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Detachable flow resistance adjusting module, method and system of space propulsion system

A technology for adjusting modules and space propulsion, which is applied in the direction of aerospace vehicle propulsion system devices, fluid flow, mechanical equipment, etc., and can solve the problem of low flow resistance adjustment efficiency and production efficiency, poor installation status of orifice plates, and difficult flow resistance Data accuracy and other issues, to achieve the effect of reducing product weight and use cost, improving production efficiency, improving flow resistance adjustment efficiency and production efficiency

Inactive Publication Date: 2021-05-14
SHANGHAI INST OF SPACE PROPULSION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, the flow resistance of many types of pipelines needs to be controlled with an accuracy better than 2%, or even 1%. According to the current flow resistance adjustment mode, one is to directly use the system product pipelines and valves for flow resistance debugging. Pipeline cutting and cleaning, this mode can ensure the accuracy of flow resistance adjustment, but directly using the product pipeline for debugging, and then cutting and cleaning, there is a risk of excess material, affecting product safety, and increasing product weight, affecting the progress of the main product line
Another mode is to use the process pipeline for flow resistance debugging. After the debugging is completed, the debugged orifice plate is removed separately, and then installed into the system. This mode has little impact on the main line of the system product and will not generate extra However, due to the difference in the installation state of the orifice plate, it is difficult to control the accuracy of the flow resistance data at 2% after the orifice plate is removed and reinstalled to the product pipeline of the system
[0004] In view of the related technologies mentioned above, the inventor believes that there are problems of low flow resistance adjustment efficiency and low production efficiency, therefore, a technical solution needs to be proposed to improve the above technical problems

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  • Detachable flow resistance adjusting module, method and system of space propulsion system
  • Detachable flow resistance adjusting module, method and system of space propulsion system
  • Detachable flow resistance adjusting module, method and system of space propulsion system

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Embodiment Construction

[0032] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0033] refer to figure 1 and figure 2 , The present invention provides a detachable flow resistance adjustment module of a space propulsion system, which includes a flow resistance adjustment module housing, an adjustment orifice plate, a compression nut, and a detachable casing nut. The flow resistance adjustment module is connected to the process pipeline through the detachable jacket nut to adjust the flow resistance of the pipeline. The flow resistance adjustment device is designed as a detachable...

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Abstract

The invention provides a detachable flow resistance adjusting module of a space propulsion system. The detachable flow resistance adjusting module comprises a flow resistance adjusting module shell, an adjusting pore plate is arranged in the flow resistance adjusting module shell, a compression nut is arranged in the flow resistance adjusting module shell, and a detachable jacket nut is arranged on the outer side wall of the flow resistance adjusting module shell. According to the detachable flow resistance adjusting module, method and system of the space propulsion system, the detachable module type flow resistance adjusting device is adopted for an engine propellant supply system in the space propulsion field for the first time, the flow resistance adjusting efficiency and the production efficiency are improved, the weight and the use cost of a system product are reduced, and meanwhile, the flow resistance adjusting precision can be ensured.

Description

technical field [0001] The present invention relates to the technical field of flow resistance adjustment, in particular to a detachable flow resistance adjustment module of a space propulsion system and an implementation method thereof. Background technique [0002] With the development of aerospace technology, aerospace products have more and more precise control over the flow resistance of the engine pipeline, and more and more stringent weight control, and because many aerospace products require a suitable launch window, the production schedule requirements for many products are relatively strict, and at the same time It is also common for a product to be produced on multiple lines. [0003] At present, the flow resistance of many types of pipelines needs to be controlled with an accuracy better than 2%, or even 1%. According to the current flow resistance adjustment mode, one is to directly use the system product pipelines and valves for flow resistance debugging. Pipe...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/40F15D1/02B23K31/02
CPCB64G1/40F15D1/02B23K31/02
Inventor 赵正钟雪莹王浩陈晓王亚平朱鹏程易凌宇叶青
Owner SHANGHAI INST OF SPACE PROPULSION