of the accompanying drawings in which: Figure 1 is a longitudinal cross-sectional view of a conventional scroll compressor; 3 is a perspective view showing an orbiting scroll member according to an embodiment of the present invention; and FIG. 4 is a view showing an embodiment of the present invention. FIG. 5A is a partially cutaway perspective view showing a movable scroll member according to an embodiment of the present invention, and FIG. 5B is a partially enlarged view of a portion B of FIG. 5A; FIG. FIG. 7 is a schematic view showing a compression state of an orbiting scroll member and a fixed scroll member according to an embodiment of the present invention; FIG. 8 is a schematic view showing a compression process of an orbiting scroll member and a fixed scroll member according to an embodiment of the present invention; A schematic view showing an extension range of a protrusion (step portion) of an orbiting scroll member according to an embodiment; 9 is a perspective view showing a movable scroll member according to a modification of the embodiment of the present invention; FIG. 10 is a perspective view showing an orbiting scroll member according to another modification of the embodiment of the present invention; and FIG. Is a perspective view showing a fixed scroll member according to still another modification of the embodiment of the present invention. detailed description
下面对优选实施方式的描述仅仅是示范性的, 而绝不是对本发明及其 应用或用法的限制。 在各个附图中采用相同的附图标记来表示相同的部 件, 因此相同部件的构造将不再重复描述。  The following description of the preferred embodiments is merely exemplary and is in no way limiting of the invention The same reference numerals are used to denote the same parts in the respective drawings, and thus the description of the same components will not be repeated.
首先将参照图 1-2描述根据常规的涡旋压缩机 100的基本构造和原 理。 如图 1-2所示, 常规的涡旋压缩机 100一般包括壳体 110、 设置在 壳体 110—端的顶盖 112、 设置在壳体 110另一端的底盖 114以及设置 在顶盖 112和壳体 110之间以将压缩机的内部空间分隔成高压侧和低压 侧的隔板 116。 隔板 116和顶盖 112之间构成高压侧, 而隔板 116、 壳体 110和底盖 114之间构成低压侧。 在低压侧设置有用于吸入流体的进气 接头 118, 在高压侧设置有用于排出压缩后的流体的排气接头 119。 壳 体 110中设置有由定子 122和转子 124构成的电机 120。 转子 124中设 置有驱动轴 130以驱动由定涡旋部件 150和动涡旋部件 160构成的压缩 机构。 动涡旋部件 160包括端板 164、 形成在端板一侧的毂部 162和形 成在端板另一侧的螺旋状的叶片 166。 定涡旋部件 150包括端板 154、 形成在端板一侧的螺旋状的叶片 156和形成在端板的大致中央位置处的 排气口 152。 在定涡旋部件 150的涡旋叶片 156和动涡旋部件 160的涡 旋叶片 166之间形成一系列体积从径向外侧向径向内侧逐渐减小的压缩 腔 C l、 C2和 C3。 其中, 径向最外侧的压缩腔 C 1处于吸气压力, 径向 最内侧的压缩腔 C3处于排气压力。 中间的压缩腔 C2处于吸气压力和 排气压力之间, 从而也被称之为中压腔。 动涡旋部件 160的一侧由主轴承座 140的上部(该部分构成止推构 件)支撑, 驱动轴 130的一端由设置在主轴承座 140中的主轴承 144支 撑。 驱动轴 130的一端设置有偏心曲柄销 132, 在偏心曲柄销 132和动 涡旋部件 160的毂部 162之间设置有卸载衬套 142。 通过电机 120的驱 动, 动涡旋部件 160将相对于定涡旋部件 150平动转动(即, 动涡旋部 件 160的中心轴线绕定涡旋部件 150的中心轴线旋转,但是动涡旋部件 160本身不会绕自身的中心轴线旋转) 以实现流体的压缩。 上述平动转 动通过定涡旋部件 150和动涡旋部件 160之间设置的十字滑环 190来实 现。经过定涡旋部件 150和动涡旋部件 160压缩后的流体通过排气口 152 排出到高压侧。为了防止高压侧的流体在特定情况下经由排气口 152回 流到低压侧, 在排气口 152处设置有单向阀或排气阀 170。 为了实现流体的压缩, 定涡旋部件 150和动涡旋部件 160之间必须 有效密封。 一方面, 定涡旋部件 150的涡旋叶片 156的远端部与动涡旋 部件 160的端板 164之间以及动涡旋部件 160的涡旋叶片 166的远端部 与定涡旋部件 150的端板 154之间需要轴向密封。 通常, 在定涡旋部件 150的端板 154的与涡旋叶片 156相反的一侧 设置有背压腔 158。 背压腔 158 中设置有密封组件 180, 密封组件 180 的轴向位移受到隔板 116的限制。 背压腔 158通过端板 154中形成的轴 向延伸的通孔(未示出) 与中压腔 C2流体连通从而形成将定涡旋部件 150朝向动涡旋部件 160压的力。 由于动涡旋部件 160的一侧由主轴承 座 140的上部支撑, 所以利用背压腔 158中的压力可以有效地将定涡旋 部件 150和动涡旋部件 160压在一起。 当各个压缩腔中的压力超过设定 值时,这些压缩腔中的压力所产生的合力将超过背压腔 158中提供的下 压力从而使得定涡旋部件 150向上运动。 此时, 压缩腔中的流体将通过 定涡旋部件 150的涡旋叶片 156的远端部与动涡旋部件 160的端板 164 之间的间隙以及动涡旋部件 160的涡旋叶片 166的远端部与定涡旋部件 150的端板 154之间的间隙泄漏到低压侧以实现卸载, 从而为涡旋压缩 机提供了轴向柔性。 另一方面, 定涡旋部件 150的涡旋叶片 156的侧表面与动涡旋部件 160的涡旋叶片 166的侧表面之间也需要径向密封。 二者之间的这种径 向密封通常借助于动涡旋部件 160 在运转过程中的离心力以及驱动轴 130提供的驱动力来实现。 具体地, 在运转过程中, 通过电机 120的驱 动, 动涡旋部件 160将相对于定涡旋部件 150平动转动, 从而动涡旋部 件 160将产生离心力。 另一方面, 驱动轴 130的偏心曲柄销 132在旋转 过程中也会产生有助于实现定涡旋部件和动涡旋部件径向密封的驱动 力分量。动涡旋部件 160的涡旋叶片 166将借助于上述离心力和驱动力 分量贴靠在定涡旋部件 150的涡旋叶片 156上,从而实现二者之间的径 向密封。 当不可压缩物质(诸如固体杂质、 润滑油以及液态制冷剂)进 入压缩腔中而卡在涡旋叶片 156和涡旋叶片 166之间时, 涡旋叶片 156 和涡旋叶片 166能够暂时沿径向彼此分开以允许异物通过, 因此防止了 涡旋叶片 156或 166损坏。这种能够径向分开的能力为涡旋压缩机提供 了径向柔性, 提高了压缩机的可靠性。 然而, 在涡旋压缩机高速旋转的状态下, 动涡旋部件或定涡旋部件 的涡旋叶片有可能由于受到过大的离心力和驱动力而破裂。 更具体地, 如图 2所示, 在动涡旋部件 160的实际运转过程中, 由于温度和气体力 等的共同作用, 在最不利的情况下, 涡旋叶片 166的远端部(图 2中的 上端)将与定涡旋部件 160的端板 154与涡旋叶片 156之间的连接部相 互作用从而承受作用力 f, 此时, 涡旋叶片 166的近端部 (图 2中的下 端)将承受弯矩 M l=f*h, 其中 h为涡旋叶片 166的轴向方向的高度。 随着电机 120的转速的增加, 作用力 f也增加, 因此涡旋叶片 166可能 在近端部处断裂。 图 3-8示出了根据本发明一种实施方式的构造的示例。 在根据该实 施方式的构造中,仅对动涡旋部件 60的涡旋叶片 66的构造进行了改进。 定涡旋部件 50 (如图 4所示) 的构造则与图 1-2所示的定涡旋部件 150 的构造相同, 即, 定涡旋部件 50包括端板 54和形成在端板 54上的螺 旋状的涡旋叶片 56。 首先, 参照图 3所示的动涡旋部件 60的立体图, 根据本发明一种 实施方式的动涡旋部件 60包括端板 64以及形成在端板 64上的螺旋状的 涡旋叶片 66。 动涡旋部件 60还可以包括形成在端板 64另一侧的毂部 62 以接收驱动轴 130的偏心曲柄销 132和卸载衬套 142。涡旋叶片 66在轴向 方向 (即平行于动涡旋部件 60的旋转轴线的方向)上包括靠近端板 64的 近端部 66A和远离端板 64的远端部 66B。 涡旋叶片 66在周向方向(更准 确地,涡旋叶片 66的螺旋线的延伸方向)上包括靠近端板的大致中心位置 的内端部 66C和靠近端板的外周侧的外端部 66D。 涡旋叶片 66还包括面 向端板的中心位置的径向内侧面 66E 和面向端板的外周侧的径向外侧面 66F。 在根据本实施方式的动涡旋部件 60中, 在径向内侧面 66E和径向外 侧面 66F二者上形成有适于与相配的另一涡旋部件例如定涡旋部件 50的 涡旋叶片 56接触的突起部 70,该突出部 70在轴向方向上的位置设计成使 得涡旋叶片 66的远端部 66B在涡旋压缩机运转过程中不会与定涡旋部件 50的涡旋叶片 56接触。 或者, 换言之, 突出部 70与涡旋叶片 66的远端 部 66B隔开预定距离, 从而在涡^^缩机的运转过程中, 该突出部 70可 以与定涡旋部件的涡旋叶片 56接触。 在这种情况下, 由于突出部 70与端 板 64之间的距离小于远端部 66B与端板 64之间的距离, 所以在离心力相 同的情况下, 由于力臂(从接触点到端板的距离)减小, 所以涡旋叶片 66 的近端部 66A处的弯矩也能够被减小,从而能够减小涡旋叶片破裂的可能 性。 在一种优选方式中, 突起部 70在径向内侧面 66E和径向外侧面 66F 上形成台阶部 80。 即, 在径向内侧面 66E和径向外侧面 66F上, 从近端 部 66A到台阶部 80的范围内构成所述突起部 70。 更具体地, 涡旋叶片 66 的位于台阶部 80的靠近近端部 66A—侧的第一部分 66-1的径向方向的厚 度大于涡旋叶片 66的位于台阶部 80的靠近远端部 66B—侧的第二部分 66-2的径向方向的厚度, 由此,在厚度较大的第一部分 66-1和厚度较小的 第二部分 66-2之间形成台阶部 80。 例如, 为了加工和制造的方便, 第一 部分 66-1和第二部分 66-2的在平行于轴向方向的平面上的纵向截面均为 矩形, 如图 5A和 5B所示。 台阶部 80的径向方向的厚度 T可以设计成使 得涡旋压缩机在运行过程中涡旋叶片 66的远端部 66B在温度和气体力的 作用下仍然不会接触定涡旋部件 50的涡旋叶片 56。 例如, 台阶部 80的径 向方向的厚度 T可以在 0.01mm至 0.1mm之间。 动涡旋部件 60的涡旋叶 片 66的第二部分 66-2与定涡旋部件 50的涡旋叶片 56之间的密封例如可 以通过其间的润滑剂来实现, 因此两个涡旋叶片 56和 66之间的压缩腔仍 然可以有效地保持密封。 另外, 参见图 8, 台阶部 80 (在图 8中以粗的黑实线示出)在涡旋叶 片 66的周向方向(螺旋线延伸的方向)上的延伸范围可以如下设计。例如, 台阶部 80可以设计在涡旋叶片 66的相对容易破裂的部分。 此时可以考虑 的两个主要因素的离心力的大小和涡旋叶片的受力状态。 本领域技术人员 可以理解涡旋叶片 66 的螺旋线的曲率半径相对较大的部分为相对容易破 裂的部分。 在一种优选方式中, 台阶部 80可以至少设置在从动涡旋部件 60的涡旋叶片 66与另一涡旋部件(即定涡旋部件 50 )的涡旋叶片 56的径 向最外侧接触点 P1沿周向方向向内延伸 360度的范围内。 即, 台阶部 80 在周向方向上的延伸范围为从最外侧接触点 P1延伸到点 P2。 当以图 8中 的点 O作为涡旋叶片 66的螺旋线的中心时, 对于目前常见的涡旋部件的 设计而言,涡旋叶片 66的螺旋线延伸大致 720度的角度,则点 P1至点 P2 之间的角度大于或等于 360度。 动涡旋部件 60的涡旋叶片 66的未形成有 台阶部 80的部分(即, 靠近动涡旋部件 60的中心的部分, 或者换言之, 从点 P2开始向内延伸的部分)的径向方向的厚度可以设计成与第一部分 66-1的径向方向的厚度相同。 即, 涡旋叶片 66的未形成有台阶部 80的部 分也形成的较厚, 由此更不易破裂。 First, the basic configuration and principle of a conventional scroll compressor 100 will be described with reference to Figs. As shown in FIGS. 1-2, a conventional scroll compressor 100 generally includes a housing 110, a top cover 112 disposed at the end of the housing 110, a bottom cover 114 disposed at the other end of the housing 110, and a top cover 112 and The partitions 116 between the housings 110 partition the internal space of the compressor into a high pressure side and a low pressure side. A high pressure side is formed between the partition 116 and the top cover 112, and a low pressure side is formed between the partition 116, the casing 110 and the bottom cover 114. An intake joint 118 for sucking a fluid is provided on the low pressure side, and an exhaust joint 119 for discharging the compressed fluid is provided on the high pressure side. A motor 120 composed of a stator 122 and a rotor 124 is disposed in the housing 110. A drive shaft 130 is provided in the rotor 124 to drive a compression mechanism composed of the fixed scroll member 150 and the movable scroll member 160. The movable scroll member 160 includes an end plate 164, a hub portion 162 formed on one side of the end plate, and a spiral blade 166 formed on the other side of the end plate. The fixed scroll member 150 includes an end plate 154, a spiral blade 156 formed on one side of the end plate, and an exhaust port 152 formed at a substantially central position of the end plate. Between the scroll vanes 156 of the fixed scroll member 150 and the scroll vanes 166 of the orbiting scroll member 160, a series of compression chambers C1, C2, and C3 whose volume gradually decreases from the radially outer side to the radially inner side are formed. Wherein, the radially outermost compression chamber C1 is at the suction pressure, and the radially innermost compression chamber C3 is at the exhaust pressure. The intermediate compression chamber C2 is between the suction pressure and the discharge pressure, and is also referred to as a medium pressure chamber. One side of the movable scroll member 160 is supported by an upper portion of the main bearing housing 140 (which constitutes a thrust member), and one end of the drive shaft 130 is supported by a main bearing 144 provided in the main bearing housing 140. One end of the drive shaft 130 is provided with an eccentric crank pin 132, and the eccentric crank pin 132 and the movement An unloading bushing 142 is disposed between the hub portions 162 of the scroll member 160. By the driving of the motor 120, the orbiting scroll member 160 will rotate normally with respect to the fixed scroll member 150 (i.e., the central axis of the orbiting scroll member 160 is rotated about the central axis of the scroll member 150, but the orbiting scroll member 160 is rotated. It does not rotate itself about its central axis) to achieve fluid compression. The above translational rotation is achieved by the cross slip ring 190 disposed between the fixed scroll member 150 and the movable scroll member 160. The fluid compressed by the fixed scroll member 150 and the orbiting scroll member 160 is discharged to the high pressure side through the exhaust port 152. In order to prevent the fluid on the high pressure side from flowing back to the low pressure side via the exhaust port 152 under certain conditions, a check valve or exhaust valve 170 is provided at the exhaust port 152. In order to achieve fluid compression, an effective seal must be provided between the fixed scroll member 150 and the orbiting scroll member 160. In one aspect, the distal end portion of the scroll blade 156 of the fixed scroll member 150 and the end plate 164 of the orbiting scroll member 160 and the distal end portion of the scroll blade 166 of the orbiting scroll member 160 and the fixed scroll member 150 An axial seal is required between the end plates 154. Typically, a back pressure chamber 158 is provided on the opposite side of the end plate 154 of the fixed scroll member 150 from the scroll vanes 156. A seal assembly 180 is disposed in the back pressure chamber 158, and the axial displacement of the seal assembly 180 is limited by the diaphragm 116. The back pressure chamber 158 is in fluid communication with the intermediate pressure chamber C2 through an axially extending through bore (not shown) formed in the end plate 154 to form a force that urges the fixed scroll member 150 toward the orbiting scroll member 160. Since one side of the orbiting scroll member 160 is supported by the upper portion of the main bearing housing 140, the fixed scroll member 150 and the orbiting scroll member 160 can be effectively pressed together by the pressure in the back pressure chamber 158. When the pressure in each compression chamber exceeds a set value, the resultant force generated by the pressure in these compression chambers will exceed the downward pressure provided in the back pressure chamber 158 to cause the fixed scroll member 150 to move upward. At this time, the fluid in the compression chamber will pass through the gap between the distal end portion of the scroll vane 156 of the fixed scroll member 150 and the end plate 164 of the orbiting scroll member 160 and the scroll vane 166 of the orbiting scroll member 160. The gap between the distal end portion and the end plate 154 of the fixed scroll member 150 leaks to the low pressure side to effect unloading, thereby providing axial flexibility to the scroll compressor. On the other hand, a radial seal is also required between the side surface of the scroll vane 156 of the fixed scroll member 150 and the side surface of the scroll vane 166 of the orbiting scroll member 160. This radial sealing between the two is typically achieved by the centrifugal force of the orbiting scroll member 160 during operation and the driving force provided by the drive shaft 130. Specifically, during operation, by the driving of the motor 120, the orbiting scroll member 160 will rotate in translation with respect to the fixed scroll member 150, so that the orbiting scroll member 160 will generate centrifugal force. On the other hand, the eccentric crank pin 132 of the drive shaft 130 also generates a drive that facilitates radial sealing of the fixed scroll member and the orbiting scroll member during rotation. Force component. The scroll vanes 166 of the orbiting scroll member 160 abut against the scroll vanes 156 of the fixed scroll member 150 by means of the above-described centrifugal force and driving force components, thereby achieving radial sealing therebetween. When incompressible substances (such as solid impurities, lubricating oil, and liquid refrigerant) enter the compression chamber and get caught between the scroll vanes 156 and the swirl vanes 166, the scroll vanes 156 and the scroll vanes 166 can be temporarily radially They are separated from each other to allow foreign matter to pass, thus preventing the scroll blades 156 or 166 from being damaged. This ability to be radially separated provides radial flexibility to the scroll compressor, increasing compressor reliability. However, in a state where the scroll compressor is rotated at a high speed, the scroll blades of the orbiting scroll member or the fixed scroll member may be broken due to excessive centrifugal force and driving force. More specifically, as shown in FIG. 2, during the actual operation of the orbiting scroll member 160, due to the interaction of temperature and gas force, etc., in the most unfavorable case, the distal end portion of the scroll blade 166 (in FIG. 2 The upper end) will interact with the joint between the end plate 154 of the fixed scroll member 160 and the scroll vane 156 to withstand the force f, at which point the proximal end of the scroll vane 166 (lower end in Fig. 2) It will withstand the bending moment M l=f*h, where h is the height of the scroll blade 166 in the axial direction. As the rotational speed of the motor 120 increases, the force f also increases, so the scroll blade 166 may break at the proximal end. 3-8 illustrate an example of a configuration in accordance with an embodiment of the present invention. In the configuration according to this embodiment, only the configuration of the scroll vanes 66 of the orbiting scroll member 60 is improved. The configuration of the fixed scroll member 50 (shown in FIG. 4) is the same as that of the fixed scroll member 150 shown in FIGS. 1-2, that is, the fixed scroll member 50 includes the end plate 54 and is formed on the end plate 54. The spiral wrap vanes 56. First, referring to a perspective view of the orbiting scroll member 60 shown in FIG. 3, the orbiting scroll member 60 according to an embodiment of the present invention includes an end plate 64 and a spiral wrap blade 66 formed on the end plate 64. The orbiting scroll member 60 may also include a hub portion 62 formed on the other side of the end plate 64 to receive the eccentric crank pin 132 and the unloading bushing 142 of the drive shaft 130. The scroll blade 66 includes a proximal end portion 66A proximate the end plate 64 and a distal end portion 66B distal from the end plate 64 in an axial direction (ie, a direction parallel to the axis of rotation of the orbiting scroll member 60). The scroll blade 66 includes an inner end portion 66C near a substantially central position of the end plate and an outer end portion 66D near the outer peripheral side of the end plate in the circumferential direction (more precisely, the extending direction of the spiral of the scroll blade 66) . The scroll blade 66 further includes a radially inner side surface 66E facing the center position of the end plate and a radially outer side surface 66F facing the outer peripheral side of the end plate. In the orbiting scroll member 60 according to the present embodiment, the radially inner side surface 66E and the radially outer side The side faces 66F are formed with protrusions 70 adapted to contact the matching scroll members 56 of the other scroll member, such as the fixed scroll member 50, the positions of the protrusions 70 in the axial direction are designed such that the scrolls The distal end portion 66B of the vane 66 does not contact the scroll vanes 56 of the fixed scroll member 50 during operation of the scroll compressor. Or, in other words, the projection 70 is spaced apart from the distal end portion 66B of the scroll vane 66 by a predetermined distance so that the projection 70 can come into contact with the scroll vane 56 of the fixed scroll member during operation of the scroll reducer . In this case, since the distance between the projection 70 and the end plate 64 is smaller than the distance between the distal end portion 66B and the end plate 64, in the case of the same centrifugal force, due to the force arm (from the contact point to the end plate) The distance is reduced, so that the bending moment at the proximal end portion 66A of the scroll blade 66 can also be reduced, thereby making it possible to reduce the possibility of the vortex blade breaking. In a preferred form, the projection 70 forms a step 80 on the radially inner side 66E and the radially outer side 66F. That is, the projections 70 are formed in the range from the proximal end portion 66A to the step portion 80 on the radially inner side surface 66E and the radially outer side surface 66F. More specifically, the thickness of the scroll blade 66 in the radial direction of the first portion 66-1 of the step portion 80 near the proximal end portion 66A side is larger than the near distal end portion 66B of the scroll blade 66 at the step portion 80. The thickness of the second portion 66-2 of the side is in the radial direction, whereby a step portion 80 is formed between the first portion 66-1 having a larger thickness and the second portion 66-2 having a smaller thickness. For example, for ease of processing and manufacturing, the longitudinal sections of the first portion 66-1 and the second portion 66-2 in a plane parallel to the axial direction are both rectangular, as shown in Figs. 5A and 5B. The thickness T of the step portion 80 in the radial direction may be designed such that the end portion 66B of the scroll blade 66 does not contact the vortex of the fixed scroll member 50 under the action of temperature and gas force during operation of the scroll compressor. Blade 56. For example, the thickness T of the step portion 80 in the radial direction may be between 0.01 mm and 0.1 mm. The seal between the second portion 66-2 of the scroll blade 66 of the orbiting scroll member 60 and the scroll blade 56 of the fixed scroll member 50 can be achieved, for example, by a lubricant therebetween, thus the two scroll blades 56 and The compression chamber between 66 can still effectively maintain a seal. In addition, referring to FIG. 8, the extending range of the step portion 80 (shown by a thick black solid line in FIG. 8) in the circumferential direction of the scroll blade 66 (the direction in which the spiral extends) may be designed as follows. For example, the step portion 80 may be designed in a portion of the scroll blade 66 that is relatively easily broken. The magnitude of the centrifugal force and the force state of the scroll blades can be considered at this time. Those skilled in the art will appreciate that the relatively large portion of the radius of curvature of the spiral of the scroll blade 66 is a relatively easily broken portion. In a preferred form, the step portion 80 can be disposed at least radially in outermost contact of the scroll vanes 66 of the driven scroll member 60 with the scroll vanes 56 of the other scroll member (i.e., the fixed scroll member 50). The point P1 extends inwardly within a range of 360 degrees in the circumferential direction. That is, the step portion 80 The extent in the circumferential direction extends from the outermost contact point P1 to the point P2. When the point O in Fig. 8 is taken as the center of the spiral of the scroll blade 66, for the design of the scroll member which is currently common, the spiral of the scroll blade 66 extends at an angle of approximately 720 degrees, then the point P1 to The angle between points P2 is greater than or equal to 360 degrees. The radial direction of the portion of the scroll blade 66 of the orbiting scroll member 60 where the step portion 80 is not formed (i.e., the portion near the center of the orbiting scroll member 60, or in other words, the portion extending inward from the point P2) The thickness may be designed to be the same as the thickness in the radial direction of the first portion 66-1. That is, the portion of the scroll blade 66 where the step portion 80 is not formed is also formed thicker, thereby making it less likely to be broken.
图 7示出了动涡旋部件 60与定涡旋部件 50之间在运转过程中的相对 位置。 在图 7中, 定涡旋部件 50的位置保持不变, 而动涡旋部件 60按照 图 7中的箭头所示相对于定涡旋部件 50平动转动。在图 7的左上角的图中, 最外侧的压缩腔 C 1处于吸气状态。 在图 7的左下角的图中, 最外侧的压 缩腔 C 1仍然处于吸气状态并且即将闭合。 在图 7的右下角的图中, 最外 侧的压缩腔 C 1 已经闭合。 在图 7的右上角的图中, 开始了下一次循环并 形成新的最外侧的压缩腔 Cl, 而上一次循环中的最外侧的压缩腔 C 1则变 成了本次循环中的中间的压缩腔 C2。从图 7所示的压缩循环可以看出,借 助于上述构造,在涡旋压缩机的运转过程中,不论动涡旋部件 60相对于定 涡旋部件 50运动到任何位置, 在最外侧的压缩腔 C 1的范围内, 动涡旋部 件 60的涡旋叶片 66总是能够通过其上的台阶部 80与定涡旋部件 50的涡 旋叶片 56接触。  Figure 7 shows the relative position between the orbiting scroll member 60 and the fixed scroll member 50 during operation. In Fig. 7, the position of the fixed scroll member 50 remains unchanged, and the orbiting scroll member 60 is rotated relative to the fixed scroll member 50 as indicated by the arrow in Fig. 7. In the upper left corner view of Fig. 7, the outermost compression chamber C 1 is in an inhaled state. In the lower left corner of Fig. 7, the outermost compression chamber C1 is still in the inhalation state and is about to close. In the lower right corner of Fig. 7, the outermost compression chamber C 1 has been closed. In the figure in the upper right corner of Fig. 7, the next cycle is started and a new outermost compression chamber C1 is formed, and the outermost compression chamber C1 in the previous cycle becomes the middle of the current cycle. Compression chamber C2. As can be seen from the compression cycle shown in Fig. 7, with the above configuration, during the operation of the scroll compressor, the movable scroll member 60 is moved to any position with respect to the fixed scroll member 50, and the outermost compression is performed. In the range of the cavity C1, the scroll blades 66 of the orbiting scroll member 60 can always come into contact with the scroll blades 56 of the fixed scroll member 50 through the step portion 80 thereon.
下面参照图 6描述台阶部 80的距端板 64的轴向方向的高度(以下筒 称为台阶部 80的高度)的设计。 在一种优选方式中, 台阶部 80的高度 H 可以在动涡旋部件 60的涡旋叶片 66的轴向方向的高度 h (可以参见图 2 ) 的 40%至 60%之间。 更优选地, 台阶部 80高度 H可以为涡旋叶片 66的 高度 h的大致 50%。如图 6所示, 当台阶部 80的高度为 H=0.5h时并且当 涡旋叶片 66的台阶部 80与定涡旋部件 50的涡旋叶片 56接触而受到的反 作用力为 F时, 则涡旋叶片 66的近端部 66A处的弯矩 M2=F*H=0.5Fh。 由于力 f和 F基本上主要与动涡旋部件 60的离心力(即转速)相关, 因此 排除其他干扰因素之后, 可以认为 f和 F大致相同。 由此, 当将台阶部 80 的高度 H设计成涡旋叶片 66的高度 h的 50%时, 涡旋叶片 66的近端部 66A处的弯矩 M2仅为没有台阶部 80的现有设计的涡旋叶片的近端部处的 弯矩 Ml (参见图 2 )的 50%, 由此根据本发明实施方式的涡旋叶片 66在 同样的高转速工况下, 更不容易破裂。 另一方面, 考虑到涡旋叶片 66的整 体强度以及压缩机的总体工作效率, 台阶部 80的高度 H—般设计为在涡 旋叶片 66的高度 h的 10%至 90%之间。 The design of the height of the step portion 80 from the axial direction of the end plate 64 (hereinafter referred to as the height of the step portion 80) will be described below with reference to FIG. In a preferred manner, the height H of the step portion 80 may be between 40% and 60% of the height h (see Fig. 2) of the scroll vanes 66 of the orbiting scroll member 60 in the axial direction. More preferably, the height H of the step portion 80 may be approximately 50% of the height h of the scroll blade 66. As shown in FIG. 6, when the height of the step portion 80 is H = 0.5 h and when the step portion 80 of the scroll blade 66 comes into contact with the scroll blade 56 of the fixed scroll member 50 and the reaction force is F, The bending moment M2 at the proximal end portion 66A of the scroll blade 66 is F*H = 0.5 Fh. Since the forces f and F are substantially primarily related to the centrifugal force (i.e., rotational speed) of the orbiting scroll member 60, it is considered that f and F are substantially the same after excluding other interference factors. Thus, when the height H of the step portion 80 is designed to be 50% of the height h of the scroll blade 66, the bending moment M2 at the proximal end portion 66A of the scroll blade 66 is only the existing design without the step portion 80. The bending moment M1 (see Fig. 2) at the proximal end portion of the scroll blade is 50%, whereby the scroll blade 66 according to the embodiment of the present invention is less likely to be broken under the same high rotation speed condition. On the other hand, considering the overall strength of the scroll vanes 66 and the overall operating efficiency of the compressor, the height H of the step portion 80 is generally designed to be in the vortex The height of the rotor blade 66 is between 10% and 90%.
上述构造的动涡旋部件 60可以通过例如模铸工艺制造,也可以例如通 t^t现有的动涡旋部件进行铣削来形成该台阶部, 因此根据本发明构造的 动涡旋部件的制作工艺仍然相对简单并且制造成 ^目对较低。 另外, 如上 所述, 采用根据本发明构造的动涡旋部件, 可以有效地降低涡旋叶片近端 部处的弯矩, 从而可以有效地降低涡旋叶片破裂的可能性, 由此提高了涡 旋部件的耐久性。 另一方面, 由于动涡旋部件的涡旋叶片的厚度较小的第 二部分与定涡旋部件的涡旋叶片之间的间隙可以通过润滑剂有效地密封, 所以压缩机的压缩效率也不会降低。  The orbiting scroll member 60 of the above configuration may be manufactured by, for example, a die casting process, or may be formed by milling, for example, by using an existing orbiting scroll member, and thus the production of the orbiting scroll member constructed in accordance with the present invention The process is still relatively simple and the manufacturing is lower. In addition, as described above, with the movable scroll member constructed according to the present invention, the bending moment at the proximal end portion of the scroll blade can be effectively reduced, thereby effectively reducing the possibility of the vortex blade rupture, thereby improving the vortex The durability of the rotating parts. On the other hand, since the gap between the second portion of the scroll blade having a small thickness of the orbiting scroll member and the scroll blade of the fixed scroll member can be effectively sealed by the lubricant, the compression efficiency of the compressor is not Will decrease.
上述已经对本发明的一种实施方式进行了了描述, 但是本领域技术人 员应该理解可以对上述实施方式进行各种变型。  An embodiment of the present invention has been described above, but those skilled in the art will appreciate that various modifications can be made to the above-described embodiments.
例如, 在上述实施方式中, 动涡旋部件 60的涡旋叶片 66的未形成有 台阶部的部分(靠近动涡旋部件中心的部分)的径向方向的厚度设计成与 厚度相对较大的第一部分 66-1的径向方向的厚度相同,但是, 动涡旋部件 60的涡旋叶片 66的未形成有台阶部的部分的径向方向的厚度也可以与厚 度相对较小的第二部分 66-2的径向方向的厚度相同。  For example, in the above embodiment, the thickness of the portion of the scroll blade 66 of the orbiting scroll member 60 where the step portion is not formed (the portion near the center of the movable scroll member) is designed to have a relatively large thickness. The thickness of the first portion 66-1 in the radial direction is the same, but the thickness of the portion of the scroll blade 66 of the orbiting scroll member 60 in which the step portion is not formed may be the thickness of the second portion having a relatively small thickness. The thickness of the 66-2 in the radial direction is the same.
例如,在上述非对称设计的涡旋部件的实施方式中, 台阶部 90至少设 置在从动涡旋部件 60的涡旋叶片 66与另一涡旋部件 50的涡旋叶片 56的 径向最外侧接触点 P1沿周向方向向内延伸 360度的范围内,但是,在图 9 所示的对称设计的涡旋部件中, 台阶部 80可以至少设置在从动涡旋部件 60的涡旋叶片 66的外端部 66D沿周向方向向内延伸 360度的范围内。 在 这种情况下, 动涡旋部件 60的涡旋叶片 66的未形成有所述台阶部的部分 的径向方向的厚度可以设计成与第一部分 66-1的径向方向的厚度相同,或 者可以设计成与第二部分 66-2的径向方向的厚度相同。  For example, in the above-described embodiment of the asymmetrically designed scroll member, the step portion 90 is provided at least at the radially outermost side of the scroll blade 66 of the driven scroll member 60 and the scroll blade 56 of the other scroll member 50. The contact point P1 extends inwardly in the circumferential direction by 360 degrees, but in the symmetrical design of the scroll member shown in FIG. 9, the step portion 80 may be provided at least at the scroll blade 66 of the driven scroll member 60. The outer end portion 66D extends inwardly within a range of 360 degrees in the circumferential direction. In this case, the thickness of the portion of the scroll blade 66 of the movable scroll member 60 in which the step portion is not formed may be designed to have the same thickness as the radial direction of the first portion 66-1, or It may be designed to be the same thickness as the radial direction of the second portion 66-2.
例如, 在另一种变型中, 台阶部 80可以设置在从动涡旋部件 60的涡 旋叶片 66的外端部 66D到内端部 66C的范围内, 如图 10所示。  For example, in another variation, the step portion 80 may be disposed within the range from the outer end portion 66D of the scroll blade 66 of the driven scroll member 60 to the inner end portion 66C, as shown in FIG.
例如, 在上述实施方式中, 形成有台阶部 80的突起部 70形成在涡旋 叶片 66的径向内,面 66 径向外侧面 66F 者上, '但是形成有,阶部 侧面 66F上。  For example, in the above embodiment, the projection 70 formed with the step portion 80 is formed in the radial direction of the scroll blade 66, and the surface 66 is formed on the radially outer side surface 66F, but is formed on the step side surface 66F.
例如, 在上述实施方式中, 形成有台阶部 80的突起部 70形成在动涡 旋部件 60上, 但是形成有台阶部 80的突起部 70也可以形成定涡旋部件 50上, 如图 11所示。 在这种情况下, 定涡旋部件 50可以包括端板 54以 及形成在端板 54上的螺旋状的涡旋叶片 56。 涡旋叶片 56在轴向方向(即 平行于定涡旋部件 50的中心轴线的方向)上包括靠近端板 54的近端部 56A 和远离端板 54的远端部 56B。 涡旋叶片 56在周向方向 (更准确地, 涡旋 叶片 56 的螺旋线的延伸方向)上包括靠近端板的大致中心位置的内端部 56C和靠近端板的外周侧的外端部 56D。涡旋叶片 56还包括面向端板的中 心位置的径向内侧面 56E和面向端板的外周侧的径向外侧面 56F。在图 11 中,径向内侧面 56E和径向外侧面 56F二者上形成有适于与相配的另一涡 旋部件例如动涡旋部件 60的涡旋叶片 66接触的突起部 70。 特别是, 突起 部 70在径向内侧面 56E和径向外侧面 56F上形成台阶部 80。 台阶部 80 的厚度、 高度和周向延伸范围等参数以及其他变型可以参照上述动涡旋部 件 60的构造和变型来确定。 For example, in the above embodiment, the protrusion 70 in which the step portion 80 is formed is formed on the orbiting scroll member 60, but the protrusion portion 70 in which the step portion 80 is formed may also form a fixed scroll member. 50, as shown in Figure 11. In this case, the fixed scroll member 50 may include an end plate 54 and a spiral wrap vane 56 formed on the end plate 54. The scroll vanes 56 include a proximal end portion 56A proximate the end plate 54 and a distal end portion 56B distal from the end plate 54 in an axial direction (ie, a direction parallel to the central axis of the fixed scroll member 50). The scroll blade 56 includes an inner end portion 56C near a substantially central position of the end plate and an outer end portion 56D near the outer peripheral side of the end plate in the circumferential direction (more precisely, the extending direction of the spiral of the scroll blade 56) . The scroll blade 56 further includes a radially inner side surface 56E facing the center position of the end plate and a radially outer side surface 56F facing the outer peripheral side of the end plate. In Fig. 11, both the radially inner side surface 56E and the radially outer side surface 56F are formed with projections 70 adapted to contact the corresponding scroll member of the other scroll member, such as the orbiting scroll member 60. In particular, the projection 70 forms a step portion 80 on the radially inner side surface 56E and the radially outer side surface 56F. Parameters such as the thickness, height, and circumferential extent of the step portion 80, as well as other variations, can be determined with reference to the configuration and variations of the orbiting scroll member 60 described above.
例如, 在上述实施方式中, 突起部 70以台阶部 80的形式来构造, 但 是突起部 70也可以构造成其他形式, 例如突起部 70可以构造成形成在涡 旋叶片 66的径向内侧面 66E和 /或径向外侧面 66F上的隆起部。 在这种情 况下, 该隆起部可以至少设置在从涡旋部件的涡旋叶片与另一涡旋部件的 涡旋叶片的径向最外侧接触点沿周向方向向内延伸 360度的范围内。 该隆 起部的隆起高度可以在 0.01mm至 0.1mm之间。该隆起部的距端板的轴向 方向的高度可以在涡旋部件的涡旋叶片的轴向方向的高度的 10%至 90% 之间。  For example, in the above embodiment, the protrusion 70 is configured in the form of a step portion 80, but the protrusion 70 may be configured in other forms, for example, the protrusion 70 may be configured to be formed on the radially inner side surface 66E of the scroll blade 66. And/or a raised portion on the radially outer side 66F. In this case, the ridge portion may be provided at least in a range extending 360 degrees inward from the radially outermost contact point of the scroll blade of the scroll member and the scroll blade of the other scroll member in the circumferential direction. . The ridge height of the ridge may be between 0.01 mm and 0.1 mm. The height of the ridge portion in the axial direction from the end plate may be between 10% and 90% of the height in the axial direction of the scroll blade of the scroll member.
上述已经对本发明的实施方式和各种变型进行了描述, 现将本发明的 基本构思总结如下:  The embodiments and various modifications of the present invention have been described above, and the basic concepts of the present invention are summarized as follows:
根据本发明的第一方面, 提供了一种用于涡旋压缩机的涡旋部件, 包 括: 端板; 以及形成在所述端板上的螺旋状的涡旋叶片, 所述涡旋叶片在 轴向方向上包括靠近所述端板的近端部和远离所述端板的远端部, 所述涡 旋叶片在周向方向上包括靠近所述端板的大致中心位置的内端部和靠近 所述端板的外周侧的外端部, 并且所述涡旋叶片包括面向所述端板的中心 位置的径向内侧面和面向所述端板的外周侧的径向外侧面, 其中在所述径 向内侧面和所述径向外侧面中的至少一者上可以形成有适于与相配的另 一涡旋部件的涡旋叶片接触的突起部, 所述突出部在轴向方向上的位置设 计成使得所述涡旋叶片的远端部在所述涡旋压缩机运转过程中不会与所 述另一涡旋部件的涡旋叶片接触。  According to a first aspect of the present invention, a scroll member for a scroll compressor is provided, comprising: an end plate; and a spiral wrap blade formed on the end plate, the wrap blade The axial direction includes a proximal end portion adjacent the end plate and a distal end portion remote from the end plate, the scroll blade including an inner end portion in a circumferential direction near a substantially central position of the end plate and An outer end portion on an outer peripheral side of the end plate, and the scroll blade includes a radially inner side surface facing a center position of the end plate and a radially outer side surface facing an outer peripheral side of the end plate, wherein At least one of the radially inner side surface and the radially outer side surface may be formed with a protrusion adapted to contact a corresponding scroll blade of another scroll member, the protrusion being axially oriented The position is such that the distal end of the scroll vane does not contact the scroll vanes of the other scroll member during operation of the scroll compressor.
根据本发明的第二方面, 所述突起部可以构造成在所述径向内侧面和 / 或所述径向外侧面上形成台阶部。 According to a second aspect of the present invention, the protrusion may be configured to be on the radially inner side and/or Or a step portion is formed on the radially outer side surface.
根据本发明的第三方面, 所述涡旋部件的涡旋叶片的位于所述台阶部 的靠近所述近端部一侧的第一部分的径向方向的厚度可以大于所述涡旋 部件的涡旋叶片的位于所述台阶部的靠近所述远端部一侧的第二部分的 径向方向的厚度。  According to a third aspect of the invention, the thickness of the scroll blade of the scroll member in the radial direction of the first portion of the step portion near the proximal end portion may be larger than the vortex of the scroll member The thickness of the spiral blade in the radial direction of the second portion of the step portion near the distal end portion.
根据本发明的第四方面, 所述台阶部可以至少设置在从所述涡旋部件 的涡旋叶片与所述另一涡旋部件的涡旋叶片的径向最外侧接触点沿周向 方向向内延伸 360度的范围内。  According to a fourth aspect of the invention, the step portion may be provided at least in a circumferential direction from a radially outermost contact point of the scroll blade of the scroll member and the scroll blade of the other scroll member The inside extends within a range of 360 degrees.
根据本发明的第五方面, 所述涡旋部件的涡旋叶片的未形成有所述台 阶部的部分的径向方向的厚度可以与所述第一部分的径向方向的厚度相 同。  According to the fifth aspect of the invention, the thickness of the portion of the scroll blade of the scroll member where the step portion is not formed may be the same as the thickness of the first portion in the radial direction.
根据本发明的第六方面, 所述涡旋部件的涡旋叶片的未形成有所述台 阶部的部分的径向方向的厚度可以与所述第二部分的径向方向的厚度相 同。  According to the sixth aspect of the invention, the thickness of the portion of the scroll blade of the scroll member where the step portion is not formed may be the same as the thickness of the second portion in the radial direction.
根据本发明的第七方面, 所述台阶部可以至少设置在从所述涡旋部件 的涡旋叶片的外端部沿周向方向向内延伸 360度的范围内。  According to a seventh aspect of the invention, the step portion may be provided at least in a range extending 360 degrees inward from the outer end portion of the scroll blade of the scroll member in the circumferential direction.
根据本发明的第八方面, 所述涡旋部件的涡旋叶片的未形成有所述台 阶部的部分的径向方向的厚度可以与所述第一部分的径向方向的厚度相 同。  According to the eighth aspect of the invention, the thickness of the portion of the scroll blade of the scroll member where the step portion is not formed may be the same as the thickness of the first portion in the radial direction.
根据本发明的第九方面, 所述涡旋部件的涡旋叶片的未形成有所述台 阶部的部分的径向方向的厚度可以与所述第二部分的径向方向的厚度相 同。  According to the ninth aspect of the invention, the thickness of the portion of the scroll blade of the scroll member where the step portion is not formed may be the same as the thickness of the second portion in the radial direction.
根据本发明的第十方面, 所述台阶部可以设置在从所述涡旋部件的涡 旋叶片的外端部到所述内端部的范围内。  According to a tenth aspect of the invention, the step portion may be provided in a range from an outer end portion of the scroll blade of the scroll member to the inner end portion.
根据本发明的第十一方面, 所述台阶部的径向方向的厚度可以在 According to an eleventh aspect of the present invention, the thickness of the step portion in the radial direction may be
0.01mm至 0.1mm之间。 Between 0.01mm and 0.1mm.
根据本发明的第十二方面, 所述台阶部的距所述端板的轴向方向的高 度可以在所述涡旋部件的涡旋叶片的轴向方向的高度的 10%至 90%之间。  According to a twelfth aspect of the invention, the height of the step portion from the axial direction of the end plate may be between 10% and 90% of the height of the scroll blade in the axial direction of the scroll member .
根据本发明的第十三方面, 所述台阶部的高度可以在所述涡旋部件的 涡旋叶片的高度的 40%至 60%之间。  According to a thirteenth aspect of the invention, the height of the step portion may be between 40% and 60% of the height of the scroll blade of the scroll member.
根据本发明的第十四方面, 所述台阶部的高度可以为所述涡旋部件的 涡旋叶片的高度的 50%。 According to a fourteenth aspect of the invention, the height of the step portion may be the scroll member 50% of the height of the vortex blade.
根据本发明的第十五方面, 所述第一部分和所述第二部分的在平行于 轴向方向的平面上的纵向截面可以均为矩形。  According to a fifteenth aspect of the invention, the longitudinal section of the first portion and the second portion in a plane parallel to the axial direction may be both rectangular.
根据本发明的第十六方面, 可以在所述径向内侧面和所述径向外侧面 二者上均形成有所述突起部。  According to a sixteenth aspect of the invention, the protrusion portion may be formed on both the radially inner side surface and the radially outer side surface.
根据本发明的第十七方面, 所述涡旋部件可以为动涡旋部件, 所述另 一涡旋部件可以为定涡旋部件。  According to a seventeenth aspect of the invention, the scroll member may be a movable scroll member, and the other scroll member may be a fixed scroll member.
根据本发明的第十八方面, 所述涡旋部件为可以定涡旋部件, 所述另 一涡旋部件为可以动涡旋部件。  According to an eighteenth aspect of the invention, the scroll member is a fixed scroll member, and the other scroll member is a movable scroll member.
根据本发明的第十九方面, 所述涡旋部件可以为非对称设计的涡旋部 件。  According to a nineteenth aspect of the invention, the scroll member may be an asymmetrically designed scroll member.
根据本发明的第二十方面,所述涡旋部件可以为对称设计的涡旋部件。 根据本发明的第二十一方面, 所述突起部在所述径向内侧面和 /或所述 径向外侧面上可以形成为隆起部。  According to a twentieth aspect of the invention, the scroll member may be a vortex member of a symmetrical design. According to a twenty first aspect of the invention, the protrusion may be formed as a ridge on the radially inner side surface and/or the radially outer side surface.
根据本发明的第二十二方面, 所述隆起部可以至少设置在从所述涡旋 部件的涡旋叶片与所述另一涡旋部件的涡旋叶片的径向最外侧接触点沿 周向方向向内延伸 360度的范围内。  According to a twenty-second aspect of the invention, the ridge portion may be disposed at least in a circumferential direction from a radially outermost contact point of the scroll blade of the scroll member and the scroll blade of the other scroll member The direction extends inward by 360 degrees.
根据本发明的第二十三方面, 所述隆起部的隆起高度可以在 0.01mm 至 0.1mm之间。  According to a twenty-third aspect of the invention, the ridge height of the ridge portion may be between 0.01 mm and 0.1 mm.
根据本发明的第二十四方面, 所述隆起部的距所述端板的轴向方向的 高度可以在所述涡旋部件的涡旋叶片的轴向方向的高度的 10%至 90%之 间。  According to a twenty-fourth aspect of the invention, the height of the ridge portion from the axial direction of the end plate may be 10% to 90% of the height of the scroll blade in the axial direction of the scroll member. between.
根据本发明的第二十五方面, 提供了一种包括上述涡旋部件的涡旋压 缩机。  According to a twenty-fifth aspect of the invention, there is provided a scroll compressor comprising the above scroll member.
尽管在此已详细描述本发明的各种实施方式, 但是应该理解本发明并 不局限于这里详细描述和示出的具体实施方式, 在不偏离本发明的实质和 范围的情况下可由本领域的技术人员实现其它的变型和变体。 所有这些变 型和变体都落入本发明的范围内。 而且, 所有在此描述的构件都可以由其 他技术性上等同的构件来代替。  Although the various embodiments of the present invention have been described in detail herein, it is understood that the invention is not limited to The skilled person implements other variations and variants. All such variations and modifications are intended to fall within the scope of the invention. Moreover, all of the components described herein can be replaced by other technically equivalent components.

Claims

权 利 要 求 书 claims
1、 一种用于涡旋压缩机的涡旋部件(60, 50), 包括: 1. A scroll component (60, 50) for a scroll compressor, including:
端板(64, 54); 以及 End plates (64, 54); and
形成在所述端板(64, 54)上的螺旋状的涡旋叶片 (66, 56), 所述涡 旋叶片(66, 56)在轴向方向上包括靠近所述端板(64, 54)的近端部(66八, 56A)和远离所述端板(64, 54) 的远端部 (66B, 56B ), 所述涡旋叶片 (66, 56)在周向方向上包括靠近所述端板(64, 54)的大致中心位置的 内端部( 66C, 56C )和靠近所述端板 ( 64, 54 )的外周侧的外端部( 66D, 56D), 并且所述涡旋叶片 (66, 56) 包括面向所述端板(64, 54)的中心 位置的径向内侧面(66E, 56E)和面向所述端板(64, 54)的外周侧的径 向外侧面 (66F, 56F ), 其中在所述径向内侧面 (66E, 56E )和所述径向 外侧面( 66F, 56F )中的至少一者上形成有适于与相配的另一涡旋部件( 50, 60)的涡旋叶片 (56, 66)接触的突起部(70), 所述突出部(70)在轴向 方向上的位置设计成使得所述涡旋叶片 (66, 56)的远端部(66B, 56B ) 在所述涡旋压缩机运转过程中不会与所述另一涡旋部件(50, 60)的涡旋 叶片 (56, 66)接触。 Spiral vortex blades (66, 56) are formed on the end plates (64, 54). The vortex blades (66, 56) include those close to the end plates (64, 54) in the axial direction. ) and the distal end portion (66B, 56B) away from the end plate (64, 54). The scroll blades (66, 56) include those close to the end plate (66, 56) in the circumferential direction. The inner end (66C, 56C) at the substantially central position of the end plate (64, 54) and the outer end (66D, 56D) close to the outer peripheral side of the end plate (64, 54), and the vortex The blades (66, 56) include a radially inner side (66E, 56E) facing the center position of the end plate (64, 54) and a radial outer side (66E, 56E) facing the outer peripheral side of the end plate (64, 54). 66F, 56F), wherein another scroll component (50) adapted to match is formed on at least one of the radially inner side (66E, 56E) and the radial outer side (66F, 56F) , The protrusion (70) in contact with the scroll blades (56, 66) of 60), the position of the protrusion (70) in the axial direction is designed such that the distal end of the scroll blade (66, 56) The portions (66B, 56B) will not come into contact with the scroll blades (56, 66) of the other scroll component (50, 60) during operation of the scroll compressor.
2、如权利要求 1所述的涡旋部件, 其中所述突起部(70)构造成在所 述径向内侧面 (66E, 56E)和 /或所述径向外侧面 (66F, 56F )上形成台 阶部 ( 80 )。 2. The scroll component of claim 1, wherein the protrusion (70) is configured on the radially inner side (66E, 56E) and/or the radially outer side (66F, 56F) Form a step part (80).
3、 如权利要求 2所述的涡旋部件, 其中所述涡旋部件(60, 50)的涡 旋叶片 ( 66, 56 )的位于所述台阶部 ( 80 )的靠近所述近端部( 66A, 56A ) 一侧的第一部分(66-1, 56-1)的径向方向的厚度大于所述涡旋部件(60, 50)的涡旋叶片(66, 56)的位于所述台阶部(80)的靠近所述远端部(66B, 56B)一侧的第二部分 ( 66-2, 56-2)的径向方向的厚度。 3. The scroll component according to claim 2, wherein the scroll blades (66, 56) of the scroll component (60, 50) are located near the proximal end portion (80) of the step portion (80). 66A, 56A) The thickness of the first part (66-1, 56-1) on one side in the radial direction is greater than that of the scroll blade (66, 56) of the scroll component (60, 50) located at the step portion The thickness of the second part (66-2, 56-2) of the (80) near the distal end portion (66B, 56B) in the radial direction.
4、如权利要求 3所述的涡旋部件, 其中所述台阶部( 80 )至少设置在 从所述涡旋部件(60, 50)的涡旋叶片(66, 56)与所述另一涡旋部件(50, 60)的涡旋叶片 (56, 66)的径向最外侧接触点(P1)沿周向方向向内延 伸 360度的范围内。 4. The scroll member according to claim 3, wherein the step portion (80) is provided at least between the scroll blade (66, 56) of the scroll member (60, 50) and the other scroll member. rotating parts (50, The radially outermost contact point (P1) of the scroll blades (56, 66) of 60) extends inward within a range of 360 degrees in the circumferential direction.
5、 如权利要求 4所述的涡旋部件, 其中所述涡旋部件(60, 50)的涡 旋叶片 (66, 56)的未形成有所述台阶部的部分的径向方向的厚度与所述 第一部分(66-1, 56-1)的径向方向的厚度相同。 5. The scroll member according to claim 4, wherein a thickness in the radial direction of the portion of the scroll blade (66, 56) of the scroll member (60, 50) where the step portion is not formed is equal to The thickness of the first part (66-1, 56-1) in the radial direction is the same.
6、 如权利要求 4所述的涡旋部件, 其中所述涡旋部件(60, 50)的涡 旋叶片 (66, 56)的未形成有所述台阶部的部分的径向方向的厚度与所述 第二部分(66-2, 56-2)的径向方向的厚度相同。 6. The scroll member according to claim 4, wherein a thickness in the radial direction of the portion of the scroll blade (66, 56) of the scroll member (60, 50) where the step portion is not formed is equal to The thickness of the second part (66-2, 56-2) in the radial direction is the same.
7、如权利要求 3所述的涡旋部件, 其中所述台阶部( 80 )至少设置在 从所述涡旋部件(60, 50)的涡旋叶片 (66, 56)的外端部( 66D, 56D) 沿周向方向向内延伸 360度的范围内。 7. The scroll component according to claim 3, wherein the step portion (80) is provided at least from an outer end portion (66D) of the scroll blade (66, 56) of the scroll component (60, 50). , 56D) extending inward within a range of 360 degrees along the circumferential direction.
8、 如权利要求 7所述的涡旋部件, 其中所述涡旋部件(60, 50)的涡 旋叶片 (66, 56)的未形成有所述台阶部的部分的径向方向的厚度与所述 第一部分(66-1, 56-1)的径向方向的厚度相同。 8. The scroll member according to claim 7, wherein a thickness in the radial direction of the portion of the scroll blade (66, 56) of the scroll member (60, 50) where the step portion is not formed is equal to The thickness of the first part (66-1, 56-1) in the radial direction is the same.
9、 如权利要求 7所述的涡旋部件, 其中所述涡旋部件(60, 50)的涡 旋叶片 (66, 56)的未形成有所述台阶部的部分的径向方向的厚度与所述 第二部分(66-2, 56-2)的径向方向的厚度相同。 9. The scroll member according to claim 7, wherein a thickness in the radial direction of the portion of the scroll blade (66, 56) of the scroll member (60, 50) where the step portion is not formed is equal to The thickness of the second part (66-2, 56-2) in the radial direction is the same.
10、 如权利要求 3所述的涡旋部件, 其中所述台阶部(80)设置在从 所述涡旋部件( 60, 50 )的涡旋叶片 ( 66, 56 )的所述外端部( 66D, 56D ) 到所述内端部(66C, 56C)的范围内。 10. The scroll component according to claim 3, wherein the step portion (80) is provided from the outer end (66, 56) of the scroll blade (66, 56) of the scroll component (60, 50) 66D, 56D) to the inner end (66C, 56C).
11、 如权利要求 3所述的涡旋部件, 其中所述台阶部 (80) 的径向方 向的厚度 (T)在 0.01mm至 0.1mm之间。 11. The scroll component according to claim 3, wherein the thickness (T) of the step portion (80) in the radial direction is between 0.01 mm and 0.1 mm.
12、 如权利要求 3所述的涡旋部件, 其中所述台阶部 (80)的距所述 端板(64, 54) 的轴向方向的高度 (H)在所述涡旋部件(60, 50) 的涡 旋叶片 (66, 56)的轴向方向的高度 (h) 的 10%至 90%之间。 12. The scroll component according to claim 3, wherein the height (H) of the step portion (80) from the end plate (64, 54) in the axial direction is within the range of the scroll component (60, 54). 50) The height (h) of the scroll blades (66, 56) in the axial direction is between 10% and 90%.
13、如权利要求 12所述的涡旋部件,其中所述台阶部( 80 )的高度( H ) 在所述涡旋部件(60, 50)的涡旋叶片 (66, 56)的高度(h)的 40%至 60%之间。 13. The scroll component according to claim 12, wherein the height (H) of the step portion (80) is equal to the height (h) of the scroll blades (66, 56) of the scroll component (60, 50). ) between 40% and 60%.
14、如权利要求 13所述的涡旋部件,其中所述台阶部( 80 )的高度( H ) 为所述涡旋部件(60, 50)的涡旋叶片 (66, 56)的高度(h)的 50%。 14. The scroll component according to claim 13, wherein the height (H) of the step portion (80) is the height (h) of the scroll blades (66, 56) of the scroll component (60, 50). ) 50%.
15、 如权利要求 3所述的涡旋部件, 其中所述第一部分(66-1, 56-1) 和所述第二部分(66-2, 56-2) 的在平行于轴向方向的平面上的纵向截面 均为矩形。 15. The scroll member according to claim 3, wherein the first part (66-1, 56-1) and the second part (66-2, 56-2) are parallel to the axial direction. The longitudinal sections on the plane are all rectangular.
16、如权利要求 1-15中任一项所述的涡旋部件, 其中在所述径向内侧 面 (66E, 56E)和所述径向外侧面 (66F, 56F )二者上均形成有所述突 起部 ( 70 )。 16. The scroll member according to any one of claims 1 to 15, wherein a scroll element is formed on both the radially inner side (66E, 56E) and the radially outer side (66F, 56F). The protrusion (70).
17、如权利要求 16所述的涡旋部件,其中所述涡旋部件为动涡旋部件 (60), 所述另一涡旋部件为定涡旋部件(50)。 17. The scroll component of claim 16, wherein the scroll component is an orbiting scroll component (60) and the other scroll component is a fixed scroll component (50).
18、如权利要求 16所述的涡旋部件,其中所述涡旋部件为定涡旋部件 (50), 所述另一涡旋部件为动涡旋部件(60)。 18. The scroll component of claim 16, wherein the scroll component is a fixed scroll component (50) and the other scroll component is an orbiting scroll component (60).
19、 如权利要求 16所述的涡旋部件, 其中所述涡旋部件(60, 50)为 非对称设计的涡旋部件。 19. The scroll component according to claim 16, wherein the scroll component (60, 50) is an asymmetrically designed scroll component.
20、 如权利要求 16所述的涡旋部件, 其中所述涡旋部件(60, 50)为 对称设计的涡旋部件。 20. The scroll component according to claim 16, wherein the scroll component (60, 50) is a symmetrically designed scroll component.
21、 如权利要求 1所述的涡旋部件, 其中所述突起部 ( 70 )在所述径 向内侧面 (66E, 56E )和 /或所述径向外侧面 (66F, 56F )上形成为隆起 部。 21. The scroll member according to claim 1, wherein the protrusion (70) is formed on the radially inner side (66E, 56E) and/or the radial outer side (66F, 56F). The bulge.
22、如权利要求 21所述的涡旋部件,其中所述隆起部至少设置在从所 述涡旋部件的涡旋叶片与所述另一涡旋部件的涡旋叶片的径向最外侧接 触点沿周向方向向内延伸 360度的范围内。 22. The scroll member according to claim 21, wherein the ridge is provided at least at a radially outermost contact point from a scroll vane of the scroll member to a scroll vane of the other scroll member. Extending 360 degrees inward along the circumferential direction.
23、 如权利要求 21 所述的涡旋部件, 其中所述隆起部的隆起高度在23. The scroll member according to claim 21, wherein the ridge height of the ridge is between
0.01mm至 0.1mm之间。 Between 0.01mm and 0.1mm.
24、 如权利要求 21-23中任一项所述的涡旋部件, 其中所述隆起部的 距所述端板的轴向方向的高度在所述涡旋部件的涡旋叶片的轴向方向的 高度的 10%至 90%之间。 24. The scroll component according to any one of claims 21 to 23, wherein the axial height of the ridge from the end plate is in the axial direction of the scroll blades of the scroll component. between 10% and 90% of the height.
25、一种涡旋压缩机,包括如权利要求 1-24中任一项所述的涡旋部件。 25. A scroll compressor comprising the scroll component according to any one of claims 1-24.
PCT/CN2013/090720 2013-03-04 2013-12-27 Scroll component and scroll compressor WO2014134961A1 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
CN201320097796.8 2013-03-04
CN 201320097796 CN203114634U (en) 2013-03-04 2013-03-04 scroll component and scroll compressor
CN201310068431.7 2013-03-04
CN201310068431.7A CN104033386B (en) 2013-03-04 2013-03-04 scroll component and scroll compressor

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Cited By (2)

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Publication number Priority date Publication date Assignee Title
EP3633198A1 (en) * 2016-04-26 2020-04-08 LG Electronics Inc. Scroll compressor
US11209001B2 (en) 2016-04-26 2021-12-28 Lg Electronics Inc. Scroll compressor having wrap with reinforcing portion

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JPS5958791U (en) * 1982-10-09 1984-04-17 サンデン株式会社 scroll compressor
JPH1089268A (en) * 1996-09-19 1998-04-07 Hitachi Ltd Scroll-type fluid machine
JP2001329974A (en) * 2000-05-19 2001-11-30 Fujitsu General Ltd Scroll compressor
CN203114634U (en) * 2013-03-04 2013-08-07 艾默生环境优化技术(苏州)有限公司 scroll component and scroll compressor

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Publication number Priority date Publication date Assignee Title
JPS5958791U (en) * 1982-10-09 1984-04-17 サンデン株式会社 scroll compressor
JPH1089268A (en) * 1996-09-19 1998-04-07 Hitachi Ltd Scroll-type fluid machine
JP2001329974A (en) * 2000-05-19 2001-11-30 Fujitsu General Ltd Scroll compressor
CN203114634U (en) * 2013-03-04 2013-08-07 艾默生环境优化技术(苏州)有限公司 scroll component and scroll compressor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3633198A1 (en) * 2016-04-26 2020-04-08 LG Electronics Inc. Scroll compressor
US10648470B2 (en) 2016-04-26 2020-05-12 Lg Electronics Inc. Scroll compressor having wrap with an offset portion
US11209001B2 (en) 2016-04-26 2021-12-28 Lg Electronics Inc. Scroll compressor having wrap with reinforcing portion
US11408423B2 (en) 2016-04-26 2022-08-09 Lg Electronics Inc. Scroll compressor

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