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A three-rocker arm test device for composite motion microgravity deployment of space mechanism

A compound motion and test device technology, which is applied in the testing of machine/structural components, testing of mechanical components, simulation devices for space navigation conditions, etc., to achieve the effect of precise motion

Active Publication Date: 2022-07-29
TIANJIN AEROSPACE ELECTROMECHANICAL EQUIP RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the difference in the ground gravity environment, the gravity of the mechanism needs to be unloaded on the ground, and the microgravity ground verification test is carried out. The development process of the microgravity unloading system is also constantly improving; the simulation technology of the rocker suspension test device is widely used in spacecraft For the ground microgravity deployment test of mechanisms, for the mechanism deployed around a fixed axis in the plane, the rocker suspension unloading method is often used, but for the working condition that the center of mass of the deployment mechanism changes continuously with the deployment process, the traditional suspension The hanging method cannot be satisfied with the microgravity deployment of the mechanism, and it is necessary to develop a test device for multi-rocker suspension unloading

Method used

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  • A three-rocker arm test device for composite motion microgravity deployment of space mechanism
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  • A three-rocker arm test device for composite motion microgravity deployment of space mechanism

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Embodiment Construction

[0030] It should be noted that the embodiments of the present invention and the features of the embodiments may be combined with each other under the condition of no conflict.

[0031] In the description of the present invention, it should be understood that the terms "center", "portrait", "horizontal", "top", "bottom", "front", "rear", "left", "right", " The orientation or positional relationship indicated by vertical, horizontal, top, bottom, inner, outer, etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and The description is simplified rather than indicating or implying that the device or element referred to must have a particular orientation, be constructed and operate in a particular orientation, and therefore should not be construed as limiting the invention. In addition, the terms "first", "second", etc. are used for descriptive purposes only, and should not be constru...

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Abstract

The present invention provides a three-rocker arm test device for composite motion microgravity deployment of a space mechanism, comprising a rocker arm support, a No. 1 spindle support, a No. 2 spindle support, a No. 1 rocker arm assembly, a No. 2 rocker arm assembly, a No. No. 1 rocker arm assembly, No. 1 spindle body, No. 2 spindle body, double shaft assembly and single shaft assembly; the rocker arm bracket is mounted to the truss, and the top and bottom ends of one side of the rocker arm bracket are respectively installed with a No. A No. 1 spindle body is installed between the No. 1 spindle brackets, a No. 2 spindle bracket is installed on the top and middle of the other side of the rocker arm bracket, and a No. 2 spindle body is installed between the two No. 2 spindle brackets; the No. 1 rocker arm The assembly and the No. 2 rocker arm assembly are connected to the No. 1 spindle body through a double shaft assembly, and the No. 3 rocker arm assembly is connected to the No. 2 spindle body through a single shaft assembly. The invention always provides a device for deployment in a microgravity environment, which reliably verifies the feasibility of the ground deployment test of the deployment mechanism.

Description

technical field [0001] The invention belongs to the field of test devices, in particular to a three-rocker test device used for compound motion microgravity deployment of a space mechanism. Background technique [0002] With the continuous development of human space exploration technology, the continuous expansion of the scale of exploration, the increasing frequency of human activities, and the increasing number of launchers, in the face of high development and launch costs, space agencies gradually tend to have a high storage ratio. The weight of the mechanism is continuously reduced, and the launch cost can be reduced as much as possible while realizing its function. For the lightweight design of the mechanism, it is very important to be able to realize its function. For the deployment mechanism, the robustness of the system design needs to be verified on the ground. Due to the difference of the ground gravity environment, it is necessary to carry out the microgravity gr...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G7/00G01M13/00
CPCB64G7/00G01M13/00
Inventor 刘海腾李占芯王利桐胡政谢旭超
Owner TIANJIN AEROSPACE ELECTROMECHANICAL EQUIP RES INST
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