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CN112771272B - Scroll compressor having a discharge port - Google Patents

Scroll compressor having a discharge port Download PDF

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Publication number
CN112771272B
CN112771272B CN201980063461.4A CN201980063461A CN112771272B CN 112771272 B CN112771272 B CN 112771272B CN 201980063461 A CN201980063461 A CN 201980063461A CN 112771272 B CN112771272 B CN 112771272B
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China
Prior art keywords
scroll
body portion
orbiting scroll
main frame
frame
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CN201980063461.4A
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CN112771272A (en
Inventor
上川隆司
赵洋熙
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Samsung Electronics Co Ltd
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Samsung Electronics Co Ltd
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Priority claimed from PCT/KR2019/012532 external-priority patent/WO2020067739A1/en
Publication of CN112771272A publication Critical patent/CN112771272A/en
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    • 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
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/007General arrangements of parts; Frames and supporting elements
    • 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
    • F04C27/00Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
    • F04C27/005Axial sealings for working fluid
    • 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
    • F04C29/005Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions
    • 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
    • F04C29/12Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
    • 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
    • F04C2210/00Fluid
    • F04C2210/26Refrigerants with particular properties, e.g. HFC-134a
    • 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
    • F04C2240/00Components
    • F04C2240/20Rotors
    • 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
    • F04C2240/00Components
    • F04C2240/50Bearings
    • 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
    • F04C2240/00Components
    • F04C2240/50Bearings
    • F04C2240/56Bearing bushings or details thereof
    • 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
    • F04C2240/00Components
    • F04C2240/60Shafts
    • 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
    • F04C2240/00Components
    • F04C2240/80Other components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2210/00Working fluid
    • F05B2210/10Kind or type
    • F05B2210/14Refrigerants with particular properties, e.g. HFC-134a
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/50Bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/57Seals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/60Shafts

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)

Abstract

Disclosed herein is a scroll compressor capable of optimizing a position where a load is applied from a support member to an orbiting scroll. The scroll compressor includes: a fixed scroll fixed to an inside of the body; an orbiting scroll configured to orbit in engagement with the fixed scroll; a rotation shaft configured to allow the orbiting scroll to orbit; a holding member configured to hold the fixed scroll from a side opposite to the orbiting scroll; and a support member disposed between the rotation shaft and the holding member to support the orbiting scroll by a load applied to a position away from a center of the orbiting scroll.

Description

涡旋式压缩机scroll compressor

技术领域technical field

本公开涉及涡旋式压缩机。The present disclosure relates to scroll compressors.

背景技术Background technique

涡旋式压缩机被如下配置。被密封的容器保持在高压力。在被密封的容器中提供:固定涡旋件和绕动涡旋件,配置为使得其螺旋形卷体(wrap)彼此接合以在支撑板上形成压缩室;主轴,配置为通过将偏心轴部分插入到提供在绕动涡旋件的与螺旋形卷体相反的一侧上的凸起部分中而驱动绕动涡旋件;顺从框架(compliant frame),配置为在轴向方向上支撑绕动涡旋件,同时在提供于主轴中的主轴部分上径向地支撑驱动绕动涡旋件的主轴;以及引导框架,配置为在径向方向上支撑顺从框架以便固定到密封容器中。因此,通过顺从框架关于引导框架在径向方向上的滑动运动,绕动涡旋件在轴向方向上可移动(参照专利文件)。The scroll compressor is configured as follows. The sealed container is kept under high pressure. Provided in a sealed container are: a fixed scroll and an orbiting scroll configured such that their spiral wraps (wrap) engage with each other to form a compression chamber on a support plate; a main shaft configured to pass the eccentric shaft portion The orbiting scroll is driven by being inserted into a raised portion provided on the side of the orbiting scroll opposite to the spiral wrap; a compliant frame configured to support the orbiting scroll in the axial direction A scroll while radially supporting a main shaft driving an orbiting scroll on a main shaft portion provided in the main shaft; and a guide frame configured to support a compliant frame in a radial direction so as to be fixed into the hermetic container. Therefore, the orbiting scroll is movable in the axial direction by complying with the sliding movement of the frame with respect to the guide frame in the radial direction (refer to patent documents).

[相关技术文件][Related Technical Documents]

[专利文件][Patent Document]

日本专利5641978(2014.11.07)Japanese patent 5641978 (2014.11.07)

发明内容Contents of the invention

技术问题technical problem

在支撑构件(其布置在允许绕动涡旋件绕动的旋转轴和保持固定涡旋件的保持构件之间)支撑绕动涡旋件的状态下,当采用其中通过支撑构件关于保持构件在轴向方向上的滑动运动而使绕动涡旋件仅在轴向方向上可移动的配置时,难以优化负载从支撑构件施加到绕动涡旋件的位置。In a state where the orbiting scroll is supported by the support member (which is arranged between the rotating shaft that allows the orbiting scroll to orbit and the holding member that holds the fixed scroll), when the orbiting scroll is supported by the support member with respect to the holding member In an arrangement in which the orbiting scroll is movable only in the axial direction due to the sliding movement in the axial direction, it is difficult to optimize the position where the load is applied from the support member to the orbiting scroll.

因此,本公开的一方面是提供一种涡旋式压缩机,其能够优化负载从支撑构件施加到绕动涡旋件的位置。Accordingly, an aspect of the present disclosure is to provide a scroll compressor capable of optimizing a position where a load is applied from a support member to an orbiting scroll.

对问题的技术方案technical solution to the problem

根据本公开的一方面,一种涡旋式压缩机包括:固定到主体的固定涡旋件;绕动涡旋件,配置为与固定涡旋件接合地绕动;旋转轴,配置为允许绕动涡旋件绕动;保持构件,配置为从与绕动涡旋件相反的一侧保持固定涡旋件;以及支撑构件,布置在旋转轴和保持构件之间以通过施加到远离绕动涡旋件的中心的位置的负载来支撑绕动涡旋件。According to an aspect of the present disclosure, a scroll compressor includes: a fixed scroll fixed to a main body; an orbiting scroll configured to orbit in engagement with the fixed scroll; a rotary shaft configured to allow orbiting The orbiting scroll orbits; a retaining member configured to retain the fixed scroll from a side opposite to the orbiting scroll; and a support member arranged between the rotating shaft and the retaining member to The load at the position of the center of the scroll member is used to support the orbiting scroll member.

支撑构件可以关于保持构件在一个方向上可移动。The support member may be movable in one direction with respect to the holding member.

支撑构件可以在沿着旋转轴的方向上移动并且还在关于大致垂直于旋转轴的虚拟轴线的旋转方向上可移动。The support member is movable in a direction along the rotational axis and is also movable in a rotational direction about an imaginary axis substantially perpendicular to the rotational axis.

在绕虚拟轴线的旋转方向当中,支撑构件可以在与绕动涡旋件中产生的力矩相反的方向上可移动。The support member may be movable in a direction opposite to a moment generated in the orbiting scroll, among rotation directions about the virtual axis.

支撑构件可以通过从在绕动涡旋件侧的特定位置而不是旋转轴中的接收负载的位置接收反作用力而在与绕动涡旋件中产生的力矩相反的旋转方向上可移动,该反作用力在保持构件中抵抗绕动涡旋件接收的负载。该特定位置可以在支撑构件的旋转轴轴承的在绕动涡旋件侧的端面与绕动涡旋件的板在其上与固定涡旋件接合的表面之间。The supporting member may be movable in a rotational direction opposite to a moment generated in the orbiting scroll by receiving a reaction force from a specific position on the side of the orbiting scroll instead of a position receiving a load in the rotary shaft, the reaction force The force is in the retaining member against the load received by the orbiting scroll. The specific position may be between an end surface of the rotary shaft bearing of the supporting member on the side of the orbiting scroll and a surface on which the plate of the orbiting scroll engages with the fixed scroll.

支撑构件可以在与绕动涡旋件中产生的力矩相反的旋转方向上可移动,因为关于接收绕旋转轴的负载的位置,在与绕动涡旋件相同侧与保持构件的最小间隙小于在与绕动涡旋件的相反侧与保持构件的最小间隙。该特定位置可以在支撑构件的旋转轴轴承的在绕动涡旋件侧的端面与绕动涡旋件的板在其上与固定涡旋件接合的表面之间。The supporting member can be movable in the rotational direction opposite to the moment generated in the orbiting scroll because the minimum clearance with the retaining member on the same side as the orbiting scroll is smaller than in The minimum clearance between the side opposite to the orbiting scroll and the retaining member. The specific position may be between an end surface of the rotary shaft bearing of the supporting member on the side of the orbiting scroll and a surface on which the plate of the orbiting scroll engages with the fixed scroll.

支撑构件可以通过与提供在保持构件上的突起接触而在与绕动涡旋件中产生的力矩相反的旋转方向上可移动。The supporting member may be movable in a rotational direction opposite to a moment generated in the orbiting scroll by contacting a protrusion provided on the holding member.

支撑构件的一部分可以具有在与一表面接触时可弹性变形的形状,在该表面上绕动涡旋件的板由于支撑构件的倾斜而与固定涡旋件接合。A part of the support member may have a shape elastically deformable upon contact with a surface on which the plate of the orbiting scroll engages with the fixed scroll due to inclination of the support member.

涡旋式压缩机还可以包括配置为防止绕动涡旋件的枢转的奥尔德姆环,并且奥尔德姆环可以联接到绕动涡旋件和支撑构件、绕动涡旋件和保持构件、或绕动涡旋件和固定涡旋件。The scroll compressor may further include an Oldham ring configured to prevent pivoting of the orbiting scroll, and the Oldham ring may be coupled to the orbiting scroll and the support member, the orbiting scroll and A retaining member, or an orbiting scroll and a fixed scroll.

涡旋式压缩机还可以包括密封机构,该密封机构配置为通过密封保持构件和支撑构件之间的间隙的至少一部分而在至少保持构件和支撑构件之间形成内部空间。The scroll compressor may further include a sealing mechanism configured to form an inner space between at least the holding member and the supporting member by sealing at least a portion of a gap between the holding member and the supporting member.

保持构件可以提供有保持构件内部通道,该保持构件内部通道配置为将从压缩室引入的制冷剂引入到内部空间中,该压缩室形成为使得绕动涡旋件通过与固定涡旋件接合而绕动。The retaining member may be provided with a retaining member internal passage configured to introduce into the internal space refrigerant introduced from a compression chamber formed such that the orbiting scroll engages with the fixed scroll. orbit.

固定涡旋件可以提供有固定涡旋件内部通道,该固定涡旋件内部通道配置为使来自压缩室的制冷剂移动并将制冷剂引入到保持构件内部通道中。The fixed scroll may be provided with a fixed scroll inner passage configured to move refrigerant from the compression chamber and introduce the refrigerant into the retaining member inner passage.

固定涡旋件可以提供有固定涡旋件内部通道,该固定涡旋件内部通道配置为使来自压缩室的制冷剂移动并将制冷剂引入到保持构件内部通道中,绕动涡旋件可以提供有绕动涡旋件内部通道,该绕动涡旋件内部通道配置为使来自压缩室的制冷剂移动并将制冷剂引入到固定涡旋件内部通道中。在这种情况下,固定涡旋件内部通道可以在绕动涡旋件绕动的周期的至少一部分中与绕动涡旋件内部通道连通。固定涡旋件内部通道可以包括在绕动涡旋件绕动时在绕动涡旋件内部通道的出口的轨迹上的入口以及连接到凹槽部分的入口,该凹槽部分在绕动涡旋件绕动时覆盖绕动涡旋件内部通道的出口的整个轨迹。The fixed scroll may be provided with a fixed scroll internal passage configured to move refrigerant from the compression chamber and introduce the refrigerant into the retaining member internal passage, and the orbiting scroll may provide There is an orbiting scroll inner passage configured to move refrigerant from the compression chamber and introduce refrigerant into the fixed scroll inner passage. In this case, the fixed scroll internal passage may communicate with the orbiting scroll internal passage during at least a part of a cycle in which the orbiting scroll orbits. The fixed scroll internal passage may include an inlet on the track of an outlet of the orbiting scroll internal passage when the orbiting scroll orbits, and an inlet connected to a groove portion that passes through the orbiting scroll. Cover the entire trajectory of the outlet of the inner channel of the orbiting scroll when the member orbits.

发明的有益效果Beneficial Effects of the Invention

可以优化负载从支撑构件施加到绕动涡旋件的位置。The position where the load is applied from the support member to the orbiting scroll can be optimized.

附图说明Description of drawings

图1示出根据本公开的一实施方式的涡旋式压缩机的轴向剖视图;FIG. 1 shows an axial sectional view of a scroll compressor according to an embodiment of the present disclosure;

图2示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图;2 illustrates an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure;

图3示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图;3 illustrates an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure;

图4示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图;4 illustrates an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure;

图5示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图;5 illustrates an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure;

图6示出根据本公开的一实施方式的涡旋式压缩机的轴向剖视图;Fig. 6 shows an axial sectional view of a scroll compressor according to an embodiment of the present disclosure;

图7a是示出绕动涡旋件接收的力矩的透视图,图7b是示出绕动涡旋件将要倾斜的形状的视图;FIG. 7a is a perspective view showing a moment received by the orbiting scroll, and FIG. 7b is a view showing a shape in which the orbiting scroll is about to tilt;

图8示出当施加到子框架的力矩在与施加到绕动涡旋件的力矩相同的方向上时压缩部分和旋转轴的轴向剖视图;8 shows an axial sectional view of the compression portion and the rotary shaft when the moment applied to the subframe is in the same direction as that applied to the orbiting scroll;

图9示出当施加到子框架的力矩在与施加到绕动涡旋件的力矩相反的方向上时压缩部分和旋转轴的轴向剖视图;9 shows an axial sectional view of the compression portion and the rotary shaft when the moment applied to the subframe is in a direction opposite to that applied to the orbiting scroll;

图10示出根据涡旋式压缩机的一实现方式的压缩部分和旋转轴的轴向剖视图;Fig. 10 shows an axial cross-sectional view of a compression portion and a rotating shaft according to an implementation of a scroll compressor;

图11示出根据涡旋式压缩机的一实现方式的压缩部分和旋转轴的轴向剖视图;Fig. 11 shows an axial cross-sectional view of a compression portion and a rotating shaft according to an implementation of a scroll compressor;

图12示出根据涡旋式压缩机的一实现方式的压缩部分和旋转轴的轴向剖视图;Figure 12 shows an axial cross-sectional view of the compression section and the rotating shaft according to an implementation of a scroll compressor;

图13示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图;13 shows an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure;

图14是示出根据按照本公开的一实施方式的涡旋式压缩机的变型、当从顶部观看时在压缩部分中的绕动涡旋件的板的端部的俯视图;14 is a plan view showing an end portion of a plate of an orbiting scroll in a compression portion when viewed from the top according to a modification of the scroll compressor according to an embodiment of the present disclosure;

图15是示出根据按照本公开的一实施方式的涡旋式压缩机的变型、当从底部观看时在压缩部分中的固定涡旋件的主体部分的仰视图;15 is a bottom view illustrating a main body portion of a fixed scroll in a compression portion when viewed from the bottom according to a modification of the scroll compressor according to an embodiment of the present disclosure;

图16示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图;以及16 shows an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure; and

图17是根据按照本公开的一实施方式的涡旋式压缩机的变型、当从底部观看时在压缩部分中的固定涡旋件的主体部分的仰视图。17 is a bottom view of a main body portion of a fixed scroll in a compression portion when viewed from the bottom according to a modification of the scroll compressor according to an embodiment of the present disclosure.

具体实施方式Detailed ways

在下文,将参照附图描述本公开的实施方式。在以下的详细描述中,“前端”、“后端”、“上部”、“下部”、“上端”、“下端”等的术语可以通过附图来定义,但是部件的形状和位置不受该术语限制。Hereinafter, embodiments of the present disclosure will be described with reference to the accompanying drawings. In the following detailed description, the terms "front end", "rear end", "upper part", "lower part", "upper end", "lower end" etc. may be defined by the drawings, but the shapes and positions of parts are not affected by the Terminology restrictions.

根据实施方式,一种涡旋式压缩机提供有:固定涡旋件;绕动涡旋件,配置为与固定涡旋件接合地绕动;旋转轴,配置为允许绕动涡旋件绕动;保持构件,配置为将固定涡旋件保持在绕动涡旋件的相对侧;以及支撑构件,布置在旋转轴和保持构件之间。支撑构件通过施加到远离绕动涡旋件的中心的位置的负载而支撑绕动涡旋件。也就是,可以提供支撑构件以在远离绕动涡旋件的中心的位置支撑绕动涡旋件。作为用于通过施加到支撑构件从绕动涡旋件的中心偏移的位置的负载来支撑绕动涡旋件的具体配置,可以考虑一些配置。在下文,这些配置将作为实施方式被描述。According to an embodiment, a scroll compressor is provided with: a fixed scroll; an orbiting scroll configured to orbit engaged with the fixed scroll; a rotary shaft configured to allow the orbiting scroll to orbit a holding member configured to hold the fixed scroll on an opposite side of the orbiting scroll; and a supporting member disposed between the rotation shaft and the holding member. The support member supports the orbiting scroll by a load applied to a position away from the center of the orbiting scroll. That is, a support member may be provided to support the orbiting scroll at a position away from the center of the orbiting scroll. As a specific configuration for supporting the orbiting scroll by a load applied to a position of the support member offset from the center of the orbiting scroll, some configurations can be considered. Hereinafter, these configurations will be described as embodiments.

图1示出根据本公开的一实施方式的涡旋式压缩机1的轴向剖视图。FIG. 1 shows an axial sectional view of a scroll compressor 1 according to an embodiment of the present disclosure.

涡旋式压缩机1是被广泛用于空调、冰箱和泵的压缩机。图1是用于空调的制冷剂回路中的气密涡旋式压缩机的纵向剖视图。The scroll compressor 1 is a compressor widely used in air conditioners, refrigerators, and pumps. FIG. 1 is a longitudinal sectional view of a hermetic scroll compressor used in a refrigerant circuit of an air conditioner.

涡旋式压缩机1包括配置为压缩制冷剂的压缩部分10、配置为驱动压缩部分10的驱动电机20以及与配置为接收压缩部分10和驱动电机20的主体相对应的壳体30。根据一实施方式,涡旋式压缩机1是垂直涡旋式压缩机,其中驱动电机20的将在后面描述的旋转轴23的轴向方向与重力方向一致。在下文,旋转轴23的轴向方向将被称为“垂直方向”,并且基于图1,较高侧可以被称为“上侧”,较低侧可以被称为“下侧”。尽管垂直涡旋式压缩机作为示例被描述,但是本公开的实施方式将可应用于水平涡旋式压缩机。The scroll compressor 1 includes a compression part 10 configured to compress refrigerant, a driving motor 20 configured to drive the compression part 10 , and a housing 30 corresponding to a body configured to receive the compression part 10 and the driving motor 20 . According to an embodiment, the scroll compressor 1 is a vertical scroll compressor in which an axial direction of a rotation shaft 23 to be described later of the drive motor 20 coincides with a gravity direction. Hereinafter, the axial direction of the rotation shaft 23 will be referred to as "vertical direction", and based on FIG. 1 , the higher side may be referred to as "upper side" and the lower side may be referred to as "lower side". Although a vertical scroll compressor is described as an example, embodiments of the present disclosure will be applicable to a horizontal scroll compressor.

首先,将描述压缩部分10。First, the compression section 10 will be described.

压缩部分10包括:固定涡旋件11,固定到壳体30;绕动涡旋件12,通过与固定涡旋件11接合而绕动;主框架13,固定到壳体30并配置为支撑固定涡旋件11;子框架14,布置在由绕动涡旋件和主框架13围绕的空间中并配置为支撑绕动涡旋件12;以及奥尔德姆环(Oldham ring)15,配置为允许绕动涡旋件12绕动而不使绕动涡旋件12枢转。The compression part 10 includes: a fixed scroll 11 fixed to a casing 30; an orbiting scroll 12 orbiting by being engaged with the fixed scroll 11; a main frame 13 fixed to the casing 30 and configured to support a fixed a scroll 11; a subframe 14 arranged in a space surrounded by the orbiting scroll and the main frame 13 and configured to support the orbiting scroll 12; and an Oldham ring 15 configured to The orbiting scroll 12 is allowed to orbit without pivoting the orbiting scroll 12 .

固定涡旋件11可以包括固定涡旋件主体和从固定涡旋件主体突出的固定卷体114。固定卷体114可以从固定涡旋件主体向下突出。The fixed scroll 11 may include a fixed scroll body and a fixed wrap 114 protruding from the fixed scroll body. The fixed wrap 114 may protrude downwardly from the fixed scroll body.

固定涡旋件主体可以包括圆筒形主体部分111、配置为覆盖主体部分111 的上侧中的开口的板112以及从主体部分111的下端在径向向外的方向上延伸的突起113。固定卷体114可以从板112的下部向下突出并且当从底部观看时具有螺旋形状。The fixed scroll body may include a cylindrical body portion 111 , a plate 112 configured to cover an opening in an upper side of the body portion 111 , and a protrusion 113 extending in a radially outward direction from a lower end of the body portion 111 . The fixed roll 114 may protrude downward from a lower portion of the plate 112 and have a spiral shape when viewed from the bottom.

固定涡旋件11可以由铸铁形成,诸如灰色铸铁FC 250。The fixed scroll 11 may be formed from cast iron, such as gray cast iron FC 250 .

主体部分111可以在径向方向上提供有通孔111a。通孔111a可以用作吸入口,该吸入口配置为将制冷剂吸入到由主体部分111、板112和绕动涡旋件12围绕的空间中。The body part 111 may be provided with a through hole 111a in a radial direction. The through hole 111 a may serve as a suction port configured to suck refrigerant into a space surrounded by the main body portion 111 , the plate 112 and the orbiting scroll 12 .

在垂直方向上的通孔112a形成在板112的中心处。通孔112a可以用作排出口,该排出口配置为将制冷剂从由板112、固定卷体114和绕动涡旋件 12围绕的空间排出。A through hole 112 a in the vertical direction is formed at the center of the board 112 . The through hole 112 a may serve as a discharge port configured to discharge refrigerant from a space surrounded by the plate 112 , the fixed wrap 114 and the orbiting scroll 12 .

如上所述构造的固定涡旋件11通过穿过在垂直方向上形成在突起113 中的通孔的定位机构诸如螺栓或定位销而被固定到主框架13。The fixed scroll 11 configured as described above is fixed to the main frame 13 by a positioning mechanism such as a bolt or a positioning pin passing through a through hole formed in the protrusion 113 in the vertical direction.

绕动涡旋件12可以包括绕动涡旋件主体和绕动卷体122,绕动卷体122 从绕动涡旋件主体突出以通过与固定涡旋件11的固定卷体114接合而形成压缩室16。绕动卷体122可以从绕动涡旋件主体向上突出。The orbiting scroll 12 may include an orbiting scroll body and an orbiting wrap 122 protruding from the orbiting scroll body to be formed by being engaged with the fixed wrap 114 of the fixed scroll 11 . Compression chamber 16. The orbiting wrap 122 may protrude upward from the orbiting scroll body.

绕动涡旋件12可以通过联接旋转轴23来执行绕动运动。The orbiting scroll 12 may perform an orbiting motion by being coupled to a rotary shaft 23 .

绕动涡旋件主体可以包括具有盘形状的板121以及从板121的下端向下突出的圆筒形主体部分123。绕动卷体122可以从板121的上端向上突出并且当从顶部观看时具有螺旋形状。The orbiting scroll body may include a plate 121 having a disk shape and a cylindrical body portion 123 protruding downward from a lower end of the plate 121 . The winding roll 122 may protrude upward from the upper end of the plate 121 and have a spiral shape when viewed from the top.

绕动涡旋件12可以由FC材料或FCD材料形成。The orbiting scroll 12 may be formed of FC material or FCD material.

绕动涡旋件12的绕动卷体122可以与固定涡旋件11的固定卷体114接合。此外,绕动涡旋件12的绕动卷体122和固定涡旋件11的固定卷体114 可以设置在由固定涡旋件11的主体部分111和板112以及板121形成的空间中从而形成压缩室16。由于绕动卷体122围绕被固定的固定卷体114圆周地运动,所以压缩室16的体积减小并且压缩室16的制冷剂被压缩。换句话说,由于固定卷体114和绕动卷体122之间的内部空间被朝向旋转中心减小,所以制冷剂被压缩。The orbiting wrap 122 of the orbiting scroll 12 may be engaged with the fixed wrap 114 of the fixed scroll 11 . In addition, the orbiting wrap 122 of the orbiting scroll 12 and the fixed wrap 114 of the fixed scroll 11 may be disposed in a space formed by the body portion 111 and the plate 112 and the plate 121 of the fixed scroll 11 to form Compression chamber 16. As the orbiting coil 122 moves circularly around the fixed fixed coil 114 , the volume of the compression chamber 16 is reduced and the refrigerant of the compression chamber 16 is compressed. In other words, since the inner space between the fixed wrap 114 and the orbiting wrap 122 is reduced toward the center of rotation, the refrigerant is compressed.

随后描述的旋转轴23的偏心轴232通过滑动轴承被插入到主体部分123 中。如上所述,主体部分123用作偏心轴232的轴承。An eccentric shaft 232 of the rotating shaft 23 described later is inserted into the main body portion 123 through a sliding bearing. As mentioned above, the main body portion 123 serves as a bearing for the eccentric shaft 232 .

主框架13是配置为保持固定涡旋件11的保持构件的示例。主框架13 可以包括圆筒形的第一主体部分131、从第一主体部分131的下端的径向内侧向下突出的圆筒形的第二主体部分132、从第二主体部分132的下端径向向内突出的圆筒形的第三主体部分133以及从第三主体部分133的内端向上和向下突出的圆筒形的第四主体部分134。主框架13的第一主体部分131 的外周表面被固定到壳体30的随后描述的中央壳体31。此外,尽管轴颈轴承(journal bearing)插置在它们之间,但是随后描述的驱动电机20的旋转轴23被插入到第四主体部分134的内部中。如上所述,主框架13还用作可旋转地支撑旋转轴23的轴承。The main frame 13 is an example of a holding member configured to hold the fixed scroll 11 . The main frame 13 may include a cylindrical first body portion 131, a cylindrical second body portion 132 protruding downward from the radially inner side of the lower end of the first body portion 131, a diameter A cylindrical third body portion 133 protruding inward and a cylindrical fourth body portion 134 protruding upward and downward from an inner end of the third body portion 133 . The outer peripheral surface of the first main body portion 131 of the main frame 13 is fixed to a later-described center case 31 of the case 30 . Furthermore, the rotation shaft 23 of the drive motor 20 described later is inserted into the inside of the fourth main body portion 134 although a journal bearing is interposed therebetween. As described above, the main frame 13 also functions as a bearing that rotatably supports the rotary shaft 23 .

在第一主体部分131的外周部分上,安装从上端表面向上突出的突起 131a。在突起131a中形成凹形螺钉,并且穿过形成在固定涡旋件11的突起 113中的通孔的螺栓与该凹形螺钉接合。因此,固定涡旋件11被固定到主框架13。On an outer peripheral portion of the first main body portion 131, a protrusion 131a protruding upward from an upper end surface is installed. A female screw is formed in the protrusion 131a, and a bolt passing through a through hole formed in the protrusion 113 of the fixed scroll 11 is engaged with the female screw. Therefore, the fixed scroll 11 is fixed to the main frame 13 .

在第一主体部分131的外周部分上,可以提供在垂直方向上伸长的凹槽 131b。也就是,在第一主体部分131中,可以形成从外周部分的中心到下部在垂直方向上延伸的凹槽131b。在第一主体部分131中,形成凹槽131b的部分可以与中央壳体31间隔开。On an outer peripheral portion of the first body portion 131, a groove 131b elongated in a vertical direction may be provided. That is, in the first body part 131, a groove 131b extending in a vertical direction from the center to the lower part of the outer peripheral part may be formed. In the first body part 131 , a portion forming the groove 131 b may be spaced apart from the center case 31 .

旋转轴23装配在第四主体部分134的内周中,轴颈轴承插置在它们之间,因此第四主体部分134用作可旋转地支撑旋转轴23的轴承。The rotation shaft 23 is fitted in the inner periphery of the fourth body portion 134 with journal bearings interposed therebetween, so the fourth body portion 134 functions as a bearing that rotatably supports the rotation shaft 23 .

主框架13还可以包括配置为支撑固定涡旋件11的固定涡旋件支撑表面 11a。固定涡旋件支撑表面11a可以形成在突起131a上。The main frame 13 may further include a fixed scroll support surface 11 a configured to support the fixed scroll 11 . A fixed scroll supporting surface 11a may be formed on the protrusion 131a.

子框架14是用于支撑绕动涡旋件12的支撑构件的示例。间隙可以形成在主框架13和子框架14之间,使得子框架14相对于主框架13可移动。换句话说,子框架14可以布置在主框架13内以与主框架13间隔开。The sub-frame 14 is an example of a support member for supporting the orbiting scroll 12 . A gap may be formed between the main frame 13 and the sub frame 14 such that the sub frame 14 is movable relative to the main frame 13 . In other words, the sub-frame 14 may be disposed within the main frame 13 to be spaced apart from the main frame 13 .

子框架14可以包括圆筒形的第一主体部分141以及从第一主体部分141 的下端表面向下突出的圆筒形的第二主体部分142。在子框架14的第一主体部分141的外周表面和主框架13的第一主体部分131的内周表面之间以及在子框架14的第二主体部分142的内周表面和主框架13的第四主体部分 134的外周表面之间,子框架14可以以一间隙布置在由绕动涡旋件12和主框架13围绕的空间中,在该间隙中子框架14仅在旋转轴23的轴向方向上关于主框架13可移动。The sub-frame 14 may include a cylindrical first body part 141 and a cylindrical second body part 142 protruding downward from a lower end surface of the first body part 141 . Between the outer peripheral surface of the first body portion 141 of the sub-frame 14 and the inner peripheral surface of the first body portion 131 of the main frame 13 and between the inner peripheral surface of the second body portion 142 of the sub-frame 14 and the second body of the main frame 13 Between the outer peripheral surfaces of the four main body portions 134, the subframe 14 may be arranged in a space surrounded by the orbiting scroll 12 and the main frame 13 with a gap in which the subframe 14 is only in the axial direction of the rotating shaft 23. Directionally movable with respect to the main frame 13 .

此外,在由主框架13的第四主体部分134和子框架14的第一主体部分 141形成的部分以及由主框架13的第一主体部分131和子框架14的第一主体部分141形成的部分中,形成从上端表面向下凹陷的第一凹槽141a和第二凹槽141b。在径向方向上,第一凹槽141a形成在中心部分中,第二凹槽 141b形成在第一凹槽141a和突起131a之间。此外,绕动涡旋件12的主体部分123被插入到第一凹槽141a中。在第二凹槽141b中,防止绕动涡旋件 12枢转的奥尔德姆环15布置在主框架13和绕动涡旋件12之间。Furthermore, in the portion formed by the fourth main body portion 134 of the main frame 13 and the first main body portion 141 of the sub frame 14 and the portion formed by the first main body portion 131 of the main frame 13 and the first main body portion 141 of the sub frame 14, A first groove 141 a and a second groove 141 b recessed downward from the upper end surface are formed. In the radial direction, a first groove 141a is formed in the central portion, and a second groove 141b is formed between the first groove 141a and the protrusion 131a. In addition, the main body portion 123 of the orbiting scroll 12 is inserted into the first groove 141a. In the second groove 141b, the Oldham ring 15 that prevents the orbiting scroll 12 from pivoting is disposed between the main frame 13 and the orbiting scroll 12.

此外,在上述压缩部分10中,形成排出在压缩室16中压缩的制冷剂的排出通道。对于配置为排出高压力的制冷剂的排出通道,其一端连接到板112 的通孔112a(该通孔112a配置为从由固定涡旋件11和绕动涡旋件12围绕的空间排出高压力的制冷剂),其另一端连接到在壳体30中低于主框架13 的空间并且还连接到腔室121a。对于配置为排出中间压力的制冷剂的排出通道,其一端连接到排出口(该排出口配置为将中间压力制冷剂从由固定涡旋件11和绕动涡旋件12围绕的空间排出),其另一端连接到腔室121b和142a。Further, in the above-described compression portion 10 , a discharge passage for discharging the refrigerant compressed in the compression chamber 16 is formed. As for the discharge channel configured to discharge high-pressure refrigerant, one end thereof is connected to the through hole 112a of the plate 112 (the through hole 112a is configured to discharge high-pressure refrigerant from the space surrounded by the fixed scroll 11 and the orbiting scroll 12). refrigerant), the other end of which is connected to the space below the main frame 13 in the case 30 and is also connected to the chamber 121a. As for the discharge passage configured to discharge intermediate-pressure refrigerant, one end thereof is connected to a discharge port configured to discharge intermediate-pressure refrigerant from a space surrounded by the fixed scroll 11 and the orbiting scroll 12, Its other end is connected to chambers 121b and 142a.

接下来,将描述驱动电机20。Next, the drive motor 20 will be described.

驱动电机20在压缩部分10下面固定到壳体30。驱动电机20可以包括构成定子的定子21、构成转子的转子22、支撑转子22并相对于壳体30旋转的旋转轴23以及可旋转地支撑旋转轴23的支撑构件24。The drive motor 20 is fixed to the housing 30 below the compression portion 10 . The driving motor 20 may include a stator 21 constituting a stator, a rotor 22 constituting a rotor, a rotation shaft 23 supporting the rotor 22 and rotating relative to the case 30 , and a support member 24 rotatably supporting the rotation shaft 23 .

定子21可以包括定子主体211和绕定子主体211缠绕的线圈212。定子主体211是其中层叠多个电钢板的层叠体,并具有近似圆筒形。定子主体211 的外周表面的直径形成为大于随后描述的壳体30的中央壳体31的内周表面的直径。定子主体211(定子21)被强制地插入到中央壳体31中。将定子主体211插入到中央壳体31的方法可以采用收缩配合或压配合方法。The stator 21 may include a stator body 211 and a coil 212 wound around the stator body 211 . The stator main body 211 is a laminated body in which a plurality of electrical steel sheets are laminated, and has an approximately cylindrical shape. The diameter of the outer peripheral surface of the stator main body 211 is formed larger than the diameter of the inner peripheral surface of the center case 31 of the case 30 described later. The stator main body 211 (stator 21 ) is forcibly inserted into the center case 31 . A method of inserting the stator main body 211 into the center case 31 may employ a shrink fit or a press fit method.

此外,定子主体211在面向转子22的外周的内侧部分上具有在周向上的多个齿。线圈212布置在形成于相邻的齿之间的狭槽中。在根据一实施方式的定子21中,其中线圈212被插入到位于多个相邻的齿之间的狭槽中的集中绕组(concentrated winding)将作为线圈212的示例被描述。In addition, the stator main body 211 has a plurality of teeth in the circumferential direction on an inner portion facing the outer circumference of the rotor 22 . The coil 212 is arranged in a slot formed between adjacent teeth. In the stator 21 according to an embodiment, concentrated winding in which the coil 212 is inserted into a slot positioned between a plurality of adjacent teeth will be described as an example of the coil 212 .

转子22是层叠体,其中层叠具有环形的多个电工钢片,并具有近似圆筒形。转子22的内周表面的直径形成为小于旋转轴23的外周表面的直径。转子22被强制地插入到旋转轴23。用于将转子22插入到旋转轴23的方法可以采用压配合方法。转子22被固定到旋转轴23并与旋转轴23一起旋转。此外,其中一个永磁体嵌入其中的转子作为转子22的示例被描述。The rotor 22 is a laminated body in which a plurality of electrical steel sheets having a ring shape are laminated, and has an approximately cylindrical shape. The diameter of the inner peripheral surface of the rotor 22 is formed smaller than the diameter of the outer peripheral surface of the rotary shaft 23 . The rotor 22 is forcibly inserted into the rotating shaft 23 . A method for inserting the rotor 22 into the rotary shaft 23 may employ a press-fit method. The rotor 22 is fixed to the rotary shaft 23 and rotates together with the rotary shaft 23 . In addition, a rotor in which one permanent magnet is embedded is described as an example of the rotor 22 .

转子22的外周表面的直径小于定子21的定子主体211的内周表面的直径,并且在转子22和定子21之间形成间隙。The diameter of the outer peripheral surface of the rotor 22 is smaller than the diameter of the inner peripheral surface of the stator main body 211 of the stator 21 , and a gap is formed between the rotor 22 and the stator 21 .

旋转轴23可以包括:主轴231,转子22装配到主轴231并且联接到主轴231;以及偏心轴232,提供在主轴231的上部上并具有从主轴231的轴线偏心的轴线。The rotary shaft 23 may include: a main shaft 231 to which the rotor 22 is fitted and coupled; and an eccentric shaft 232 provided on an upper portion of the main shaft 231 and having an axis eccentric from the axis of the main shaft 231 .

主轴231的下部由支撑构件24可旋转地支撑,主轴231的上部由压缩部分10的主框架13可旋转地支撑。偏心轴232由绕动涡旋件12的主体部分123可旋转地支撑。A lower portion of the main shaft 231 is rotatably supported by the supporting member 24 , and an upper portion of the main shaft 231 is rotatably supported by the main frame 13 of the compression part 10 . The eccentric shaft 232 is rotatably supported by the main body portion 123 of the orbiting scroll 12 .

旋转轴23提供有在轴向方向上穿过旋转轴23的通孔233。在旋转轴23 中,允许通孔233与支撑构件24的轴承连通的第一连通孔234、允许通孔 233与主框架13的轴承连通的第二连通孔235以及允许通孔233与主体部分 123的轴承连通的第三连通孔236形成在径向方向上。The rotary shaft 23 is provided with a through hole 233 passing through the rotary shaft 23 in the axial direction. In the rotating shaft 23, the first communication hole 234 allowing the through hole 233 to communicate with the bearing of the support member 24, the second communication hole 235 allowing the through hole 233 to communicate with the bearing of the main frame 13, and the second communication hole 235 allowing the through hole 233 to communicate with the main body portion 123 The third communication hole 236 through which the bearing communicates is formed in the radial direction.

支撑构件24包括圆筒形的第一主体部分241和从第一主体部分241的下端向下突出的圆筒形的第二主体部分242。支撑构件24以这样的方式固定到中央壳体31,使得第一主体部分241的外周表面面对随后描述的壳体30 的中央壳体31的内周表面。此外,旋转轴23被插入到第一主体部分241和第二主体部分242的内部中,轴颈轴承插置在它们之间。如上所述,支撑构件24用作可旋转地支撑旋转轴23的轴承。The support member 24 includes a cylindrical first body portion 241 and a cylindrical second body portion 242 protruding downward from a lower end of the first body portion 241 . The support member 24 is fixed to the center case 31 in such a manner that the outer peripheral surface of the first body portion 241 faces the inner peripheral surface of the center case 31 of the case 30 described later. Further, the rotating shaft 23 is inserted into the inside of the first body portion 241 and the second body portion 242 with a journal bearing interposed therebetween. As described above, the support member 24 functions as a bearing that rotatably supports the rotary shaft 23 .

此外,在第一主体部分241中,形成允许比第一主体部分241高的空间与比第一主体部分241低的空间连通的孔和凹槽。Further, in the first body portion 241 , holes and grooves that allow a space higher than the first body portion 241 to communicate with a space lower than the first body portion 241 are formed.

泵送润滑剂的泵243被安装到支撑构件24的第二主体部分242的下端。A pump 243 that pumps lubricant is mounted to the lower end of the second body portion 242 of the support member 24 .

接下来,将描述壳体30。Next, the casing 30 will be described.

壳体30可以包括:中央壳体31,在垂直方向上布置在中心并具有圆筒形状;上壳体32,覆盖中央壳体31的上开口;以及下壳体33,覆盖中央壳体31的下开口。此外,壳体30可以包括排出部分34和吸入部分35,该排出部分34将由压缩部分10压缩的高压力制冷剂排出到壳体30的外部,该吸入部分35从壳体30的外部吸入制冷剂。The housing 30 may include: a central housing 31 arranged at the center in the vertical direction and having a cylindrical shape; an upper housing 32 covering an upper opening of the central housing 31; and a lower housing 33 covering an opening of the central housing 31. Lower the opening. In addition, the case 30 may include a discharge part 34 that discharges the high-pressure refrigerant compressed by the compression part 10 to the outside of the case 30 , and a suction part 35 that sucks the refrigerant from the outside of the case 30 . .

如上所述,压缩部分10的主框架13以及驱动电机20的定子21和支撑构件24被固定到中央壳体31。通过将管子插入到形成在中央壳体31中的通孔中,提供排出部分34和吸入部分35。吸入部分35安装在与形成在固定涡旋件11的主体部分111中的通孔111a对应的位置。吸入部分35将制冷剂从壳体30的外部吸入到由固定涡旋件11和绕动涡旋件12围绕的空间中。As described above, the main frame 13 of the compression section 10 and the stator 21 and the supporting member 24 of the drive motor 20 are fixed to the center case 31 . A discharge portion 34 and a suction portion 35 are provided by inserting pipes into through holes formed in the center case 31 . The suction portion 35 is installed at a position corresponding to the through hole 111 a formed in the body portion 111 of the fixed scroll 11 . The suction portion 35 sucks refrigerant from the outside of the housing 30 into a space surrounded by the fixed scroll 11 and the orbiting scroll 12 .

下壳体33形成为碗形状,因此可以收集润滑剂。The lower case 33 is formed in a bowl shape so that lubricant can be collected.

接下来,将描述涡旋式压缩机1的操作。Next, the operation of the scroll compressor 1 will be described.

当涡旋式压缩机1的驱动电机20驱动时,旋转轴23旋转,并且装配在旋转轴23的偏心轴232中的绕动涡旋件12绕固定涡旋件11绕动。由于绕动涡旋件12绕固定涡旋件11绕动,低压力制冷剂通过吸入部分35从壳体 30的外部吸入到由固定涡旋件11和绕动涡旋件12围绕的空间中。根据压缩室16的体积变化,制冷剂被压缩。压缩室16中的高压力制冷剂被排出到压缩部分10的下侧。When the driving motor 20 of the scroll compressor 1 is driven, the rotary shaft 23 rotates, and the orbiting scroll 12 fitted in the eccentric shaft 232 of the rotary shaft 23 orbits around the fixed scroll 11 . As the orbiting scroll 12 orbits around the fixed scroll 11, low-pressure refrigerant is sucked from the outside of the casing 30 into a space surrounded by the fixed scroll 11 and the orbiting scroll 12 through the suction portion 35. The refrigerant is compressed according to the volume change of the compression chamber 16 . The high-pressure refrigerant in the compression chamber 16 is discharged to the lower side of the compression part 10 .

排出到压缩部分10的下侧的高压力制冷剂通过提供在壳体30中的排出部分34被排出到壳体30的外部。在被排出到壳体30的外部的过程中,高压力制冷剂分布到转子22和定子21之间的间隙以及定子21和中央壳体31 之间的间隙。在制冷剂回路中的冷凝、膨胀和蒸发的每个操作之后,排出到壳体30的外部的高压力制冷剂被再次吸入到吸入部分35中。The high-pressure refrigerant discharged to the lower side of the compression part 10 is discharged to the outside of the case 30 through the discharge part 34 provided in the case 30 . In being discharged to the outside of the case 30 , the high-pressure refrigerant is distributed to the gap between the rotor 22 and the stator 21 and the gap between the stator 21 and the center case 31 . After each operation of condensation, expansion, and evaporation in the refrigerant circuit, the high-pressure refrigerant discharged to the outside of the case 30 is sucked into the suction part 35 again.

另一方面,储存在壳体30的下壳体33中的润滑剂被泵243泵送上来,并通过形成在旋转轴23中的通孔233升高。升高的润滑剂通过形成在旋转轴23中的第一连通孔234、第二连通孔235和第三连通孔236被供应到旋转轴23的每个轴承,或者被供应到压缩部分10的滑动构件。被供应到压缩部分10的滑动构件的润滑剂或通过第二连通孔235和第三连通孔236供应到旋转轴23的轴承的润滑剂通过形成在主框架13中的连通孔131e和凹槽 131b、转子22和定子21之间的间隙以及形成在支撑构件24中的轴向孔而返回到下壳体33,然后储存在壳体30的下部中。在此过程中并且在高压力制冷剂在被排出到壳体30的外部之前被分配到转子22和定子21之间的间隙的过程中,润滑剂和制冷剂流入低压力侧,同时冷却驱动电机20。已经与高压力制冷剂一起分配的润滑剂与制冷剂分离,然后储存在壳体30的下部中。On the other hand, the lubricant stored in the lower case 33 of the case 30 is pumped up by the pump 243 and raised through the through hole 233 formed in the rotation shaft 23 . The raised lubricant is supplied to each bearing of the rotary shaft 23 through the first communication hole 234 , the second communication hole 235 , and the third communication hole 236 formed in the rotary shaft 23 , or to the sliding portion of the compression portion 10 . member. The lubricant supplied to the sliding member of the compression portion 10 or the lubricant supplied to the bearing of the rotary shaft 23 through the second communication hole 235 and the third communication hole 236 passes through the communication hole 131e and the groove 131b formed in the main frame 13 , the gap between the rotor 22 and the stator 21 and the axial hole formed in the support member 24 are returned to the lower case 33 , and then stored in the lower portion of the case 30 . During this process and while the high-pressure refrigerant is distributed into the gap between the rotor 22 and the stator 21 before being discharged to the outside of the housing 30, the lubricant and refrigerant flow into the low-pressure side while cooling the drive motor 20. The lubricant that has been dispensed with the high-pressure refrigerant is separated from the refrigerant and then stored in the lower portion of the case 30 .

如上所述,在根据一实施方式的涡旋式压缩机1中,支撑绕动涡旋件12 的子框架14布置在由绕动涡旋件12和主框架13围绕的空间中。As described above, in the scroll compressor 1 according to an embodiment, the sub-frame 14 supporting the orbiting scroll 12 is disposed in a space surrounded by the orbiting scroll 12 and the main frame 13 .

由于常规的涡旋式压缩机不提供有子框架14,所以从由吸入部分35吸入的制冷剂施加到绕动涡旋件12的力矩负载被固定涡旋件11中的上推力负载和绕动涡旋件12中的背压力负载抵消。然而,在根据一实施方式的绕动涡旋件12中,从由吸入部分35吸入的制冷剂施加到绕动涡旋件12的力矩负载FM被固定涡旋件11中的上推力反作用力FU和子框架14中的下表面推力反作用力FL抵消。Since the conventional scroll compressor is not provided with the subframe 14, the moment load applied to the orbiting scroll 12 from the refrigerant sucked by the suction portion 35 is replaced by the upper thrust load and the orbiting scroll in the fixed scroll 11. Back pressure loads in scroll 12 cancel out. However, in the orbiting scroll 12 according to an embodiment, the moment load F M applied to the orbiting scroll 12 from the refrigerant sucked by the suction portion 35 is counteracted by the upward thrust reaction force in the fixed scroll 11 . F U and the lower surface thrust reaction force F L in the subframe 14 cancel.

在这种情况下,由于从上表面推力反作用力FU的操作点到下表面推力反作用力FL的操作点的距离变长,所以允许下表面推力反作用力FL小于常规涡旋式压缩机的后表面负载。此外,允许上表面推力反作用力FU小。因此,根据一实施方式的涡旋式压缩机1通过减小固定涡旋件11和绕动涡旋件12之间的摩擦损失来提高效率,并通过减小绕动涡旋件12的板121的上表面和下表面滑动部分上的负载来提高可靠性。In this case, since the distance from the operating point of the upper surface thrust reaction force FU to the operating point of the lower surface thrust reaction force FL becomes longer, the lower surface thrust reaction force FL is allowed to be smaller than that of the conventional scroll compressor rear surface load. In addition, the upper surface thrust reaction force F U is allowed to be small. Therefore, the scroll compressor 1 according to an embodiment improves efficiency by reducing friction loss between the fixed scroll 11 and the orbiting scroll 12 , and by reducing the plate 121 of the orbiting scroll 12 . The load on the sliding part of the upper surface and the lower surface improves reliability.

接下来,将描述根据一实施方式的涡旋式压缩机1的变型。Next, a modification of the scroll compressor 1 according to an embodiment will be described.

图2是根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图。2 is an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure.

根据涡旋式压缩机1的一变型,压缩部分10可以包括如图1所示的固定涡旋件11、绕动涡旋件12、主框架13、子框架14和奥尔德姆环。此外,配置为密封主框架13的第四主体部分134和绕动涡旋件12的主体部分123 之间的间隙的密封构件123c和123d提供在绕动涡旋件12的主体部分123 中。也就是,密封构件123c和123d可以提供在绕动涡旋件12的主体部分 123和主框架13的第四主体部分134之间。根据该变型,由于提供了密封构件123c和123d,所以可以将腔室121a的内部保持在高压力。此外,作为第一密封构件的示例的密封构件141c和141d提供在子框架14的第一主体部分141中以密封子框架14的第一主体部分141和主框架13的第一主体部分 131之间的间隙(在子框架14和主框架13之间的第一间隙),并且同时,作为第二密封构件的示例的密封构件142c和142d提供在子框架14的第二主体部分142中以密封子框架14的第二主体部分142和主框架13的第四主体部分134之间的间隙(在子框架14和主框架13之间的第二间隙)。因此,根据一变型,通过提供密封构件141c、141d、142c和142d,可以将腔室142a 的压力保持在特定的中间压力。According to a modification of the scroll compressor 1 , the compression part 10 may include a fixed scroll 11 , an orbiting scroll 12 , a main frame 13 , a subframe 14 and an Oldham ring as shown in FIG. 1 . In addition, sealing members 123 c and 123 d configured to seal a gap between the fourth body portion 134 of the main frame 13 and the body portion 123 of the orbiting scroll 12 are provided in the body portion 123 of the orbiting scroll 12 . That is, the sealing members 123c and 123d may be provided between the main body portion 123 of the orbiting scroll 12 and the fourth main body portion 134 of the main frame 13. Referring to FIG. According to this modification, since the sealing members 123c and 123d are provided, it is possible to keep the inside of the chamber 121a at a high pressure. In addition, sealing members 141c and 141d as examples of first sealing members are provided in the first body portion 141 of the sub-frame 14 to seal between the first body portion 141 of the sub-frame 14 and the first body portion 131 of the main frame 13 gap (the first gap between the subframe 14 and the main frame 13), and at the same time, sealing members 142c and 142d as an example of a second sealing member are provided in the second main body portion 142 of the subframe 14 to seal the subframe. The gap between the second body portion 142 of the frame 14 and the fourth body portion 134 of the main frame 13 (the second gap between the sub frame 14 and the main frame 13 ). Therefore, according to a modification, by providing the sealing members 141c, 141d, 142c and 142d, the pressure of the chamber 142a can be maintained at a certain intermediate pressure.

此外,根据一变型,提供了配置为密封子框架14和主框架13之间的间隙的密封构件141c、141d、142c和142d。然而,应当理解,提供了配置为密封子框架14和面对子框架14的至少一个构件之间的间隙的密封构件。Furthermore, according to a modification, sealing members 141c, 141d, 142c, and 142d configured to seal gaps between the sub-frame 14 and the main frame 13 are provided. However, it should be understood that a sealing member configured to seal a gap between the subframe 14 and at least one member facing the subframe 14 is provided.

图3示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图。3 illustrates an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure.

对于根据涡旋式压缩机1的变型的压缩部分10,与根据如图2所示的变型的涡旋式压缩机1的压缩部分10相比,子框架14的外径增大。由于奥尔德姆环15径向向内移动,所以子框架14的第一主体部分141支撑绕动涡旋件12的位置径向向外移动。根据一变型,由于从上推力反作用力的操作点到下推力反作用力的操作点的距离变得增大,所以可以减小上推力反作用力和下推力反作用力。With the compression portion 10 according to the modification of the scroll compressor 1 , the outer diameter of the subframe 14 is increased compared to the compression portion 10 according to the modification of the scroll compressor 1 shown in FIG. 2 . As the Oldham ring 15 moves radially inward, the position where the first body portion 141 of the sub-frame 14 supports the orbiting scroll 12 moves radially outward. According to a modification, since the distance from the operating point of the upper thrust reaction force to the operating point of the lower thrust reaction force becomes larger, the upper thrust reaction force and the lower thrust reaction force can be reduced.

图4示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图。4 illustrates an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure.

对于根据涡旋式压缩机1的变型的压缩部分10,与根据如图3所示的变型的涡旋式压缩机1的压缩部分10相比,引导构件134g和134h提供在主框架13的第四主体部分134中。轨道可以作为引导构件的示例被描述。替代地,在轨道上滚动的轮子可以被使用并提供在子框架14中。根据变型,由于引导构件134g和134h提供在主框架13的第四主体134中,所以子框架14可以不倾斜并仅在旋转轴23的轴向方向上可移动。With the compression portion 10 according to the modification of the scroll compressor 1, compared with the compression portion 10 according to the modification of the scroll compressor 1 shown in FIG. Four main body parts 134 . A rail can be described as an example of a guide member. Alternatively, wheels rolling on rails may be used and provided in the subframe 14 . According to a modification, since the guide members 134g and 134h are provided in the fourth body 134 of the main frame 13 , the sub-frame 14 may not be inclined and be movable only in the axial direction of the rotation shaft 23 .

图5示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图。5 illustrates an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure.

对于根据涡旋式压缩机1的变型的压缩部分10,配置为密封子框架14 的第一主体部分141和绕动涡旋件12的板121之间的间隙的密封构件141e 和141f提供在子框架14的第一主体部分141中,代替根据如图2所示的变型的涡旋式压缩机1的压缩部分10中的配置为密封子框架14的第二主体部分142和主框架13的第四主体部分134之间的间隙的密封构件142c和142d。根据变型,由于提供了密封构件141c、141d、141e和141f,所以通过将腔室142a的制冷剂移动到腔室121b,可以将腔室121b的内部的压力保持在与腔室142a的内部的压力相同的特定中间压力。With the compression portion 10 according to the modification of the scroll compressor 1, sealing members 141e and 141f configured to seal the gap between the first body portion 141 of the subframe 14 and the plate 121 of the orbiting scroll 12 are provided on the subframe. In the first body portion 141 of the frame 14, instead of the second body portion 142 configured to seal the sub-frame 14 and the first body portion 142 of the main frame 13 in the compression portion 10 of the scroll compressor 1 according to the modification shown in FIG. The gaps between the four body parts 134 are sealed by members 142c and 142d. According to a modification, since the sealing members 141c, 141d, 141e, and 141f are provided, by moving the refrigerant of the chamber 142a to the chamber 121b, the pressure inside the chamber 121b can be kept at the same pressure as the inside of the chamber 142a. Same specific intermediate pressure.

此外,在变型中,提供配置为密封子框架14和主框架13之间的间隙的密封构件141c和141d以及配置为密封子框架14和绕动涡旋件12之间的间隙的密封构件141e和141f。然而,应当理解,提供了配置为密封子框架14 和面对子框架14的至少一个构件之间的间隙的密封构件。Furthermore, in a modification, seal members 141c and 141d configured to seal the gap between the subframe 14 and the main frame 13 and seal members 141e and 141e configured to seal the gap between the subframe 14 and the orbiting scroll 12 are provided. 141f. However, it should be understood that a sealing member configured to seal a gap between the subframe 14 and at least one member facing the subframe 14 is provided.

如上所述,根据一实施方式,配置为支撑绕动涡旋件12的子框架14提供在由绕动涡旋件12、旋转轴23和主框架13围绕的空间中以关于主框架 13仅在旋转轴23的轴向方向上可移动。因此,无论位置如何,从子框架14 施加到绕动涡旋件12的压力可以被均衡,并且可以减小用于稳定绕动涡旋件12的推力负载,从而提高涡旋式压缩机1的效率和可靠性。As described above, according to an embodiment, the subframe 14 configured to support the orbiting scroll 12 is provided in a space surrounded by the orbiting scroll 12 , the rotating shaft 23 and the main frame 13 so as to The rotary shaft 23 is movable in the axial direction. Therefore, regardless of the position, the pressure applied from the subframe 14 to the orbiting scroll 12 can be equalized, and the thrust load for stabilizing the orbiting scroll 12 can be reduced, thereby improving the performance of the scroll compressor 1. efficiency and reliability.

此外,在一实施方式中,子框架14配置为关于主框架13仅在沿着旋转轴23的方向上可移动。然而,它并不表示,除了关于主框架13在沿着旋转轴23的方向上的移动,子框架14根本不移动。除了在旋转轴23的方向上的移动之外,当在绕旋转轴23的旋转当中不允许绕垂直于旋转轴23的轴线的旋转时,可以允许在沿着垂直于旋转轴23的轴线的方向上的移动以及关于垂直于旋转轴23的轴线的旋转、其它运动或旋转。此外,应当理解,子框架14可以关于主框架13在沿着旋转轴23的方向上可移动。此外,子框架14可以关于主框架13在一个方向上可移动。Furthermore, in one embodiment, the sub-frame 14 is configured to be movable only in a direction along the rotation axis 23 with respect to the main frame 13 . However, it does not mean that the sub-frame 14 does not move at all except with respect to the movement of the main frame 13 in the direction along the rotation axis 23 . In addition to movement in the direction of the rotation shaft 23, when rotation about an axis perpendicular to the rotation shaft 23 is not permitted among rotations around the rotation shaft 23, movement in a direction along an axis perpendicular to the rotation shaft 23 may be allowed. Movement on and rotation about an axis perpendicular to the axis of rotation 23, other motions or rotations. Furthermore, it should be understood that the sub-frame 14 may be movable in a direction along the rotation axis 23 with respect to the main frame 13 . In addition, the sub-frame 14 may be movable in one direction with respect to the main frame 13 .

图6示出根据本公开的一实施方式的涡旋式压缩机的轴向剖视图。FIG. 6 illustrates an axial sectional view of a scroll compressor according to an embodiment of the present disclosure.

涡旋式压缩机2是广泛用于空调、冰箱和热泵的压缩机。图6示出在空调的制冷剂回路中使用的气密涡旋式压缩机的纵向剖视图。The scroll compressor 2 is a compressor widely used in air conditioners, refrigerators, and heat pumps. Fig. 6 shows a longitudinal sectional view of a hermetic scroll compressor used in a refrigerant circuit of an air conditioner.

涡旋式压缩机2包括:压缩部分10,配置为压缩制冷剂;驱动电机20,配置为驱动压缩部分10;以及壳体30,与配置为接收压缩部分10和驱动电机20的主体相对应。根据一实施方式,涡旋式压缩机2是垂直涡旋式压缩机,其中驱动电机20的旋转轴23(将在后面描述)的轴向方向与重力方向一致。在下文,旋转轴23的轴向方向将被称为“垂直方向”,并且基于图6,较高侧可以被称为“上侧”,较低侧可以被称为“下侧”。尽管垂直涡旋式压缩机作为示例被描述,但是本公开的实施方式将可应用于水平涡旋式压缩机。The scroll compressor 2 includes: a compression part 10 configured to compress refrigerant; a driving motor 20 configured to drive the compression part 10 ; and a housing 30 corresponding to a body configured to receive the compression part 10 and the driving motor 20 . According to an embodiment, the scroll compressor 2 is a vertical scroll compressor in which an axial direction of a rotating shaft 23 (to be described later) of a drive motor 20 coincides with a gravity direction. Hereinafter, the axial direction of the rotation shaft 23 will be referred to as "vertical direction", and based on FIG. 6 , the higher side may be referred to as "upper side" and the lower side may be referred to as "lower side". Although a vertical scroll compressor is described as an example, embodiments of the present disclosure will be applicable to a horizontal scroll compressor.

首先,将描述压缩部分10。First, the compression section 10 will be described.

压缩部分10可以包括:固定到壳体30的固定涡旋件11;绕动涡旋件 12,通过与固定涡旋件11接合而绕动;主框架13,固定到壳体30并配置为支撑固定涡旋件11;子框架14,布置在旋转轴23和主框架13之间并配置为支撑绕动涡旋件12;以及奥尔德姆环15,配置为允许绕动涡旋件12绕动而不使绕动涡旋件12枢转。The compression part 10 may include: a fixed scroll 11 fixed to the housing 30; an orbiting scroll 12 orbiting by being engaged with the fixed scroll 11; a main frame 13 fixed to the housing 30 and configured to support the fixed scroll 11; the subframe 14 arranged between the rotary shaft 23 and the main frame 13 and configured to support the orbiting scroll 12; and the Oldham ring 15 configured to allow the orbiting scroll 12 to orbit move without pivoting the orbiting scroll 12.

固定涡旋件11可以包括固定涡旋件主体和从固定涡旋件主体突出的固定卷体114。固定卷体114可以从固定涡旋件主体向下突出。The fixed scroll 11 may include a fixed scroll body and a fixed wrap 114 protruding from the fixed scroll body. The fixed wrap 114 may protrude downwardly from the fixed scroll body.

固定涡旋件主体可以包括:圆筒形主体部分111;板112,配置为覆盖主体部分111的上侧中的开口;以及突起113,从主体部分111的下端在径向向外的方向上延伸。固定卷体114可以从板112的下端向下突出并且当从底部观看时具有螺旋形状。The fixed scroll body may include: a cylindrical body portion 111; a plate 112 configured to cover an opening in an upper side of the body portion 111; and a protrusion 113 extending in a radially outward direction from a lower end of the body portion 111. . The fixed roll 114 may protrude downward from the lower end of the plate 112 and have a spiral shape when viewed from the bottom.

固定涡旋件11可以由铸铁形成,诸如灰色铸铁FC 250。The fixed scroll 11 may be formed from cast iron, such as gray cast iron FC 250 .

主体部分111可以在径向方向上提供有通孔111a。通孔111a可以用作吸入口,该吸入口配置为将制冷剂吸入到由主体部分111、板112和绕动涡旋件12围绕的空间中。The body part 111 may be provided with a through hole 111a in a radial direction. The through hole 111 a may serve as a suction port configured to suck refrigerant into a space surrounded by the main body portion 111 , the plate 112 and the orbiting scroll 12 .

在垂直方向上的通孔112a形成在板112的中心处。通孔112a可以用作排出口,该排出口配置为将制冷剂从由板112、固定涡旋件114和绕动涡旋件12围绕的空间排出。A through hole 112 a in the vertical direction is formed at the center of the board 112 . The through hole 112 a may serve as a discharge port configured to discharge refrigerant from a space surrounded by the plate 112 , the fixed scroll 114 and the orbiting scroll 12 .

如上所述构造的固定涡旋件11通过诸如螺栓的定位机构或穿过在垂直方向上形成在突起113中的通孔的定位销而被固定到主框架13。The fixed scroll 11 configured as described above is fixed to the main frame 13 by a positioning mechanism such as a bolt or a positioning pin passing through a through hole formed in the protrusion 113 in the vertical direction.

绕动涡旋件12可以包括绕动涡旋件主体和绕动卷体122,该绕动卷体 122从绕动涡旋件主体突出以通过与固定涡旋件11的固定卷体114接合而形成压缩室16。绕动卷体122可以从绕动涡旋件主体向上突出。The orbiting scroll 12 may include an orbiting scroll main body and an orbiting wrap 122 protruding from the orbiting scroll main body to engage with the fixed wrap 114 of the fixed scroll 11 . A compression chamber 16 is formed. The orbiting wrap 122 may protrude upward from the orbiting scroll body.

绕动涡旋件主体可以包括具有盘形状的板121以及从板121的下端向下突出的圆筒形主体部分123。绕动卷体122可以从板121的上端向上突出并且当从顶部观看时具有螺旋形状。The orbiting scroll body may include a plate 121 having a disk shape and a cylindrical body portion 123 protruding downward from a lower end of the plate 121 . The winding roll 122 may protrude upward from the upper end of the plate 121 and have a spiral shape when viewed from the top.

绕动涡旋件12可以由FC材料或FCD材料形成。The orbiting scroll 12 may be formed of FC material or FCD material.

绕动涡旋件12的绕动卷体122可以与固定涡旋件11的固定卷体114接合。此外,绕动涡旋件12的绕动卷体122和固定涡旋件11的固定卷体114 可以放置在由固定涡旋件11的主体部分111和板112以及板121形成的空间中从而形成压缩室16。由于绕动卷体122围绕被固定的固定卷体114圆周地运动,所以压缩室16的体积减小,并且压缩室16的制冷剂被压缩。换句话说,当固定卷体114和绕动卷体122之间的内部空间被朝向旋转中心减小时,制冷剂被压缩。The orbiting wrap 122 of the orbiting scroll 12 may be engaged with the fixed wrap 114 of the fixed scroll 11 . In addition, the orbiting wrap 122 of the orbiting scroll 12 and the fixed wrap 114 of the fixed scroll 11 may be placed in a space formed by the body portion 111 of the fixed scroll 11 and the plate 112 and the plate 121 to form Compression chamber 16. Since the orbiting coil 122 moves circularly around the fixed fixed coil 114 , the volume of the compression chamber 16 is reduced, and the refrigerant of the compression chamber 16 is compressed. In other words, when the inner space between the fixed wrap 114 and the orbiting wrap 122 is reduced toward the center of rotation, the refrigerant is compressed.

随后描述的旋转轴23的偏心轴232通过滑动轴承被插入到主体部分123 中。因此,主体部分123用作偏心轴232的轴承。An eccentric shaft 232 of the rotating shaft 23 described later is inserted into the main body portion 123 through a sliding bearing. Accordingly, the main body portion 123 serves as a bearing for the eccentric shaft 232 .

主框架13是配置为保持固定涡旋件11的保持构件的示例。主框架13 可以包括圆筒形的第一主体部分131、从第一主体部分131的下端的径向内侧向下突出的圆筒形的第二主体部分132以及从第二主体部分132的下端径向向内突出的圆筒形的第三主体部分133。在第三主体部分133中,可以提供旋转轴23插入到其的通孔133a。主框架13的第一主体部分131的外周表面被固定到壳体30的随后描述的中央壳体31。根据一实施方式,主框架13 不支撑驱动电机20的随后描述的旋转轴23。The main frame 13 is an example of a holding member configured to hold the fixed scroll 11 . The main frame 13 may include a cylindrical first body portion 131 , a cylindrical second body portion 132 protruding downward from a radially inner side of a lower end of the first body portion 131 , and a diameter A cylindrical third body portion 133 protruding inward. In the third body part 133, a through hole 133a into which the rotation shaft 23 is inserted may be provided. The outer peripheral surface of the first main body portion 131 of the main frame 13 is fixed to a later-described center case 31 of the case 30 . According to an embodiment, the main frame 13 does not support a later-described rotating shaft 23 of the driving motor 20 .

在第一主体部分131的外周部分上,安装从上端表面向上突出的突起 131a。在突起131a中形成凹形螺钉,并且穿过形成在固定涡旋件11的突起 113中的通孔的螺栓与该凹形螺钉接合。因此,固定涡旋件11被安装到主框架13。On an outer peripheral portion of the first main body portion 131, a protrusion 131a protruding upward from an upper end surface is installed. A female screw is formed in the protrusion 131a, and a bolt passing through a through hole formed in the protrusion 113 of the fixed scroll 11 is engaged with the female screw. Therefore, the fixed scroll 11 is mounted to the main frame 13 .

在第一主体部分131的外周部分上,可以提供在垂直方向上伸长的凹槽 131b。也就是,在第一主体部分131中,可以形成从外周部分的中心到下部在垂直方向上延伸的凹槽131b。在第一主体部分131中,形成凹槽131b的部分可以与中央壳体31间隔开。On an outer peripheral portion of the first body portion 131, a groove 131b elongated in a vertical direction may be provided. That is, in the first body part 131, a groove 131b extending in a vertical direction from the center to the lower part of the outer peripheral part may be formed. In the first body part 131 , a portion forming the groove 131 b may be spaced apart from the center case 31 .

主框架13还可以包括配置为支撑固定涡旋件11的固定涡旋件支撑表面 11a。固定涡旋件支撑表面11a可以形成在突起131a上。The main frame 13 may further include a fixed scroll support surface 11 a configured to support the fixed scroll 11 . A fixed scroll supporting surface 11a may be formed on the protrusion 131a.

子框架14是用于支撑绕动涡旋件12的支撑构件的示例。间隙可以形成在主框架13和子框架14之间以允许子框架14关于主框架13可移动。换句话说,子框架14可以布置在主框架13内以与主框架13间隔开。The sub-frame 14 is an example of a support member for supporting the orbiting scroll 12 . A gap may be formed between the main frame 13 and the sub frame 14 to allow the sub frame 14 to be movable with respect to the main frame 13 . In other words, the sub-frame 14 may be disposed within the main frame 13 to be spaced apart from the main frame 13 .

子框架14可以包括圆筒形的第一主体部分141、从第一主体部分141 的下端表面向下突出的圆筒形的第二主体部分142以及从第二主体部分142 的内端表面向下突出的圆筒形的第三主体部分143。第三主体部分143可以具有比第一主体部分141和第二主体部分142小的宽度。具体地,第三主体部分143的内周表面的宽度可以小于第一主体部分141的内周表面的宽度和第二主体部分142的内周表面的宽度。第三主体部分143可以被插入到轴通孔133a中以位于旋转轴23和主框架13的第三主体部分133之间。此外,尽管轴颈轴承被插置在其间,但是驱动电机20的后面描述的旋转轴23被插入到第三主体部分143的内部中。因此,子框架14用作可旋转地支撑旋转轴23的轴承。子框架14可以配置为沿着旋转轴23的轴向方向和垂直于旋转轴23的轴向方向的方向中的至少一个关于主框架13可移动。在另一方面,在第一主体部分141的外周表面和主框架13的第一主体部分131的内周表面之间以及在第三主体部分143的外周表面和主框架13的第三主体部分133 的内周表面之间,子框架14可以以一间隙布置在旋转轴23和主框架13之间,该间隙允许子框架14在旋转轴23的轴向方向上关于主框架13可移动并在绕大致垂直于旋转轴23的虚拟轴线的旋转方向上可移动。The sub-frame 14 may include a cylindrical first body portion 141 , a cylindrical second body portion 142 protruding downward from a lower end surface of the first body portion 141 , and a cylindrical second body portion 142 protruding downward from an inner end surface of the second body portion 142 . A protruding cylindrical third body portion 143 . The third body part 143 may have a smaller width than the first body part 141 and the second body part 142 . Specifically, the width of the inner peripheral surface of the third body part 143 may be smaller than the width of the inner peripheral surface of the first body part 141 and the width of the inner peripheral surface of the second body part 142 . The third body part 143 may be inserted into the shaft through hole 133 a to be located between the rotation shaft 23 and the third body part 133 of the main frame 13 . Furthermore, a later-described rotary shaft 23 of the drive motor 20 is inserted into the inside of the third body portion 143 although journal bearings are interposed therebetween. Therefore, the sub-frame 14 functions as a bearing that rotatably supports the rotary shaft 23 . The sub-frame 14 may be configured to be movable with respect to the main frame 13 at least one of an axial direction of the rotation shaft 23 and a direction perpendicular to the axial direction of the rotation shaft 23 . On the other hand, between the outer peripheral surface of the first body portion 141 and the inner peripheral surface of the first body portion 131 of the main frame 13 and between the outer peripheral surface of the third body portion 143 and the third body portion 133 of the main frame 13 Between the inner peripheral surfaces of the inner peripheral surfaces, the sub-frame 14 may be arranged between the rotating shaft 23 and the main frame 13 with a gap that allows the sub-frame 14 to be movable in the axial direction of the rotating shaft 23 with respect to the main frame 13 and to move around the It is movable in a rotational direction substantially perpendicular to an imaginary axis of the rotational shaft 23 .

此外,在由主框架13的第一主体部分131和子框架14的第三主体部分 143形成的部分以及由主框架13的第一主体部分131和子框架14的第一主体部分141形成的部分中,形成从上端表面向下凹陷的第一凹槽141a和第二凹槽141b。在径向方向上,第一凹槽141a形成在中心部分中,第二凹槽 141b形成在第一凹槽141a和突起131a之间。此外,绕动涡旋件12的主体部分123被插入到第一凹槽141a中。在第二凹槽141b中,防止绕动涡旋件 12枢转的奥尔德姆环15布置在主框架13和绕动涡旋件12之间。Furthermore, in the portion formed by the first body portion 131 of the main frame 13 and the third body portion 143 of the sub frame 14 and the portion formed by the first body portion 131 of the main frame 13 and the first body portion 141 of the sub frame 14, A first groove 141 a and a second groove 141 b recessed downward from the upper end surface are formed. In the radial direction, a first groove 141a is formed in the central portion, and a second groove 141b is formed between the first groove 141a and the protrusion 131a. In addition, the main body portion 123 of the orbiting scroll 12 is inserted into the first groove 141a. In the second groove 141b, the Oldham ring 15 that prevents the orbiting scroll 12 from pivoting is disposed between the main frame 13 and the orbiting scroll 12.

此外,在上述压缩部分10中,形成排出在压缩室16中被压缩的制冷剂的排出通道。对于配置为排出高压力制冷剂的排出通道,其一端连接到板112 的通孔112a(该通孔112a配置为将高压力制冷剂从由固定涡旋件11和绕动涡旋件12围绕的空间排出),其另一端连接到壳体30中的低于主框架13 的空间并且还连接到腔室121a。对于配置为排出中间压力制冷剂的排出通道,其一端连接到排出口(该排出口配置为将制冷剂从具有中间压力制冷剂并被固定涡旋件11和绕动涡旋件12围绕的空间排出),其另一端连接到腔室121b和142a。Further, in the above-described compression portion 10 , a discharge passage for discharging the refrigerant compressed in the compression chamber 16 is formed. As for the discharge channel configured to discharge high-pressure refrigerant, one end thereof is connected to the through hole 112a of the plate 112 (the through hole 112a is configured to discharge the high-pressure refrigerant from the fixed scroll 11 and the orbiting scroll 12 surrounding space discharge), the other end of which is connected to the space below the main frame 13 in the casing 30 and also connected to the chamber 121a. As for the discharge passage configured to discharge intermediate-pressure refrigerant, one end thereof is connected to a discharge port (the discharge port is configured to discharge refrigerant from a space having intermediate-pressure refrigerant and surrounded by the fixed scroll 11 and the orbiting scroll 12 discharge), the other end of which is connected to chambers 121b and 142a.

由于驱动电机20和壳体30与先前描述的那些相同,所以将省略其描述。Since the drive motor 20 and the housing 30 are the same as those described previously, descriptions thereof will be omitted.

由于涡旋式压缩机2的操作也与先前描述的操作相同,所以将省略其描述。Since the operation of the scroll compressor 2 is also the same as the previously described operation, description thereof will be omitted.

另一方面,在这样的涡旋式压缩机2中,由于气体的压缩负载,绕动涡旋件12将倾斜。On the other hand, in such a scroll compressor 2, the orbiting scroll 12 will incline due to the compression load of gas.

图7a是示出绕动涡旋件接收的力矩的透视图。如图7a所示,绕动涡旋件12从旋转轴23的主轴231接收来自在一平面上与偏心轴232的偏心方向垂直的方向的压缩负载Ft。因此,在绕动涡旋件12中,产生当从视点A 观看时的顺时针力矩MSFig. 7a is a perspective view showing the torque received by the orbiting scroll. As shown in FIG. 7 a , the orbiting scroll 12 receives a compressive load F t from a direction perpendicular to the eccentric direction of the eccentric shaft 232 on a plane from the main shaft 231 of the rotary shaft 23 . Therefore, in the orbiting scroll 12, a clockwise moment M S when viewed from the viewpoint A is generated.

图7b是示出其中绕动涡旋件将要倾斜的形状的视图。具体地,图7b 是示出当从图7a的视点A观看时绕动涡旋件12将要倾斜的情况的视图。如图7b所示,绕动涡旋件12接收压缩负载Ft并产生顺时针力矩负载,因此绕动涡旋件将要倾斜。Fig. 7b is a view showing a shape in which the orbiting scroll is to be inclined. Specifically, FIG. 7b is a view showing a situation where the orbiting scroll 12 is about to tilt when viewed from the viewpoint A of FIG. 7a. As shown in FIG. 7b, the orbiting scroll 12 receives the compression load Ft and generates a clockwise moment load, so that the orbiting scroll will be inclined.

另外,子框架14从该轴接收横向负载,因此试图在负载方向上移动。In addition, the sub-frame 14 receives lateral loads from this shaft and thus attempts to move in the direction of the load.

图8示出当施加到子框架的力矩在与施加到绕动涡旋件的力矩相同的方向上时压缩部分和旋转轴的轴向剖视图。8 shows an axial sectional view of the compression portion and the rotary shaft when the moment applied to the subframe is in the same direction as that applied to the orbiting scroll.

假设在轴线上的支撑横向负载FMJ的位置关于横向负载FMJ与绕动涡旋件12相反,如图8所示。例如,假设当主框架13的突起135与子框架14 接触时施加到子框架14的反作用力RMJ在如图8所示的位置产生。因此,难以有效地抑制绕动涡旋件12的倾斜,因为施加到子框架14的力矩MF和施加到绕动涡旋件12的力矩MS在顺时针方向上产生。Assume that the position on the axis supporting the lateral load F MJ is opposite to the orbiting scroll 12 with respect to the lateral load F MJ , as shown in FIG. 8 . For example, assume that the reaction force R MJ applied to the sub-frame 14 is generated at a position as shown in FIG. 8 when the protrusion 135 of the main frame 13 is in contact with the sub-frame 14 . Therefore, it is difficult to effectively suppress the inclination of the orbiting scroll 12 because the moment M F applied to the sub-frame 14 and the moment M S applied to the orbiting scroll 12 are generated in the clockwise direction.

因此,根据一实施方式,通过利用横向负载在子框架14中产生在与绕动涡旋件12相反的方向上的力矩来抑制绕动涡旋件12的倾斜。这是允许子框架14在绕与旋转轴23大致正交的虚拟轴线的旋转方向当中的与绕动涡旋件12中产生的力矩相反的方向上可移动的示例。Therefore, according to an embodiment, the inclination of the orbiting scroll 12 is suppressed by generating a moment in the sub-frame 14 in a direction opposite to that of the orbiting scroll 12 by a lateral load. This is an example in which the sub-frame 14 is allowed to be movable in a direction opposite to the moment generated in the orbiting scroll 12 among the rotation directions about the virtual axis substantially orthogonal to the rotation shaft 23 .

图9示出当施加到子框架的力矩在与施加到绕动涡旋件的力矩相反的方向上时压缩部分和旋转轴的轴向剖视图。Fig. 9 shows an axial sectional view of the compression portion and the rotary shaft when the moment applied to the subframe is in a direction opposite to that applied to the orbiting scroll.

根据一实施方式,假设在该轴线上的支撑横向负载FMJ的位置关于横向负载FMJ在与绕动涡旋件12的相同侧,如图9所示。例如,假设,当形成在主框架13的内周表面中的突起136与子框架14接触时施加到子框架14的反作用力RMJ在如图9所示的位置产生。因此,可以有效地抑制绕动涡旋件 12的倾斜,因为施加到子框架14的力矩MF在逆时针方向上产生。这是其中保持构件针对绕动涡旋件接收的负载的反作用力在绕动涡旋件侧的预定位置而不是旋转轴中的接收该负载的位置被接收的示例。产生施加到子框架 14的反作用力RMJ的位置可以在L1和L2之间,如图9所示。L1是绕动涡旋件12侧的子框架14的第三主体部分143的末端表面的位置。当该末端表面倾斜时,它可以是该末端表面的最低位置。L1是在绕动涡旋件侧的支撑构件的旋转轴轴承的末端表面的位置的示例。此外,L2是在其上形成绕动涡旋件12的板121的绕动卷体122的表面的位置。换句话说,绕动涡旋件 12的板121可以包括在其上形成绕动卷体122的绕动卷体形成表面121aa, L2是绕动卷体形成表面121aa的位置。当此表面倾斜时,它可以是该表面的最上面的位置。L2是在其上绕动涡旋件的板与固定涡旋件接合的表面的位置的示例。According to one embodiment, it is assumed that the position on the axis supporting the lateral load F MJ is on the same side as the orbiting scroll 12 with respect to the lateral load F MJ , as shown in FIG. 9 . For example, assume that a reaction force R MJ applied to the sub-frame 14 is generated at a position as shown in FIG. 9 when the protrusion 136 formed in the inner peripheral surface of the main frame 13 comes into contact with the sub-frame 14 . Therefore, the inclination of the orbiting scroll 12 can be effectively suppressed because the moment M F applied to the sub-frame 14 is generated in the counterclockwise direction. This is an example in which the reaction force of the holding member against the load received by the orbiting scroll is received at a predetermined position on the side of the orbiting scroll instead of a position in the rotary shaft that receives the load. The position where the reaction force R MJ applied to the sub-frame 14 is generated may be between L1 and L2 as shown in FIG. 9 . L1 is the position of the tip surface of the third main body portion 143 of the sub-frame 14 on the side of the orbiting scroll 12 . When the end surface is inclined, it may be the lowest position of the end surface. L1 is an example of the position of the tip surface of the rotary shaft bearing of the support member on the side of the orbiting scroll. In addition, L2 is a position on which the surface of the orbiting wrap 122 of the plate 121 of the orbiting scroll 12 is formed. In other words, the plate 121 of the orbiting scroll 12 may include an orbiting wrap forming surface 121aa on which the orbiting wrap 122 is formed, and L2 is a position of the orbiting wrap forming surface 121aa. When the surface is sloped, it may be the uppermost position of the surface. L2 is an example of the position of the surface on which the plate of the orbiting scroll engages with the fixed scroll.

此外,为了在如图9所示的位置产生施加到子框架14的反作用力RMJ,当绕动涡旋件12即将倾斜时,主框架13的第一主体部分131和子框架14 的第一主体部分141可以在主框架13的第三主体部分133和子框架14的第三主体部分143接触之前接触。也就是,当子框架14由于运动而倾斜时,主框架13的突起136和子框架14的第一主体部分141可以在主框架13的第三主体部分133和子框架14的第三主体部分143接触之前接触。更具体地,当支撑绕动涡旋件12的子框架14的推力表面与固定涡旋件11的推力表面大致平行时,主框架13的第一主体部分131和子框架14的第一主体部分141可以在主框架13的第三主体部分133和子框架14的第三主体部分143 接触之前接触。In addition, in order to generate the reaction force R MJ applied to the sub-frame 14 at the position shown in FIG. The portion 141 may be in contact before the third body portion 133 of the main frame 13 and the third body portion 143 of the sub frame 14 are in contact. That is, when the sub-frame 14 is tilted due to movement, the protrusion 136 of the main frame 13 and the first main body portion 141 of the sub-frame 14 may contact the third main body portion 133 of the main frame 13 and the third main body portion 143 of the sub-frame 14 touch. More specifically, when the thrust surface of the subframe 14 supporting the orbiting scroll 12 is substantially parallel to the thrust surface of the fixed scroll 11, the first main body portion 131 of the main frame 13 and the first main body portion 141 of the subframe 14 The contact may be made before the third body part 133 of the main frame 13 and the third body part 143 of the sub frame 14 come into contact.

为此,主框架13的第一主体部分131和子框架14的第一主体部分141 之间的间隙小于主框架13的第三主体部分133和子框架14的第三主体部分 143之间的间隙。这是一示例,其中关于接收关于旋转轴的负载的位置,在与绕动涡旋件的相同侧与保持构件的最小间隙小于在与绕动涡旋件的相反侧与保持构件的最小间隙。主框架13的第一主体部分131和子框架14的第一主体部分141之间的间隙的位置可以在L1和L2之间,如图9所示。L1 是绕动涡旋件12侧的子框架14的第三主体部分143的末端表面的位置。当该末端表面倾斜时,它可以是该末端表面的最低位置。L1是绕动涡旋件侧的支撑构件的旋转轴轴承的末端表面的位置的示例。此外,L2是在其上形成绕动涡旋件12的板121的绕动卷体122的表面的位置。当此表面倾斜时,它可以是该表面的最上面的位置。L2是在其上绕动涡旋件的板与固定涡旋件接合的表面的位置的示例。For this, the gap between the first body part 131 of the main frame 13 and the first body part 141 of the sub frame 14 is smaller than the gap between the third body part 133 of the main frame 13 and the third body part 143 of the sub frame 14. This is an example in which the minimum clearance with the retaining member on the same side as the orbiting scroll is smaller than the minimum clearance with the retaining member on the opposite side to the orbiting scroll with respect to the position receiving the load about the rotary shaft. The position of the gap between the first body part 131 of the main frame 13 and the first body part 141 of the sub frame 14 may be between L1 and L2, as shown in FIG. 9 . L1 is the position of the tip end surface of the third body portion 143 of the sub-frame 14 on the side of the orbiting scroll 12 . When the end surface is inclined, it may be the lowest position of the end surface. L1 is an example of the position of the tip end surface of the rotary shaft bearing of the support member on the orbiting scroll side. In addition, L2 is a position on which the surface of the orbiting wrap 122 of the plate 121 of the orbiting scroll 12 is formed. When the surface is sloped, it may be the uppermost position of the surface. L2 is an example of the position of the surface on which the plate of the orbiting scroll engages with the fixed scroll.

此外,根据一实施方式,如图9所示,子框架14可以包括推力轴承144,推力轴承144具有支撑绕动涡旋件12的绕动涡旋件支撑表面144a。推力轴承144可以具有可弹性变形的形状。具体地,子框架14的推力轴承144的外周侧可以倾斜,因此当与绕动涡旋件12的其上没有形成绕动涡旋件12的一个表面接触时,子框架14的推力轴承144可以弹性变形。以这种方式,推力负载被分布以抑制局部接触。然而,图9所示的推力轴承144的形状不限于此,因此推力轴承144可以具有各种形状,只要弹性变形即可。推力轴承144是用于支撑绕动涡旋件的支撑构件的一部分的示例,图9的推力轴承 144的形状是由于绕动涡旋件的倾斜而与一表面接触时弹性变形的形状的示例,在该表面上绕动涡旋件的板没有与固定涡旋件接合。Furthermore, according to an embodiment, as shown in FIG. 9 , the sub-frame 14 may include a thrust bearing 144 having an orbiting scroll supporting surface 144 a supporting the orbiting scroll 12 . The thrust bearing 144 may have an elastically deformable shape. Specifically, the outer peripheral side of the thrust bearing 144 of the sub-frame 14 may be inclined so that when in contact with a surface of the orbiting scroll 12 on which the orbiting scroll 12 is not formed, the thrust bearing 144 of the sub-frame 14 may be Elastic deformation. In this way, thrust loads are distributed to suppress local contact. However, the shape of the thrust bearing 144 shown in FIG. 9 is not limited thereto, and thus the thrust bearing 144 may have various shapes as long as it is elastically deformable. The thrust bearing 144 is an example of a part of the supporting member for supporting the orbiting scroll, and the shape of the thrust bearing 144 of FIG. 9 is an example of a shape elastically deformed when in contact with a surface due to the inclination of the orbiting scroll, The plate of the orbiting scroll does not engage the fixed scroll on this surface.

接下来,将描述根据一实施方式的涡旋式压缩机2的奥尔德姆环15的实现方式。Next, implementation of the Oldham ring 15 of the scroll compressor 2 according to an embodiment will be described.

图10示出根据涡旋式压缩机的一实现示例的压缩部分和旋转轴的轴向剖视图。10 shows an axial sectional view of a compression portion and a rotating shaft according to an implementation example of a scroll compressor.

根据涡旋式压缩机2的一实现方式的压缩部分10可以包括如图1所示的固定涡旋件11、绕动涡旋件12、主框架13、子框架14和奥尔德姆环15。在一实现方式中,奥尔德姆环15联接到绕动涡旋件12和子框架14,或与绕动涡旋件12和子框架14接合。具体地,一对(两件)奥尔德姆环引导槽121g 在绕动涡旋件12的板121的下表面上形成为基本上直线。形成在奥尔德姆环15的环形部分15a的上表面上的一对(两件)键部分15b可以可滑动地联接到奥尔德姆环引导槽121g或与奥尔德姆环引导槽121g接合。此外,具有与绕动涡旋件12的奥尔德姆环引导槽121g约90°的相位差的一对(两件) 奥尔德姆环引导槽141g在子框架14的第一主体部分141的上表面上形成为基本上直线。形成在奥尔德姆环15的环形部分15a的下表面上的一对(两件)键部分15c可以可滑动地联接到奥尔德姆环引导槽141g或与奥尔德姆环引导槽141g接合。通过如上所述配置的奥尔德姆环15,绕动涡旋件12 可以执行绕动运动而不枢转。The compression section 10 according to an implementation of the scroll compressor 2 may include a fixed scroll 11 , an orbiting scroll 12 , a main frame 13 , a subframe 14 and an Oldham ring 15 as shown in FIG. 1 . . In one implementation, the Oldham ring 15 is coupled to, or engaged with, the orbiting scroll 12 and the subframe 14 . Specifically, a pair (two pieces) of Oldham ring guide grooves 121 g are formed in a substantially straight line on the lower surface of the plate 121 of the orbiting scroll 12 . A pair (two pieces) of key portions 15b formed on the upper surface of the ring portion 15a of the Oldham ring 15 can be slidably coupled to the Oldham ring guide groove 121g or with the Oldham ring guide groove 121g. join. In addition, a pair (two pieces) of Oldham ring guide grooves 141g having a phase difference of about 90° from the Oldham ring guide grooves 121g of the orbiting scroll 12 are formed in the first main body portion 141 of the sub-frame 14. The upper surface of is formed as a substantially straight line. A pair (two pieces) of key portions 15c formed on the lower surface of the ring portion 15a of the Oldham ring 15 can be slidably coupled to the Oldham ring guide groove 141g or with the Oldham ring guide groove 141g. join. With the Oldham ring 15 configured as described above, the orbiting scroll 12 can perform an orbiting motion without pivoting.

图11示出根据涡旋式压缩机的一实现方式的压缩部分和旋转轴的轴向剖视图。Fig. 11 shows an axial sectional view of a compression portion and a rotating shaft according to an implementation of a scroll compressor.

根据涡旋式压缩机2的一实现方式的压缩部分10可以包括如图1所示的固定涡旋件11、绕动涡旋件12、主框架13、子框架14和奥尔德姆环15。在一实现方式中,奥尔德姆环15联接到绕动涡旋件12和子框架14,或与绕动涡旋件12和子框架14接合。具体地,一对(两件)奥尔德姆环引导槽121g 在绕动涡旋件12的板121的下表面上形成为基本上直线。形成在奥尔德姆环15的环形部分15a的上表面上的一对(两件)键部分15b可以可滑动地联接到奥尔德姆环引导槽121g或与奥尔德姆环引导槽121g接合。此外,与绕动涡旋件12的奥尔德姆环引导槽121g具有约90°的相位差的一对(两件) 奥尔德姆环引导槽131g在主框架13的第一主体部分131的上表面上形成为基本上直线。形成在奥尔德姆环15的环形部分15a的下表面上的一对(两件)键部分15d可以可滑动地联接到奥尔德姆环引导槽131g或与奥尔德姆环引导槽131g接合。通过如上所述配置的奥尔德姆环15,绕动涡旋件12 可以执行绕动运动而不枢转。The compression section 10 according to an implementation of the scroll compressor 2 may include a fixed scroll 11 , an orbiting scroll 12 , a main frame 13 , a subframe 14 and an Oldham ring 15 as shown in FIG. 1 . . In one implementation, the Oldham ring 15 is coupled to, or engaged with, the orbiting scroll 12 and the subframe 14 . Specifically, a pair (two pieces) of Oldham ring guide grooves 121 g are formed in a substantially straight line on the lower surface of the plate 121 of the orbiting scroll 12 . A pair (two pieces) of key portions 15b formed on the upper surface of the ring portion 15a of the Oldham ring 15 can be slidably coupled to the Oldham ring guide groove 121g or with the Oldham ring guide groove 121g. join. In addition, a pair (two pieces) of Oldham ring guide grooves 131g having a phase difference of about 90° from the Oldham ring guide grooves 121g of the orbiting scroll 12 are formed in the first main body portion 131 of the main frame 13. The upper surface of is formed as a substantially straight line. A pair (two pieces) of key portions 15d formed on the lower surface of the ring portion 15a of the Oldham ring 15 can be slidably coupled to the Oldham ring guide groove 131g or with the Oldham ring guide groove 131g. join. With the Oldham ring 15 configured as described above, the orbiting scroll 12 can perform an orbiting motion without pivoting.

图12示出根据涡旋式压缩机的一实现方式的压缩部分和旋转轴的轴向剖视图。Fig. 12 shows an axial sectional view of a compression portion and a rotating shaft according to an implementation of a scroll compressor.

根据涡旋式压缩机2的一实现方式的压缩部分10可以包括如图1所示的固定涡旋件11、绕动涡旋件12、主框架13、子框架14和奥尔德姆环15。在一实现方式中,奥尔德姆环15联接到绕动涡旋件12和固定涡旋件11,或与绕动涡旋件12和固定涡旋件11接合。具体地,一对(两件)奥尔德姆环引导槽121g在绕动涡旋件12的板121的下表面上形成为基本上直线。形成在奥尔德姆环15的环形部分15a的上表面上的一对(两件)键部分15b可以可滑动地联接到奥尔德姆环引导槽121g或与奥尔德姆环引导槽121g接合。此外,与绕动涡旋件12的奥尔德姆环引导槽121g具有约90°的相位差的一对(两件)奥尔德姆环引导槽112g在固定涡旋件11的板112的下表面上形成为基本上直线。形成在奥尔德姆环15的环形部分15a的上表面上的一对(两件)键部分15e可以可滑动地联接到奥尔德姆环引导槽112g或与奥尔德姆环引导槽112g接合。通过如上所述配置的奥尔德姆环15,绕动涡旋件12可以执行绕动运动而不枢转。The compression section 10 according to an implementation of the scroll compressor 2 may include a fixed scroll 11 , an orbiting scroll 12 , a main frame 13 , a subframe 14 and an Oldham ring 15 as shown in FIG. 1 . . In one implementation, the Oldham ring 15 is coupled to or engaged with the orbiting scroll 12 and the fixed scroll 11 . Specifically, a pair (two pieces) of Oldham ring guide grooves 121 g are formed in a substantially straight line on the lower surface of the plate 121 of the orbiting scroll 12 . A pair (two pieces) of key portions 15b formed on the upper surface of the ring portion 15a of the Oldham ring 15 can be slidably coupled to the Oldham ring guide groove 121g or with the Oldham ring guide groove 121g. join. In addition, a pair (two pieces) of Oldham ring guide grooves 112g having a phase difference of about 90° from the Oldham ring guide grooves 121g of the orbiting scroll 12 are formed in the plate 112 of the fixed scroll 11. A substantially straight line is formed on the lower surface. A pair (two pieces) of key portions 15e formed on the upper surface of the ring portion 15a of the Oldham ring 15 can be slidably coupled to the Oldham ring guide groove 112g or with the Oldham ring guide groove 112g. join. With the Oldham ring 15 configured as described above, the orbiting scroll 12 can perform an orbiting motion without pivoting.

然而,在其中支撑绕动涡旋件12的子框架14仅在沿着旋转轴23的方向上可移动的配置中,难以控制施加到子框架14的力矩,因此只是顺应该趋势。因此,难以有效地选择下推力反作用力的位置,因此不获得所述效果。根据一实施方式,可以有效地选择下推力反作用力的位置,从而最大化所述效果。However, in a configuration in which the sub-frame 14 supporting the orbiting scroll 12 is movable only in the direction along the rotation shaft 23, it is difficult to control the moment applied to the sub-frame 14, thus simply following the trend. Therefore, it is difficult to effectively select the position of the downward thrust reaction force, so the effect is not obtained. According to one embodiment, the position of the downthrust reaction can be efficiently chosen so as to maximize the effect.

在一些实施方式中,由主框架13和子框架14围绕的空间由在主框架13 和子框架14之间的两个密封构件形成。通过在此空间中的压缩操作期间引导来自压缩室16的特定压力(中间压力),子框架14可以被对着绕动涡旋件12推动。至于其实现方式,可以主要使用两种方法,并将通过一些变型详细描述。In some embodiments, the space surrounded by the main frame 13 and the sub-frame 14 is formed by two sealing members between the main frame 13 and the sub-frame 14 . By introducing a certain pressure (intermediate pressure) from the compression chamber 16 during the compression operation in this space, the sub-frame 14 can be pushed against the orbiting scroll 12 . As for its implementation, mainly two methods can be used and will be described in detail with some variants.

图13示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图。换句话说,图13示出根据涡旋式压缩机2的变型的压缩部分10和旋转轴23的轴向剖视图。13 illustrates an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure. In other words, FIG. 13 shows an axial sectional view of the compression portion 10 and the rotary shaft 23 according to a modification of the scroll compressor 2 .

根据涡旋式压缩机2的变型的压缩部分10可以包括如图6所示的固定涡旋件11、绕动涡旋件12、主框架13和子框架14。绕动涡旋件12通过与固定涡旋件11接合以形成压缩室16而绕动。压缩室16如在径向方向上的通孔111a中的箭头所示吸入和压缩低压力制冷剂,并如在垂直方向上的通孔112a中的箭头所示排出高压力制冷剂。将省略对奥尔德姆环15的描述。The compression part 10 according to a modification of the scroll compressor 2 may include a fixed scroll 11 , an orbiting scroll 12 , a main frame 13 and a sub frame 14 as shown in FIG. 6 . The orbiting scroll 12 orbits by being engaged with the fixed scroll 11 to form a compression chamber 16 . The compression chamber 16 sucks and compresses low-pressure refrigerant as indicated by arrows in the through-hole 111a in the radial direction, and discharges high-pressure refrigerant as indicated by the arrow in the through-hole 112a in the vertical direction. A description of the Oldham ring 15 will be omitted.

在压缩部分10中,提供配置为密封绕动涡旋件12的主体部分123和子框架14的第三主体部分143之间的间隙的密封构件171a。根据变型,通过提供密封构件171a,形成腔室171并且腔室171保持在高压力。In the compression portion 10, a sealing member 171a configured to seal a gap between the main body portion 123 of the orbiting scroll 12 and the third main body portion 143 of the sub-frame 14 is provided. According to a modification, by providing the sealing member 171a, the chamber 171 is formed and maintained at high pressure.

此外,配置为密封主框架13和子框架14之间的间隙的密封构件172a 和172b可以提供在压缩部分10中从而在主框架13和子框架14之间形成腔室172。提供配置为密封主框架13的第二主体部分132和子框架14的第一主体部分141之间的间隙的密封构件172a,并且同时,提供配置为密封主框架13的第三主体部分133和子框架14的第三主体部分143之间的间隙的密封构件172b。这些密封构件172a和172b对应于上述两个密封构件。根据变型,腔室172通过提供密封构件172a和172b来形成。In addition, sealing members 172 a and 172 b configured to seal a gap between the main frame 13 and the sub-frame 14 may be provided in the compression part 10 to form a cavity 172 between the main frame 13 and the sub-frame 14 . A sealing member 172a configured to seal a gap between the second body portion 132 of the main frame 13 and the first body portion 141 of the sub-frame 14 is provided, and at the same time, a third body portion 133 configured to seal the main frame 13 and the sub-frame 14 is provided. The gap between the third main body portion 143 is sealed by the sealing member 172b. These sealing members 172a and 172b correspond to the above-mentioned two sealing members. According to a variant, the chamber 172 is formed by providing sealing members 172a and 172b.

此外,在压缩部分10中,可以提供配置为将从压缩室16排出的制冷剂引导到腔室172的制冷剂通道181、182和183。具体地,在压缩部分10中,提供配置为将处于特定压力的制冷剂从压缩室16引导到腔室172的第一通道181、第二通道182和第三通道183。第一通道181可以提供在绕动涡旋件12中以与压缩室16连通。第一通道181是穿过绕动涡旋件12的内部的通道,并且是绕动涡旋件的内部通道的示例。第一通道181将制冷剂移出压缩室16并将制冷剂引入到第二通道182中。第二通道182可以提供在固定涡旋件11中以将第一通道181连接到第三通道183。第二通道182是穿过固定涡旋件11的通道,并且是固定涡旋件的内部通道的示例。第二通道182 使从第一通道181引入的制冷剂移动,并将制冷剂引入到第三通道183中。第三通道183可以提供在主框架13中以与腔室172连通。第三通道183是穿过主框架13的通道,并且是保持构件的内部通道的示例。第三通道183 使从第二通道182引入的制冷剂移动并将制冷剂引入到腔室172中。因此,腔室172中的压力被保持在特定中间压力。Also, in the compression part 10 , refrigerant passages 181 , 182 , and 183 configured to guide refrigerant discharged from the compression chamber 16 to the chamber 172 may be provided. Specifically, in the compression part 10, a first passage 181, a second passage 182, and a third passage 183 configured to guide refrigerant at a certain pressure from the compression chamber 16 to the chamber 172 are provided. A first passage 181 may be provided in the orbiting scroll 12 to communicate with the compression chamber 16 . The first passage 181 is a passage passing through the inside of the orbiting scroll 12, and is an example of an inner passage of the orbiting scroll. The first passage 181 moves refrigerant out of the compression chamber 16 and introduces refrigerant into the second passage 182 . A second passage 182 may be provided in the fixed scroll 11 to connect the first passage 181 to the third passage 183 . The second passage 182 is a passage passing through the fixed scroll 11 and is an example of an internal passage of the fixed scroll. The second passage 182 moves the refrigerant introduced from the first passage 181 and introduces the refrigerant into the third passage 183 . A third passage 183 may be provided in the main frame 13 to communicate with the chamber 172 . The third passage 183 is a passage passing through the main frame 13, and is an example of an internal passage of the holding member. The third passage 183 moves the refrigerant introduced from the second passage 182 and introduces the refrigerant into the chamber 172 . Therefore, the pressure in the chamber 172 is maintained at a certain intermediate pressure.

图14是示出根据本公开的一实施方式的根据涡旋式压缩机的一变型、当从顶部观看时压缩部分中的绕动涡旋件的板的端部的俯视图。换句话说,图14示出当从顶部观看时绕动涡旋件12的板121的端部的平面图。14 is a plan view illustrating an end portion of a plate of an orbiting scroll in a compression portion when viewed from the top according to a modification of the scroll compressor according to an embodiment of the present disclosure. In other words, FIG. 14 shows a plan view of the end portion of the plate 121 of the orbiting scroll 12 when viewed from the top.

在板121的上部区域当中,第一通道181的入口181a提供在面对压缩室16的区域125a(在虚线圆弧的右侧的区域)中,第一通道181的出口181b 提供在与固定涡旋件11的主体部分111接触的区域125b(在虚线圆弧的左侧的区域)中。当从顶部观看板121时,第一通道181实际上不可见,但是为清楚起见,第一通道181在附图中以虚线示出。此外,第一通道181的入口181a被示出为布置在装配在最外面且彼此相邻的两个绕动卷体122中的区域中,但是入口181a的位置不限于此。因此,入口181a的位置可以根据要被引导到腔室172的中间压力的大小来选择。因此,压缩室16中的所需的中间压力制冷剂流动到第一通道181。Among the upper regions of the plate 121, the inlet 181a of the first passage 181 is provided in the region 125a facing the compression chamber 16 (the region on the right side of the dotted arc), and the outlet 181b of the first passage 181 is provided in the In the region 125b (the region to the left of the dashed arc) that the body portion 111 of the rotary member 11 contacts. The first channel 181 is not actually visible when viewing the plate 121 from the top, but is shown in dashed lines in the figures for clarity. In addition, the inlet 181a of the first passage 181 is shown to be arranged in a region in two orbiting rolls 122 that are fitted outermost and adjacent to each other, but the location of the inlet 181a is not limited thereto. Therefore, the location of the inlet 181 a may be selected according to the magnitude of the intermediate pressure to be introduced into the chamber 172 . Accordingly, the desired intermediate-pressure refrigerant in the compression chamber 16 flows to the first passage 181 .

图15是示出根据按本公开的一实施方式的涡旋式压缩机的变型、当从底部观看时压缩部分中的固定涡旋件的主体部分的仰视图。换句话说,图15 示出当从底部观看时固定涡旋件11的主体部分111的仰视图。15 is a bottom view illustrating a main body portion of a fixed scroll in a compression portion when viewed from the bottom according to a modification of the scroll compressor according to an embodiment of the present disclosure. In other words, FIG. 15 shows a bottom view of the main body portion 111 of the fixed scroll 11 when viewed from the bottom.

在主体部分111的下部区域当中,第二通道182的入口182a提供在与绕动涡旋件12的板121接触的区域115a(在虚线圆弧的右侧的区域)中,第二通道182的出口182b提供在与主框架13接触的区域115b(在虚线圆弧的左侧的区域)中。当从底部观看固定涡旋件11的主体部分111时,第二通道182实际上不可见,但是为清楚起见,第二通道182在附图中以虚线示出。此外,在变型中,第二通道182的入口182a提供在绕动涡旋件12绕动时在第一通道181的出口181b的轨迹181c上的点中。因此,入口181a面对的压缩室16中的特定范围的中间压力制冷剂从第一通道181流动到第二通道182。In the lower region of the main body portion 111, the inlet 182a of the second passage 182 is provided in the region 115a (the region on the right side of the dotted arc) in contact with the plate 121 of the orbiting scroll 12, and the inlet 182a of the second passage 182 The outlet 182b is provided in the region 115b (the region on the left side of the dotted line arc) in contact with the main frame 13 . When viewing the main body portion 111 of the fixed scroll 11 from the bottom, the second passage 182 is not actually visible, but is shown in dashed lines in the drawings for clarity. Furthermore, in a modification, the inlet 182a of the second passage 182 is provided in a point on the locus 181c of the outlet 181b of the first passage 181 when the orbiting scroll 12 orbits. Accordingly, a certain range of intermediate-pressure refrigerant in the compression chamber 16 facing the inlet 181 a flows from the first passage 181 to the second passage 182 .

图16示出根据本公开的一实施方式的涡旋式压缩机的变型的压缩部分和旋转轴的轴向剖视图。换句话说,图16示出根据涡旋式压缩机2的变型的压缩部分10和旋转轴23的轴向剖视图。16 shows an axial sectional view of a compression portion and a rotary shaft of a modification of a scroll compressor according to an embodiment of the present disclosure. In other words, FIG. 16 shows an axial sectional view of the compression portion 10 and the rotary shaft 23 according to a modification of the scroll compressor 2 .

与根据图13所示的涡旋式压缩机2的变型的压缩部分10相比,根据涡旋式压缩机2的变型的压缩部分10还可以包括布置在第一通道181和第二通道182之间的埋头孔(counter bore)184。Compared with the compression portion 10 according to the modification of the scroll compressor 2 shown in FIG. 13 , the compression portion 10 according to the modification of the scroll compressor 2 may further include The counter bore (counter bore) 184 between.

因为先前已经描述了当从顶部观看时绕动涡旋件12的板121的端部的俯视图,所以将省略其描述。Since the top view of the end portion of the plate 121 of the orbiting scroll 12 when viewed from the top has been described previously, description thereof will be omitted.

图17是示出根据按本公开的一实施方式的涡旋式压缩机的变型、当从底部观看时压缩部分中的固定涡旋件的主体部分的仰视图。17 is a bottom view illustrating a main body portion of a fixed scroll in a compression portion when viewed from the bottom according to a modification of the scroll compressor according to an embodiment of the present disclosure.

在主体部分111的下部区域当中,第二通道182的入口182a提供在与绕动涡旋件12的板121接触的区域115a(在虚线圆弧的右侧的区域)中,第二通道182的出口182b提供在与主框架13接触的区域115b(在虚线圆弧的左侧的区域)中。当从底部观看固定涡旋件11的主体部分111时,第二通道182实际上不可见,但是为清楚起见,第二通道182在附图中以虚线示出。此外,在变型中,第二通道182的入口182a被提供为与埋头孔184接触,该埋头孔184对应于在绕动涡旋件12绕动时覆盖第一通道181的出口 181b的轨迹181c的全部的凹槽部分的示例。因此,入口181a面对的压缩室 16中的中间压力制冷剂从第一通道181流动到第二通道182。In the lower region of the main body portion 111, the inlet 182a of the second passage 182 is provided in the region 115a (the region on the right side of the dotted arc) in contact with the plate 121 of the orbiting scroll 12, and the inlet 182a of the second passage 182 The outlet 182b is provided in the region 115b (the region on the left side of the dotted line arc) in contact with the main frame 13 . When viewing the main body portion 111 of the fixed scroll 11 from the bottom, the second passage 182 is not actually visible, but is shown in dashed lines in the drawings for clarity. Furthermore, in a modification, the inlet 182a of the second passage 182 is provided to be in contact with a counterbore 184 corresponding to the trajectory 181c covering the outlet 181b of the first passage 181 when the orbiting scroll 12 orbits. Example of a full groove section. Accordingly, the intermediate-pressure refrigerant in the compression chamber 16 facing the inlet 181a flows from the first passage 181 to the second passage 182.

根据变型,第二通道182的入口182a被提供为与埋头孔184接触,该埋头孔184覆盖当绕动涡旋件12绕动时第一通道181的出口181b的轨迹 181c的全部,但不限于此。替代地,第二通道182的入口182a被提供为与埋头孔184接触,该埋头孔184覆盖当绕动涡旋件12绕动时第一通道181 的出口181b的轨迹181c的一部分。也就是,在绕动涡旋件12绕动的周期的至少一部分中,第二通道182的入口182a可以与第一通道181的出口181b 连通。According to a variant, the inlet 182a of the second passage 182 is provided in contact with a counterbore 184 covering the entirety of the trajectory 181c of the outlet 181b of the first passage 181 when the orbiting scroll 12 orbits, but not limited to this. Alternatively, the inlet 182a of the second passage 182 is provided in contact with a counterbore 184 covering a part of the trajectory 181c of the outlet 181b of the first passage 181 when the orbiting scroll 12 orbits. That is, the inlet 182a of the second passage 182 may communicate with the outlet 181b of the first passage 181 during at least a part of a period in which the orbiting scroll 12 orbits.

此外,根据一些变型,假设配置为将制冷剂移出压缩室16并将制冷剂引入到固定涡旋件11中的第二通道182中的第一通道181提供在绕动涡旋件12中,并且配置为将从绕动涡旋件12中的第一通道181引入的制冷剂引入到主框架13中的第三通道183的第二通道182提供在固定涡旋件11中,但是不限于此。替代地,可以假设配置为将制冷剂移出压缩室16并将制冷剂直接引入到主框架13的第三通道183中的通道提供在固定涡旋件11中。通过使用上述配置,可以不需要在一些变型中提到的第一通道181和第二通道182之间的连通定时(communication timing)的控制。Furthermore, according to some modifications, it is assumed that the first passage 181 configured to move refrigerant out of the compression chamber 16 and introduce the refrigerant into the second passage 182 in the fixed scroll 11 is provided in the orbiting scroll 12, and The second passage 182 configured to introduce refrigerant introduced from the first passage 181 in the orbiting scroll 12 to the third passage 183 in the main frame 13 is provided in the fixed scroll 11 , but is not limited thereto. Alternatively, it may be assumed that a passage configured to move refrigerant out of the compression chamber 16 and directly introduce the refrigerant into the third passage 183 of the main frame 13 is provided in the fixed scroll 11 . By using the above configuration, the control of communication timing between the first channel 181 and the second channel 182 mentioned in some modifications may not be required.

此外,根据一些变型,假设主框架13和子框架14的形状如图6、图10 和图12所示,通过使用密封构件172a和172b密封主框架13和子框架14 之间的间隙而在主框架13和子框架14之间形成腔室172,其配置为将中间压力从压缩室16引入到腔室172,但是不限于此。例如,假设主框架13和子框架14的形状如图11所示,通过使用两个密封构件密封主框架13和子框架14之间的间隙而在主框架13和子框架14之间形成腔室,其可以配置为将中间压力从压缩室16引入到该腔室。In addition, according to some modifications, assuming that the main frame 13 and the sub-frame 14 have shapes as shown in FIGS. A chamber 172 is formed between the subframe 14 and configured to introduce intermediate pressure from the compression chamber 16 into the chamber 172 , but is not limited thereto. For example, assuming that the main frame 13 and the sub-frame 14 have shapes as shown in FIG. It is configured to introduce intermediate pressure from the compression chamber 16 into the chamber.

替代地,当根据一实施方式在假设主框架13和子框架14的形状的情况下图2至图4的腔室142a对应于图13至图16的腔室172时,中间压力可以从压缩室16引入到腔室172。此外,当假设由图5的腔室142a和腔室121b 形成的空间对应于图13至图16的腔室172时,中间压力可以从压缩室16 引入到腔室172。Alternatively, when the chamber 142a of FIGS. 2 to 4 corresponds to the chamber 172 of FIGS. Introduced into chamber 172. In addition, when it is assumed that the space formed by the chamber 142a and the chamber 121b of FIG. 5 corresponds to the chamber 172 of FIGS. 13 to 16 , intermediate pressure may be introduced from the compression chamber 16 to the chamber 172 .

在这个意义上,应当理解,通过使用密封构件172a和172b密封主框架 13和子框架14之间的间隙而在主框架13和子框架14之间形成腔室172从而将中间压力从压缩室16引入到腔室172可以包括:通过至少在主框架13 和子框架14之间形成内部空间并通过使用密封机构至少密封主框架13和子框架14之间的间隙而将中间压力从压缩室16引入到腔室172。In this sense, it should be understood that the intermediate pressure is introduced from the compression chamber 16 into The chamber 172 may include introducing intermediate pressure from the compression chamber 16 into the chamber 172 by forming an inner space at least between the main frame 13 and the sub-frame 14 and by sealing at least a gap between the main frame 13 and the sub-frame 14 using a sealing mechanism. .

尽管已经用各种实施方式描述了本公开,但是可以向本领域技术人员提出各种改变和变型。本公开旨在涵盖落入所附权利要求的范围内的这样的改变和变型。Although the present disclosure has been described with various embodiments, various changes and modifications may be suggested to those skilled in the art. The present disclosure is intended to cover such changes and modifications as come within the scope of the appended claims.

Claims (11)

1.一种涡旋式压缩机,包括:1. A scroll compressor, comprising: 主体;main body; 固定涡旋件,固定到所述主体的内部并提供有固定卷体;a fixed scroll fixed to the interior of the main body and provided with a fixed wrap; 绕动涡旋件,配置为关于所述固定涡旋件绕动并提供有绕动卷体,所述绕动卷体与所述固定卷体一起形成压缩室;an orbiting scroll configured to orbit with respect to the fixed scroll and provided with an orbiting wrap forming a compression chamber together with the fixed wrap; 主框架,配置为支撑所述固定涡旋件;a main frame configured to support the fixed scroll; 子框架,布置在所述主框架内以在远离所述绕动涡旋件的中心的位置支撑所述绕动涡旋件,a subframe disposed within the main frame to support the orbiting scroll at a position away from the center of the orbiting scroll, 密封构件,配置为密封所述主框架和所述子框架之间的间隙以在所述主框架和所述子框架之间形成腔室,a sealing member configured to seal a gap between the main frame and the sub-frame to form a chamber between the main frame and the sub-frame, 通道,配置为将从所述压缩室排出的制冷剂引导到所述腔室,a channel configured to direct refrigerant discharged from the compression chamber to the chamber, 其中所述通道包括:Wherein said channels include: 第一通道,提供在所述绕动涡旋件中以与所述压缩室连通;a first passage provided in the orbiting scroll to communicate with the compression chamber; 第二通道,提供在所述主框架中以与所述腔室连通;以及a second passage provided in the main frame to communicate with the chamber; and 第三通道,提供在所述固定涡旋件中以将所述第一通道连接到所述第二通道,以及a third passage provided in the fixed scroll to connect the first passage to the second passage, and 其中间隙形成在所述主框架和所述子框架之间以允许所述子框架关于所述主框架可移动。wherein a gap is formed between the main frame and the sub-frame to allow the sub-frame to be movable with respect to the main frame. 2.根据权利要求1所述的涡旋式压缩机,其中:2. The scroll compressor of claim 1, wherein: 所述第一通道的出口根据所述绕动涡旋件的绕动运动形成轨迹,以及The outlet of the first passage forms a trajectory according to the orbiting motion of the orbiting scroll, and 所述第三通道的入口布置在所述轨迹上。The entrance of the third channel is arranged on the track. 3.根据权利要求1所述的涡旋式压缩机,还包括:3. The scroll compressor of claim 1, further comprising: 旋转轴,所述绕动涡旋件联接到所述旋转轴并且所述绕动涡旋件沿所述旋转轴绕动,a rotary shaft to which the orbiting scroll is coupled and along which the orbiting scroll orbits, 其中所述子框架配置为在沿着所述旋转轴延伸的第一方向或者与所述第一方向正交的第二方向中的至少一个上关于所述主框架可移动。Wherein the sub-frame is configured to be movable with respect to the main frame in at least one of a first direction extending along the rotation axis or a second direction orthogonal to the first direction. 4.根据权利要求1所述的涡旋式压缩机,还包括:4. The scroll compressor of claim 1, further comprising: 旋转轴,被插入到形成在所述主框架中的轴通孔中并且联接到所述绕动涡旋件以允许所述绕动涡旋件绕动,a rotary shaft inserted into a shaft through hole formed in the main frame and coupled to the orbiting scroll to allow the orbiting scroll to orbit, 其中所述主框架包括第一主体部分和第二主体部分,所述第一主体部分包括配置为支撑所述固定涡旋件的固定涡旋件支撑表面,所述第二主体部分位于所述第一主体部分下面并包括所述轴通孔,Wherein the main frame includes a first body portion and a second body portion, the first body portion includes a fixed scroll support surface configured to support the fixed scroll, and the second body portion is positioned on the first body portion. a body portion below and including said shaft through hole, 其中所述子框架包括布置在所述主框架的所述第一主体部分内的第一主体部分以及被插入到所述轴通孔中以布置在所述旋转轴和所述主框架的所述第二主体部分之间的第二主体部分,以及Wherein the sub-frame includes a first main body portion arranged in the first main body portion of the main frame and inserted into the shaft through hole to be arranged between the rotation shaft and the main body of the main frame. a second body portion between the second body portions, and 其中间隙形成在所述主框架的所述第一主体部分和所述子框架的所述第一主体部分之间,并且间隙形成在所述主框架的所述第二主体部分和所述子框的所述第二主体部分之间。wherein a gap is formed between the first body portion of the main frame and the first body portion of the sub-frame, and a gap is formed between the second body portion of the main frame and the sub-frame between the second body portion. 5.根据权利要求4所述的涡旋式压缩机,其中在所述主框架的所述第一主体部分与所述子框架的所述第一主体部分之间的所述间隙小于在所述主框架的所述第二主体部分和所述子框架的所述第二主体部分之间的所述间隙。5. The scroll compressor according to claim 4, wherein said gap between said first body portion of said main frame and said first body portion of said subframe is smaller than that between said The gap between the second body portion of the main frame and the second body portion of the subframe. 6.根据权利要求4所述的涡旋式压缩机,其中所述子框架配置为关于所述主框架可移动,6. The scroll compressor of claim 4, wherein the subframe is configured to be movable with respect to the main frame, 其中所述子框架还包括推力轴承,所述推力轴承位于所述子框架的所述第一主体部分之上并包括配置为支撑所述绕动涡旋件的绕动涡旋件支撑表面,以及wherein the subframe further includes a thrust bearing positioned above the first body portion of the subframe and including an orbiting scroll support surface configured to support the orbiting scroll, and 其中所述推力轴承具有可弹性变形的形状。Wherein the thrust bearing has an elastically deformable shape. 7.根据权利要求4所述的涡旋式压缩机,其中所述子框架配置为关于所述主框架可移动,以及7. The scroll compressor of claim 4, wherein the subframe is configured to be movable with respect to the main frame, and 配置为与所述子框架的所述第一主体部分接触的突起形成在所述主框架的所述第一主体部分的内表面上。A protrusion configured to be in contact with the first body portion of the sub-frame is formed on an inner surface of the first body portion of the main frame. 8.根据权利要求7所述的涡旋式压缩机,其中当所述子框架在关于所述主框架移动的同时倾斜时,在所述主框架的所述第二主体部分与所述子框架的所述第二主体部分接触之前,所述主框架的所述突起与所述子框架的所述第一主体部分接触。8. The scroll compressor according to claim 7, wherein when the sub-frame tilts while moving with respect to the main frame, there is a gap between the second main body portion of the main frame and the sub-frame The protrusion of the main frame is in contact with the first body portion of the sub-frame before the second body portion is in contact. 9.根据权利要求1所述的涡旋式压缩机,还包括:9. The scroll compressor of claim 1, further comprising: 奥尔德姆环,配置为防止所述绕动涡旋件的枢转,an Oldham ring configured to prevent pivoting of the orbiting scroll, 其中所述奥尔德姆环联接到所述绕动涡旋件和所述子框架。Wherein the Oldham ring is coupled to the orbiting scroll and the subframe. 10.根据权利要求1所述的涡旋式压缩机,还包括:10. The scroll compressor of claim 1, further comprising: 奥尔德姆环,配置为防止所述绕动涡旋件的枢转,an Oldham ring configured to prevent pivoting of the orbiting scroll, 其中所述奥尔德姆环联接到所述绕动涡旋件和所述主框架。Wherein the Oldham ring is coupled to the orbiting scroll and the main frame. 11.根据权利要求1所述的涡旋式压缩机,还包括:11. The scroll compressor of claim 1, further comprising: 奥尔德姆环,配置为防止所述绕动涡旋件的枢转,an Oldham ring configured to prevent pivoting of the orbiting scroll, 其中所述奥尔德姆环联接到所述绕动涡旋件和所述固定涡旋件。Wherein the Oldham ring is coupled to the orbiting scroll and the fixed scroll.
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