CN114810586A - scroll compressor - Google Patents
scroll compressor Download PDFInfo
- Publication number
- CN114810586A CN114810586A CN202110063622.9A CN202110063622A CN114810586A CN 114810586 A CN114810586 A CN 114810586A CN 202110063622 A CN202110063622 A CN 202110063622A CN 114810586 A CN114810586 A CN 114810586A
- Authority
- CN
- China
- Prior art keywords
- scroll
- orbiting scroll
- orbiting
- compression mechanism
- cylindrical wall
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000006835 compression Effects 0.000 claims abstract description 101
- 238000007906 compression Methods 0.000 claims abstract description 101
- 239000012530 fluid Substances 0.000 claims abstract description 31
- 238000000926 separation method Methods 0.000 claims abstract description 10
- 230000002093 peripheral effect Effects 0.000 claims description 24
- 238000004891 communication Methods 0.000 claims description 5
- 238000007789 sealing Methods 0.000 description 18
- 239000012535 impurity Substances 0.000 description 7
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 239000003507 refrigerant Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000008094 contradictory effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/02—Rotary-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
- F04C18/0207—Rotary-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
- F04C18/0215—Rotary-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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C23/00—Combinations 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
- F04C23/001—Combinations 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 of similar working principle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C27/00—Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/12—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/30—Casings or housings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rotary Pumps (AREA)
Abstract
Description
技术领域technical field
本公开涉及一种涡旋压缩机,特别是,涉及一种具有双压缩机构的涡旋压缩机。The present disclosure relates to a scroll compressor, and more particularly, to a scroll compressor with a dual compression mechanism.
背景技术Background technique
本部分的内容仅提供了与本公开相关的背景信息,其可能并不构成现有技术。The content in this section merely provides background information related to the present disclosure and may not constitute prior art.
涡旋压缩机可以包括第一涡旋压缩机构和第二涡旋压缩机构以满足容量需求。第一涡旋压缩机构和第二涡旋压缩机构各自包括定涡旋和动涡旋,其中,动涡旋相对于对应的定涡旋绕动以压缩工作流体。The scroll compressor may include a first scroll compression mechanism and a second scroll compression mechanism to meet capacity requirements. The first scroll compression mechanism and the second scroll compression mechanism each include a fixed scroll and an orbiting scroll, wherein the orbiting scroll orbits relative to the corresponding fixed scroll to compress the working fluid.
在压缩机运行期间,不可避免地会将杂质引入压缩机构中,具体地,引入定涡旋与动涡旋的相互啮合的涡卷之间。此时,为避免对涡卷造成损害,期望的是,定涡旋和动涡旋的涡卷能够彼此分离。这种允许定涡旋和动涡旋的涡卷能够彼此分离的性能也被称为柔性性能。例如,允许定涡旋和动涡旋能够沿轴向彼此分离的结构被称为轴向柔性结构,而允许定涡旋和动涡旋能够沿径向彼此分离的结构则被称为径向柔性结构。During the operation of the compressor, impurities are inevitably introduced into the compression mechanism, specifically, between the intermeshing wraps of the fixed scroll and the movable scroll. At this time, in order to avoid damage to the wraps, it is desirable that the wraps of the fixed scroll and the movable scroll can be separated from each other. This capability of allowing the wraps of the fixed scroll and the movable scroll to be able to be separated from each other is also referred to as the flexibility capability. For example, a structure that allows the fixed scroll and the movable scroll to be able to be separated from each other in the axial direction is called an axially flexible structure, and a structure that allows the fixed scroll and the movable scroll to be able to be separated from each other in the radial direction is called a radially flexible structure structure.
然而,对于具有双涡旋压缩机构的压缩机而言,由于双涡旋压缩机构的运动情况以及各个部件的受力情况比较复杂,因此结构设计比较困难且比较复杂,尺寸也较大。特别地,现有的具有双涡旋压缩机构的压缩机不具有径向柔性结构和/或轴向柔性结构,或者具有很复杂的轴向柔性结构。However, for a compressor with a twin-scroll compression mechanism, the structure design is difficult and complicated, and the size is larger because the motion of the twin-scroll compression mechanism and the stress of each component are complex. In particular, the existing compressors with the double scroll compression mechanism do not have a radially flexible structure and/or an axially flexible structure, or have a very complex axially flexible structure.
鉴于上述事实,本领域中期望提供一种具有实现轴向和/或径向柔性的双涡旋压缩机构的压缩机,该压缩机具有紧凑和简单的结构。In view of the above-mentioned facts, it is desirable in the art to provide a compressor having a twin scroll compression mechanism realizing axial and/or radial flexibility, which compressor has a compact and simple structure.
发明内容SUMMARY OF THE INVENTION
在本部分中提供本发明的总体概要,而不是本发明完全范围或本发明所有特征的全面公开。A general summary of the invention is provided in this section, rather than a comprehensive disclosure of its full scope or all of its features.
本公开的一个目的是提供一种具有实现径向柔性的双涡旋压缩机构的压缩机,该压缩机提高了涡旋压缩机的可靠性并且具有简单的结构。An object of the present disclosure is to provide a compressor having a twin scroll compression mechanism realizing radial flexibility, which improves the reliability of the scroll compressor and has a simple structure.
本公开的另一个目的是提供一种具有实现轴向柔性的双涡旋压缩机构的压缩机,该压缩机具有紧凑和简单的结构。Another object of the present disclosure is to provide a compressor having a twin scroll compression mechanism realizing axial flexibility, which has a compact and simple structure.
根据本公开的一个方面,提供了一种涡旋压缩机,该涡旋压缩机包括第一涡旋压缩机构、第二涡旋压缩机构、驱动轴以及衬套。第一涡旋压缩机构具有第一定涡旋和能够相对于第一定涡旋运动以压缩工作流体的第一动涡旋。第二涡旋压缩机构具有第二定涡旋和能够相对于第二定涡旋运动以压缩工作流体的第二动涡旋。驱动轴包括第一偏心轴颈和第二偏心轴颈,第一偏心轴颈与第一动涡旋接合以能够驱动第一动涡旋,第二偏心轴颈与第二动涡旋接合以能够驱动第二动涡旋。衬套布置在第一动涡旋与第一偏心轴颈之间和/或在第二动涡旋与第二偏心轴颈之间,并且构造成允许所述第一定涡旋与第一动涡旋之间和/或允许所述第二定涡旋与所述第二动涡旋之间在特定情况时能够径向分离。According to one aspect of the present disclosure, there is provided a scroll compressor including a first scroll compression mechanism, a second scroll compression mechanism, a drive shaft, and a bushing. The first scroll compression mechanism has a first fixed scroll and a first orbiting scroll movable relative to the first fixed scroll to compress the working fluid. The second scroll compression mechanism has a second fixed scroll and a second orbiting scroll movable relative to the second fixed scroll to compress the working fluid. The drive shaft includes a first eccentric journal and a second eccentric journal, the first eccentric journal is engaged with the first orbiting scroll to be able to drive the first orbiting scroll, and the second eccentric journal is engaged with the second orbiting scroll to enable The second orbiting scroll is driven. A bushing is arranged between the first orbiting scroll and the first eccentric journal and/or between the second orbiting scroll and the second eccentric journal, and is configured to allow the first fixed scroll to communicate with the first orbiting scroll. Radial separation between the scrolls and/or between the second fixed scroll and the second movable scroll is allowed under certain circumstances.
本文中所述的“特定情况”指的是在涡旋压缩机运行时会损害定涡旋和动涡旋的叶片的诸如在其间存在异物或压缩腔内的压力超过安全阈值等情况。在特定情况下,期望的是动涡旋(叶片)能够相对于定涡旋(叶片)径向分离,由此允许异物或高压流体等排出。"Specific conditions" as described herein refers to conditions such as the presence of foreign objects therebetween or the pressure within the compression chamber exceeding a safe threshold that may damage the vanes of the fixed and orbiting scrolls during operation of the scroll compressor. In certain circumstances, it is desirable that the orbiting scroll (vanes) be able to be radially separated relative to the fixed scroll (vanes), thereby allowing foreign matter or high pressure fluid, etc. to escape.
根据该涡旋压缩机,由于衬套允许定涡旋与相应动涡旋之间在特定情况时能够径向分离,即,为涡旋压缩机提供径向柔性性能,因此可以防止对定涡旋和动涡旋的叶片造成损坏,从而提高了涡旋压缩机的可靠性并且具有简单的结构。According to the scroll compressor, since the bushing allows radial separation between the fixed scroll and the corresponding movable scroll under certain conditions, that is, provides radial flexibility to the scroll compressor, it is possible to prevent the fixed scroll and the vanes of the movable scroll, thereby improving the reliability of the scroll compressor and having a simple structure.
在根据本公开的一些实施方式中,所述衬套包括筒形壁和由所述筒形壁的内周面限定的内部通孔。所述内部通孔用于接收所述第一偏心轴颈和/或所述第二偏心轴颈。所述筒形壁沿周向方向具有不同的厚度,以允许所述筒形壁沿所述周向方向相对于所述驱动轴在预定范围内转动从而实现所述径向分离。In some embodiments according to the present disclosure, the bushing includes a cylindrical wall and an inner through hole defined by an inner peripheral surface of the cylindrical wall. The inner through hole is used to receive the first eccentric journal and/or the second eccentric journal. The cylindrical wall has different thicknesses in the circumferential direction to allow the cylindrical wall to rotate in the circumferential direction relative to the drive shaft within a predetermined range to achieve the radial separation.
在根据本公开的一些实施方式中,所述筒形壁的外周面具有圆形横截面。所述筒形壁的内周面具有圆形横截面。In some embodiments according to the present disclosure, the outer peripheral surface of the cylindrical wall has a circular cross-section. The inner peripheral surface of the cylindrical wall has a circular cross-section.
在根据本公开的一些实施方式中,所述衬套包括筒形壁和由所述筒形壁的内周面限定的内部通孔。所述内部通孔用于接收所述第一偏心轴颈和/或所述第二偏心轴颈。所述第一偏心轴颈和/或所述第二偏心轴颈上设置有驱动平面部。所述筒形壁的内周面上设置有从动平面部。所述驱动平面部与所述从动平面部配合使得所述筒形壁能够相对于所述驱动轴沿径向方向滑动。In some embodiments according to the present disclosure, the bushing includes a cylindrical wall and an inner through hole defined by an inner peripheral surface of the cylindrical wall. The inner through hole is used to receive the first eccentric journal and/or the second eccentric journal. A drive plane portion is provided on the first eccentric journal and/or the second eccentric journal. A driven plane portion is provided on the inner peripheral surface of the cylindrical wall. The drive plane portion cooperates with the driven plane portion so that the cylindrical wall can slide in a radial direction relative to the drive shaft.
在根据本公开的一些实施方式中,所述内部通孔具有D形的横截面。In some embodiments according to the present disclosure, the inner through hole has a D-shaped cross-section.
在根据本公开的一些实施方式中,所述第一偏心轴颈从所述驱动轴的第一侧径向向外凸出,所述第二偏心轴颈从所述驱动轴的与所述第一侧相反的第二侧径向向外凸出。In some embodiments according to the present disclosure, the first eccentric journal protrudes radially outward from the first side of the drive shaft, and the second eccentric journal protrudes from the drive shaft and the first side of the drive shaft. A second side opposite to one side projects radially outward.
在根据本公开的一些实施方式中,所述第一动涡旋与所述第二动涡旋具有相同的结构。In some embodiments according to the present disclosure, the first orbiting scroll and the second orbiting scroll have the same structure.
在根据本公开的一些实施方式中,所述第一动涡旋的端板与所述第二动涡旋的端板在轴向上彼此相邻地设置,并且所述第一定涡旋的端板与所述第二定涡旋的端板在轴向上彼此远离地设置。In some embodiments according to the present disclosure, the end plate of the first orbiting scroll and the end plate of the second orbiting scroll are disposed adjacent to each other in the axial direction, and the end plate of the first fixed scroll is adjacent to each other in the axial direction. The end plate and the end plate of the second fixed scroll are disposed away from each other in the axial direction.
在根据本公开的一些实施方式中,在所述第一动涡旋的端板与所述第二动涡旋的端板之间形成有背压腔。所述背压腔中的流体的压力将所述第一动涡旋推向所述第一定涡旋并且将所述第二动涡旋推向所述第二定涡旋。In some embodiments according to the present disclosure, a back pressure cavity is formed between the end plate of the first orbiting scroll and the end plate of the second orbiting scroll. The pressure of the fluid in the back pressure chamber pushes the first orbiting scroll toward the first fixed scroll and the second orbiting scroll toward the second fixed scroll.
在根据本公开的一些实施方式中,所述第一动涡旋的端板与所述第二动涡旋的端板之间设置有第一密封件和第二密封件,所述背压腔限定在第一密封件和第二密封件之间,所述第一密封件位于所述第二密封件的径向外侧。In some embodiments according to the present disclosure, a first sealing member and a second sealing member are provided between the end plate of the first orbiting scroll and the end plate of the second orbiting scroll, and the back pressure chamber Defined between a first seal and a second seal, the first seal located radially outward of the second seal.
在根据本公开的一些实施方式中,在所述第一动涡旋的端板和/或所述第二动涡旋的端板上设置有用于容置所述第一密封件的第一凹槽以及用于容置所述第二密封件的第二凹槽。In some embodiments according to the present disclosure, a first recess for accommodating the first seal is provided on the end plate of the first orbiting scroll and/or the end plate of the second orbiting scroll a groove and a second groove for accommodating the second seal.
在根据本公开的一些实施方式中,所述第一涡旋压缩机构和所述第二涡旋压缩机构能够独立控制。或者,所述第一涡旋压缩机构的排气口连通至所述第二涡旋压缩机构的吸气口。In some embodiments according to the present disclosure, the first scroll compression mechanism and the second scroll compression mechanism are independently controllable. Alternatively, the discharge port of the first scroll compression mechanism communicates with the intake port of the second scroll compression mechanism.
根据本公开的另一方面,提供一种涡旋压缩机,包括第一涡旋压缩机构、第二涡旋压缩机构和驱动轴。所述第一涡旋压缩机构具有第一定涡旋和能够相对于所述第一定涡旋运动以压缩工作流体的第一动涡旋。所述第二涡旋压缩机构具有第二定涡旋和能够相对于所述第二定涡旋运动以压缩工作流体的第二动涡旋。所述驱动轴包括第一偏心轴颈和第二偏心轴颈,所述第一偏心轴颈与所述第一动涡旋接合以能够驱动所述第一动涡旋,所述第二偏心轴颈与所述第二动涡旋接合以能够驱动所述第二动涡旋。在所述第一涡旋压缩机构与所述第二涡旋压缩机构之间设置有第一密封件和第二密封件,所述第一密封件位于所述第二密封件的径向外侧。在所述第一密封件与所述第二密封件之间形成有引入流体压力的背压腔。According to another aspect of the present disclosure, there is provided a scroll compressor including a first scroll compression mechanism, a second scroll compression mechanism and a drive shaft. The first scroll compression mechanism has a first fixed scroll and a first orbiting scroll movable relative to the first fixed scroll to compress the working fluid. The second scroll compression mechanism has a second fixed scroll and a second orbiting scroll movable relative to the second fixed scroll to compress the working fluid. The drive shaft includes a first eccentric journal and a second eccentric journal, the first eccentric journal is engaged with the first orbiting scroll to be able to drive the first orbiting scroll, the second eccentric shaft A neck engages the second orbiting scroll to be able to drive the second orbiting scroll. A first sealing member and a second sealing member are provided between the first scroll compression mechanism and the second scroll compression mechanism, and the first sealing member is located radially outside the second sealing member. A back pressure cavity into which fluid pressure is introduced is formed between the first seal and the second seal.
根据该涡旋压缩机,由于通过第一密封件和第二密封件限定的背压腔可以提供轴向柔性性能,因此提高了涡旋压缩机的可靠性,具有紧凑和简单的结构,并且能够降低成本。According to the scroll compressor, since the axial flexibility can be provided by the back pressure chamber defined by the first seal and the second seal, the reliability of the scroll compressor is improved, the structure is compact and simple, and it is possible to cut costs.
在根据本公开的一些实施方式中,所述第一动涡旋的端板与所述第二动涡旋的端板在轴向上彼此相邻地设置,并且所述第一定涡旋的端板与所述第二定涡旋的端板在轴向上彼此远离地设置。In some embodiments according to the present disclosure, the end plate of the first orbiting scroll and the end plate of the second orbiting scroll are disposed adjacent to each other in the axial direction, and the end plate of the first fixed scroll is adjacent to each other in the axial direction. The end plate and the end plate of the second fixed scroll are disposed away from each other in the axial direction.
在根据本公开的一些实施方式中,所述第一动涡旋的端板和/或所述第二动涡旋的端板中形成有用于将压缩腔中的流体引入所述背压腔中的连通通道。In some embodiments according to the present disclosure, the end plate of the first orbiting scroll and/or the end plate of the second orbiting scroll is formed with a fluid for introducing the fluid in the compression chamber into the back pressure chamber the communication channel.
在根据本公开的一些实施方式中,在所述第一动涡旋的端板和/或所述第二动涡旋的端板上设置有用于容置所述第一密封件的第一凹槽以及用于容置所述第二密封件的第二凹槽。In some embodiments according to the present disclosure, a first recess for accommodating the first seal is provided on the end plate of the first orbiting scroll and/or the end plate of the second orbiting scroll a groove and a second groove for accommodating the second seal.
在根据本公开的一些实施方式中,所述第一偏心轴颈从所述驱动轴的第一侧径向向外凸出,并且所述第二偏心轴颈从所述驱动轴的与所述第一侧相反的第二侧径向向外凸出。In some embodiments according to the present disclosure, the first eccentric journal protrudes radially outward from the first side of the drive shaft, and the second eccentric journal protrudes from the drive shaft and the A second side opposite the first side projects radially outward.
在根据本公开的一些实施方式中,所述第一动涡旋与所述第二动涡旋具有相同的结构。In some embodiments according to the present disclosure, the first orbiting scroll and the second orbiting scroll have the same structure.
在根据本公开的一些实施方式中,涡旋压缩机还包括衬套。所述衬套设置在所述第一动涡旋与所述第一偏心轴颈之间和/或在所述第二动涡旋与所述第二偏心轴颈之间。所述衬套构造成允许所述第一定涡旋与第一动涡旋之间和/或允许所述第二定涡旋与所述第二动涡旋之间在特定情况时能够径向分离。In some embodiments according to the present disclosure, the scroll compressor further includes a liner. The bushing is arranged between the first orbiting scroll and the first eccentric journal and/or between the second orbiting scroll and the second eccentric journal. The bushing is configured to allow radial direction between the first fixed scroll and the first orbiting scroll and/or to allow the radial direction between the second fixed scroll and the second orbiting scroll under certain circumstances separation.
在根据本公开的一些实施方式中,所述衬套包括筒形壁和由所述筒形壁的内周面限定的内部通孔。所述内部通孔用于接收所述第一偏心轴颈和/或所述第二偏心轴颈。所述筒形壁沿周向方向具有不同的厚度,以允许所述筒形壁沿所述周向方向相对于所述驱动轴在预定范围内转动从而实现所述径向分离。In some embodiments according to the present disclosure, the bushing includes a cylindrical wall and an inner through hole defined by an inner peripheral surface of the cylindrical wall. The inner through hole is used to receive the first eccentric journal and/or the second eccentric journal. The cylindrical wall has different thicknesses in the circumferential direction to allow the cylindrical wall to rotate in the circumferential direction relative to the drive shaft within a predetermined range to achieve the radial separation.
在根据本公开的一些实施方式中,所述筒形壁的外周面具有圆形横截面,并且所述筒形壁的内周面具有圆形横截面。In some embodiments according to the present disclosure, the outer peripheral surface of the cylindrical wall has a circular cross-section, and the inner peripheral surface of the cylindrical wall has a circular cross-section.
在根据本公开的一些实施方式中,所述衬套包括筒形壁和由所述筒形壁的内周面限定的内部通孔,所述内部通孔用于接收所述第一偏心轴颈和/或所述第二偏心轴颈。所述第一偏心轴颈和/或所述第二偏心轴颈上设置有驱动平面部。所述筒形壁的内周面上设置有从动平面部。所述驱动平面部与所述从动平面部配合使得所述筒形壁能够相对于所述驱动轴沿径向方向滑动。In some embodiments according to the present disclosure, the bushing includes a cylindrical wall and an inner through hole defined by an inner peripheral surface of the cylindrical wall, the inner through hole for receiving the first eccentric journal and/or the second eccentric journal. A drive plane portion is provided on the first eccentric journal and/or the second eccentric journal. A driven plane portion is provided on the inner peripheral surface of the cylindrical wall. The drive plane portion cooperates with the driven plane portion so that the cylindrical wall can slide in a radial direction relative to the drive shaft.
在根据本公开的一些实施方式中,所述内部通孔具有D形的横截面。In some embodiments according to the present disclosure, the inner through hole has a D-shaped cross-section.
在根据本公开的一些实施方式中,所述第一涡旋压缩机构和所述第二涡旋压缩机构能够独立控制。或者,所述第一涡旋压缩机构的排气口连通至所述第二涡旋压缩机构的吸气口。In some embodiments according to the present disclosure, the first scroll compression mechanism and the second scroll compression mechanism are independently controllable. Alternatively, the discharge port of the first scroll compression mechanism communicates with the intake port of the second scroll compression mechanism.
附图说明Description of drawings
通过以下参照附图的描述,本发明的一个或几个实施方式的特征和优点将变得更加容易理解,其中:The features and advantages of one or more embodiments of the present invention will become more readily understood from the following description with reference to the accompanying drawings, wherein:
图1是根据本公开实施方式的涡旋压缩机的纵剖示意图;1 is a schematic longitudinal cross-sectional view of a scroll compressor according to an embodiment of the present disclosure;
图2是图1的涡旋压缩机的压缩机构的局部放大示意图;Fig. 2 is the partial enlarged schematic diagram of the compression mechanism of the scroll compressor of Fig. 1;
图3是图2的压缩机构的变型的示意图;Figure 3 is a schematic diagram of a variation of the compression mechanism of Figure 2;
图4是根据本公开实施方式的衬套的立体示意图;4 is a schematic perspective view of a bushing according to an embodiment of the present disclosure;
图5是根据本公开另一实施方式的衬套的立体示意图;5 is a schematic perspective view of a bushing according to another embodiment of the present disclosure;
图6A是图1的涡旋压缩机的驱动轴的立体示意图;6A is a schematic perspective view of a drive shaft of the scroll compressor of FIG. 1;
图6B是图6A的驱动轴的端视示意图。6B is a schematic end view of the drive shaft of FIG. 6A.
具体实施方式Detailed ways
下面对本发明各种实施方式的描述仅仅是示范性的,而绝不是对本发明及其应用或用法的限制。在各个附图中采用相同的附图标记来表示相同的部件,因此相同部件的构造将不再重复描述。The following descriptions of various embodiments of the present invention are exemplary only, and in no way limit the invention and its application or usage. The same reference numerals are used to denote the same components in the various drawings, and thus the configuration of the same components will not be described repeatedly.
图1是根据本公开实施方式的涡旋压缩机的纵剖示意图;图2是图1的涡旋压缩机的压缩机构的局部放大示意图。下面将参照图1和图2来描述根据本公开的涡旋压缩机。1 is a schematic longitudinal cross-sectional view of a scroll compressor according to an embodiment of the present disclosure; FIG. 2 is a partially enlarged schematic view of a compression mechanism of the scroll compressor of FIG. 1 . The scroll compressor according to the present disclosure will be described below with reference to FIGS. 1 and 2 .
如图1和图2所示,涡旋压缩机100包括壳体110.设置在壳体110一端的顶盖112以及设置在壳体110另一端的底盖114。壳体110.顶盖112和底盖114构成了涡旋压缩机100的外壳并且限定了密闭的内部空间。As shown in FIGS. 1 and 2 , the
涡旋压缩机100包括由定子122和转子124构成的马达120。马达120为涡旋压缩机100的压缩机构提供动力。马达120可以置于涡旋压缩机100的内部空间中。定子122可以固定至壳体110,转子124可以位于定子122的径向内侧并能够相对于定子122旋转。The
涡旋压缩机100包括驱动轴130,其也可以被称为旋转轴或曲轴。驱动轴130用于将马达120的动力传递至涡旋压缩机100的压缩机构。驱动轴130例如以过盈配合的方式固定地安装在转子124中以随着转子124一起旋转。此外,驱动轴130以偏心驱动的方式联接至涡旋压缩机100的压缩机构的动涡旋。在图示的示例中,驱动轴130经由轴承座(例如,上轴承座和/或下轴承座)置于涡旋压缩机100的内部空间中。然而,应理解的是,马达120和驱动轴130的一部分可以位于涡旋压缩机100的外壳之外。The
涡旋压缩机100包括第一压缩机构CM1和第二压缩机构CM2。第一压缩机构CM1和第二压缩机构CM2容置于涡旋压缩机100的内部空间中。在壳体110中设置有第一进气接头In1和第二进气接头In2。通过第一进气接头In1将工作流体(例如,制冷剂)引入第一压缩机构CM1中以将其进行压缩。通过第二进气接头In2将工作流体(例如,制冷剂)引入第二压缩机构CM2中以将其进行压缩。The
第一压缩机构CM1和第二压缩机构CM2可以单独地进行控制。第一压缩机构CM1和第二压缩机构CM2可以以并联的方式联接在一起。第一压缩机构CM1的运行(进气和排气)独立于第二压缩机构CM2的运行(进气和排气)。例如,经由第一压缩机构CM1压缩后的工作流体从其大致中央处排至内部空间中。经由第二压缩机构CM2压缩后的工作流体从其大致中央处排至内部空间中。内部空间中的压缩气体可以经由涡旋压缩机100的外壳上的排气接头(未示出)排出。可以对第一压缩机构CM1和/或第二压缩机构CM2设置旁通结构,以调节涡旋压缩机100的容量。The first compression mechanism CM1 and the second compression mechanism CM2 can be individually controlled. The first compression mechanism CM1 and the second compression mechanism CM2 may be coupled together in parallel. The operation (intake and exhaust) of the first compression mechanism CM1 is independent of the operation (intake and exhaust) of the second compression mechanism CM2. For example, the working fluid compressed by the first compression mechanism CM1 is discharged into the inner space from approximately the center thereof. The working fluid compressed by the second compression mechanism CM2 is discharged into the inner space from the approximate center thereof. The compressed gas in the interior space may be exhausted via a discharge fitting (not shown) on the casing of the
第一压缩机构CM1和第二压缩机构CM2可以以串联的方式联接在一起。例如,第一压缩机构CM1的排气口经由管路连通至第二压缩机构CM2的吸气口。这样,可以将经由第一压缩机构CM1压缩的工作流体引入至第二压缩机构CM2的吸气口中以进行二级压缩。经由二级压缩后的工作流体可以排出至内部空间中,然后再经由涡旋压缩机100的外壳上的排气接头(未示出)排出。The first compression mechanism CM1 and the second compression mechanism CM2 may be coupled together in series. For example, the discharge port of the first compression mechanism CM1 communicates with the intake port of the second compression mechanism CM2 via a pipeline. In this way, the working fluid compressed via the first compression mechanism CM1 can be introduced into the suction port of the second compression mechanism CM2 for secondary compression. The working fluid compressed through the second stage may be discharged into the interior space, and then discharged through a discharge connection (not shown) on the casing of the
第一压缩机构CM1包括第一定涡旋151和第一动涡旋152。第一定涡旋151包括端板153和从端板153的一侧延伸的定涡卷155。第一动涡旋152包括端板154和从端板154的一侧延伸的动涡卷156。驱动轴130具有与第一压缩机构CM1的第一动涡旋152接合以驱动第一动涡旋152的第一偏心轴颈131。在驱动轴130旋转时,第一动涡旋152相对于第一定涡旋151绕动,以在动涡卷156与定涡卷155之间压缩工作流体。The first compression mechanism CM1 includes a first
第二压缩机构CM2包括第二定涡旋161和第二动涡旋162。第二定涡旋161包括端板163和从端板163的一侧延伸的定涡卷165。第二动涡旋162包括端板164和从端板164的一侧延伸的动涡卷166。驱动轴130具有与第二压缩机构CM2的第二动涡旋162接合以驱动第二动涡旋162的第二偏心轴颈132。在驱动轴130旋转时,第二动涡旋162相对于第二定涡旋161绕动,以在动涡卷166与定涡卷165之间压缩工作流体。The second compression mechanism CM2 includes a second
第一压缩机构CM1和第二压缩机构CM2的压缩工作流体的过程与现有涡旋压缩机构的类似,因此此处不再详细描述。The process of compressing the working fluid by the first compression mechanism CM1 and the second compression mechanism CM2 is similar to that of the existing scroll compression mechanism, so it will not be described in detail here.
在图1和图2所示的示例中,第一动涡旋152和第二动涡旋162位于第一定涡旋151和第二定涡旋152之间。具体地,第一动涡旋152的端板154面向并且邻近第二动涡旋162的端板164。第一定涡旋151的端板153和第二定涡旋161的端板163彼此远离并位于第一动涡旋152和第二动涡旋162的相反的两侧(图中为上侧和下侧)。In the example shown in FIGS. 1 and 2 , the
在第一动涡旋152的端板154与第二动涡旋162的端板164之间设置有第一密封件171和第二密封件172。第一密封件171位于第二密封件172的径向外侧。例如,第一密封件171和第二密封件172为O形圈或者任何其他合适类型的密封件。A
在图1和图2的示例中,第二压缩机构CM2的第二动涡旋162的端板164上设置有用于容置第一密封件171的第一环形凹槽167和用于容置第二密封件172的第二环形凹槽168。相应地,第一环形凹槽167位于第二环形凹槽168的径向外侧。In the example of FIGS. 1 and 2 , the
在第二动涡旋162的端板164中设置有连通通道173。连通通道173将其中一个压缩腔中的流体引入第一密封件171与第二密封件172之间的空间中。因此,第一密封件171与第二密封件172之间的空间形成了背压腔170。背压腔170中的流体的压力将第一动涡旋152推向第一定涡旋151并且将第二动涡旋162推向第二定涡旋161。A
由于背压腔170中的流体压力的作用,每个涡旋压缩机构的定涡旋与动涡旋之间的轴向距离可以发生变化,由此为涡旋压缩机100提供了轴向柔性性能。第一密封件171、第二密封件172以及其间的背压腔170构成了轴向柔性结构。Due to the fluid pressure in the
如上所述的轴向柔性结构允许第一动涡旋152的端板154与第二动涡旋162的端板164彼此尽可能地靠近,因此整个双压缩机构的结构非常紧凑,而且可以改善动平衡问题,甚至可以省去平衡块。而且,仅需要对端板164加工以形成用于容置第一密封件171和第二密封件172的凹槽,而无需设置额外的部件来提供轴向柔性性能,因此可以减少部件数量,简化涡旋压缩机100的结构,而且还能够简化各部件的加工和组装过程,由此显著降低涡旋压缩机100的成本。如上所述,第一密封件171和第二密封件172可以是例如O形圈,因此可以进一步降低涡旋压缩机100的成本。The axially flexible structure as described above allows the
第一定涡旋151的外周可以设置有第一凸缘159。第二定涡旋161的外周可以设置有第二凸缘169。第一凸缘159和第二凸缘169可以通过螺栓102联接在一起。可选地,借助于螺栓102的引导,第一定涡旋151和第二定涡旋161可以相对于彼此轴向运动。第一凸缘159和第二凸缘169可以朝向彼此延伸,由此便于其间的联接和导向。The outer circumference of the first
应理解的是,根据本公开的轴向柔性结构不局限于图1和图2所示的具体示例。例如,图3是图2的压缩机构的变型的示意图。如图3所示,涡旋压缩机200如同涡旋压缩机100包括第一压缩机构CM1和第二压缩机构CM2。第一压缩机构CM1包括第一定涡旋251和第一动涡旋252。第一定涡旋251包括端板253和定涡卷255。第一动涡旋252包括端板254和动涡卷256。第二压缩机构CM2包括第二定涡旋261和第二动涡旋262。第二定涡旋261包括端板263和定涡卷265。第二动涡旋262包括端板264和动涡卷266。It should be understood that the axially flexible structures according to the present disclosure are not limited to the specific examples shown in FIGS. 1 and 2 . For example, FIG. 3 is a schematic diagram of a variation of the compression mechanism of FIG. 2 . As shown in FIG. 3 , the
涡旋压缩机200与涡旋压缩机100的不同之处在于轴向柔性结构的设置。具体地,在图3所示的示例中,第一压缩机构CM1的第一动涡旋252的端板254上设置有用于容置第一密封件271的第一环形凹槽257和用于容置第二密封件272的第二环形凹槽258。第一环形凹槽257位于第二环形凹槽258的径向外侧。在第一密封件271与第二密封件272之间形成有背压腔270。在第一动涡旋252的端板254上设置有将压缩腔连通至背压腔270中的连通通道273。The
参照图1至图3,在第一定涡旋151(具体为端板153)与驱动轴130之间设置有轴承181。类似地,在第二定涡旋161(具体为端板163)与驱动轴130之间设置有轴承184。轴承181和轴承184可以是例如具有恒定厚度的筒形形状的滑动轴承,用于缓解对端板153和163造成的磨损。1 to 3 , a
在第一动涡旋152(具体为动涡卷156的中央部分)与驱动轴130(具体为第一偏心轴颈131)之间设置有轴承182。类似地,在第二动涡旋162(具体为动涡卷166的中央部分)与驱动轴130(具体为第二偏心轴颈132)之间设置有轴承183。轴承182和轴承183可以是与轴承181和182类似的轴承,用于缓解对动涡卷156和166造成的磨损。A
在轴承182与第一偏心轴颈131之间可以设置有第一衬套191。第一衬套191构造成在第一定涡旋151(具体为定涡卷155)与第一动涡旋152(具体为动涡卷156)之间存在杂质时允许第一定涡旋151与第一动涡旋152彼此径向分离,由此防止其受力过大而损坏。A
类似地,在轴承183与第二偏心轴颈132之间可以设置有第二衬套192。第二衬套192构造成在第二定涡旋161(具体为定涡卷165)与第二动涡旋162(具体为动涡卷166)之间存在杂质时允许第二定涡旋161与第二动涡旋162彼此径向分离,由此防止其受力过大而损坏。第一衬套191和第二衬套192构成了本公开的径向柔性结构。Similarly, a
本文中所述的“杂质”指的是受到压缩时体积不易变化的物质,例如固体或液态物质等。The "impurities" mentioned herein refer to substances whose volume is not easily changed when compressed, such as solid or liquid substances.
第一衬套191可以具有与第二衬套192相同或不同的结构,如图4或图5所示的结构。The
图4是根据本公开实施方式的衬套10的立体示意图。如图4所示,衬套10包括筒形壁15和由筒形壁15的内周面12限定的内部通孔13。内部通孔13用于接收第一偏心轴颈131或第二偏心轴颈132。筒形壁15沿周向方向具有变化的厚度。这样,当压缩机构中例如存在杂质时,筒形壁15受到的力超过预定值时会沿着周向方向朝着厚度较薄的部分转动。由于筒形壁15转到了厚度较薄的部分,因此动涡卷(动涡卷156或166)的对应部分能够相对于定涡卷(定涡卷155或165)的相应部分径向分离,由此保护动涡卷和定涡卷以免损坏。4 is a schematic perspective view of the
筒形壁15的外周面11可以具有圆形横截面以与动涡卷匹配。筒形壁15的内周面12的轮廓或尺寸可以设计成在杂质进入压缩机构内时允许筒形壁15沿周向方向在预定范围内转动。例如,筒形壁15的内周面12可以具有圆形横截面或椭圆形横截面。The outer
图5是根据本公开另一实施方式的衬套20的立体示意图。如图5所示,衬套20包括筒形壁25和由筒形壁25的内周面22限定的内部通孔23。内部通孔23用于接收第一偏心轴颈131或第二偏心轴颈132。筒形壁25的内周面22上设置有平面部24,相应地,第一偏心轴颈131或第二偏心轴颈132上设置有与平面部24配合的驱动平面部(未示出)。因此,平面部24也可以称为从动平面部。从动平面部24与驱动平面部配合使得筒形壁25能够相对于驱动轴130沿径向方向滑动。这样,当压缩机构中例如存在杂质时,筒形壁25受到的力超过预定值时会沿着径向方向朝着驱动轴130滑动。由于筒形壁25沿着径向方向朝着驱动轴130移动,因此动涡卷(动涡卷156或166)的对应部分能够相对于定涡卷(定涡卷155或165)的相应部分径向分离,由此保护动涡卷和定涡卷以免损坏。FIG. 5 is a schematic perspective view of a
内部通孔23可以具有大致呈D形的横截面。类似地,第一偏心轴颈131或第二偏心轴颈132也可以具有大致呈D形的横截面。The inner through
图6A是图1的涡旋压缩机的驱动轴的立体示意图;图6B是图6A的驱动轴的端视示意图。下面将参照图6A和图6B来描述根据本公开实施方式的驱动轴130的结构。6A is a schematic perspective view of a drive shaft of the scroll compressor of FIG. 1 ; FIG. 6B is a schematic end view of the drive shaft of FIG. 6A . The structure of the
如图6A和图6B所示,驱动轴130包括与第一定涡旋151和第二定涡旋161接合的主轴颈135、与第一动涡旋152接合的第一偏心轴颈131以及与第二动涡旋162接合的第二偏心轴颈132。As shown in FIGS. 6A and 6B , the
主轴颈135具有中心轴线CA。第一偏心轴颈131从主轴颈135的第一侧(图中为右侧,其也为驱动轴的第一侧)径向向外凸出(图中向右凸出)并且具有中心轴线CA1。在图示的示例中,由于第一偏心轴颈131相对于主轴颈135向右凸出,因此中心轴线CA1相对于中心轴线CA向右偏置。即,径向向外凸出的第一偏心轴颈131形成了相对于中心轴线CA(主轴颈135)偏心的结构。第一偏心轴颈131的外周的第二侧(图中为左侧,其也为驱动轴的第二侧)1312可以与主轴颈135的外周的左侧1352重合,如图6B所示。即,第一偏心轴颈131的外周的第二侧1312相对于主轴颈135的外周的左侧1352线性地延伸。这样,有利于轴承或衬套的(例如,从上方)安装和拆卸。The
第二偏心轴颈132可以具有与第一偏心轴颈131类似的结构,但相对于第一偏心轴颈131沿周向方向偏置180度。即,第二偏心轴颈132相对于主轴颈135的第二侧径向向外凸出(图中向左凸出)并且具有中心轴线CA2。中心轴线CA2相对于中心轴线CA向左偏置。第二偏心轴颈132的外周的第一侧1323可以与主轴颈135的外周的右侧1353重合,如图6B所示。即,第二偏心轴颈132的外周的第一侧1323相对于主轴颈135的外周的右侧1353线性地延伸。同样,这有利于轴承或衬套的(例如,从下方)安装和拆卸。The second
通常轴承181、184的内径ID与驱动轴130的外径(主轴颈135的外径)大致相等。第一偏心轴颈131和第二偏心轴颈132的外径OD大于轴承181、184的内径ID。参见图6B的截面图,内径ID=外径OD-2*轴偏心距。在图6B所示的截面图中,主轴颈135与偏心轴颈(清楚地示出第二偏心轴颈132)内切。这样,可以最大化轴承181、184的尺寸。Usually, the inner diameter ID of the
由于第一偏心轴颈131相对于第二偏心轴颈132偏转180度,因此可以良好地改善动平衡。有利的是,第一动涡旋152和第二动涡旋162具有大致相同的结构和尺寸。这样,可以基本消除动平衡问题。Since the first
如图6B所示,第一偏心轴颈131和第二偏心轴颈132各自具有大致椭圆形的横截面。应理解的是,本公开的驱动轴不局限于图示的具体示例,而是可以根据需要而改变。As shown in FIG. 6B , the first
尽管在此已详细描述本发明的各种实施方式,但是应该理解本发明并不局限于这里详细描述和示出的具体实施方式,在不偏离本发明的实质和范围的情况下可由本领域的技术人员实现其它的变型。例如,在不矛盾的情况下,各个实施方式的特征可以相互结合,或者可以省去某个特征(例如,轴承182和183)。所有这些变型都落入本发明的范围内。而且,所有在此描述的构件都可以由其他技术性上等同的构件来代替。Although various embodiments of the present invention have been described in detail herein, it is to be understood that the invention is not limited to the specific embodiments described and illustrated in detail herein, but may be modified by those skilled in the art without departing from the spirit and scope of the present invention. The skilled person implements other variations. For example, the features of the various embodiments may be combined with each other, or a feature (eg,
Claims (24)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110063622.9A CN114810586A (en) | 2021-01-18 | 2021-01-18 | scroll compressor |
| PCT/CN2022/071904 WO2022152228A1 (en) | 2021-01-18 | 2022-01-14 | Scroll compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110063622.9A CN114810586A (en) | 2021-01-18 | 2021-01-18 | scroll compressor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114810586A true CN114810586A (en) | 2022-07-29 |
Family
ID=82523676
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110063622.9A Pending CN114810586A (en) | 2021-01-18 | 2021-01-18 | scroll compressor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114810586A (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR920012747A (en) * | 1990-12-06 | 1992-07-27 | 이헌조 | Eccentric Bushing Structure of Scroll Compressor |
| CN1450268A (en) * | 2002-04-11 | 2003-10-22 | 倪诗茂 | Suspension type scroll fluid compressor with omnibearing complying structure |
| CN103883514A (en) * | 2012-12-21 | 2014-06-25 | 丹佛斯商用压缩机有限公司 | Scroll compressor having a first and second oldham couplings |
| CN205172937U (en) * | 2015-11-23 | 2016-04-20 | 艾默生环境优化技术(苏州)有限公司 | Scroll compressor and unloader bushing for scroll compressor |
| CN206092405U (en) * | 2016-09-22 | 2017-04-12 | 艾默生环境优化技术(苏州)有限公司 | Scroll compressor having a plurality of scroll members |
| US20180066656A1 (en) * | 2016-09-08 | 2018-03-08 | Emerson Climate Technologies, Inc. | Oil Flow Through The Bearings Of A Scroll Compressor |
| WO2018145091A1 (en) * | 2017-02-06 | 2018-08-09 | Emerson Climate Technologies, Inc. | Scroll compressor with axial flux motor |
| CN111089055A (en) * | 2018-10-23 | 2020-05-01 | 艾默生环境优化技术(苏州)有限公司 | Scroll compressor having a plurality of scroll members |
| WO2020238110A1 (en) * | 2019-05-30 | 2020-12-03 | 艾默生环境优化技术(苏州)有限公司 | Scroll compressor |
| CN214998201U (en) * | 2021-01-18 | 2021-12-03 | 艾默生环境优化技术(苏州)有限公司 | scroll compressor |
-
2021
- 2021-01-18 CN CN202110063622.9A patent/CN114810586A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR920012747A (en) * | 1990-12-06 | 1992-07-27 | 이헌조 | Eccentric Bushing Structure of Scroll Compressor |
| CN1450268A (en) * | 2002-04-11 | 2003-10-22 | 倪诗茂 | Suspension type scroll fluid compressor with omnibearing complying structure |
| CN103883514A (en) * | 2012-12-21 | 2014-06-25 | 丹佛斯商用压缩机有限公司 | Scroll compressor having a first and second oldham couplings |
| CN205172937U (en) * | 2015-11-23 | 2016-04-20 | 艾默生环境优化技术(苏州)有限公司 | Scroll compressor and unloader bushing for scroll compressor |
| US20180066656A1 (en) * | 2016-09-08 | 2018-03-08 | Emerson Climate Technologies, Inc. | Oil Flow Through The Bearings Of A Scroll Compressor |
| CN206092405U (en) * | 2016-09-22 | 2017-04-12 | 艾默生环境优化技术(苏州)有限公司 | Scroll compressor having a plurality of scroll members |
| WO2018145091A1 (en) * | 2017-02-06 | 2018-08-09 | Emerson Climate Technologies, Inc. | Scroll compressor with axial flux motor |
| CN111089055A (en) * | 2018-10-23 | 2020-05-01 | 艾默生环境优化技术(苏州)有限公司 | Scroll compressor having a plurality of scroll members |
| WO2020238110A1 (en) * | 2019-05-30 | 2020-12-03 | 艾默生环境优化技术(苏州)有限公司 | Scroll compressor |
| CN214998201U (en) * | 2021-01-18 | 2021-12-03 | 艾默生环境优化技术(苏州)有限公司 | scroll compressor |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10400771B2 (en) | Eccentric compensating torsional drive system | |
| EP2416015B1 (en) | Scroll compressor | |
| US6439867B1 (en) | Scroll compressor having a clearance for the oldham coupling | |
| CN106062369B (en) | scroll compressor | |
| US20150104342A1 (en) | Scroll-type compressor | |
| WO2012005150A1 (en) | Scroll compressor | |
| CN101952551A (en) | Key coupling and scroll compressor incorporating same | |
| EP3214263B1 (en) | Two-cylinder hermetic compressor | |
| CN108779774B (en) | Scroll compressor having a discharge port | |
| US8047823B2 (en) | Scroll-type fluid machine including pressure-receiving piece | |
| US20150159652A1 (en) | Scroll-type compressor | |
| CN109563833B (en) | Double-rotation scroll compressor and design method thereof | |
| JP2017166366A (en) | Scroll compressor | |
| EP2484909B1 (en) | Scroll fluid machine | |
| CN214998201U (en) | scroll compressor | |
| US8092199B2 (en) | Scroll compressor including a plurality of shoulder sections | |
| CN114144586B (en) | scroll compressor | |
| CN102597525A (en) | Rotary compressor | |
| CN114810586A (en) | scroll compressor | |
| US8714950B2 (en) | Scroll compressor having tip seals of different lengths having different thickness or widths | |
| WO2022152228A1 (en) | Scroll compressor | |
| US6544014B2 (en) | Scroll-type compressors | |
| CN212717155U (en) | Scroll compressor having a plurality of scroll members | |
| JP4822943B2 (en) | Fluid machinery | |
| KR200392423Y1 (en) | Structure of sealing for twin rotary compressor |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information |
Address after: No. 69 Suhong West Road, Industrial Park, Suzhou City, Jiangsu Province, 215101 Applicant after: Gulun Environmental Technology (Suzhou) Co.,Ltd. Address before: Emerson R & D and overall solution center, 35 Suhong West Road, Suzhou Industrial Park, Jiangsu Province, 215021 Applicant before: EMERSON CLIMATE TECHNOLOGIES (SUZHOU) Co.,Ltd. |
|
| CB02 | Change of applicant information |