Compressor shell and compressor

Abstract

The utility model provides a compressor shell which is characterized in that the compressor shell comprises a shell of a compressor in a vehicle machine or a ship machine and comprises a pressing shell and a middle shell; a diffusion channel is arranged between the pressure shell and the middle shell; a guide vane is integrated on the face, facing the diffusion channel, of the middle shell, and the guide vane and the middle shell are of an integrated structure. According to the compressor shell provided by the embodiment of the invention, the guide vanes are integrated on the middle shell, an elastic component in a related technical scheme is omitted, leakage of diffusion gas is reduced, the performance of a compressor is improved, deterioration of the compressor caused by installation of an O-shaped ring or other elastic components is avoided, and the service life of the compressor is prolonged.

Description

Technical Field

[0001] This application belongs to the field of compressor technology, specifically relating to a compressor housing and a compressor. Background Technology

[0002] A compressor is a mechanical device that reduces the volume of gas and increases its pressure. It transforms low-pressure gas into high-pressure gas through various physical processes and is widely used in automotive and marine engines. However, compressors typically have separate guide vanes installed inside the compressor via O-rings or other elastic components. These O-rings and other elastic components have a relatively short lifespan, affecting the compressor's overall lifespan. Furthermore, the use of O-rings or other elastic components can create gaps behind the guide vane's back plate, leading to leakage of diffused gas and impacting the compressor's efficiency and pressure ratio. Additionally, the installation of O-rings or other elastic components introduces variations to the compressor, affecting its performance consistency. Utility Model Content

[0003] To address the problems existing in the prior art, a compressor housing and compressor are proposed, which can improve the service life and performance of the compressor.

[0004] This application provides the following solutions.

[0005] In a first aspect, this application provides a compressor housing, which includes the housing of a compressor in a vehicle or ship engine, comprising: a pressure shell and an intermediate shell;

[0006] A pressure diffusion channel is provided between the pressure shell and the intermediate shell;

[0007] The middle shell has integrated guide vanes on the side facing the diffuser channel, and the guide vanes and the middle shell are an integral structure.

[0008] In some possible embodiments, the pressure shell includes an upper expanding surface, and the intermediate shell includes a lower expanding surface;

[0009] The upper and lower expansion surfaces form a diffusion channel.

[0010] In some possible embodiments, there is a gap between the top surface of the guide vane and the upper expansion surface.

[0011] In some possible embodiments, the width of the gap is less than or equal to 1 mm.

[0012] In some possible embodiments, the width of the gap includes 0.1 mm.

[0013] Secondly, this application provides a compressor that is used in vehicle or marine machinery. The compressor includes a compressor housing and a compressor assembly inside the compressor housing.

[0014] The compressor housing includes a pressure shell and an intermediate shell;

[0015] A pressure diffusion channel is provided between the pressure shell and the intermediate shell;

[0016] The middle shell has integrated guide vanes on the side facing the diffuser channel, and the guide vanes and the middle shell are an integral structure.

[0017] In some possible embodiments, the pressure shell includes an upper expanding surface, and the intermediate shell includes a lower expanding surface;

[0018] The upper and lower expansion surfaces form a diffusion channel.

[0019] In some possible embodiments, there is a gap between the top surface of the guide vane and the upper expansion surface.

[0020] In some possible embodiments, the width of the gap is less than or equal to 1 mm.

[0021] In some possible embodiments, the width of the gap includes 0.1 mm.

[0022] The compressor housing provided in this application integrates the guide vanes onto the intermediate shell, omitting the elastic components in related technical solutions, reducing leakage of diffused gas, improving compressor performance, and avoiding the degradation caused by installing O-rings or other elastic components, thus extending the compressor's service life.

[0023] Other advantages of this application will be explained in more detail with reference to the following description and figures.

[0024] It should be understood that the above description is merely an overview of the technical solution of this application, so as to enable a clearer understanding of the technical means of this application and thus allow for its implementation in accordance with the contents of the specification. To make the above and other objects, features, and advantages of this application more apparent and understandable, specific embodiments of this application are illustrated below. Attached Figure Description

[0025] By reading the detailed description of the exemplary embodiments below, those skilled in the art will understand the advantages and benefits described herein, as well as other advantages and benefits. The accompanying drawings are for illustrative purposes only and are not intended to limit the scope of this application. Furthermore, the same reference numerals denote the same parts throughout the drawings. In the drawings:

[0026] Figure 1 A schematic diagram of a compressor housing provided for an embodiment of this application;

[0027] Figure 2 A partial schematic diagram of region A provided in an embodiment of this application;

[0028] Figure 3 A schematic diagram of an intermediate shell provided for an embodiment of this application;

[0029] Figure 4 This is a schematic diagram of a compressor provided in an embodiment of this application.

[0030] In the accompanying drawings, the same or corresponding reference numerals indicate the same or corresponding parts. Detailed Implementation

[0031] Exemplary embodiments of this application will now be described in more detail with reference to the accompanying drawings. While exemplary embodiments of this application are shown in the drawings, it should be understood that this application can be implemented in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided to enable a more thorough understanding of this application and to fully convey the scope of this application to those skilled in the art.

[0032] In the description of embodiments of this application, it should be understood that terms such as "comprising" or "having" are intended to indicate the presence of the disclosed features, numbers, steps, actions, components, portions, or combinations thereof in this specification, and do not exclude the possibility of the presence of one or more other features, numbers, steps, actions, components, portions, or combinations thereof. The terms "first," "second," etc., are used only for ease of description to distinguish identical or similar technical features and should not be construed as indicating or implying the relative importance or number of these technical features. Thus, a feature defined by "first," "second," etc., may explicitly or implicitly include one or more of that feature. In the description of embodiments of this application, unless otherwise stated, the term "multiple" means two or more.

[0033] Unless otherwise stated, " / " signifies "or," for example, A / B can mean either A or B. "And / or" in this document is merely a description of the relationship between related objects, indicating that three relationships can exist. For example, A and / or B can represent: A alone, A and B simultaneously, and B alone. For ease of description, spatial relation terms such as "below," "under," "above," and "upper" may be used here to describe the relationship between one element or feature shown in the accompanying drawings and other elements or features. It will be understood that these spatial relation terms are intended to include directions other than those depicted in the accompanying drawings for devices in use or operation.

[0034] It should also be noted that, unless otherwise specified, the embodiments and features described in this application can be combined with each other. This application will now be described in detail with reference to the accompanying drawings and embodiments.

[0035] See Figure 1The figure is a schematic diagram of a compressor housing provided in an embodiment of this application.

[0036] The compressor housing provided in this application includes the housing of a compressor in a vehicle or ship engine. For example... Figure 1 As shown, the compressor housing provided in this embodiment includes: a pressure shell 200 and an intermediate shell 100;

[0037] A pressure diffusion channel 300 is provided between the pressure shell 200 and the intermediate shell 100;

[0038] The middle shell 100 has a guide vane 101 integrated on the side facing the diffuser channel 300. The guide vane 101 and the middle shell 100 are an integral structure.

[0039] It should be noted that a compressor assembly may be disposed inside the compressor housing in this embodiment. The compressor housing and the compressor assembly together constitute the compressor. The compressor in this embodiment can be applied to marine engines or vehicle engines. The compressor provided in this application can be applied to traditional automobiles or new energy vehicles, and can also be applied to off-road vehicles, such as excavators, etc., which are not limited here. In this embodiment, by integrating the guide vanes onto the intermediate shell, the integrated guide vanes can perform the same function as the guide vanes in related technical solutions, and since the guide vanes and the intermediate shell are an integrated design structure, no other components are needed to fix the guide vanes. Thus, the technical solution of this embodiment can improve the performance of the compressor and extend its service life.

[0040] like Figure 2 As shown in the partial view of region A, in this embodiment of the application, the pressure shell 200 includes an upper expanding surface 201, and the intermediate shell 100 includes a lower expanding surface 102. The upper expanding surface 201 and the lower expanding surface 102 form a diffuser channel 300. In this embodiment of the application, there is a gap between the top surface of the guide vane 101 and the upper expanding surface 201. In practical applications, the width of the gap is less than or equal to 1 mm. As one possible implementation, the width of the gap in this embodiment of the application can be 0.1 mm.

[0041] It should be noted that in this embodiment, the guide vane 101 is integrated into the intermediate shell, and a gap is provided between the guide vane 101 and the upper expanded surface 201, which can improve the compressor performance to a certain extent. Specifically, compared with the technical solution of fixing the guide vane with O-rings, the position of the gap corresponding to the guide vane in the technical solution of this application has a smaller impact on the compressor performance, and can improve the peak efficiency of the compressor by about 0.8 percentage points. In the technical solution of this application, the guide vane is integrated into the intermediate shell. Compared with the technical solution of fixing the guide vane to the intermediate shell with bolts, the guide vane and the intermediate shell can be integrally processed in this application, and there is no gap between the guide vane and the intermediate shell. Using the technical solution of this application, compared with the technical solution of fixing the guide vane with bolts, the compressor efficiency can be improved by about 1 to 1.5 percentage points, and the compressor pressure ratio is higher. It should also be noted that compared with the technical solution of integrating the guide vane 101 into the pressure shell, the technical solution of integrating the guide vane 101 into the intermediate shell in this application improves the compressor performance more significantly.

[0042] like Figure 3 As shown in the intermediate shell 100, a guide vane 101 is integrated on the lower expanded surface 102 of the intermediate shell. The guide vane 101 and the intermediate shell are an integral structure. In practical applications, the intermediate shell with the guide vane can be integrated into the intermediate shell through casting and mechanized machining. This embodiment of the application does not limit this.

[0043] In summary, the embodiments of this application integrate the guide vanes onto the intermediate shell and position the gap between the guide vanes and the upper expansion surface. The structure of the guide vanes and the location of the gap reduce leakage of diffused gas in the compressor, thereby improving compressor performance. Furthermore, since the guide vanes and the intermediate shell are an integrated design, no other components are needed to fix the guide vanes. Thus, on the one hand, the technical solution of this application improves compressor performance; on the other hand, the technical solution of this application omits the elastic components found in related technical solutions, extending the compressor's service life.

[0044] Based on the compressor housing provided in the above embodiments, this application also provides a compressor.

[0045] like Figure 4 As shown, the compressor provided in this application embodiment is applied to vehicle or ship machinery. The compressor includes: a compressor housing 1000 and a compressor assembly 2000 inside the compressor housing 1000.

[0046] The compressor housing includes a pressure shell and an intermediate shell;

[0047] A pressure diffusion channel is provided between the pressure shell and the intermediate shell;

[0048] The middle shell has integrated guide vanes on the side facing the diffuser channel, and the guide vanes and the middle shell are an integral structure.

[0049] As one possible implementation, the pressure shell includes an upper expanding surface, and the intermediate shell includes a lower expanding surface; the upper expanding surface and the lower expanding surface form a pressure diffusion channel.

[0050] As one possible implementation, there is a gap between the top surface of the guide vane and the upper expansion surface.

[0051] As one possible implementation, the width of the gap is less than or equal to 1 mm. As an example, the width of the gap can be 0.1 mm.

[0052] In summary, the embodiments of this application integrate the guide vanes onto the intermediate shell and position the gap between the guide vanes and the upper expanding surface. The structure of the guide vanes and the location of the gap reduce leakage of diffused gas in the compressor, thereby improving compressor performance. Furthermore, since the guide vanes and the intermediate shell are an integrated design, no other components are needed to fix the guide vanes. Thus, on the one hand, the technical solution of this application improves compressor performance; on the other hand, the technical solution of this application omits the elastic components found in related technical solutions, extending the compressor's service life.

[0053] While illustrative embodiments of this application have been detailed and described in the accompanying drawings and foregoing description, they should be considered illustrative rather than restrictive. It should be understood that only certain exemplary embodiments have been shown and described, and all variations and modifications intended to protect within the spirit and scope of the claimed invention are intended to be protected. It should be understood that while the use of terms such as preferred, preferred, or more preferred in the above description to indicate that such described features may be more desirable, it may not be necessary, and implementations without these features may be contemplated, for example, within the scope of the invention defined by the appended claims. When reading the claims, the use of terms such as “a,” “an,” “at least one,” or “at least a portion” is not intended to limit the claim to one item unless specifically stated otherwise in the claim. When the language “at least a portion” and / or “a portion” is used, an item may include a portion and / or the entire item unless specifically stated otherwise.

[0054] While the spirit and principles of this application have been described above with reference to several specific embodiments, it should be understood that this application is not limited to the disclosed specific embodiments, and the division of aspects does not imply that features in these aspects cannot be combined. This application is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.

Claims

1. A compressor housing, characterized in that, The compressor housing includes the housing of a compressor in a vehicle or ship engine, comprising: a pressure shell and an intermediate shell; A pressure diffusion channel is provided between the pressure shell and the intermediate shell; The intermediate shell has a guide vane integrated on the side facing the diffuser channel, and the guide vane and the intermediate shell are an integral structure.

2. The compressor housing according to claim 1, characterized in that, The pressure shell includes an upper expanding surface, and the intermediate shell includes a lower expanding surface; The upper expanding surface and the lower expanding surface together form the pressure diffusion channel.

3. The compressor housing according to claim 2, characterized in that, There is a gap between the top surface of the guide vane and the upper expansion surface.

4. The compressor housing according to claim 3, characterized in that, The width of the gap is less than or equal to 1 mm.

5. The compressor housing according to claim 3, characterized in that, The width of the gap includes 0.1 mm.

6. A compressor, characterized in that, The compressor is used in vehicle or ship machinery, and the compressor includes: a compressor housing and a compressor assembly inside the compressor housing; The compressor housing includes a pressure shell and an intermediate shell; A pressure diffusion channel is provided between the pressure shell and the intermediate shell; The intermediate shell has a guide vane integrated on the side facing the diffuser channel, and the guide vane and the intermediate shell are an integral structure.

7. The compressor according to claim 6, characterized in that, The pressure shell includes an upper expanding surface, and the intermediate shell includes a lower expanding surface; The upper expanding surface and the lower expanding surface together form the diffusion channel.

8. The compressor according to claim 7, characterized in that, There is a gap between the top surface of the guide vane and the upper expansion surface.

9. The compressor according to claim 8, characterized in that, The width of the gap is less than or equal to 1 mm.

10. The compressor according to claim 8, characterized in that, The width of the gap includes 0.1 mm.

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