Gas supply assembly

A technology for components and gas cylinders, applied in jet propulsion devices, gas/liquid distribution and storage, container filling methods, etc., can solve the problems of inconvenient maintenance, cumbersome installation, complicated structure and layout, etc., to save space and reduce production costs , the effect of enhancing system reliability and maintainability

Pending Publication Date: 2021-01-22
北京宇航推进科技有限公司
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  • Abstract
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Problems solved by technology

[0004] The main purpose of the present invention is to provide an air supply assembly to solve the problems of cumbersome installation and inconvenient maintenance caused by the complicated structural layout of the air circuit system in the space orbit attitude control engine in the prior art

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Embodiment Construction

[0020] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0021] In order to enable those skilled in the art to better understand the solutions of the present invention, the following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only It is an embodiment of a part of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts shall fall within the protection scope of the present invention.

[0022] It should be noted that the terms "first...

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Abstract

The invention provides a gas supply assembly. The gas supply assembly comprises a main body structure, a gas cylinder and gas circuit control elements. The main body structure comprises a gas cylindermounting part, a gas circuit mounting part and an external connection part. The gas circuit mounting part is arranged at the upper end of the gas cylinder mounting part. The external connection partis arranged at the lower end of the gas cylinder mounting part. The gas cylinder is mounted on the gas cylinder mounting part and located between the gas cylinder mounting part and the external connection part. The gas cylinder mounting part and the external connection part are matched to clamp the gas cylinder. The gas circuit control elements are mounted on the upper side of the gas circuit mounting part and connected with the gas cylinder. All the gas circuit control elements and the gas cylinder of the gas supply assembly are integrated to the main body structure, so that the gas circuit control elements are mounted conveniently, all the components of the gas supply assembly form an independent module, the final assembly efficiency of a power system is greatly improved, the productioncost is reduced, the structure is compact, space is saved, and the reliability and maintainability of the system are enhanced.

Description

technical field [0001] The invention relates to the technical field of rockets, in particular to an air supply assembly. Background technique [0002] Space orbit attitude control engines are widely used in the upper stages of rockets and satellites, and are the key to the success or failure of missions. The two-component attitude-orbit control power system is widely used in the aerospace field because of its advantages such as high specific impulse, high precision, multiple starts, and wide thrust range. [0003] The gas circuit system in the space-orbit attitude control engine is an important part of the dual-component engine. However, when the gas circuit system in the prior art is installed and used, there are many system components and complicated structural layout, which leads to cumbersome installation and maintenance. Inconvenience and other issues. Contents of the invention [0004] The main purpose of the present invention is to provide an air supply assembly t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F17D1/02F17D3/01F17C13/08F02K9/60
CPCF02K9/60F17C13/084F17D1/02F17D3/01
Inventor 孙夺王明哲郭利明刘业奎李文鹏余鹏杨海峰
Owner 北京宇航推进科技有限公司
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