CN104251198A - Lubricating structure for linear compressor - Google Patents
Lubricating structure for linear compressor Download PDFInfo
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Abstract
本发明公开了一种直线压缩机的润滑结构,包括气缸和前法兰,所述前法兰上设置有供油管路,其中所述前法兰与气缸结合面之间设有可使润滑油从供油管路输送至活塞表面的第一油路。本发明直线压缩机的润滑结构可以降低活塞与气缸壁间的摩擦,抑制二者之间的接触部位温度升高,使直线压缩机的性能提高。
The invention discloses a lubricating structure of a linear compressor, which comprises a cylinder and a front flange. An oil supply pipeline is arranged on the front flange, and a lubricating oil is provided between the front flange and the joint surface of the cylinder. Oil is delivered from the oil supply line to the first oil passage on the surface of the piston. The lubricating structure of the linear compressor of the present invention can reduce the friction between the piston and the cylinder wall, suppress the temperature rise of the contact part between the two, and improve the performance of the linear compressor.
Description
技术领域 technical field
本发明涉及一种直线压缩机,特别指一种直线压缩机的润滑结构。 The invention relates to a linear compressor, in particular to a lubricating structure of a linear compressor.
背景技术 Background technique
现有的直线压缩机包括外壳,外壳的内腔底部储存有润滑油。外壳内装有圆筒形外定子,外定子的内腔设置有圆筒形内定子,外定子与内定子同轴心,在外定子与内定子之间插置有圆筒形动子。内定子内置有线圈,在内定子的内腔中设置有同轴心的活塞,活塞的一端活动插置于动子上,另一端活动插置于气缸内腔中,气缸内设有排气阀片,活塞、气缸及排气阀片共同围成了内置有制冷剂气体的压缩腔。当线圈通电时,内定子和外定子形成磁场强度变化的磁场。在磁场力的作用下,动子沿轴向往复运动,动子带动活塞沿气缸的内腔往复运动,从而压缩填充在压缩腔内的制冷剂气体,制冷剂气体被压缩后释放出大量热量,同时,活塞的外表面与气缸的内腔壁之间相互摩擦,使活塞和气缸相接触部位温度长高,这些热量使气缸的温度升高,容易导致直线压缩机的性能降低。 The existing linear compressor includes a shell, and lubricating oil is stored at the bottom of the inner cavity of the shell. The shell is equipped with a cylindrical outer stator, the inner cavity of the outer stator is provided with a cylindrical inner stator, the outer stator and the inner stator are coaxial, and a cylindrical mover is inserted between the outer stator and the inner stator. The inner stator has a built-in coil, and a coaxial piston is set in the inner cavity of the inner stator. One end of the piston is movably inserted on the mover, and the other end is movably inserted in the inner cavity of the cylinder, and an exhaust valve is installed in the cylinder. Piston, cylinder and exhaust valve together form a compression chamber with built-in refrigerant gas. When the coil is energized, the inner stator and the outer stator form a magnetic field with varying magnetic field strength. Under the action of the magnetic field force, the mover reciprocates in the axial direction, and the mover drives the piston to reciprocate along the inner cavity of the cylinder, thereby compressing the refrigerant gas filled in the compression chamber. After the refrigerant gas is compressed, a large amount of heat is released. At the same time, the friction between the outer surface of the piston and the inner wall of the cylinder will increase the temperature of the contact part between the piston and the cylinder, and the heat will increase the temperature of the cylinder, which will easily lead to a decrease in the performance of the linear compressor.
发明内容 Contents of the invention
本发明的目的在于提供一种直线压缩机的润滑结构,其可以降低活塞与气缸壁间的摩擦,抑制二者之间的接触部位温度升高,使直线压缩机的性能提高。 The purpose of the present invention is to provide a lubricating structure for a linear compressor, which can reduce the friction between the piston and the cylinder wall, suppress the temperature rise of the contact part between the two, and improve the performance of the linear compressor.
为了实现上述目的,本发明提供了一种直线压缩机的润滑结构,包括气缸和前法兰,所述前法兰上设置有供油管路,其中所述前法兰与气缸结合面之间设有可使润滑油从供油管路输送至活塞表面的第一油路。 In order to achieve the above object, the present invention provides a lubricating structure for a linear compressor, which includes a cylinder and a front flange, and an oil supply pipeline is arranged on the front flange, wherein the joint surface between the front flange and the cylinder There is a first oil passage for delivering lubricating oil from the oil supply pipeline to the surface of the piston.
所述第一油路包括由设置于前法兰壁上的水平向凹槽与气缸壁相互配合形成的通路,或包括由设置于气缸壁上的水平向凹槽与前法兰壁相互配合形成的通路,或包括由设置于前法兰壁上的水平向凹槽与设置于气缸壁上的凹槽配合形成的通路。 The first oil passage includes a passage formed by the cooperation of the horizontal groove provided on the front flange wall and the cylinder wall, or a passage formed by the cooperation of the horizontal groove provided on the cylinder wall and the front flange wall The passage, or the passage formed by the cooperation of the horizontal groove arranged on the front flange wall and the groove arranged on the cylinder wall.
所述前法兰的内壁面一侧形成有台阶部,所述气缸一侧嵌入该台阶部,所述第一油路包括由所述气缸和/或所述台阶部上于两者相接触处形成的竖直向凹槽,所述竖直向凹槽与所述水平向凹槽连通。 A step portion is formed on one side of the inner wall of the front flange, and one side of the cylinder is embedded in the step portion, and the first oil passage includes the contact between the cylinder and/or the step portion A vertical groove is formed, and the vertical groove communicates with the horizontal groove.
还包括连通第一油路和供油机构的回油管路。 It also includes an oil return line connecting the first oil line and the oil supply mechanism.
采用上述方案后,本发明直线压缩机的润滑结构通过在前法兰与气缸结合面之间设置可使润滑油从供油管路输送至活塞表面的第一油路,这样设计可以使润滑油进入气缸与活塞之间,使二者保持润滑,避免了活塞运行时干摩擦发生,从而抑制了活塞与气缸之间接触部位温度升高,达到活塞与气缸的润滑效果,使直线压缩机的性能提高。 After adopting the above scheme, the lubricating structure of the linear compressor of the present invention can make the lubricating oil transported from the oil supply pipeline to the first oil passage on the surface of the piston by setting the first oil path between the front flange and the cylinder joint surface. This design can make the lubricating oil It enters between the cylinder and the piston to keep them lubricated, avoiding the occurrence of dry friction when the piston is running, thereby inhibiting the temperature rise of the contact part between the piston and the cylinder, achieving the lubrication effect of the piston and the cylinder, and improving the performance of the linear compressor improve.
本发明的进一步有益效果是:将第一油路设计为包括由设置于前法兰壁上的水平向凹槽与气缸壁相互配合形成的通路,或由设置于气缸壁上的水平向凹槽与前法兰壁相互配合形成的通路,或包括由设置于前法兰壁上的水平向凹槽与设置于气缸壁上的水平向凹槽配合形成的通路,这样设计的第一油路在保证能进入活塞表面的同时,该第一油路便于加工,且加工工艺简单,节省成本,结构简单紧凑。 A further beneficial effect of the present invention is: the first oil passage is designed to include a passage formed by the cooperation between the horizontal groove arranged on the front flange wall and the cylinder wall, or the horizontal groove arranged on the cylinder wall The passage formed by cooperating with the front flange wall, or the passage formed by the cooperation of the horizontal groove provided on the front flange wall and the horizontal groove provided on the cylinder wall, the first oil passage designed in this way is While ensuring that it can enter the surface of the piston, the first oil passage is easy to process, has a simple process, saves costs, and has a simple and compact structure.
本发明的进一步有益效果是:通过设计与第一油路和供油机构连通的回油管路,可以保证润滑油能够循环流动进入气缸与活塞之间,使气缸与活塞之间始终保持润滑。 The further beneficial effect of the present invention is: by designing the oil return line connected with the first oil line and the oil supply mechanism, it can ensure that the lubricating oil can circulate and flow between the cylinder and the piston, so that the cylinder and the piston are always lubricated.
附图说明 Description of drawings
图1为本发明直线压缩机的润滑结构第一实施例结构示意图; Fig. 1 is a structural schematic diagram of the first embodiment of the lubricating structure of the linear compressor of the present invention;
图2为图1的A-A向剖面示意图; Fig. 2 is the A-A direction sectional schematic diagram of Fig. 1;
图3为本发明直线压缩机的润滑结构第二实施例结构示意图; Fig. 3 is a structural schematic diagram of the second embodiment of the lubrication structure of the linear compressor of the present invention;
图4为本发明直线压缩机的润滑结构第三实施例结构示意图。 Fig. 4 is a structural schematic diagram of the third embodiment of the lubricating structure of the linear compressor of the present invention.
具体实施方式 Detailed ways
下面结合附图和具体实施例对本发明作进一步说明,以使本领域的技术人员可以更好的理解本发明并能予以实施,但所举实施例不作为对本发明的限定。 The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments, so that those skilled in the art can better understand the present invention and implement it, but the examples given are not intended to limit the present invention.
如图1和图2所示,为本发明直线压缩机的润滑结构第一实施例结构示意图,包括外壳1,外壳1的内腔底部储存有润滑油。外壳1内装有圆筒形外定子14,外定子14的内腔设置有圆筒形内定子15,外定子14与内定子15同轴心,在外定子14与内定子15之间插置有圆筒形动子16。内定子15内置有线圈17,在内定子15的内腔中设置有同轴心的活塞10,活塞10的左端活动插置于动子16的内壁上,右端插置于位于外壳1内的气缸3的内腔中。气缸3内设有排气阀片18,活塞10、气缸3及排气阀片18共同围成了内置有制冷剂气体的压缩腔。外壳1内的润滑油与供油机构2连通,供油机构2置于外壳1内的润滑油中。气缸3的外表面安装有前法兰4,气缸3和前法兰4均为圆筒形。 As shown in Fig. 1 and Fig. 2, it is a structural schematic diagram of the first embodiment of the lubricating structure of the linear compressor of the present invention, including a casing 1, and lubricating oil is stored at the bottom of the inner cavity of the casing 1. The shell 1 is equipped with a cylindrical outer stator 14, the inner cavity of the outer stator 14 is provided with a cylindrical inner stator 15, the outer stator 14 and the inner stator 15 are coaxial, and a circle is inserted between the outer stator 14 and the inner stator 15. Cylindrical mover 16. The inner stator 15 has a built-in coil 17, and a coaxial piston 10 is arranged in the inner cavity of the inner stator 15. The left end of the piston 10 is movably inserted on the inner wall of the mover 16, and the right end is inserted into the cylinder located in the casing 1. 3 in the lumen. An exhaust valve plate 18 is arranged in the cylinder 3, and the piston 10, the cylinder 3 and the exhaust valve plate 18 together form a compression chamber with a built-in refrigerant gas. The lubricating oil in the shell 1 communicates with the oil supply mechanism 2, and the oil supply mechanism 2 is placed in the lubricating oil in the shell 1. A front flange 4 is installed on the outer surface of the cylinder 3, and both the cylinder 3 and the front flange 4 are cylindrical.
前法兰4上沿径向延伸有供油管路7和第三油路8。供油管路7和第三油路8围绕前法兰4的周向对称设置。供油管路7位于第三油路8的下方。前法兰4的内壁面右端形成台阶部6,气缸3的左端嵌置在台阶部6上。气缸3上与台阶部6相接触处形成由水平向凹槽与竖直向凹槽构成的L形第一凹槽12,该第一凹槽12与台阶部6相接触面形成第一油路。该第一油路可使润滑油流在活塞10的外表面,第一油路与供油管路7及第三油路8均连通。第三油路8用以将流经第一油路的润滑油排至外壳1内的润滑油中。该第一油路位于活塞10的上部。 An oil supply line 7 and a third oil line 8 extend radially on the front flange 4 . The oil supply pipeline 7 and the third oil passage 8 are arranged symmetrically around the circumference of the front flange 4 . The oil supply line 7 is located below the third oil line 8 . The right end of the inner wall surface of the front flange 4 forms a stepped portion 6 , and the left end of the cylinder 3 is embedded on the stepped portion 6 . An L-shaped first groove 12 composed of a horizontal groove and a vertical groove is formed on the cylinder 3 in contact with the stepped portion 6, and the contact surface of the first groove 12 and the stepped portion 6 forms a first oil passage . The first oil passage can make lubricating oil flow on the outer surface of the piston 10 , and the first oil passage communicates with the oil supply pipeline 7 and the third oil passage 8 . The third oil passage 8 is used to discharge the lubricating oil flowing through the first oil passage into the lubricating oil in the housing 1 . The first oil passage is located on the upper part of the piston 10 .
气缸3上与台阶部6相接触处沿周向还形成有环形第二凹槽13,第二凹槽13通过具有规定硬度的油管9与供油机构2连通。该第二凹槽13与台阶部6相接触面形成第二油路。该第二油路可供润滑油流通,且其与第一油路、供油管路7及第三油路8均连通。第二油路、第三油路8及油管9形成回油管路。 A ring-shaped second groove 13 is also formed on the cylinder 3 in contact with the stepped portion 6 along the circumferential direction, and the second groove 13 communicates with the oil supply mechanism 2 through the oil pipe 9 with a predetermined hardness. The contact surface of the second groove 13 and the step portion 6 forms a second oil passage. The second oil passage can circulate lubricating oil, and it is in communication with the first oil passage, the oil supply pipeline 7 and the third oil passage 8 . The second oil passage, the third oil passage 8 and the oil pipe 9 form an oil return pipeline.
如图3所示,为本发明直线压缩机的润滑结构第二实施例结构示意图,其大部分结构与上述实施例一的结构相同,其不同之处是:台阶部6上与气缸3相接触处形成L形第一凹槽12’,该第一凹槽12’与气缸3相接触面形成第一油路。台阶部6上与气缸3相接触处沿周向还形成有环形第二凹槽13’,该第二凹槽13’与气缸3相接触面形成第二油路。 As shown in Figure 3, it is a schematic structural diagram of the second embodiment of the lubrication structure of the linear compressor of the present invention. Most of its structure is the same as that of the first embodiment above, and the difference is that the step part 6 is in contact with the cylinder 3 An L-shaped first groove 12' is formed at the position, and the contact surface of the first groove 12' and the cylinder 3 forms a first oil passage. A ring-shaped second groove 13' is also formed on the part of the step part 6 that is in contact with the cylinder 3 along the circumferential direction, and the surface of the second groove 13' that contacts the cylinder 3 forms a second oil passage.
如图4所示,为本发明直线压缩机的润滑结构第三实施例结构示意图,其大部分结构与上述实施例一的结构相同,其不同之处是:台阶部6与气缸3相接触处分别形成L形第一凹槽12″,两个L形第一凹槽12″形成第一油路。台阶部6与气缸3相接触处分别沿周向形成环形第二凹槽13″,两个第二凹槽13″形成第二油路。 As shown in Figure 4, it is a schematic structural diagram of the third embodiment of the lubrication structure of the linear compressor of the present invention. Most of its structure is the same as that of the first embodiment above, and the difference is that the step part 6 is in contact with the cylinder 3 L-shaped first grooves 12" are formed respectively, and two L-shaped first grooves 12" form a first oil passage. Ring-shaped second grooves 13 ″ are respectively formed in the contact positions of the stepped portion 6 and the cylinder 3 along the circumferential direction, and the two second grooves 13 ″ form a second oil passage.
以上所述实施例仅是为充分说明本发明而所举的较佳的实施例,本发明的保护范围不限于此。本技术领域的技术人员在本发明基础上所作的等同替代或变换,均在本发明的保护范围之内。本发明的保护范围以权利要求书为准。 The above-mentioned embodiments are only preferred embodiments for fully illustrating the present invention, and the protection scope of the present invention is not limited thereto. Equivalent substitutions or transformations made by those skilled in the art on the basis of the present invention are all within the protection scope of the present invention. The protection scope of the present invention shall be determined by the claims.
Claims (4)
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| CN201310255133.9A CN104251198B (en) | 2013-06-25 | 2013-06-25 | The lubrication system of linear compressor |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109058078A (en) * | 2018-08-07 | 2018-12-21 | 青岛海尔智能技术研发有限公司 | A kind of compressor and refrigeration equipment |
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Application publication date: 20141231 Assignee: WanBao Group Compressor Co., Ltd. Assignor: Intellectual technology research and development Co., Ltd of Qingdao Haier Contract record no.: 2015990000261 Denomination of invention: Lubricating structure for linear compressor License type: Common License Record date: 20150429 |
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Application publication date: 20141231 Assignee: Jiaxibeila Compressor Co., Ltd. Assignor: Intellectual technology research and development Co., Ltd of Qingdao Haier Contract record no.: 2015990000349 Denomination of invention: Lubricating structure for linear compressor License type: Common License Record date: 20150525 |
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