CN2761877Y - Scroll compressor axial seal structure - Google Patents
Scroll compressor axial seal structure Download PDFInfo
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- CN2761877Y CN2761877Y CN 200420112362 CN200420112362U CN2761877Y CN 2761877 Y CN2761877 Y CN 2761877Y CN 200420112362 CN200420112362 CN 200420112362 CN 200420112362 U CN200420112362 U CN 200420112362U CN 2761877 Y CN2761877 Y CN 2761877Y
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Abstract
Description
技术领域technical field
本实用新型提供一种涡卷式压缩机轴向密封结构,尤其涉及一种可简化涡卷式压缩机的组装程序及增加装配的容易度,提高产品品质及降低组装成本涡卷式压缩机轴向密封结构。The utility model provides an axial sealing structure of a scroll compressor, in particular relates to a scroll compressor shaft which can simplify the assembly procedure of the scroll compressor and increase the ease of assembly, improve product quality and reduce assembly cost. To the sealing structure.
背景技术Background technique
涡卷式压缩机主要由两个涡线型的涡卷件组成,其中一个涡卷件固定不动,称为静涡卷(Fixed Scroll),另一个涡卷件则对应于静涡卷作公转运动,称之为动涡卷(Orbiting Scroll)。两涡卷件的涡线叶片相互啮合,用来促使工作流体由其吸入口进入压缩室,再经过动涡卷的连续转动,对工作流体进行压缩推动,再从静涡卷的通气孔吐出,从而完成工作流体的压缩行程。因为该工作流体在压缩行程中体积减少而压力增加,于是在两涡卷件间产生轴向气压力、径向气压力与切向气压力,其中所述轴向气压力会使两涡卷件沿轴向分离,而径向气压力与切向气压力会产生倾覆力矩。另外,所述压缩室间的压力差,将使工作流体从两涡卷的端面或叶片侧面间产生泄漏,从而降低压缩机的容积效率。另外,当碰到异常高压(如液压缩)或有异物进入压缩室时,将使涡卷叶片产生变形或刮伤壁面的情况;此外,影响压缩机的使用寿命及密封效果的另一原因在于各组成组件间的装配结构,所以如何改进压缩机的容积效率、减少涡卷件的损坏及装配结构,成为本领域技术人员所研究的重要课题。The scroll compressor is mainly composed of two scroll-type scroll parts, one of which is fixed, called the fixed scroll, and the other scroll is corresponding to the fixed scroll for orbital motion , called Orbiting Scroll. The vortex blades of the two scroll parts mesh with each other to make the working fluid enter the compression chamber from its suction port, and then through the continuous rotation of the movable scroll, the working fluid is compressed and pushed, and then spit out from the vent hole of the static scroll. Thus, the compression stroke of the working fluid is completed. Because the volume of the working fluid decreases and the pressure increases during the compression stroke, axial air pressure, radial air pressure and tangential air pressure are generated between the two scroll members, wherein the axial air pressure will make the two scroll members Separation along the axial direction, while the radial air pressure and tangential air pressure will produce an overturning moment. In addition, the pressure difference between the compression chambers will cause the working fluid to leak from the end surfaces of the two scrolls or the side surfaces of the vanes, thereby reducing the volumetric efficiency of the compressor. In addition, when encountering abnormal high pressure (such as liquid compression) or foreign matter entering the compression chamber, the scroll blade will be deformed or the wall surface will be scratched; in addition, another reason that affects the service life and sealing effect of the compressor is that The assembly structure among the various components, so how to improve the volumetric efficiency of the compressor, reduce the damage of scroll parts and the assembly structure has become an important subject to be studied by those skilled in the art.
公知的涡卷式压缩机轴向密封结构,如美国专利公告号Re.35216,其主要在静涡卷背面设有一环形槽穴(Cavity),在所述槽穴内设置有一环形浮动件,该浮动件至少具有两唇片形密封环,各密封环分别抵接于槽穴的内、外墙面周缘上,利用所述涡卷组件导引工作流体并产生背压,使静涡卷紧靠在动涡卷上,达成轴向密封的效果。The well-known scroll compressor axial sealing structure, such as U.S. Patent Publication No. Re.35216, is mainly provided with an annular groove (Cavity) on the back of the static scroll, and an annular floating member is arranged in the groove. The component has at least two lip-shaped sealing rings, and each sealing ring abuts against the inner and outer walls of the groove respectively, and uses the scroll assembly to guide the working fluid and generate back pressure, so that the static scroll is close to the On the movable scroll, the effect of axial sealing is achieved.
然而,公知的涡卷式压缩机轴向密封结构仍存在下述的缺陷:由于所述浮动件在向下装入静涡卷的槽穴时,将使得设于浮动件内、外的密封环末端,跟随浮动件的装入而向上翻起,从而使抵接于槽穴外墙的密封环,因反向设置而丧失其阻挡效果。鉴于上述现有技术中存在的缺陷,本领域技术人员为提高组装的速度及易装性,适应现场组装的要求,额外设置有特殊工具,先将所述浮动件压入治具的锥形孔口中,使密封环的末端产生缩小变形后,再将浮动件置入静涡卷的槽穴内,从而使密封环的末端紧密贴抵在静涡卷的槽穴墙面后,再将工具从槽穴中抽出,由于静涡卷及浮动件的结构形状,造成组装过程相当繁琐复杂,大幅增加装配工时,使制造成本无法有效获得改进。However, the known axial sealing structure of the scroll compressor still has the following defects: when the floating member is installed downward into the groove of the fixed scroll, the sealing rings located inside and outside the floating member will The end is turned up following the installation of the floating part, so that the sealing ring abutting against the outer wall of the groove loses its blocking effect due to the reverse setting. In view of the defects in the above-mentioned prior art, in order to improve the assembly speed and ease of assembly, and meet the requirements of on-site assembly, those skilled in the art are provided with additional special tools, and first press the floating part into the tapered hole of the jig After shrinking and deforming the end of the sealing ring, put the floating part into the groove of the static scroll, so that the end of the sealing ring is closely attached to the wall of the groove of the static scroll, and then remove the tool from the groove. Due to the structural shape of the static scroll and the floating part, the assembly process is quite cumbersome and complicated, which greatly increases the assembly man-hours and makes it impossible to effectively improve the manufacturing cost.
鉴于此,本设计人为改进并解决上述现有技术中存在的缺陷,经过潜心研究并配合学理的运用,终于提出一种设计合理且有效改进上述缺陷的本实用新型。In view of this, this design artificially improves and solves the defects in the above-mentioned prior art. After painstaking research and the application of theories, a utility model with reasonable design and effective improvement of the above-mentioned defects is finally proposed.
本实用新型的内容Contents of the utility model
本实用新型的一个目的在于提供一种涡卷式压缩机轴向密封结构,其是将密封组件呈顺向设置在浮动件及静涡卷上,可简化组装程序及增加装配的容易度,大幅提高产品品质及降低组装成本。One purpose of this utility model is to provide a scroll compressor axial sealing structure, which is to arrange the sealing assembly on the floating part and the static scroll in a forward direction, which can simplify the assembly procedure and increase the ease of assembly, greatly Improve product quality and reduce assembly costs.
本实用新型的另一个目的在于提供一种涡卷式压缩机轴向密封结构,其是将浮动件设置在分隔件及静涡卷背面之间,并在静涡卷与浮动件间形成有背压室,用来推动静涡卷与动涡卷紧密贴合,从而提高所述压缩机的容积效率。Another object of the present utility model is to provide a scroll compressor axial sealing structure, which is that the floating part is arranged between the separator and the back of the static scroll, and a back is formed between the static scroll and the floating part. The pressure chamber is used to push the fixed scroll and the movable scroll to be in close contact, so as to improve the volumetric efficiency of the compressor.
本实用新型的再一目的在于提供一种涡卷式压缩机轴向密封结构,其是利用浮动件的设置,当液压缩或异物进入压缩室时,静涡卷能产生轴向退让,从而减少涡卷组件的损坏机率,而且在浮动件的端面设有磨耗自动补偿,从而大幅提高压缩机的可靠度。Another object of the present utility model is to provide a scroll compressor axial sealing structure, which uses the setting of floating parts. When the liquid is compressed or foreign matter enters the compression chamber, the static scroll can produce axial retreat, thereby reducing The damage probability of the scroll assembly is reduced, and the end face of the floating part is equipped with automatic wear compensation, thereby greatly improving the reliability of the compressor.
为了实现上述目的,本实用新型提供一种涡卷式压缩机轴向密封结构,包括:In order to achieve the above purpose, the utility model provides an axial sealing structure of a scroll compressor, including:
一壳体,包括有一第一壳体及一第二壳体,所述第一壳体内部形成有一容置室,在该容置室内设有一分隔件,用来将壳体内部的流体分隔为高压区及低压区;A casing, including a first casing and a second casing, an accommodating chamber is formed inside the first casing, and a partition is provided in the accommodating chamber to separate the fluid inside the casing into High pressure area and low pressure area;
一涡卷组件,由一静涡卷及一设于其下方的动涡卷所组成,在两涡卷件间形成有压缩室,所述静涡卷设置在第一壳体内,在其背面设有凸出部,该凸出部开设有与压缩室相通的通气孔;以及A scroll assembly is composed of a static scroll and a movable scroll below it, a compression chamber is formed between the two scroll parts, the static scroll is arranged in the first casing, and a a protruding portion opening with a vent hole communicating with the compression chamber; and
一浮动件,设置在所述分隔件及静涡卷之间,所述浮动件设有连通孔及凹入部,所述连通孔与静涡卷的通气孔对应设置,而凹入部则与静涡卷的凸出部相应配合,而且在静涡卷与浮动件之间设有密封组件并形成有背压室,从而实现上述目的。A floating part is arranged between the partition part and the static scroll, and the floating part is provided with a communication hole and a recessed part, the communication hole is arranged corresponding to the air hole of the static scroll, and the recessed part is connected with the static scroll The protruding part of the roll is matched accordingly, and a sealing assembly and a back pressure chamber are formed between the fixed scroll and the floating part, so as to achieve the above purpose.
本实用新型的涡卷式压缩机轴向密封结构能够简化组装程序及增加装配的容易度,大幅提高产品品质及降低组装成本;提高压缩机的容积效率;减少两涡卷间的摩擦损耗,使压缩机的使用寿命大幅提高。The scroll compressor axial sealing structure of the utility model can simplify the assembly procedure and increase the ease of assembly, greatly improve the product quality and reduce the assembly cost; improve the volumetric efficiency of the compressor; reduce the friction loss between the two scrolls, so that The service life of the compressor is greatly improved.
附图的简要说明Brief description of the drawings
图1为本实用新型第一实施例的组合剖视图;Fig. 1 is the combined sectional view of the first embodiment of the utility model;
图2为图1中A部分的局部放大图;Fig. 2 is a partially enlarged view of part A in Fig. 1;
图3为本实用新型第一实施例的使用状态图;Fig. 3 is the use status diagram of the first embodiment of the utility model;
图4为本实用新型第二实施例的组合剖视图。Fig. 4 is a combined sectional view of the second embodiment of the present invention.
附图中,各标号所代表的部件列表如下:In the accompanying drawings, the list of parts represented by each label is as follows:
10-壳体10-shell
11-第一壳体 12-第二壳体11-First shell 12-Second shell
13-容置室 14-分隔件13-Accommodating chamber 14-Separator
141-开口 15-高压区141-opening 15-high pressure zone
16-低压区 17-排气口16-Low pressure zone 17-Exhaust port
18-传动轴18-drive shaft
20-涡卷组件20-Scroll assembly
21-静涡卷 211-,221-叶片21-static scroll 211-, 221-blade
22-动涡卷 23-凸出部22-moving scroll 23-bulge
24-通气孔 25-通孔24-vent hole 25-through hole
26-压缩室 27-轴孔26-compression chamber 27-shaft hole
30-浮动件30-floating piece
31-第一圆环 32-第二圆环31-First Ring 32-Second Ring
33-凹入部 34-连通孔33-recessed part 34-communicating hole
35-筒体 36-抵接部35-Cylinder 36-Abutting part
37-密封组件 38-背压室37-Seal assembly 38-Back pressure chamber
具体实施方式Detailed ways
为了使本领域技术人员进一步了解本实用新型的特征及技术内容,请参阅以下有关本实用新型的详细说明与附图,附图仅提供参考与说明用,并非用来限制本实用新型。In order for those skilled in the art to further understand the features and technical contents of the present utility model, please refer to the following detailed description and accompanying drawings of the present utility model. The accompanying drawings are provided for reference and illustration only, and are not intended to limit the present utility model.
图1及图2分别为本实用新型第一实施例的组合剖视图及图1中A部分的局部放大图。如图1及图2所示,本实用新型提供一种涡卷式压缩机轴向密封结构,包括有一壳体10、一涡卷组件20及一浮动件30,其中:FIG. 1 and FIG. 2 are a combined cross-sectional view of the first embodiment of the present invention and a partial enlarged view of part A in FIG. 1, respectively. As shown in Figure 1 and Figure 2, the utility model provides a scroll compressor axial sealing structure, including a
壳体10包括有一第一壳体11及一第二壳体12,各壳体都具有一中空容腔,而且可以用螺栓等固定组件或以焊接方式将第一壳体11与第二壳体12相连接。第一壳体11内部形成有一容置室13,在容置室13内部设有一分隔件14,用来将壳体10内部的流体区分为高压区15及低压区16。分隔件14可以是一圆形平板,在该平板的中央开设有一圆形开口141;另外,在容置室13的一端连接有一排气口17。第二壳体12的周缘上开设有一工作流体进流口(图中未示出),在其内部安装有多个压缩机组件、传动机构及马达等构件,其中马达中心设置有一传动轴18,由于所述构件及机构都与公知技术相同,在此不再予于赘述。The
涡卷组件20设置于壳体10的内部,由一静涡卷21及一动涡卷22组成。静涡卷21的下方设置有涡线形叶片211,上方设置有一圆形凸出部23。在凸出部23的中央处开设有一个或一个以上的通气孔24,通气孔24为呈上大下小的阶梯状圆孔,其对应于分隔件14的开口141设置,在其两侧间隔一适当距离处分别开设有通孔25。在动涡卷22的上方也设有涡旋形叶片221,叶片221与静涡卷21的叶片211相应配合,并在两叶片211、221间形成有多个压缩室26。在动涡卷22的下方设有轴孔27,轴孔27内部设置有轴承(Bearing)及偏心衬套,该衬套供马达的传动轴18穿设连接。The
浮动件30设置在第一壳体11的分隔件14及涡卷组件20的静涡卷21之间,其底部由第一圆环31及第二圆环32构成,在所述圆环的间隔处形成有一凹入部33,凹入部33可供静涡卷21的凸出部23设置。在第一圆环31的中央开设有连通孔34,连通孔34分别与凸出部23的通气孔24及分隔件14的开口141对应设置。在浮动件30的第一圆环31的顶面延伸凸出有一筒体35,筒体35可插入分隔件14的开口141中,并与开口141的内缘相配合。在筒体35的外部周围设有一环形抵接部36,抵接部36可与分隔件14的底面相贴合。The floating
在静涡卷21的凸出部23及浮动件30的凹入部33间设置有两密封组件37,密封组件37可为唇片(Lip Seal)、O形环(O-Ring)、U形密封圈(断面为U字形)、机械轴封(Meachanical Seal)或其它形式的密封组件,本实施例为唇片。其中一密封组件37的一端固定于第二圆环32的端面上,并用固定环及螺丝等组件锁紧固定,另一端则抵接于静涡卷21的凸出部23的外部周缘;另一密封组件37的一端固定于凸出部23的通气孔24周围上,并用固定环及螺丝等组件锁紧固定,另一端则抵接于第一圆环31的外部周缘。于是,在凹入部33、凸出部23及密封组件37间围绕形成有一背压室38,背压室38可利用凸出部23的通孔25与压缩室26连通,而导入中压的工作流体,从而形成一中压背压室的形态。Two
组合时先将唇片形密封组件37分别固定于第二圆环32及通气孔24周缘的端面上,再将浮动件30直接由上往下置入并与静涡卷21相连接。因为固定于第二圆环32及通气孔24周缘的密封组件37的末端都朝向内侧设置,使得浮动件30在移动装入时,可一并推开密封组件37的末端,从而产生相应的向上与向下变形,该变形方向正好与密封组件37的装设方向相同,由此,即可增加装配的容易度及简化组装程序,还能省略公知治具的设计与操作,从而大幅提高产品品质及降低组装成本。When assembling, the lip-shaped
图3为本实用新型第一实施例的使用状态图。如图3所示,通过上述组件的组合,当动涡卷22受传动轴17的驱动而转动时,低压工作流体从第二壳体12的进流口吸入,并进入静涡卷21的叶片211与动涡卷22的叶片221所构成的压缩室26内,随着动涡卷22的公转运动,工作流体会由涡卷组件20的外缘逐渐往中央部位移动,其体积逐渐减小而压力则由低压状态升至中压状态,所述中压流体将从凸出部23的通孔25进入背压室38中,从而推动浮动件30向上移动,并使静涡卷21产生向下的移动,与动涡卷22紧密贴合,从而达到密封效果。Fig. 3 is a diagram of the usage state of the first embodiment of the utility model. As shown in Figure 3, through the combination of the above components, when the
图4为本实用新型第二实施例的组合剖视图。如图4所示,第一壳体11的容置室13内延伸有一分隔件14,本实施例的分隔件14为一圆筒柱,所述圆筒柱中央具有一圆形开口141,开口141与第一壳体11的排气口17相连通,且其内缘直径与浮动件30的筒体35外缘直径相应配合,并使圆筒柱的底部端面与浮动件30的抵接部36相互对应贴合。Fig. 4 is a combined sectional view of the second embodiment of the present invention. As shown in Figure 4, a
本实用新型的涡卷式压缩机轴向密封结构具有以下优点:利用本实用新型密封组件呈顺向设置于浮动件及静涡卷上,可简化组装程序及增加装配的容易度,进而大幅提升产品品质及降低组装成本。另外,将浮动件设于分隔件及静涡卷背面之间,并在静涡卷与浮动件间形成背压室,以推动静涡卷与动涡卷紧密贴合,进而提高所述压缩机的容积效率。另外,导引中压的工作流体进入背压室,迫使该工作流体推动静涡卷的背面,使静涡卷沿着轴向向下移动,以克服压缩室在运转中施加给静涡卷的轴向气压力与倾覆力矩,并能减少两涡卷间的摩擦损耗,使得压缩机的使用寿命大幅提高。The axial sealing structure of the scroll compressor of the utility model has the following advantages: the sealing assembly of the utility model is arranged on the floating member and the static scroll in a forward direction, which can simplify the assembly procedure and increase the ease of assembly, thereby greatly improving Product quality and lower assembly costs. In addition, the floating part is arranged between the separator and the back of the fixed scroll, and a back pressure chamber is formed between the fixed scroll and the floating part, so as to push the fixed scroll and the moving scroll to be closely bonded, thereby improving the performance of the compressor. volumetric efficiency. In addition, the medium-pressure working fluid is introduced into the back pressure chamber, and the working fluid is forced to push the back of the static scroll, so that the static scroll moves downward in the axial direction, so as to overcome the pressure exerted by the compression chamber on the static scroll during operation. The axial air pressure and overturning moment can reduce the friction loss between the two scrolls, so that the service life of the compressor is greatly improved.
综上所述,本实用新型的涡卷式压缩机轴向密封结构具有实用性、新颖性与创造性,且本实用新型的结构也不曾见于同类产品及公开使用过,申请前更未刊登在任何刊物上,完全符合实用新型专利申请的要求。To sum up, the scroll compressor axial sealing structure of the present utility model has practicality, novelty and creativity, and the structure of the utility model has never been seen in similar products and has been publicly used, and has not been published in any The publications fully meet the requirements for utility model patent applications.
以上所述仅为本实用新型的优选实施例,并非因此即限制本实用新型的专利范围,凡是运用本实用新型说明书及附图内容所作的等效结构变换,或直接或间接运用在其它相关的技术领域,均同理包括在本实用新型的专利范围内。The above descriptions are only preferred embodiments of the present utility model, and are not intended to limit the patent scope of the present utility model. All equivalent structural transformations made by using the description of the utility model and the contents of the accompanying drawings, or directly or indirectly used in other related Technical fields are all included in the patent scope of the present utility model in the same way.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420112362 CN2761877Y (en) | 2004-10-29 | 2004-10-29 | Scroll compressor axial seal structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420112362 CN2761877Y (en) | 2004-10-29 | 2004-10-29 | Scroll compressor axial seal structure |
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| Publication Number | Publication Date |
|---|---|
| CN2761877Y true CN2761877Y (en) | 2006-03-01 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200420112362 Expired - Fee Related CN2761877Y (en) | 2004-10-29 | 2004-10-29 | Scroll compressor axial seal structure |
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| Country | Link |
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| CN (1) | CN2761877Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103016344A (en) * | 2008-01-16 | 2013-04-03 | 艾默生环境优化技术有限公司 | Scroll machine |
| CN105570127A (en) * | 2016-02-16 | 2016-05-11 | 珠海格力节能环保制冷技术研究中心有限公司 | Compressor and air conditioner with same |
| CN115596666A (en) * | 2022-10-18 | 2023-01-13 | 旭星新能源科技(苏州)有限公司(Cn) | Split sealing structure of scroll compressor |
-
2004
- 2004-10-29 CN CN 200420112362 patent/CN2761877Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103016344A (en) * | 2008-01-16 | 2013-04-03 | 艾默生环境优化技术有限公司 | Scroll machine |
| CN103016344B (en) * | 2008-01-16 | 2015-08-12 | 艾默生环境优化技术有限公司 | Scroll machine |
| CN105570127A (en) * | 2016-02-16 | 2016-05-11 | 珠海格力节能环保制冷技术研究中心有限公司 | Compressor and air conditioner with same |
| CN115596666A (en) * | 2022-10-18 | 2023-01-13 | 旭星新能源科技(苏州)有限公司(Cn) | Split sealing structure of scroll compressor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: FUSHENG CO., LTD. Free format text: FORMER OWNER: QING-YU INTERNATIONAL CO., LTD. Effective date: 20090424 |
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| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20090424 Address after: Postcode of Taiwan, china: Patentee after: Fusheng Co., Ltd. Address before: Postcode of Taiwan, china: Patentee before: Qingyu International Co., Ltd. |
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| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20060301 Termination date: 20101029 |