WO2016169349A1 - Scroll compressor and driving shaft and unloading bush for scroll compressor - Google Patents

Scroll compressor and driving shaft and unloading bush for scroll compressor Download PDF

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Publication number
WO2016169349A1
WO2016169349A1 PCT/CN2016/075986 CN2016075986W WO2016169349A1 WO 2016169349 A1 WO2016169349 A1 WO 2016169349A1 CN 2016075986 W CN2016075986 W CN 2016075986W WO 2016169349 A1 WO2016169349 A1 WO 2016169349A1
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WO
WIPO (PCT)
Prior art keywords
crank pin
eccentric crank
scroll compressor
unloading
unloading bushing
Prior art date
Application number
PCT/CN2016/075986
Other languages
French (fr)
Chinese (zh)
Inventor
周光勇
束宏飞
李庆伟
王石
过炜华
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 CN201520251170.7U external-priority patent/CN204591668U/en
Priority claimed from CN201510196948.3A external-priority patent/CN106151029A/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
Priority to EP16782497.8A priority Critical patent/EP3287638A4/en
Priority to KR1020177033288A priority patent/KR20170138506A/en
Priority to JP2018506467A priority patent/JP2018517097A/en
Publication of WO2016169349A1 publication Critical patent/WO2016169349A1/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
    • 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
    • F04C18/0215Rotary-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
    • F04C18/0223Rotary-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 with symmetrical double 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
    • F04C28/00Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
    • F04C28/18Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids characterised by varying the volume of the working chamber
    • F04C28/22Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids characterised by varying the volume of the working chamber by changing the eccentricity between cooperating members
    • 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
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • 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
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/0042Driving elements, brakes, couplings, transmissions specially adapted for 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
    • F04C2230/00Manufacture
    • F04C2230/40Heat treatment
    • F04C2230/41Hardening; Annealing
    • 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
    • F04C2270/00Control; Monitoring or safety arrangements
    • F04C2270/16Wear
    • F04C2270/165Controlled or regulated

Definitions

  • the present invention relates to a scroll compressor and a drive shaft and an unloading bushing for a scroll compressor.
  • a scroll compressor typically has a compression mechanism that compresses a working fluid (eg, a refrigerant) including a fixed scroll component and an orbiting scroll component.
  • the compression mechanism is driven by an eccentric crank pin of the drive shaft.
  • An unloading bushing is disposed between the eccentric crank pin and the compression mechanism.
  • the unloading bushing is configured to be drivable by the eccentric crank pin and to be relatively displaceable relative to the eccentric crank pin, whereby radial flexibility between the fixed scroll member and the blades of the orbiting scroll member can be achieved.
  • Another object of the present invention is to provide a scroll compressor having a long service life.
  • Another object of the present invention is to provide a wear resistant unloading bushing.
  • Another object of the present invention is to provide a drive shaft having a wear resistant eccentric crank pin.
  • a scroll compressor comprising: a compression mechanism configured to compress a working fluid; and a drive shaft configured to drive the compression mechanism.
  • the drive shaft includes an eccentric crank pin with an unloading bushing disposed between the compression mechanism and the eccentric crank pin such that the eccentric crank pin drives the compression mechanism via the unloading bushing to achieve radial flexibility of the compression mechanism.
  • the eccentric crank pin includes an eccentric crank pin engagement portion that contacts and is displaced relative to the unloading bushing, the unloading bushing including an unloading bushing mating portion that contacts and is displaced relative to the eccentric crank pin.
  • a wear layer is disposed on at least a portion of at least one of the eccentric crank pin engagement portion and the unloading bushing engagement portion.
  • the eccentric crank pin includes a drive face extending parallel to the axis of rotation of the drive shaft, the eccentric crank pin mating portion including at least a portion of the drive face.
  • a wear resistant layer is provided on at least a portion located substantially at the center of the driving surface and convex outward.
  • the unloading bushing may include a bore capable of receiving an eccentric crank pin having a driven face that cooperates with a drive face of the eccentric crank pin, the unloading bushing mating portion including at least a portion of the driven face.
  • a wear resistant layer is provided on at least a portion of the substantially central portion of the driven surface.
  • the wear resistant layer is a hardened layer having a surface hardness in the range of 1500 HV to 3000 HV.
  • the thickness of the wear resistant layer is in the range of from 0.1 micron to 4.5 microns.
  • the wear resistant layer is formed by one of the following methods: physical vapor deposition, chemical vapor deposition, plasma vapor deposition, electroplating, electroless plating, carburizing, nitriding, carbonitriding, shot peening, and surface hardening heat treatment.
  • the wear resistant layer is formed from one of the following materials: a metal layer, a diamond-like, a carbide, a nitride, a silicide, a boride, and an oxide.
  • the wear resistant layer is formed from chromium nitride.
  • a drive shaft for a scroll compressor wherein the drive shaft includes an eccentric crank pin disposed at one end thereof for driving a compression mechanism of the scroll compressor, the eccentric crank The pin includes a drive surface that extends parallel to the axis of rotation of the drive shaft.
  • a wear layer is disposed on at least a portion of the driving surface substantially convex and outwardly, and the wear layer is formed by physical vapor deposition, chemical vapor deposition, plasma vapor deposition, electroplating, electroless plating, carburizing, nitriding, A hardened layer comprising a metal layer, a diamond-like layer, a carbide, a nitride, a silicide, a boride or an oxide formed by carbonitriding, shot peening or surface hardening heat treatment.
  • an unloading bushing for a scroll compressor wherein the unloading bushing includes a hole having a substantially D shape having a driving surface with an eccentric crank pin of a scroll compressor
  • the driven surface of the fit At least in the substantially central portion of the driven surface is provided with a wear-resistant layer by physical vapor deposition, chemical vapor deposition, plasma vapor deposition, electroplating, electroless plating, carburizing, nitriding, carbonitriding
  • a hardened layer comprising a metal layer, a diamond-like layer, a carbide, a nitride, a silicide, a boride or an oxide formed by shot peening or surface hardening heat treatment.
  • Figure 1 is a longitudinal sectional view of a scroll compressor
  • Figure 2 is a schematic view showing the assembly of the eccentric crank pin and the unloading bushing of the drive shaft of the scroll compressor of Figure 1;
  • Figure 3 is a perspective view showing the eccentric crank pin of the drive shaft of Figure 2;
  • Figure 4 shows a perspective view of the unloading bushing of Figure 2;
  • FIG. 5 schematically illustrates a method of forming an abrasion resistant layer in accordance with a first embodiment of the present invention
  • Figure 6 is a schematic illustration of a wear resistant layer.
  • FIG. 1 shows a high pressure side compressor
  • the high pressure side compressor of FIG. 1 is for illustrative purposes only and is not limiting of the invention.
  • the invention may be adapted to any type of compressor, including low pressure side compressors, vertical compressors, horizontal compressors, and the like.
  • a scroll compressor 100 (hereinafter sometimes referred to as a compressor) generally includes a housing 110, a top cover 112 disposed at one end of the housing 110, and a bottom cover 114 disposed at the other end of the housing 110. .
  • a motor 20 composed of a stator 122 and a rotor 124 is disposed in the housing 110.
  • a drive shaft 30 is provided in the rotor 124 to drive the compression mechanism 10 constituted by 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 whose volume gradually decreases from the radially outer side to the radially inner side are formed between the spiral vanes 156 of the fixed scroll member 150 and the spiral vanes 166 of the orbiting scroll member 160.
  • the radially outermost compression chamber is at the suction pressure
  • the radially innermost compression chamber is at the exhaust pressure.
  • the intermediate compression chamber is between the suction pressure and the discharge pressure, and is also referred to as the 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 surface), and a portion of the drive shaft 30 is supported by a main bearing provided in the main bearing housing 140.
  • One end of the drive shaft 30 is provided with an eccentric crank pin 32, and an unloading bushing 42 is disposed between the eccentric crank pin 32 and the hub portion 162 of the movable scroll member 160.
  • a lubricant is stored at the bottom of the compressor housing. Accordingly, a passage extending substantially in the axial direction thereof is formed in the drive shaft 30, that is, a center hole 136 formed at the lower end of the drive shaft 30 and an eccentric hole 134 extending upward from the center hole 136 to the end surface of the eccentric crank pin 32. The end of the central bore 136 is submerged in the lubricant at the bottom of the compressor housing or otherwise supplied with a lubricant.
  • one end of the center hole 136 is supplied with lubricant by the lubricant supply means, and the lubricant entering the center hole 136 is pumped or plucked to the eccentric hole by the centrifugal force during the rotation of the drive shaft 30.
  • the 134 and the upward flow along the eccentric hole 134 continue until reaching the end surface of the eccentric crank pin 32.
  • Lubricant discharged from the end face of the eccentric crank pin 32 along the gap between the unloading bushing 42 and the eccentric crank pin 32 and the unloading bushing The gap between the 42 and the hub 162 flows downward into the recess of the main bearing housing 140.
  • the translation is rotated to extend over the thrust surface of the orbiting scroll member 160 and the main bearing housing 140.
  • the lubricant supplied to the various moving parts in the compressor is scooped and splashed to form droplets or mist.
  • a radial seal is also required between the side surface of the spiral blade 156 of the fixed scroll member 150 and the side surface of the spiral blade 166 of the movable scroll member 160.
  • This radial sealing between the two is typically achieved by means of the relative displacement between the eccentric crank pin 32 and the unloading bushing 42.
  • the eccentric crank pin 32 of the drive shaft 30 also generates a driving force component that contributes to the radial sealing of the fixed scroll member 150 and the movable scroll member 160 during the rotation.
  • the helical vanes 166 of the orbiting scroll member 160 will abut against the helical vanes 156 of the fixed scroll member 150 by means of the above-described centrifugal and driving force components, thereby achieving a radial seal therebetween.
  • an incompressible substance such as solid impurities, lubricating oil, and liquid refrigerant enters the compression chamber and is caught between the spiral blade 156 and the spiral blade 166, the spiral blade 156 and the spiral blade 166 can be temporarily separated from each other in the radial direction to allow The foreign matter passes, that is, a relative displacement is generated between the eccentric crank pin 32 and the unloading bushing 42, thus preventing the spiral blade 156 or 166 from being damaged.
  • This ability to be radially separated provides radial flexibility to the scroll compressor, increasing compressor reliability.
  • the wear-resistant layer of the eccentric crank pin 32 and/or the unloading bushing 42 is coated with a wear-resistant layer to improve its hardness and wear resistance.
  • FIG. 3 a perspective view of the eccentric crank pin of the drive shaft is shown.
  • Drive shaft One end of 30 includes an eccentric crank pin 32.
  • An eccentric hole 134 is formed in the drive shaft 30 in a first direction (longitudinal direction) substantially parallel to the rotational axis of the drive shaft 30 to supply lubricant to the end of the eccentric crank pin 32.
  • the eccentric crank pin 32 of the drive shaft 30 is fitted into the hub portion 162 of the orbiting scroll member 160 via the unloading bushing 42, as shown in FIG.
  • the eccentric crank pin 32 includes a drive surface 321 that extends parallel to the axis of rotation of the drive shaft 30.
  • the generally D-shaped aperture of the unloading bushing 42 through which the eccentric crank pin 32 passes includes a driven surface 143 that is engageable with the drive surface 321 of the eccentric crank pin 32.
  • FIG 2 it shows an assembled view of the unloading bushing and the eccentric crank pin.
  • the eccentric crank pin 32 When the unloading bushing 42 is mounted to the eccentric crank pin 32, the eccentric crank pin 32 is received in the D-shaped hole of the unloading bushing 42 while the driving surface 321 of the eccentric crank pin 32 and the driven surface of the unloading bushing 42 143 fit.
  • the eccentric crank pin 32 when the eccentric crank pin 32 rotates, since the driving surface 321 of the eccentric crank pin 32 is engaged with the driven surface 143 of the unloading bush 42, the eccentric crank pin 32 can drive the unloading bush 42 to rotate.
  • the width of the driving surface 321 of the eccentric crank pin 32 (that is, the dimension perpendicular to the axial direction of the drive shaft) is smaller than the width of the driven surface 143 of the unloading bush 42 (that is, the dimension perpendicular to the axial direction of the drive shaft). .
  • the driving surface 321 of the eccentric crank pin 32 can move relative to the driven surface 143 of the unloading bushing 42.
  • the spiral vanes of the fixed scroll and the orbiting scroll can be tightly fitted when the compressor is running. Together. At this time, the distance between the center of the unloading bushing and the center of the drive shaft is the largest and substantially constant.
  • the inventors have found that the center-to-center distance of the fixed scroll member and the orbiting scroll member is not uniform due to manufacturing and installation errors, and therefore, after the compressor is operated for a period of time, an unloading bushing and an eccentric crank pin are generated.
  • the relative displacement (which corresponds to manufacturing and mounting errors), in particular, the flatness of the unloading bushing.
  • the inventors have also found that, under actual operating conditions, when encountering impurities or liquid refrigerant entering, the center of the movable scroll member can be toward the center of the drive shaft due to relative movement of the unloading bushing relative to the eccentric crank pin. Offset, so the spiral vanes of the fixed scroll and the orbiting scroll are temporarily separated to prevent damage.
  • both the driven surface 143 of the unloading bushing 42 and the driving surface 321 of the eccentric crank pin 32 are subjected to normal loads, and there is relative movement between the two driven faces 143, 321 . Therefore, the driven surface 143 of the unloading bushing 42 and the driving surface 321 of the eccentric crank pin 32 are severely worn, thereby shortening the service life thereof and affecting the working efficiency of the compressor.
  • a wear-resistant layer (which may also be referred to as a "hardened coating” or a “hardened film”) may be provided on the driven surface 143 of the unloading bushing 42 and/or the driving surface 321 of the eccentric crank pin 32. 50 to improve its wear resistance.
  • the substrate S to be coated (for example, the driven surface 143 of the unloading bushing 42 herein and/or the driving surface 321 of the eccentric crank pin 32) is housed in the chamber and Ground it or connect it to the negative supply while the target T (eg, a chromium target) is also housed in the chamber and connected to the positive supply.
  • the chamber was evacuated while filling with nitrogen.
  • the target material is ionized by nitrogen under the action of an arc generated by a low voltage and a large current, and is accelerated by the electric field to strike the workpiece to form a chromium nitride film layer attached to the surface of the substrate.
  • the above process is merely an example of physical vapor deposition and is not intended to limit the invention.
  • the wear layer 50 of the present invention can be formed by other processes known in the art, for example, chemical vapor deposition, plasma vapor deposition, electroplating, electroless plating, carburizing, nitriding, carbonitriding, shot peening , surface quenching heat treatment, etc.
  • the wear layer 50 may be formed of a metal layer, a diamond-like layer, a carbide, a nitride, a silicide, a boride or an oxide, etc. according to various processes.
  • the wear layer 50 may be formed of chromium nitride.
  • the eccentric crank pin 32 and/or the unloading bushing 42 may be made of a powder metallurgy material having a surface hardness in the range of approximately 600 HV to 800 HV.
  • the process according to FIGS. 5 and 6 is on the eccentric crank pin 32 and/or the unloading bushing 42 (eg, on the drive face 321 of the eccentric crank pin 32 and/or the driven face 143 of the unloading bushing 42
  • the surface hardness of the chromium nitride wear resistant layer 50 may range from 1500 HV to 3000 HV, optionally ranging from 1700 HV to 2700 HV.
  • the surface hardness of the driving surface of the eccentric crank pin 32 and/or the driven surface of the unloading bushing 42 can be remarkably improved, and the wear resistance can be greatly enhanced.
  • the thickness of the wear layer 50 can range from 0.1 microns to 4.5 microns.
  • the wear layer 50 can prevent the eccentric crank pin 32 and the unloading bushing after the wear layer 50 is applied to the driving surface of the eccentric crank pin 32 and/or the driven surface of the unloading bushing 42.
  • the powder metallurgy material of 42 is in direct contact, thereby preventing the powder metallurgy material from falling off.
  • the wear layer 50 greatly enhances the wear resistance of the eccentric crank pin 32 and/or the unloading bushing 42.
  • the driving surface 321 of the eccentric crank pin 32 may have a slightly convex portion substantially at the center.
  • the wear layer 50 may be provided only on a slightly convex portion at substantially the center of the driving surface 321 or substantially at the center of the driven surface 143. Alternatively, it may be provided on the entire driving surface 321 and/or the driven surface 143.
  • the wear-resistant layer may also be applied to other portions of the eccentric crank pin 32 and/or the unloading bushing 42 that are subject to wear.
  • contour and/or the position of the wear layer 50 may be shaped as desired.

Abstract

A scroll compressor comprises a compressing mechanism (10) for compressing working fluid and a driving shaft (30) for driving the compressing mechanism (10). The driving shaft (30) comprises an eccentric crank pin (32). An unloading bush (42) is arranged between the compressing mechanism (10) and the eccentric crank pin (32), so that the eccentric crank pin (32) drives the compressing mechanism (10) via the unloading bush (42) to realize radial flexibility of the compressing mechanism (10). The eccentric crank pin (32) comprises an eccentric crank pin matching part which is in contact with the unloading bush (42) and relatively displaces. The unloading bush (42) comprises an unloading bush matching part which is in contact with the eccentric crank pin (32) and relatively displaces. A wear resisting layer (50) is arranged on at least one part of at least one of the eccentric crank pin matching part and the unloading bush matching part. An unloading bush provided with a wear resisting layer for a scroll compressor and a driving shaft with an eccentric crank pin provided with the wear resisting layer. Because of the arrangement of the wear resisting layer, the service life of the scroll compressor is prolonged.

Description

涡旋压缩机以及用于涡旋压缩机的驱动轴和卸载衬套Scroll compressor and drive shaft and unloading bushing for scroll compressor
本申请要求于2015年4月23日提交中国专利局、申请号分别为201510196948.3和201520251170.7的中国专利申请的优先权,其全部内容通过引用结合在本申请中。The present application claims the priority of the Chinese Patent Application, filed on Apr. 23, 2015, the disclosure of which is hereby incorporated by reference.
技术领域Technical field
本发明涉及一种涡旋压缩机以及用于涡旋压缩机的驱动轴和卸载衬套。The present invention relates to a scroll compressor and a drive shaft and an unloading bushing for a scroll compressor.
背景技术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。The content of this section merely provides background information related to the present disclosure, which may not constitute prior art.
涡旋压缩机通常具有包括定涡旋部件和动涡旋部件的对工作流体(例如,制冷剂)进行压缩的压缩机构。该压缩机构由驱动轴的偏心曲柄销来驱动。在偏心曲柄销与压缩机构之间设置有卸载衬套。卸载衬套设置成可以由偏心曲柄销驱动且能够相对于偏心曲柄销发生相对位移,由此可以实现定涡旋部件和动涡旋部件的叶片之间的径向柔性。A scroll compressor typically has a compression mechanism that compresses a working fluid (eg, a refrigerant) including a fixed scroll component and an orbiting scroll component. The compression mechanism is driven by an eccentric crank pin of the drive shaft. An unloading bushing is disposed between the eccentric crank pin and the compression mechanism. The unloading bushing is configured to be drivable by the eccentric crank pin and to be relatively displaceable relative to the eccentric crank pin, whereby radial flexibility between the fixed scroll member and the blades of the orbiting scroll member can be achieved.
然而,卸载衬套与偏心曲柄销之间的相对移动使得它们的接触面会被快速磨损,由此影响了压缩机径向柔性的性能且缩短了卸载衬套与偏心曲柄销的使用寿命。However, the relative movement between the unloading bushing and the eccentric crank pin causes their contact faces to wear rapidly, thereby affecting the radial flexibility of the compressor and shortening the service life of the unloading bushing and the eccentric crank pin.
因此,需要一种用于涡旋压缩机中的耐磨的卸载衬套与偏心曲柄销。Therefore, there is a need for a wear resistant unloading bushing and eccentric crank pin for use in a scroll compressor.
发明内容Summary of the invention
本发明的一个目的在于提供一种具有耐磨卸载衬套和/或偏心曲柄销的涡旋压缩机。It is an object of the present invention to provide a scroll compressor having a wear resistant unloading bushing and/or an eccentric crank pin.
本发明的另一个目的在于提供一种使用寿命长的涡旋压缩机。Another object of the present invention is to provide a scroll compressor having a long service life.
本发明的另一个目的在于提供一种耐磨的卸载衬套。 Another object of the present invention is to provide a wear resistant unloading bushing.
本发明的另一个目的在于提供一种具有耐磨的偏心曲柄销的驱动轴。Another object of the present invention is to provide a drive shaft having a wear resistant eccentric crank pin.
根据本发明的一个方面,提供了一种涡旋压缩机,包括:构造成对工作流体进行压缩的压缩机构以及构造成能够驱动压缩机构的驱动轴。驱动轴包括偏心曲柄销,在压缩机构与偏心曲柄销之间设置有卸载衬套,使得偏心曲柄销经由卸载衬套驱动压缩机构以实现压缩机构的径向柔性。偏心曲柄销包括与卸载衬套接触并相对位移的偏心曲柄销配合部,卸载衬套包括与偏心曲柄销接触并相对位移的卸载衬套配合部。偏心曲柄销配合部与卸载衬套配合部中的至少一者的至少一部分上设置有耐磨层。According to an aspect of the invention, a scroll compressor is provided, comprising: a compression mechanism configured to compress a working fluid; and a drive shaft configured to drive the compression mechanism. The drive shaft includes an eccentric crank pin with an unloading bushing disposed between the compression mechanism and the eccentric crank pin such that the eccentric crank pin drives the compression mechanism via the unloading bushing to achieve radial flexibility of the compression mechanism. The eccentric crank pin includes an eccentric crank pin engagement portion that contacts and is displaced relative to the unloading bushing, the unloading bushing including an unloading bushing mating portion that contacts and is displaced relative to the eccentric crank pin. A wear layer is disposed on at least a portion of at least one of the eccentric crank pin engagement portion and the unloading bushing engagement portion.
在上述涡旋压缩机中,由于偏心曲柄销或卸载衬套的配合部上设置有耐磨层,因此提高了偏心曲柄销或卸载衬套的耐磨性,延长了偏心曲柄销或卸载衬套的使用寿命。其结果是,具有该偏心曲柄销和卸载衬套的涡旋压缩机的使用寿命得以延长。In the above scroll compressor, since the wear portion is provided on the fitting portion of the eccentric crank pin or the unloading bush, the wear resistance of the eccentric crank pin or the unload bush bush is improved, and the eccentric crank pin or the unload bush bush is extended. The service life. As a result, the life of the scroll compressor having the eccentric crank pin and the unloading bush is prolonged.
优选地,偏心曲柄销包括平行于驱动轴的旋转轴线延伸的驱动面,偏心曲柄销配合部包括驱动面的至少一部分。Preferably, the eccentric crank pin includes a drive face extending parallel to the axis of rotation of the drive shaft, the eccentric crank pin mating portion including at least a portion of the drive face.
优选地,至少在位于驱动面的大致中央处且向外凸出的部分上设置有耐磨层。Preferably, a wear resistant layer is provided on at least a portion located substantially at the center of the driving surface and convex outward.
优选地,卸载衬套可以包括能够容纳偏心曲柄销的孔,孔具有与偏心曲柄销的驱动面配合的从动面,卸载衬套配合部包括从动面的至少一部分。Preferably, the unloading bushing may include a bore capable of receiving an eccentric crank pin having a driven face that cooperates with a drive face of the eccentric crank pin, the unloading bushing mating portion including at least a portion of the driven face.
优选地,至少在从动面的大致中央的部分上设置有耐磨层。Preferably, a wear resistant layer is provided on at least a portion of the substantially central portion of the driven surface.
优选地,耐磨层为表面硬度在1500HV至3000HV的范围内的硬化层。Preferably, the wear resistant layer is a hardened layer having a surface hardness in the range of 1500 HV to 3000 HV.
优选地,耐磨层的厚度在0.1微米至4.5微米的范围内。Preferably, the thickness of the wear resistant layer is in the range of from 0.1 micron to 4.5 microns.
优选地,耐磨层通过下列方法之一形成:物理气相沉积、化学气相沉积、等离子体气相沉积、电镀、化学镀、渗碳、渗氮、碳氮共渗、喷丸以及表面淬火热处理。Preferably, the wear resistant layer is formed by one of the following methods: physical vapor deposition, chemical vapor deposition, plasma vapor deposition, electroplating, electroless plating, carburizing, nitriding, carbonitriding, shot peening, and surface hardening heat treatment.
优选地,耐磨层由下列材料之一形成:金属层、类金刚石、碳化物、氮化物、硅化物、硼化物以及氧化物。可选地,耐磨层由氮化铬形成。 Preferably, the wear resistant layer is formed from one of the following materials: a metal layer, a diamond-like, a carbide, a nitride, a silicide, a boride, and an oxide. Optionally, the wear resistant layer is formed from chromium nitride.
根据本发明的另一个方面,还涉及一种用于涡旋压缩机的驱动轴,其中,驱动轴包括设置在其一端处的用于驱动涡旋压缩机的压缩机构的偏心曲柄销,偏心曲柄销包括平行于驱动轴的旋转轴线延伸的驱动面。至少在驱动面的大致中央且向外凸出的部分上设置有耐磨层,耐磨层为通过物理气相沉积、化学气相沉积、等离子体气相沉积、电镀、化学镀、渗碳、渗氮、碳氮共渗、喷丸或表面淬火热处理形成的包含金属层、类金刚石、碳化物、氮化物、硅化物、硼化物或氧化物的硬化层。According to another aspect of the present invention, a drive shaft for a scroll compressor, wherein the drive shaft includes an eccentric crank pin disposed at one end thereof for driving a compression mechanism of the scroll compressor, the eccentric crank The pin includes a drive surface that extends parallel to the axis of rotation of the drive shaft. A wear layer is disposed on at least a portion of the driving surface substantially convex and outwardly, and the wear layer is formed by physical vapor deposition, chemical vapor deposition, plasma vapor deposition, electroplating, electroless plating, carburizing, nitriding, A hardened layer comprising a metal layer, a diamond-like layer, a carbide, a nitride, a silicide, a boride or an oxide formed by carbonitriding, shot peening or surface hardening heat treatment.
根据本发明的另一个方面,还涉及一种用于涡旋压缩机的卸载衬套,其中,卸载衬套包括呈大致D形的孔,孔具有与涡旋压缩机的偏心曲柄销的驱动面配合的从动面。至少在从动面的大致中央的部分上设置有耐磨层,耐磨层为通过物理气相沉积、化学气相沉积、等离子体气相沉积、电镀、化学镀、渗碳、渗氮、碳氮共渗、喷丸或表面淬火热处理形成的包含金属层、类金刚石、碳化物、氮化物、硅化物、硼化物或氧化物的硬化层。According to another aspect of the present invention, an unloading bushing for a scroll compressor, wherein the unloading bushing includes a hole having a substantially D shape having a driving surface with an eccentric crank pin of a scroll compressor The driven surface of the fit. At least in the substantially central portion of the driven surface is provided with a wear-resistant layer by physical vapor deposition, chemical vapor deposition, plasma vapor deposition, electroplating, electroless plating, carburizing, nitriding, carbonitriding A hardened layer comprising a metal layer, a diamond-like layer, a carbide, a nitride, a silicide, a boride or an oxide formed by shot peening or surface hardening heat treatment.
附图说明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:The features and advantages of one or more embodiments of the present invention will become more <RTIgt;
图1是涡旋压缩机的纵剖视图;Figure 1 is a longitudinal sectional view of a scroll compressor;
图2是图1中的涡旋压缩机的驱动轴的偏心曲柄销与卸载衬套的组装示意图;Figure 2 is a schematic view showing the assembly of the eccentric crank pin and the unloading bushing of the drive shaft of the scroll compressor of Figure 1;
图3示出了图2的驱动轴的偏心曲柄销的立体示意图;Figure 3 is a perspective view showing the eccentric crank pin of the drive shaft of Figure 2;
图4示出了图2的卸载衬套的立体示意图;Figure 4 shows a perspective view of the unloading bushing of Figure 2;
图5示意性地示出了根据本发明第一实施方式的形成耐磨层的方法;以及FIG. 5 schematically illustrates a method of forming an abrasion resistant layer in accordance with a first embodiment of the present invention;
图6是耐磨层的示意图。Figure 6 is a schematic illustration of a wear resistant layer.
具体实施方式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 The same reference numerals are used in the respective drawings to refer to the same components, and thus the construction of the same components will not be repeatedly described.
首先将参照图1描述涡旋压缩机的总体构造和运行原理。图1示出的是高压侧压缩机,然而,应理解的是,图1中的高压侧压缩机仅仅出于说明的目的,而非限制本发明。本发明可以适于任何类型的压缩机,包括低压侧压缩机,立式压缩机、卧式压缩机等。The overall configuration and operating principle of the scroll compressor will first be described with reference to FIG. 1 shows a high pressure side compressor, however, it should be understood that the high pressure side compressor of FIG. 1 is for illustrative purposes only and is not limiting of the invention. The invention may be adapted to any type of compressor, including low pressure side compressors, vertical compressors, horizontal compressors, and the like.
如图1所示,涡旋压缩机100(下文中有时也会称为压缩机)一般包括壳体110、设置在壳体110一端的顶盖112以及设置在壳体110另一端的底盖114。壳体110中设置有由定子122和转子124构成的马达20。转子124中设置有驱动轴30以驱动由定涡旋部件150和动涡旋部件160构成的压缩机构10。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的螺旋叶片156和动涡旋部件160的螺旋叶片166之间形成一系列体积在从径向外侧向径向内侧逐渐减小的压缩腔。其中,径向最外侧的压缩腔处于吸气压力,径向最内侧的压缩腔处于排气压力。中间的压缩腔处于吸气压力和排气压力之间,从而也被称之为中压腔。As shown in FIG. 1, a scroll compressor 100 (hereinafter sometimes referred to as a compressor) generally includes a housing 110, a top cover 112 disposed at one end of the housing 110, and a bottom cover 114 disposed at the other end of the housing 110. . A motor 20 composed of a stator 122 and a rotor 124 is disposed in the housing 110. A drive shaft 30 is provided in the rotor 124 to drive the compression mechanism 10 constituted by 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 whose volume gradually decreases from the radially outer side to the radially inner side are formed between the spiral vanes 156 of the fixed scroll member 150 and the spiral vanes 166 of the orbiting scroll member 160. Wherein, the radially outermost compression chamber is at the suction pressure, and the radially innermost compression chamber is at the exhaust pressure. The intermediate compression chamber is between the suction pressure and the discharge pressure, and is also referred to as the medium pressure chamber.
动涡旋部件160的一侧由主轴承座140的上部(其构成止推表面)支撑,驱动轴30的一部分由设置在主轴承座140中的主轴承支撑。驱动轴30的一端设置有偏心曲柄销32,在偏心曲柄销32和动涡旋部件160的毂部162之间设置有卸载衬套42。通过马达20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本身不会绕本身的中心轴线旋转)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来实现。One side of the movable scroll member 160 is supported by an upper portion of the main bearing housing 140 (which constitutes a thrust surface), and a portion of the drive shaft 30 is supported by a main bearing provided in the main bearing housing 140. One end of the drive shaft 30 is provided with an eccentric crank pin 32, and an unloading bushing 42 is disposed between the eccentric crank pin 32 and the hub portion 162 of the movable scroll member 160. By the driving of the motor 20, the orbiting scroll member 160 will rotate rotationally relative 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 around its central axis to achieve compression of the fluid. The translational rotation described above is achieved by a cross slip ring disposed between the fixed scroll member 150 and the movable scroll member 160.
在图1所示的涡旋压缩机的示例中,在压缩机壳体的底部存储有润滑剂。相应地,在驱动轴30中形成有大致沿其轴向延伸的通道,即形成在驱动轴30下端的中心孔136和从中心孔136向上延伸到偏心曲柄销32端面的偏心孔134。中心孔136的端部浸没在压缩机壳体底部的润滑剂中或者以其他方式被供给有润滑剂。在压缩机的运转过程中,中心孔136的一端被润滑剂供给装置供给有润滑剂,进入中心孔136的润滑剂在驱动轴30旋转过程中受到离心力的作用而被泵送或甩到偏心孔134中并且沿着偏心孔134向上流动一直到达偏心曲柄销32的端面。从偏心曲柄销32的端面排出的润滑剂沿着卸载衬套42与偏心曲柄销32之间的间隙以及卸载衬套 42与毂部162之间的间隙向下流动到达主轴承座140的凹部中。聚集在凹部中的一部分润滑剂流动穿过主轴承向下流动,一部分润滑剂被毂部162搅动而向上运动到达动涡旋部件160的端板164的下侧并随着动涡旋部件160的平动转动而遍布动涡旋部件160和主轴承座140的止推表面。在压缩机的运转过程中,供给到压缩机中的各种活动部件上的润滑剂被甩出和飞溅以形成液滴或雾。In the example of the scroll compressor shown in Fig. 1, a lubricant is stored at the bottom of the compressor housing. Accordingly, a passage extending substantially in the axial direction thereof is formed in the drive shaft 30, that is, a center hole 136 formed at the lower end of the drive shaft 30 and an eccentric hole 134 extending upward from the center hole 136 to the end surface of the eccentric crank pin 32. The end of the central bore 136 is submerged in the lubricant at the bottom of the compressor housing or otherwise supplied with a lubricant. During operation of the compressor, one end of the center hole 136 is supplied with lubricant by the lubricant supply means, and the lubricant entering the center hole 136 is pumped or plucked to the eccentric hole by the centrifugal force during the rotation of the drive shaft 30. The 134 and the upward flow along the eccentric hole 134 continue until reaching the end surface of the eccentric crank pin 32. Lubricant discharged from the end face of the eccentric crank pin 32 along the gap between the unloading bushing 42 and the eccentric crank pin 32 and the unloading bushing The gap between the 42 and the hub 162 flows downward into the recess of the main bearing housing 140. A portion of the lubricant collected in the recess flows downward through the main bearing, and a portion of the lubricant is agitated by the hub 162 to move upward to the lower side of the end plate 164 of the orbiting scroll member 160 and follow the movable scroll member 160. The translation is rotated to extend over the thrust surface of the orbiting scroll member 160 and the main bearing housing 140. During operation of the compressor, the lubricant supplied to the various moving parts in the compressor is scooped and splashed to form droplets or mist.
在图1所示的涡旋压缩机中,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的螺旋叶片156的顶端与动涡旋部件160的端板164之间以及动涡旋部件160的螺旋叶片166的顶端与定涡旋部件150的端板154之间需要轴向密封。涡旋压缩机的轴向柔性为本领域技术人员熟知,因此本文不再对其进行详细描述。In the scroll compressor shown in Fig. 1, in order to achieve compression of the fluid, it is necessary to effectively seal between the fixed scroll member 150 and the orbiting scroll member 160. In one aspect, between the tip end of the helical blade 156 of the fixed scroll member 150 and the end plate 164 of the movable scroll member 160 and between the tip end of the helical blade 166 of the orbiting scroll member 160 and the end plate 154 of the fixed scroll member 150. An axial seal is required. The axial flexibility of the scroll compressor is well known to those skilled in the art and will therefore not be described in detail herein.
另一方面,定涡旋部件150的螺旋叶片156的侧表面与动涡旋部件160的螺旋叶片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偏心曲柄销32与卸载衬套42之间的相对位移来实现。具体地,在运转过程中,通过马达20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30的偏心曲柄销32在旋转过程中也会产生有助于实现定涡旋部件150和动涡旋部件160的径向密封的驱动力分量。动涡旋部件160的螺旋叶片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的螺旋叶片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螺旋叶片156和螺旋叶片166之间时,螺旋叶片156和螺旋叶片166能够暂时沿径向彼此分开以允许异物通过,即,在偏心曲柄销32与卸载衬套42之间产生了相对位移,因此防止了螺旋叶片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。On the other hand, a radial seal is also required between the side surface of the spiral blade 156 of the fixed scroll member 150 and the side surface of the spiral blade 166 of the movable scroll member 160. This radial sealing between the two is typically achieved by means of the relative displacement between the eccentric crank pin 32 and the unloading bushing 42. Specifically, during operation, by the driving of the motor 20, 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 32 of the drive shaft 30 also generates a driving force component that contributes to the radial sealing of the fixed scroll member 150 and the movable scroll member 160 during the rotation. The helical vanes 166 of the orbiting scroll member 160 will abut against the helical vanes 156 of the fixed scroll member 150 by means of the above-described centrifugal and driving force components, thereby achieving a radial seal therebetween. When an incompressible substance such as solid impurities, lubricating oil, and liquid refrigerant enters the compression chamber and is caught between the spiral blade 156 and the spiral blade 166, the spiral blade 156 and the spiral blade 166 can be temporarily separated from each other in the radial direction to allow The foreign matter passes, that is, a relative displacement is generated between the eccentric crank pin 32 and the unloading bushing 42, thus preventing the spiral blade 156 or 166 from being damaged. This ability to be radially separated provides radial flexibility to the scroll compressor, increasing compressor reliability.
然而,偏心曲柄销32与卸载衬套42之间的相对位移使得它们被过快、过度磨损。为了解决该问题,在本发明中,对偏心曲柄销32和/或卸载衬套42的易磨损部分涂覆耐磨层以提高其硬度和耐磨性。However, the relative displacement between the eccentric crank pin 32 and the unloading bushing 42 causes them to be too fast and excessively worn. In order to solve this problem, in the present invention, the wear-resistant layer of the eccentric crank pin 32 and/or the unloading bushing 42 is coated with a wear-resistant layer to improve its hardness and wear resistance.
下面参照图2至图4对偏心曲柄销和卸载衬套进行详细描述。The eccentric crank pin and the unloading bushing will be described in detail below with reference to FIGS. 2 to 4.
如图3所示,其示出了驱动轴的偏心曲柄销的立体示意图。驱动轴 30的一端包括偏心曲柄销32。驱动轴30中形成有大致沿与驱动轴30的旋转轴线平行的第一方向(纵向方向)的偏心孔134以向偏心曲柄销32的端部供给润滑剂。驱动轴30的偏心曲柄销32经由卸载衬套42配合在动涡旋部件160的毂部162中,如图1所示。偏心曲柄销32包括平行于驱动轴30的旋转轴线延伸的驱动面321。相应地,卸载衬套42的供偏心曲柄销32穿过的大致D形的孔包括能够与偏心曲柄销32的驱动面321配合的从动面143。在将卸载衬套42与偏心曲柄销32装配至压缩机100之后,卸载衬套42中的大致D形的孔的尺寸大于偏心曲柄销32的尺寸以确保动涡旋部件160和定涡旋部件150之间的径向柔性。As shown in Figure 3, a perspective view of the eccentric crank pin of the drive shaft is shown. Drive shaft One end of 30 includes an eccentric crank pin 32. An eccentric hole 134 is formed in the drive shaft 30 in a first direction (longitudinal direction) substantially parallel to the rotational axis of the drive shaft 30 to supply lubricant to the end of the eccentric crank pin 32. The eccentric crank pin 32 of the drive shaft 30 is fitted into the hub portion 162 of the orbiting scroll member 160 via the unloading bushing 42, as shown in FIG. The eccentric crank pin 32 includes a drive surface 321 that extends parallel to the axis of rotation of the drive shaft 30. Accordingly, the generally D-shaped aperture of the unloading bushing 42 through which the eccentric crank pin 32 passes includes a driven surface 143 that is engageable with the drive surface 321 of the eccentric crank pin 32. After the unloading bushing 42 and the eccentric crank pin 32 are assembled to the compressor 100, the size of the generally D-shaped hole in the unloading bushing 42 is larger than the size of the eccentric crank pin 32 to ensure the orbiting scroll member 160 and the fixed scroll member. Radial flexibility between 150.
如图2所示,其示出了卸载衬套与偏心曲柄销的组装示意图。当卸载衬套42安装至偏心曲柄销32上时,偏心曲柄销32容置在卸载衬套42的D形孔中,同时,偏心曲柄销32的驱动面321与卸载衬套42的从动面143配合。通过该结构,偏心曲柄销32旋转时,由于偏心曲柄销32的驱动面321与卸载衬套42的从动面143配合,因此偏心曲柄销32可以驱动卸载衬套42旋转。另外,偏心曲柄销32的驱动面321的宽度(即,垂直于驱动轴的轴线方向的尺寸)小于卸载衬套42的从动面143的宽度(即,垂直于驱动轴的轴线方向的尺寸)。这样,偏心曲柄销32的驱动面321可以相对于卸载衬套42的从动面143发生相对运动。As shown in Figure 2, it shows an assembled view of the unloading bushing and the eccentric crank pin. When the unloading bushing 42 is mounted to the eccentric crank pin 32, the eccentric crank pin 32 is received in the D-shaped hole of the unloading bushing 42 while the driving surface 321 of the eccentric crank pin 32 and the driven surface of the unloading bushing 42 143 fit. With this configuration, when the eccentric crank pin 32 rotates, since the driving surface 321 of the eccentric crank pin 32 is engaged with the driven surface 143 of the unloading bush 42, the eccentric crank pin 32 can drive the unloading bush 42 to rotate. In addition, the width of the driving surface 321 of the eccentric crank pin 32 (that is, the dimension perpendicular to the axial direction of the drive shaft) is smaller than the width of the driven surface 143 of the unloading bush 42 (that is, the dimension perpendicular to the axial direction of the drive shaft). . Thus, the driving surface 321 of the eccentric crank pin 32 can move relative to the driven surface 143 of the unloading bushing 42.
在压缩机的理想工况及其理想设计和制造尺寸(即,无制造和安装误差)的情况下,当压缩机运行时,定涡旋部件和动涡旋部件的螺旋叶片可以紧密地贴合在一起。此时,卸载衬套的中心与驱动轴的中心之间的距离最大且基本恒定。In the ideal operating conditions of the compressor and its ideal design and manufacturing dimensions (ie, no manufacturing and installation tolerances), the spiral vanes of the fixed scroll and the orbiting scroll can be tightly fitted when the compressor is running. Together. At this time, the distance between the center of the unloading bushing and the center of the drive shaft is the largest and substantially constant.
然而,发明人发现,由于制造和安装误差而导致定涡旋部件和动涡旋部件的中心距不是一致的,因此,在压缩机运行一段时间之后,卸载衬套与偏心曲柄销之间会产生相对位移(其对应于制造和安装误差),具体地,卸载衬套的平坦。另外,发明人还发现,在实际工况下,当遇到杂质或液体制冷剂进入时,由于卸载衬套相对于偏心曲柄销发生相对运动,使得动涡旋部件的中心可以向驱动轴的中心偏移,因此定涡旋部件和动涡旋部件的螺旋叶片短暂地分离,防止其损坏。However, the inventors have found that the center-to-center distance of the fixed scroll member and the orbiting scroll member is not uniform due to manufacturing and installation errors, and therefore, after the compressor is operated for a period of time, an unloading bushing and an eccentric crank pin are generated. The relative displacement (which corresponds to manufacturing and mounting errors), in particular, the flatness of the unloading bushing. In addition, the inventors have also found that, under actual operating conditions, when encountering impurities or liquid refrigerant entering, the center of the movable scroll member can be toward the center of the drive shaft due to relative movement of the unloading bushing relative to the eccentric crank pin. Offset, so the spiral vanes of the fixed scroll and the orbiting scroll are temporarily separated to prevent damage.
在压缩机的实际运行期间,卸载衬套42的从动面143与偏心曲柄销32的驱动面321均受到法向载荷,且两个从动面143、321之间存在相对运动。因此,在卸载衬套42的从动面143与偏心曲柄销32的驱动面321产生了严重的磨损,由此缩短了其使用寿命,影响了压缩机的工作效率。 During the actual operation of the compressor, both the driven surface 143 of the unloading bushing 42 and the driving surface 321 of the eccentric crank pin 32 are subjected to normal loads, and there is relative movement between the two driven faces 143, 321 . Therefore, the driven surface 143 of the unloading bushing 42 and the driving surface 321 of the eccentric crank pin 32 are severely worn, thereby shortening the service life thereof and affecting the working efficiency of the compressor.
为此,根据本发明可以在卸载衬套42的从动面143和/或偏心曲柄销32的驱动面321上设置有耐磨层(也可以称为“硬化涂层”或“硬化薄膜”)50以提高其耐磨性。For this purpose, according to the invention, a wear-resistant layer (which may also be referred to as a "hardened coating" or a "hardened film") may be provided on the driven surface 143 of the unloading bushing 42 and/or the driving surface 321 of the eccentric crank pin 32. 50 to improve its wear resistance.
下面参见图5和图6对根据本发明的耐磨层及其工艺工程的示例进行描述。An example of the wear resistant layer and its process engineering according to the present invention will now be described with reference to Figs. 5 and 6.
如图5所示,将待涂覆涂层的基材S(例如为本文中的卸载衬套42的从动面143和/或偏心曲柄销32的驱动面321)容置于腔室中并且将其接地或者连接至负极电源,同时将靶材T(例如,铬靶材)也容置于腔室中并且将其连接至正极电源。对腔室抽真空,同时向其内填充氮气。靶材物质与氮气在低电压、大电流产生的电弧作用下发生电离,并被电场加速,撞击工件形成氮化铬薄膜层附着在基材表面上。As shown in FIG. 5, the substrate S to be coated (for example, the driven surface 143 of the unloading bushing 42 herein and/or the driving surface 321 of the eccentric crank pin 32) is housed in the chamber and Ground it or connect it to the negative supply while the target T (eg, a chromium target) is also housed in the chamber and connected to the positive supply. The chamber was evacuated while filling with nitrogen. The target material is ionized by nitrogen under the action of an arc generated by a low voltage and a large current, and is accelerated by the electric field to strike the workpiece to form a chromium nitride film layer attached to the surface of the substrate.
上述工艺过程仅仅是物理气相沉积的一个示例,并非意在限制本发明。本发明的耐磨层50可以通过本领域中已知的其他工艺过程而形成,例如,化学气相沉积、等离子体气相沉积、电镀、化学镀、渗碳、渗氮、碳氮共渗、喷丸、表面淬火热处理等。根据各种工艺过程,耐磨层50可以由金属层、类金刚石、碳化物、氮化物、硅化物、硼化物或氧化物等形成,例如,耐磨层50可以由氮化铬形成。The above process is merely an example of physical vapor deposition and is not intended to limit the invention. The wear layer 50 of the present invention can be formed by other processes known in the art, for example, chemical vapor deposition, plasma vapor deposition, electroplating, electroless plating, carburizing, nitriding, carbonitriding, shot peening , surface quenching heat treatment, etc. The wear layer 50 may be formed of a metal layer, a diamond-like layer, a carbide, a nitride, a silicide, a boride or an oxide, etc. according to various processes. For example, the wear layer 50 may be formed of chromium nitride.
在本发明中,偏心曲柄销32和/或卸载衬套42可以由粉末冶金材料制成,其表面硬度大致在600HV至800HV的范围内。当根据图5和图6所示的工艺过程在偏心曲柄销32和/或卸载衬套42上(例如,在偏心曲柄销32的驱动面321和/或卸载衬套42的从动面143上)涂覆有大致2至4微米厚的氮化铬耐磨层50时,该氮化铬耐磨层50的表面硬度可以达到1500HV至3000HV的范围,可选地达到1700HV至2700HV的范围。由此,可以明显提高偏心曲柄销32的驱动面和/或卸载衬套42的从动面的表面硬度,并且可以大大增强其耐磨损性能。另外,耐磨层50的厚度可以在0.1微米至4.5微米的范围内。In the present invention, the eccentric crank pin 32 and/or the unloading bushing 42 may be made of a powder metallurgy material having a surface hardness in the range of approximately 600 HV to 800 HV. When the process according to FIGS. 5 and 6 is on the eccentric crank pin 32 and/or the unloading bushing 42 (eg, on the drive face 321 of the eccentric crank pin 32 and/or the driven face 143 of the unloading bushing 42 When coated with a chromium nitride wear resistant layer 50 of approximately 2 to 4 microns thick, the surface hardness of the chromium nitride wear resistant layer 50 may range from 1500 HV to 3000 HV, optionally ranging from 1700 HV to 2700 HV. Thereby, the surface hardness of the driving surface of the eccentric crank pin 32 and/or the driven surface of the unloading bushing 42 can be remarkably improved, and the wear resistance can be greatly enhanced. Additionally, the thickness of the wear layer 50 can range from 0.1 microns to 4.5 microns.
发明人对上述涂覆有氮化铬耐磨层50的偏心曲柄销32和卸载衬套42进行了可靠性试验。具体地,将该偏心曲柄销32和卸载衬套42安装至压缩机,使压缩机在高速重载工况下运行500小时,发现偏心曲柄销32的驱动面和卸载衬套42的从动面几乎没有发生磨损。The inventors conducted reliability tests on the eccentric crank pin 32 and the unloading bushing 42 coated with the chromium nitride wear-resistant layer 50 described above. Specifically, the eccentric crank pin 32 and the unloading bushing 42 were mounted to the compressor, and the compressor was operated under high speed and heavy load conditions for 500 hours, and the driving surface of the eccentric crank pin 32 and the driven surface of the unloading bushing 42 were found. Almost no wear occurred.
上述试验表明:通过在偏心曲柄销32的驱动面和/或卸载衬套42的从动面上涂覆耐磨层50之后,耐磨层50可以阻止偏心曲柄销32和卸载衬套 42的粉末冶金材料直接接触,从而可以防止粉末冶金材料脱落。因此,耐磨层50大大提高了偏心曲柄销32和/或卸载衬套42的耐磨性能。The above test shows that the wear layer 50 can prevent the eccentric crank pin 32 and the unloading bushing after the wear layer 50 is applied to the driving surface of the eccentric crank pin 32 and/or the driven surface of the unloading bushing 42. The powder metallurgy material of 42 is in direct contact, thereby preventing the powder metallurgy material from falling off. Thus, the wear layer 50 greatly enhances the wear resistance of the eccentric crank pin 32 and/or the unloading bushing 42.
此外,在某些情况下,为了使偏心曲柄销32与卸载衬套42根据其运动形式可以良好配合,偏心曲柄销32的驱动面321可以具有大致位于中央处的略微凸起的部分。耐磨层50可以仅设置在驱动面321的大致中央处的略微凸起的部分上或者从动面143的大致中央处。或者,可以设置在整个驱动面321和/或从动面143上。另外,除了驱动面321和/或从动面143之外,也可以对偏心曲柄销32和/或卸载衬套42的经受磨损的其他部分涂覆耐磨层。Further, in some cases, in order to allow the eccentric crank pin 32 and the unloading bushing 42 to be well fitted according to the form of movement thereof, the driving surface 321 of the eccentric crank pin 32 may have a slightly convex portion substantially at the center. The wear layer 50 may be provided only on a slightly convex portion at substantially the center of the driving surface 321 or substantially at the center of the driven surface 143. Alternatively, it may be provided on the entire driving surface 321 and/or the driven surface 143. In addition, in addition to the drive surface 321 and/or the driven surface 143, the wear-resistant layer may also be applied to other portions of the eccentric crank pin 32 and/or the unloading bushing 42 that are subject to wear.
应理解的是,耐磨层50的外形轮廓和/或设置位置可以根据实际需要而成形。It should be understood that the contour and/or the position of the wear layer 50 may be shaped as desired.
上文已经具体描述了本发明的各种实施方式和变型,但是本领域技术人员应该理解,本发明并不局限于上述具体的实施方式和变型而是可以包括其他各种可能的组合和结合。Various embodiments and variations of the present invention have been described in detail above, but those skilled in the art should understand that the invention is not limited to the specific embodiments and variations described above, but may include various other possible combinations and combinations.
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 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 (12)

  1. 一种涡旋压缩机(100),包括:A scroll compressor (100) comprising:
    压缩机构(10),所述压缩机构(10)构造成对工作流体进行压缩;以及a compression mechanism (10) configured to compress a working fluid;
    驱动轴(30),所述驱动轴(30)构造成能够驱动所述压缩机构(10);a drive shaft (30), the drive shaft (30) being configured to be capable of driving the compression mechanism (10);
    其中,所述驱动轴(30)包括偏心曲柄销(32),在所述压缩机构(10)与所述偏心曲柄销(32)之间设置有卸载衬套(42),使得所述偏心曲柄销(32)经由所述卸载衬套(42)驱动所述压缩机构(10)以实现所述压缩机构(10)的径向柔性,Wherein the drive shaft (30) includes an eccentric crank pin (32), and an unloading bushing (42) is disposed between the compression mechanism (10) and the eccentric crank pin (32) such that the eccentric crank A pin (32) drives the compression mechanism (10) via the unloading bushing (42) to achieve radial flexibility of the compression mechanism (10),
    所述偏心曲柄销(32)包括与所述卸载衬套(42)接触并相对位移的偏心曲柄销配合部,所述卸载衬套(42)包括与所述偏心曲柄销(32)接触并相对位移的卸载衬套配合部,并且The eccentric crank pin (32) includes an eccentric crank pin engagement portion that contacts and is displaced relative to the unloading bushing (42), the unloading bushing (42) including a contact with the eccentric crank pin (32) and opposite Displacement of the unloading bushing mating portion, and
    所述偏心曲柄销配合部与所述卸载衬套配合部中的至少一者的至少一部分上设置有耐磨层(50)。A wear layer (50) is disposed on at least a portion of at least one of the eccentric crank pin engagement portion and the unloading bushing engagement portion.
  2. 如权利要求1所述的涡旋压缩机(100),其中,所述偏心曲柄销(32)包括平行于所述驱动轴(30)的旋转轴线延伸的驱动面(321),所述偏心曲柄销配合部包括所述驱动面(321)的至少一部分。The scroll compressor (100) according to claim 1, wherein said eccentric crank pin (32) includes a driving surface (321) extending parallel to an axis of rotation of said drive shaft (30), said eccentric crank The pin mating portion includes at least a portion of the drive surface (321).
  3. 如权利要求2所述的涡旋压缩机(100),其中,至少在位于所述驱动面(321)的大致中央处且向外凸出的部分上设置有所述耐磨层(50)。A scroll compressor (100) according to claim 2, wherein said wear layer (50) is provided at least at a portion located substantially at the center of said driving surface (321) and convex outward.
  4. 如权利要求2所述的涡旋压缩机(100),其中,所述卸载衬套(42)包括能够容纳所述偏心曲柄销(32)的孔,所述孔具有与所述偏心曲柄销(32)的所述驱动面(321)配合的从动面(143),所述卸载衬套配合部包括所述从动面(143)的至少一部分。The scroll compressor (100) according to claim 2, wherein said unloading bushing (42) includes a hole capable of accommodating said eccentric crank pin (32), said hole having said eccentric crank pin ( 32) The driving surface (321) of the driving surface (321) cooperates with the driven surface (143), and the unloading bushing fitting portion includes at least a portion of the driven surface (143).
  5. 如权利要求4所述的涡旋压缩机(100),其中,至少在所述从动面(143)的大致中央的部分上设置有所述耐磨层(50)。A scroll compressor (100) according to claim 4, wherein said wear layer (50) is provided at least at a substantially central portion of said driven surface (143).
  6. 如权利要求1至5中任一项所述的涡旋压缩机(100),其中,所述 耐磨层(50)为表面硬度在1500HV至3000HV的范围内的硬化层。The scroll compressor (100) according to any one of claims 1 to 5, wherein The wear resistant layer (50) is a hardened layer having a surface hardness in the range of 1500 HV to 3000 HV.
  7. 如权利要求1至5中任一项所述的涡旋压缩机(100),其中,所述耐磨层(50)的厚度在0.1微米至4.5微米的范围内。The scroll compressor (100) according to any one of claims 1 to 5, wherein the wear layer (50) has a thickness in the range of 0.1 μm to 4.5 μm.
  8. 如权利要求1至5中任一项所述的涡旋压缩机(100),其中,所述耐磨层(50)通过下列方法之一形成:物理气相沉积、化学气相沉积、等离子体气相沉积、电镀、化学镀、渗碳、渗氮、碳氮共渗、喷丸以及表面淬火热处理。The scroll compressor (100) according to any one of claims 1 to 5, wherein the wear layer (50) is formed by one of the following methods: physical vapor deposition, chemical vapor deposition, plasma vapor deposition , electroplating, electroless plating, carburizing, nitriding, carbonitriding, shot peening and surface quenching heat treatment.
  9. 如权利要求1至5中任一项所述的涡旋压缩机(100),其中,所述耐磨层(50)由下列材料之一形成:金属层、类金刚石、碳化物、氮化物、硅化物、硼化物以及氧化物。The scroll compressor (100) according to any one of claims 1 to 5, wherein the wear layer (50) is formed of one of the following materials: a metal layer, a diamond-like, a carbide, a nitride, Silicides, borides, and oxides.
  10. 如权利要求9所述的涡旋压缩机(100),其中,所述耐磨层(50)由氮化铬形成。The scroll compressor (100) according to claim 9, wherein the wear layer (50) is formed of chromium nitride.
  11. 一种用于涡旋压缩机(100)的驱动轴(30),其中,所述驱动轴(30)包括设置在其一端处的用于驱动所述涡旋压缩机(100)的压缩机构(10)的偏心曲柄销(32),所述偏心曲柄销(32)包括平行于所述驱动轴(30)的旋转轴线延伸的驱动面(321),并且A drive shaft (30) for a scroll compressor (100), wherein the drive shaft (30) includes a compression mechanism disposed at one end thereof for driving the scroll compressor (100) 10) an eccentric crank pin (32), the eccentric crank pin (32) including a drive surface (321) extending parallel to an axis of rotation of the drive shaft (30), and
    至少在所述驱动面(321)的大致中央且向外凸出的部分上设置有耐磨层(50),所述耐磨层(50)为通过物理气相沉积、化学气相沉积、等离子体气相沉积、电镀、化学镀、渗碳、渗氮、碳氮共渗、喷丸或表面淬火热处理形成的包含金属层、类金刚石、碳化物、氮化物、硅化物、硼化物或氧化物的硬化层。At least a portion of the driving surface (321) that is substantially central and outwardly convex is provided with a wear-resistant layer (50) for physical vapor deposition, chemical vapor deposition, plasma vapor phase Hardened layer of metal, diamond-like, carbide, nitride, silicide, boride or oxide formed by deposition, electroplating, electroless plating, carburizing, nitriding, carbonitriding, shot peening or surface hardening heat treatment .
  12. 一种用于涡旋压缩机(100)的卸载衬套(42),其中,所述卸载衬套(42)包括呈大致D形的孔,所述孔具有与所述涡旋压缩机(100)的偏心曲柄销(32)的驱动面(321)配合的从动面(143),并且An unloading bushing (42) for a scroll compressor (100), wherein the unloading bushing (42) includes a substantially D-shaped bore having the scroll compressor (100) a driving surface (321) of the eccentric crank pin (32) that cooperates with the driven surface (143), and
    至少在所述从动面(143)的大致中央的部分上设置有耐磨层(50), 所述耐磨层(50)为通过物理气相沉积、化学气相沉积、等离子体气相沉积、电镀、化学镀、渗碳、渗氮、碳氮共渗、喷丸或表面淬火热处理形成的包含金属层、类金刚石、碳化物、氮化物、硅化物、硼化物或氧化物的硬化层。 A wear layer (50) is disposed on at least a portion of the substantially central portion of the driven surface (143), The wear layer (50) is a metal layer formed by physical vapor deposition, chemical vapor deposition, plasma vapor deposition, electroplating, electroless plating, carburizing, nitriding, carbonitriding, shot blasting or surface hardening heat treatment. a hardened layer of diamond-like, carbide, nitride, silicide, boride or oxide.
PCT/CN2016/075986 2015-04-23 2016-03-09 Scroll compressor and driving shaft and unloading bush for scroll compressor WO2016169349A1 (en)

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