Modal test structure temperature compensator in vacuum environment

一种温度补偿器、模态试验的技术,应用在宇宙航行条件的模拟装置、宇宙航行设备、运输和包装等方向,能够解决试件热量散失等问题

Active Publication Date: 2020-04-28
INST OF MECHANICS CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The high-temperature test piece in the vacuum environment is easy to radiate heat to the surrounding space, causing heat loss inside the test piece

Method used

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Examples

Experimental program
Comparison scheme
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Embodiment Construction

[0015] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments 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 belong to the protection scope of the present invention.

[0016] In order to facilitate the understanding of the embodiments of the present invention, further explanations will be given below with specific embodiments in conjunction with the accompanying drawings, which are not intended to limit the embodiments of the present invention.

[0017] see Figure 1-2 , a temperature compensator for modal...

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PUM

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Abstract

The embodiment of the invention relates to a modal test structure temperature compensator in a vacuum environment. The modal test structure temperature compensator comprises a thermal vacuum test boxbody, an upper compensation plate and a lower compensation plate, the upper compensation plate and the lower compensation plate jointly form the temperature compensator, a test piece is fixed on the inner rear wall of the thermal vacuum test box body, and the upper compensation plate and the lower compensation plate are respectively positioned on the upper side and the lower side of the test piece, are made of the same material, have the same thermal load as the test piece, and cover most circumferential positions of the test piece to effectively reduce the radiation heat of the test piece tothe surrounding space; and an annular base is used for fixedly connecting the upper compensation plate and the lower compensation plate to the inner rear wall of the thermal vacuum test box body, threaded holes are used in cooperation with screws, and the annular base is fixed to the rear wall of the interior of the thermal vacuum test box body through the screws, so the upper compensation plate and the lower compensation plate are stably connected through the connecting mode, thereby vibration caused by external force is avoided, and the test piece is prevented from being affected.

Description

technical field [0001] The embodiment of the present invention relates to a temperature compensator for a thermal vacuum test, in particular to a temperature compensator for a modal test structure in a vacuum environment. Background technique [0002] The thermal vacuum test refers to the test to verify the performance and function of the test piece under the condition of vacuum and certain temperature. During the development process of the spacecraft, the thermal vacuum test must be carried out. The launched spacecraft, whether it is the first launch or a repeated launch, must undergo an acceptance-level thermal vacuum test for each launch. [0003] The high-temperature test piece in the vacuum environment is easy to radiate heat to the surrounding space, causing heat loss inside the test piece. Contents of the invention [0004] In view of this, in order to reduce the influence of heat radiation, an embodiment of the present invention provides a temperature compensator ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G7/00
CPCB64G7/00B64G2007/005
Inventor 郑冠男黄杰杨国伟聂雪媛黄程德宋鑫徐铭杰陈军屹
Owner INST OF MECHANICS CHINESE ACAD OF SCI
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