CN1084441C - Backpressure cavity sealing device of vortex compressor - Google Patents
Backpressure cavity sealing device of vortex compressor Download PDFInfo
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- CN1084441C CN1084441C CN96118780A CN96118780A CN1084441C CN 1084441 C CN1084441 C CN 1084441C CN 96118780 A CN96118780 A CN 96118780A CN 96118780 A CN96118780 A CN 96118780A CN 1084441 C CN1084441 C CN 1084441C
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- 238000007789 sealing Methods 0.000 title claims abstract description 55
- 239000000314 lubricant Substances 0.000 claims 2
- 230000035939 shock Effects 0.000 claims 1
- 239000010687 lubricating oil Substances 0.000 abstract description 8
- 239000003921 oil Substances 0.000 description 4
- 239000012530 fluid Substances 0.000 description 2
- 238000002955 isolation Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000003831 antifriction material Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
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Abstract
本发明公开了一种带背压腔密封装置的涡旋压缩机,包括一个非公转涡旋盘和一个公转涡旋盘;一个被容纳于上述公转涡旋盘的轴毂内的圆滑块;一个与上述圆滑块结合的被转动支承主轴;一个除与上述主轴的轴颈配合支承主轴外,具有两个环形的密封端面的支架体。支架体的第二环形端面上设环形槽,在环形槽中装密封垫;在圆滑块内孔及端面包围的润滑油腔与高压背压腔之间装密封件。本发明具有密封装置的结构简单,加工工艺性好,使用可靠的特点。
The invention discloses a scroll compressor with a back pressure cavity sealing device, which comprises a non-revolving scroll and an orbiting scroll; a circular slider accommodated in the shaft hub of the orbiting scroll; a A rotatably supported main shaft combined with the above-mentioned round slider; a support body having two ring-shaped sealing end surfaces except for cooperating with the journal of the above-mentioned main shaft to support the main shaft. An annular groove is arranged on the second annular end surface of the support body, and a sealing gasket is installed in the annular groove; a sealing member is installed between the inner hole of the circular slider and the lubricating oil chamber surrounded by the end surface and the high-pressure back pressure chamber. The invention has the characteristics of simple structure, good processability and reliable use of the sealing device.
Description
本发明涉及一种带背压腔密封装置的涡旋压缩机。The invention relates to a scroll compressor with a back pressure cavity sealing device.
专利申请号CN1060699A,公开了一种带浮动密封装置的蜗形机械。它是在无轨运行涡形体(即非公转涡旋盘)的上端面设置了一环形凹槽,在该环形槽中放置着由3个环形构件与两组密封件(或者由两个环形构件和一组密封件)构成的多功能浮动密封装置,密封组件最上端面处设置了密封唇口与筒体隔板上的耐磨环还构成了顶部密封,几处密封分别完成低压吸气腔与背压腔、背压腔与高压排气腔、高压排气腔与低压吸气腔之间的隔离密封。该专利可称为涡旋压缩机的上置式背压腔设计。在上置式背压腔设计中,需专门设置无轨涡形体沿轴向向有轨涡形体(即公转涡旋盘)偏移的导轨,组合密封件所需零件数多且结构复杂,另外为保证顶部密封的可靠性,在背压腔流体压力作用下,无轨运行涡形体必然压紧有轨运行涡形体的端板,并进而使有轨运行涡形体紧压在主轴承箱(即支架体)的环形端面上。造成较大摩擦和功率损耗。Patent application number CN1060699A discloses a volute machine with a floating sealing device. It is provided with an annular groove on the upper end surface of the non-orbiting scroll (that is, the non-revolving scroll), in which three annular members and two sets of seals (or two annular members and two sets of seals) are placed in the annular groove. A set of seals) constitutes a multi-functional floating sealing device. The sealing lip and the wear-resistant ring on the partition plate of the cylinder are set on the uppermost surface of the sealing assembly to form a top seal. Several seals respectively complete the low-pressure suction chamber and the back The isolation seal between the pressure chamber, the back pressure chamber and the high-pressure exhaust chamber, the high-pressure exhaust chamber and the low-pressure suction chamber. This patent can be called the upper-mounted back pressure chamber design of the scroll compressor. In the design of the upper-mounted back pressure chamber, it is necessary to specially set up the guide rail that the trackless scroll is axially offset from the orbiting scroll (that is, the orbiting scroll), and the combined seal requires a large number of parts and a complex structure. The reliability of the top seal, under the action of the fluid pressure in the back pressure chamber, the trackless volute will inevitably press the end plate of the orbital volute, and then make the orbital volute tightly pressed against the main bearing housing (that is, the bracket body) ring end face. Causes greater friction and power loss.
本发明的目的是提供一种结构简单,使用可靠,并且能减小公转涡旋盘与支架体之间的摩擦和功率损耗的带背压腔密封装置的涡旋压缩机。The object of the present invention is to provide a scroll compressor with a back pressure chamber sealing device which is simple in structure, reliable in use, and can reduce friction and power loss between the orbiting scroll and the support body.
本发明的目的是这样实现的,本发明包括:一个非公转涡旋盘和一个公转涡旋盘;一个被容纳于上述公转涡旋盘的轴毂内的圆滑块;一个与上述圆滑块结合的被转动支承的主轴;一个除与上述主轴的轴颈配合支承主轴外还具有两个环形的密封端面的支架体。所述的支架体的第二环形端面上设置环形槽,在环形槽中装密封垫;在圆滑块内孔及端面包围的润滑油腔与高压背压腔之间装密封件。The purpose of the present invention is achieved in that the present invention includes: a non-revolving scroll and an orbiting scroll; a circular slider accommodated in the hub of the orbiting scroll; a circular slider combined with the above-mentioned circular slider A rotatably supported main shaft; a support body having two ring-shaped sealing end faces in addition to cooperating with the shaft journal of the above-mentioned main shaft to support the main shaft. An annular groove is arranged on the second annular end surface of the support body, and a sealing gasket is installed in the annular groove; a sealing element is installed between the inner hole of the circular slider and the lubricating oil chamber surrounded by the end surface and the high-pressure back pressure chamber.
所述的环形槽的底部设有由数个小孔构成的气路与高压背压腔连通。The bottom of the annular groove is provided with an air path composed of several small holes communicating with the high-pressure back pressure chamber.
所述的环形槽中装的密封垫的截面为"П"形。The cross-section of the gasket installed in the annular groove is "П" shape.
所述的密封件是设一含直边不完全圆内孔的调整密封垫片;不完全圆内孔的内缘面形状是同曲拐的不完全圆柱形的外缘面形状相对应;调整密封垫片是嵌套在主轴曲拐的外侧,并轴向地安装在圆滑块的下面,调整密封垫片的第二端面与支架体的对应端面之间留有间隙,调整密封垫片的第一端面与圆滑块的对应端面之间仅隔一层润滑油膜。The sealing member is provided with an adjusting sealing gasket containing an incomplete circular inner hole with a straight edge; the shape of the inner edge surface of the incomplete circular inner hole is corresponding to the shape of the incomplete cylindrical outer edge surface of the crank throw; The sealing gasket is nested on the outer side of the crank throw of the main shaft, and is axially installed under the circular slider. There is a gap between the second end surface of the sealing gasket and the corresponding end surface of the bracket body, and the second end surface of the adjusting sealing gasket There is only one layer of lubricating oil film between one end face and the corresponding end face of the round slider.
本发明由于采用一种不同于现有技术组合浮动密封的下置式背压腔设计技术,采用不同的密封元件分别完成低压背压腔和高压背压腔之间的密封隔离及高压背压腔和润滑油腔之间的密封隔离,并在压缩机的吸气腔和背压腔(即高压背压腔)之间增加了一个低压背压腔,不会发生由高压背压腔向吸气腔的直接泄露,因而降低了不同压力腔之间的气体泄露和整机的功率损耗,并且借助密封元件的补偿作用有效地提高密封的可靠性。这些密封元件的结构简单,加工工艺性好,使用可靠。此外,本发明的另外两个优点是:不需要专门设置公转涡旋盘沿轴向偏移时的导轨;在背压腔流体压力作用下,公转涡旋盘向上偏移时只与非公转涡旋盘的端板是压紧的,从而使公转涡旋盘与支架体之间的摩擦力有所减小,功率损耗也较小。Since the present invention adopts a design technology of the lower back pressure chamber which is different from the combined floating seal of the prior art, different sealing elements are used to complete the sealing isolation between the low pressure back pressure chamber and the high pressure back pressure chamber and the high pressure back pressure chamber and the high pressure back pressure chamber respectively. The seal between the lubricating oil chambers is isolated, and a low-pressure back-pressure chamber is added between the suction chamber and the back-pressure chamber of the compressor (that is, the high-pressure back-pressure chamber), so that there will be no flow from the high-pressure back-pressure chamber to the suction chamber. Direct leakage, thus reducing the gas leakage between different pressure chambers and the power loss of the whole machine, and effectively improving the reliability of the seal with the help of the compensation function of the sealing element. These sealing elements are simple in structure, good in processability and reliable in use. In addition, two other advantages of the present invention are: there is no need to specially set guide rails for the axial displacement of the orbiting scroll; The end plate of the rotating disk is compressed, so that the friction between the orbiting scroll and the support body is reduced, and the power loss is also small.
下面结合附图及实施例对本发明的技术方案进行详细说明。The technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings and embodiments.
图1为实施例1中的涡旋压缩机的轴截面图。FIG. 1 is an axial sectional view of a scroll compressor in Embodiment 1. FIG.
图2为支架体的轴截面图。Fig. 2 is an axial sectional view of the bracket body.
图3为П形垫的轴截面图。Figure 3 is an axial sectional view of a П-shaped pad.
图4为调整密封垫片的附视图。Figure 4 is an attached view of the adjusting gasket.
图5为调整密封垫片的轴截面图。Fig. 5 is an axial sectional view of the adjusting gasket.
图6为实施例2中的涡旋压缩机的轴截面图。FIG. 6 is an axial sectional view of a scroll compressor in Embodiment 2. FIG.
图7为密封垫片的俯视图。Fig. 7 is a top view of the gasket.
图8为密封垫片的轴截面图。Fig. 8 is an axial sectional view of the gasket.
参照图1,本发明的实施例1中所采用的背压腔密封装置为П形垫60和调整密封垫片70。在图1中,涡旋压缩机5由一个非公转涡旋盘10和一个公转涡旋盘20,一个圆滑块30,一根主轴40,一个支架体50等零件组成。非公转涡旋盘10具有从一个端板向外伸出的第一螺旋涡卷10-1,它和公转涡旋盘20上的第二螺旋涡卷20-1相交叉,从而限定多个连续运动的流体腔;在公转涡旋盘20上的端板的第二端面上有一个向外伸出的轴毂20-2,圆滑块30的外缘面为圆柱面,并且内孔为一含直边的非圆孔,圆滑块30被容纳于上述公转涡旋盘的轴毂内,既可与公转涡旋盘作相对转动,又可沿轴向相对移动;在主轴40的轴颈40-1的第一端面上有一偏心设置的曲拐40-2,从轴颈的第二端面上主轴轴向延伸与电机转子90固结在一起,曲拐的外缘面为一含直边的不完全圆柱面(图中未示出)被容纳于上述圆滑块的一含直边的非圆孔内,既可与圆滑块沿直边相对移动,又可沿轴向相对移动,润滑油通过主转油孔40-3从曲拐的端部引出,同时润滑圆滑块的内外缘柱面;参照图2,支架体50除与上述主轴的轴颈40-1配合支承主轴外,还具有两个环形的密封端面50-11和50-12,最外侧的环形端面50-11与上述非公转涡旋盘上的对应环形端面固结,从而将筒体内的高压排气腔5-1与涡旋压缩机的低压背压腔5-2隔离,靠近内侧的第二环形端面50-12与作公转运动的公转涡旋盘端板共同作用将背压腔分为高低压两个背压腔,外侧为低压背压腔5-2,内侧为高压背压腔5-3,润滑油腔5-4是由圆滑块30和调整垫片70包围形成,在支架体的第二环形端面50-12上设置一环形槽50-21,在环形槽50-21的底都有由数个小孔50-22构成的气路与高压背压腔5-3连通。图3表示密封垫是一个环形件,其截面为″П″形的П形垫60由耐磨减摩材料制成,被容纳于上述支架体的第二环形端面50-12上的环形槽50-21中,它的第一端面为一平面或类似平面,在第二端面上制成一环形凹槽,使之形成内外缘两个环状翼片60-1和60-2,当背压腔内的气体通过气路50-22进入支架体的环形槽50-21的底部后,П形垫的内外缘翼片分别向不同方向胀开,可密封环形槽50-21内的气体不会沿槽的侧壁泄露,同时П形垫可在压力气体作用下作轴向浮动,以补偿间隙及П形垫长期工作后的磨损量。图4、5表示调整密封垫片70具一含直边的不完全圆内孔70-1,嵌套在主轴曲拐40-2的外侧,并轴向地安装在圆滑块30的下面,它的第二端面与支架体50的对应端面之间留有间隙,而它的第一端面与圆滑块30的对应端面之间仅隔一层润滑油膜,圆滑块30的第一端面受压力润滑油直接作用,提供密封压力,当主轴转动时调整密封垫片与圆滑块之间作相对直移运动,从而隔离了高压背压腔5-3的气体和曲拐40-2周围的润滑油,同时也起到了润滑相对运动零件的表面的作用。Referring to FIG. 1 , the back pressure chamber sealing device used in Embodiment 1 of the present invention is a П-
图6说明了在本发明的实施例2中所采用的背压腔密封装置为П形垫60和密封垫片80。图7、8说明密封垫片80具一含直边的非圆柱形80-1的外缘面,它可嵌套在圆滑块的非圆内孔30-1之中,采用螺栓通过中心部位的光孔80-2可动地压置到曲拐的端面上,沿轴向设置的环形台阶用于密封垫片在曲拐上的轴向定位,密封压力由作用在密封垫片第一端面上的压力油提供,密封垫片80的油孔80-3与主轴40上的油孔(40-3)是相通的。调整密封垫片70和密封垫片80均由钢材制成。FIG. 6 illustrates that the back pressure chamber sealing device used in Embodiment 2 of the present invention is a П-
除以上所述外,密封垫还可以改为截面是矩形的平垫片,或者同时使用两个或两个以上的П形垫60或平垫片,以及在支架体50的第二环形端面的环形槽50-21底部不设置气体通路而代之以弹簧,以及调整密封垫片70的不完全圆内孔改为可与主轴曲拐40-2的不完全圆柱形的外缘面嵌套的各种内孔,密封垫片80的非圆柱形的外缘面改为可与圆滑块30的非圆内孔嵌套的各种外缘柱面等设计,都是本发明的修正或变形,因而也都属于本发明的保护范围。In addition to the above, the sealing gasket can also be changed to a rectangular flat gasket in cross section, or use two or more П-
Claims (8)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN96118780A CN1084441C (en) | 1996-10-21 | 1996-10-21 | Backpressure cavity sealing device of vortex compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN96118780A CN1084441C (en) | 1996-10-21 | 1996-10-21 | Backpressure cavity sealing device of vortex compressor |
Publications (2)
| Publication Number | Publication Date |
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| CN1180793A CN1180793A (en) | 1998-05-06 |
| CN1084441C true CN1084441C (en) | 2002-05-08 |
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| CN96118780A Expired - Fee Related CN1084441C (en) | 1996-10-21 | 1996-10-21 | Backpressure cavity sealing device of vortex compressor |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100343529C (en) * | 2005-07-04 | 2007-10-17 | 兰州理工大学 | Vortex compressor |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100371600C (en) * | 2003-12-12 | 2008-02-27 | 乐金电子(天津)电器有限公司 | Vortex type compressor for preventing leakage of compressed gas |
| CN1963205B (en) * | 2005-11-12 | 2011-01-12 | 柯恩龙 | Vortex fluid machinery |
| GB0823184D0 (en) * | 2008-12-19 | 2009-01-28 | Edwards Ltd | Scroll compressor |
| CN113090527A (en) * | 2021-04-19 | 2021-07-09 | 重庆超力高科技股份有限公司 | Backpressure cavity seal structure, compressor and on-vehicle air conditioning system |
| CN119435386A (en) * | 2025-01-09 | 2025-02-14 | 珠海凌达压缩机有限公司 | Scroll compressor, air conditioner |
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|---|---|---|---|---|
| CN1060699A (en) * | 1990-10-01 | 1992-04-29 | 科普兰公司 | The scroll machine of band floating seal |
| CN2175841Y (en) * | 1993-10-25 | 1994-08-31 | 西安交通大学 | Coiled compressor with backpressure controlling mechanism |
| US5447418A (en) * | 1993-08-30 | 1995-09-05 | Mitsubishi Jukogyo Kabushiki Kaisha | Scroll-type fluid machine having a sealed back pressure chamber |
| CN1132826A (en) * | 1994-10-24 | 1996-10-09 | 株式会社日立制作所 | Vortex-type compressor |
-
1996
- 1996-10-21 CN CN96118780A patent/CN1084441C/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1060699A (en) * | 1990-10-01 | 1992-04-29 | 科普兰公司 | The scroll machine of band floating seal |
| US5447418A (en) * | 1993-08-30 | 1995-09-05 | Mitsubishi Jukogyo Kabushiki Kaisha | Scroll-type fluid machine having a sealed back pressure chamber |
| CN2175841Y (en) * | 1993-10-25 | 1994-08-31 | 西安交通大学 | Coiled compressor with backpressure controlling mechanism |
| CN1132826A (en) * | 1994-10-24 | 1996-10-09 | 株式会社日立制作所 | Vortex-type compressor |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100343529C (en) * | 2005-07-04 | 2007-10-17 | 兰州理工大学 | Vortex compressor |
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| CN1180793A (en) | 1998-05-06 |
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