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Movable support capable of adjusting test piece angle in vacuum container

A technology of moving brackets and vacuum containers, which is applied in the direction of machines/supports, simulation devices of space navigation conditions, supporting machines, etc., to achieve the effect of solving the problem of angle adjustment

Active Publication Date: 2015-04-08
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide a movable bracket that realizes the adjustable angle of the test piece in the vacuum container, aiming to solve the problem of correctly simulating the change of the external heat flow of the test piece when it moves on the track

Method used

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  • Movable support capable of adjusting test piece angle in vacuum container
  • Movable support capable of adjusting test piece angle in vacuum container
  • Movable support capable of adjusting test piece angle in vacuum container

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Embodiment Construction

[0019] The movable support for adjusting the angle of the test piece in the vacuum container of the present invention will be further described below in conjunction with the accompanying drawings.

[0020] Such as Figure 1-2 As shown, the movable bracket capable of adjusting the angle of the test piece in the vacuum container of the present invention comprises a lower bracket car body 1, an upper bracket car body 2, an upper flange 3, and a lower flange 22, and the lower bracket car body 1 is butted by a hollow tube Constitute a square frame, the four inner corners of the square frame are respectively provided with inclined reinforcing ribs and a small square frame protruding from one side of the frame, the overall shape of the lower bracket car body is similar to the shape of a common dry battery, the lower bracket car body 1 The reinforcing rib is provided with an annular lower flange 22, and the lower flange 22 is butted with an upper flange 3 of the same shape and size. ...

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Abstract

The invention discloses a movable support capable of adjusting the test piece angle in a vacuum container, which comprises a lower support body, an upper support body, an upper flange and a lower flange, wherein the lower support body and the upper support body are butted to form a square frame by hollow pipes, reinforcing ribs are arranged at four inner corners of the square frame, the ring-shaped upper flange and the ring-shaped lower flange are arranged on the reinforcing ribs on the upper support body and the lower support body respectively, and axial positions of the upper flange and the lower flange can be guaranteed to be unchanged by means of opposite rotation and a fixing block, so that the test piece angle is adjusted by means of rotation of the flanges. By the aid of the movable support capable of adjusting the test piece angle in the vacuum container, the problem of angle adjustment of a test piece in the vacuum container is effectively solved, and external heat flow change conditions of the surface of a satellite in orbiting are sufficiently simulated.

Description

technical field [0001] The invention belongs to the field of mechanical design, and in particular relates to a movable support device capable of adjusting the angle of a test piece in a vacuum container. Background technique [0002] Bracket is a relatively common tooling device in the field of mechanical design, widely used in civilian and military fields. Depending on the application requirements, the bracket is generally designed to be fixed. [0003] In recent years, with the development of satellite thermal test technology, the real and accurate simulation of external heat flow is the development trend in the field of satellite ground thermal test, so the solar simulator technology has been developed. In order to apply the solar simulator, it is necessary to design appropriate tooling so that the satellite can rotate at a certain angle in the vacuum container to simulate the change of heat flow outside the surface of the satellite when it is in orbit. [0004] At pres...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G7/00F16M13/02F16M11/06F16M11/18
Inventor 陶涛郄殿福刘毅裴一飞苏新明王晶孙继鹏
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG