CN217582493U - Double-layer shell structure of rotor type compressor - Google Patents

Double-layer shell structure of rotor type compressor Download PDF

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Publication number
CN217582493U
CN217582493U CN202123363046.4U CN202123363046U CN217582493U CN 217582493 U CN217582493 U CN 217582493U CN 202123363046 U CN202123363046 U CN 202123363046U CN 217582493 U CN217582493 U CN 217582493U
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China
Prior art keywords
shell
double
casing
compressor
filling layer
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CN202123363046.4U
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Chinese (zh)
Inventor
程晓桐
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Shanghai Highly Electrical Appliances Co Ltd
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Shanghai Highly Electrical Appliances Co Ltd
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Priority to CN202123363046.4U priority Critical patent/CN217582493U/en
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  • Applications Or Details Of Rotary Compressors (AREA)

Abstract

The application discloses rotor compressor's double-deck shell structure, a serial communication port, the compressor includes double-deck shell, and double-deck shell is equipped with shell body and interior casing, establishes to the filling layer between shell body and the interior casing, packs sound absorbing material in the filling layer. When the compressor runs, the noise generated inside the compressor can be effectively attenuated through the double-layer shell and the filling layer, and the radiation degree to the outside is reduced.

Description

Double-layer shell structure of rotor type compressor
Technical Field
The application relates to a double-layer shell structure of a rotor type compressor, and relates to the technical field of compressor structures.
Background
As the rotor compressor operates, noise is generated and radiated outward through the compressor housing. The existing compressor shell is of a single-layer structure, as shown in fig. 1, and is thin in thickness, noise generated inside the compressor cannot be attenuated and directly radiated to the outside when passing through the shell, so that the noise of the compressor during operation is large, and the actual use feeling of the air conditioner is influenced.
SUMMERY OF THE UTILITY MODEL
The technical problem that this application will be solved is the unable problem that limits inside noise to external spread of single-deck casing of rotor compressor.
In order to solve the technical problem, the technical scheme of this application provides a double shell structure of rotor compressor, rotor compressor has last cap, casing down, its characterized in that, still include with go up the cap casing down casing sealing connection's double-deck casing, double-deck casing is equipped with shell body, interior casing, and sets up filling layer between shell body, the interior casing.
Preferably, the end of the inner shell is hermetically connected with the upper shell cover and the lower shell.
Preferably, the outer shell and the inner shell are connected through a plurality of rib plates, the filling layer is divided into a plurality of areas by the plurality of rib plates, and the areas are filled with sound absorption materials.
Preferably, be equipped with a connecting pipe that runs through on the double shell for connect and locate outside reservoir, the connecting pipe is established in advance on shell body, the interior casing, pass interior casing and shell body in proper order and be connected with locating outside reservoir, the connecting pipe sets up shaft seal with interior casing/shell body junction.
Preferably, the inner shell of the area where the connecting pipe is located is of a honeycomb panel structure.
Drawings
FIG. 1 is a schematic view of a prior art single housing;
FIG. 2 is a schematic illustration of a double housing provided in an embodiment;
FIG. 3 is a high-level top cross-sectional view of the connecting tube.
Detailed Description
In order to make the present application more comprehensible, preferred embodiments accompanied with figures are described in detail below.
Examples
In the present embodiment, as shown in fig. 2 and fig. 3, a compressor adopts a double-layer shell, and includes an outer shell 1 and an inner shell 2, a filling layer 3 is arranged between the outer shell 1 and the inner shell 2, and sound absorbing cotton or sound absorbing material is filled in the filling layer 3; when the compressor runs, the noise generated inside the compressor can be effectively attenuated through the double-layer shell and the filling layer, and the radiation degree to the outside is reduced.
In some possible embodiments, as shown in fig. 2, a through connection pipe 5 is provided on a shell of the compressor for the refrigerant to enter the compressor from an accumulator 6, the connection pipe 5 sequentially passes through the inner shell 1 and the outer shell 2 to be connected with the accumulator 6 located outside, and a shaft seal is provided at a connection position of the connection pipe 5 and the inner shell 1/the outer shell 2;
the outer shell 1 and the inner shell 2 are connected through a plurality of rib plates 4 distributed along the circumference, the number of the rib plates 4 distributed along the circumference is at least 4, as shown in fig. 2, the filling layer 3 is divided into a plurality of areas by the plurality of rib plates 4, the inner shell 2 in the area of the connecting pipe 5 is set as a honeycomb plate, vibration noise is easier to transmit from the area because the area of the connecting pipe 5 needs to be perforated, therefore, the inner shell 2 in the area of the connecting pipe 5 is made of the honeycomb plate, the outer shell 3 provides strength support, and the noise reduction effect can be realized through the dual noise reduction of the honeycomb plate and the filling layer 3, and at the initial stage of assembly, through the perforated holes arranged on the honeycomb plate structure, the connecting pipe 5 is pre-pressed into the perforated holes and is arranged at the joints of the inner shell 1/the outer shell 2 respectively, and shaft sealing is arranged at the joints of the inner shell 1/the outer shell 2.

Claims (5)

1. The utility model provides a double-deck shell structure of rotor compressor, rotor compressor has last cap, casing down, its characterized in that, still include with go up the cap casing inferior valve body sealing connection's double-deck shell, double-deck shell is equipped with shell body, interior casing, and sets up filling layer between shell body, the interior casing.
2. A double shell structure of a rotor type compressor in accordance with claim 1, wherein said inner shell end is hermetically connected to said upper shell cover and said lower shell.
3. The double-shell structure of a rotor compressor according to claim 1, wherein the outer shell and the inner shell are connected by a plurality of rib plates, the plurality of rib plates divide the filling layer into a plurality of regions, and the regions are filled with sound absorbing material.
4. A double-layered casing structure of a rotor type compressor in accordance with claim 3, wherein a connection pipe is provided on the double-layered casing for connecting to an external reservoir, the connection pipe is provided on the outer casing and the inner casing, and is connected to the external reservoir through the inner casing and the outer casing in sequence, and a shaft seal is provided at a connection position of the connection pipe and the inner casing/the outer casing.
5. A double-shell structure of a rotor compressor in accordance with claim 4, wherein the inner shell of the area where the connection pipe is located is a honeycomb panel structure.
CN202123363046.4U 2021-12-29 2021-12-29 Double-layer shell structure of rotor type compressor Active CN217582493U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202123363046.4U CN217582493U (en) 2021-12-29 2021-12-29 Double-layer shell structure of rotor type compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202123363046.4U CN217582493U (en) 2021-12-29 2021-12-29 Double-layer shell structure of rotor type compressor

Publications (1)

Publication Number Publication Date
CN217582493U true CN217582493U (en) 2022-10-14

Family

ID=83526632

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202123363046.4U Active CN217582493U (en) 2021-12-29 2021-12-29 Double-layer shell structure of rotor type compressor

Country Status (1)

Country Link
CN (1) CN217582493U (en)

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