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Plume particle settling protection device for electric propulsion test and its vacuum test system

A protective device and a technology for testing, applied in the field of space propulsion systems, can solve the problems of high temperature plume particles not being discharged in time, damage to the plume particle settlement protection device, difficulty in installation and disassembly, etc., to achieve easy installation and maintenance, and long service life long-term, accurate effect

Active Publication Date: 2021-03-02
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The current plume particle settling protection device has complex structure, difficult installation and disassembly, and its heat dissipation efficiency is not high.

Method used

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  • Plume particle settling protection device for electric propulsion test and its vacuum test system
  • Plume particle settling protection device for electric propulsion test and its vacuum test system
  • Plume particle settling protection device for electric propulsion test and its vacuum test system

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Embodiment Construction

[0028] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0029] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, or in a specific orientation. construction and operation, and therefore cannot be constru...

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Abstract

The invention discloses a plume particle settlement protection device for electric propulsion tests, which comprises a protective shell body arranged in a vacuum test container, the protective shell body is an inner concave disc structure, and the inner concave axial center position of the protective shell body is There is an external convex part with an integrated structure, and the concave surface of the protective shell body is fixedly welded with multiple sets of cooling branch pipes in a circular array from its outer ring to the axial center of the external convex part, and the surface of the cooling branch pipes is fixedly welded with particle settlement protection barriers The two ends of the protective shell body are fixedly welded with liquid inlet and outlet pipes. The device of the invention has a simple structure, is easy to install and maintain, can realize the cooling of the plume particle settlement protection device, avoids its aging and damage, and prolongs its service life.

Description

technical field [0001] The invention belongs to the technical field of space propulsion systems, in particular to a plume particle settlement protection device for electric propulsion tests. Background technique [0002] With the development of my country's aerospace technology, various high-performance platforms have increasingly urgent requirements for the application of electric propulsion technology. The demand for high specific impulse multi-mode electric propulsion system, the demand for high-power and high-thrust electric propulsion system for deep space exploration, etc. [0003] At present, the development of electric propulsion technology in my country is in full swing, and the research on electric propulsion systems has entered a stage of steady development. At present, the main performance indicators have approached or reached the international advanced level, and the basic conditions for engineering applications have been met. Although the main indicators (thrus...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01L21/30
Inventor 王军伟张磊李高宁娟白冰付春雨刘然邵静怡刘洋洋
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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