A static disc intake structure for an air conditioning compressor in a new energy vehicle

Abstract

This utility model discloses a stationary disc air intake structure for a new energy vehicle air conditioning compressor, including a stationary disc housing, turbine teeth, and a stop block. The stationary disc housing is a cylindrical shape with a bottom, and a main air outlet is opened at the center of its bottom. The turbine teeth are fixed to the inner wall of the bottom of the stationary disc housing. One side of the stop block is fixed to the inner wall of the side of the stationary disc housing, and the other side is fixed to the arc-shaped surface of the turbine teeth. By setting the stop block and setting the first and second air intake holes on its two sides, the incoming gas can be evenly distributed around the turbine teeth. The third air intake hole is set at the airflow inlet near the turbine teeth to ensure that the gas is evenly distributed to the starting end of the turbine teeth. The extension surfaces set in the first, second, and third air intake holes guide the direction of the gas without affecting the gas flow rate, so that the gas can smoothly enter the turbine teeth for compression.

Description

Technical Field

[0001] This utility model relates to the field of air conditioning compressor technology, and in particular to a static disc intake structure for an air conditioning compressor for new energy vehicles. Background Technology

[0002] The scroll compressor in an automotive air conditioning system mainly consists of a moving plate and a stationary plate (collectively referred to as the scroll). The moving plate inserts into the stationary plate and drives the rotation center to rotate via an eccentric main shaft, thereby completing the compression process from intake to exhaust. Among these components, the design of the stationary plate intake structure directly affects the compressor's efficiency, noise, and reliability. Existing intake ports are unevenly distributed when gas enters the compression chamber, and eddies or backflow may occur in some areas, leading to localized over-compression or under-compression and increasing power consumption.

[0003] To address the shortcomings of existing technologies, it is necessary to design a static disc intake structure for air conditioning compressors in new energy vehicles. Utility Model Content

[0004] The purpose of this utility model is to address the shortcomings of existing technologies by proposing a static disc intake structure for a new energy vehicle air conditioning compressor.

[0005] A stationary disc air intake structure for an air conditioning compressor in a new energy vehicle includes a stationary disc housing, turbine teeth, and a stop block. The stationary disc housing is a cylindrical shape with a bottom, and a main air outlet is provided at the center of its bottom. The turbine teeth are fixed to the inner wall of the bottom of the stationary disc housing. One side of the stop block is fixed to the inner wall of the side of the stationary disc housing, and the other side is fixed to the arc-shaped surface of the turbine teeth. A first air intake hole, a second air intake hole, and a third air intake hole are provided on the side of the stationary disc housing. The first air intake hole and the second air intake hole are located on both sides of the stop block, and the third air intake hole is located near the airflow inlet of the turbine teeth. The first air intake hole, the second air intake hole, and the third air intake hole are provided with extension surfaces, and the direction of the extension surfaces is towards the airflow inlet of the turbine teeth.

[0006] Furthermore, the first air intake, the second air intake, and the third air intake are all located tangentially to the arcuate surface of the turbine teeth.

[0007] Furthermore, a sealing cavity is provided on the outer bottom of the static plate housing, auxiliary air outlets are provided on both sides of the main air outlet, a small return air hole and an oil-gas filter hole are provided at the top opening of the static plate housing, a large return air hole is provided at the bottom of the static plate housing, the oil-gas filter hole extends vertically to the bottom of the static plate housing, the small return air hole and the large return air hole are connected, and the large return air hole, auxiliary air outlets and the main air outlet are all located in the sealing cavity.

[0008] Furthermore, the sealing cavity is an annular protrusion with a sealing groove on it, and a sealing rubber ring is provided in the groove.

[0009] Furthermore, the center of the turbine tooth corresponds to the position of the main exhaust port.

[0010] Furthermore, the static disk housing has two symmetrical fixing holes at the top opening and near the bottom edge, several notches at the top and bottom edges, and several balancing air holes at the bottom.

[0011] Beneficial effects: By setting a baffle and placing the first and second air inlets on both sides, the incoming gas can be evenly distributed around the turbine teeth. The third air inlet is located near the airflow inlet of the turbine teeth, ensuring that the gas is evenly distributed to the starting end of the turbine teeth. The extension surfaces set inside the first, second, and third air inlets guide the direction of the gas without affecting the gas flow rate, allowing the gas to smoothly enter the turbine teeth for compression. Attached Figure Description

[0012] Figure 1 This is a three-dimensional structural diagram of the static disc air intake structure of the new energy vehicle air conditioning compressor of this utility model; Figure 2 This is a schematic diagram showing the positions of the first air inlet, the second air inlet, and the third air inlet of this utility model. Figure 3 This is a three-dimensional structural diagram of the bottom outer side of the static disk housing of this utility model; Figure 4 This is a three-dimensional structural diagram of the sealing cavity on the static disk housing of this utility model; In the picture: 1. Static disc housing; 1a. Main air outlet; 1b. First air inlet; 1c. Second air inlet; 1d. Third air inlet; 1e. Small return air inlet; 1f. Oil and gas filter hole; 1g. Large return air inlet; 2. Turbine gear; 3. Stop block. Detailed Implementation

[0013] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0014] Please refer to Figures 1-4This embodiment proposes a stationary disc air intake structure for a new energy vehicle air conditioning compressor, including a stationary disc housing 1, a turbine gear 2, and a stop block 3. The stationary disc housing 1 is a cylindrical shape with a bottom, and a main air outlet 1a is opened at the center of its bottom. The turbine gear 2 is fixed to the inner wall of the bottom of the stationary disc housing 1, and the center of the turbine gear 2 corresponds to the position of the main air outlet 1a. One side of the stop block 3 is fixed to the inner wall of the side of the stationary disc housing 1, and the other side is fixed to the arc-shaped surface of the turbine gear 2. A first air inlet 1b, a second air inlet 1c, and a third air inlet 1d are opened on the side of the stationary disc housing 1. The first air inlet 1b, the second air inlet 1c, and the third air inlet 1d are all located at the position of the turbine gear 2. On the tangential direction of the arc-shaped surface; the first air inlet 1b and the second air inlet 1c are located on both sides of the baffle 3. By setting the baffle 3 and placing the first air inlet 1b and the second air inlet 1c on its sides, the incoming gas can be evenly distributed around the turbine tooth 2. The third air inlet 1d is located near the airflow inlet of the turbine tooth 2, ensuring that the gas is evenly distributed to the starting end of the turbine tooth 2. The first air inlet 1b, the second air inlet 1c and the third air inlet 1d are provided with extension surfaces. The direction of the extension surfaces is towards the airflow inlet of the turbine tooth 2. By setting the extension surfaces to guide the direction of the gas without affecting the gas flow rate, the gas can smoothly enter the turbine tooth 2 for compression.

[0015] A sealing cavity is provided on the outer bottom of the stationary disc housing 1. Auxiliary vent holes are provided on both sides of the main vent hole 1a. A small return vent hole 1e and an oil-gas filter hole 1f are provided at the top opening of the stationary disc housing 1. A low-pressure oil filter screen, a one-way valve, a one-way valve spring, and a one-way valve plug are sequentially arranged in the oil-gas filter hole 1f from the top opening to the bottom of the stationary disc housing 1. A large return vent hole 1g is provided at the bottom of the stationary disc housing 1. The oil-gas filter hole 1f extends vertically to the bottom of the stationary disc housing 1. The small return vent hole 1e and the large return vent hole 1g... The air vents 1g are interconnected. The large return air vent 1g, the auxiliary air vent, and the main air vent 1a are all located inside the sealing cavity. The sealing cavity is an annular protrusion with a sealing groove. A sealing ring is installed in the groove to ensure the internal sealing effect. Two symmetrical fixing holes are opened at the top opening and near the bottom edge of the stationary plate housing 1. Several notches are opened at the top and bottom edges of the stationary plate housing 1. Several balancing air vents are also opened at the bottom of the stationary plate housing 1. The balancing air vents can be set as through holes of different sizes.

[0016] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. A new energy automobile air conditioner compressor static disc air inlet structure, characterized in that: The device includes a stationary disk housing (1), a turbine tooth (2), and a stop block (3). The stationary disk housing (1) is a cylindrical shape with a bottom. A main air outlet (1a) is provided at the center of the bottom. The turbine tooth (2) is fixed to the inner wall of the bottom of the stationary disk housing (1). One side of the stop block (3) is fixed to the inner wall of the side of the stationary disk housing (1), and the other side is fixed to the arc surface of the turbine tooth (2). A first air inlet (1b), a second air inlet (1c), and a third air inlet (1d) are provided on the side of the stationary disk housing (1). The first air inlet (1b) and the second air inlet (1c) are located on both sides of the stop block (3), and the third air inlet (1d) is located near the airflow inlet of the turbine tooth (2). An extension surface is provided in the first air inlet (1b), the second air inlet (1c), and the third air inlet (1d). The direction of the extension surface is towards the airflow inlet of the turbine tooth (2).

2. The static disc intake structure of claim 1, wherein: The first air inlet (1b), the second air inlet (1c) and the third air inlet (1d) are all located on the tangential direction to the arc surface of the turbine tooth (2).

3. The static disc intake structure of claim 1, wherein: A sealing cavity is provided on the outer bottom of the static disk housing (1). Auxiliary air outlets are provided on both sides of the main air outlet (1a). A small return air outlet (1e) and an oil and gas filter (1f) are provided at the top opening of the static disk housing (1). A large return air outlet (1g) is provided at the bottom of the static disk housing (1). The oil and gas filter (1f) extends vertically to the bottom of the static disk housing (1). The small return air outlet (1e) and the large return air outlet (1g) are connected. The large return air outlet (1g), the auxiliary air outlets, and the main air outlet (1a) are all located in the sealing cavity.

4. The static disc intake structure of claim 3, wherein: The sealing cavity is an annular protrusion with a sealing groove, and a sealing ring is placed in the groove.

5. The static disc intake structure of claim 1, wherein: The center of the turbine tooth (2) corresponds to the position of the main exhaust port (1a).

6. The static disc intake structure according to claim 1, characterized in that: The static disk housing (1) has two symmetrical fixing holes at the top opening and near the bottom edge. The static disk housing (1) also has several notches at the top and bottom edges, and several balancing air holes at the bottom.

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