A device for exposing materials outside the cabin

A technology of assembly cavity and assembly port, which is applied in the field of material exposure device outside the cabin

Active Publication Date: 2021-08-24
TECH & ENG CENT FOR SPACE UTILIZATION CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, my country is still in its infancy in terms of space material exposure. In order to meet the task requirements of material space exposure, it is urgent to involve a test system that can be repeatedly installed, repeatedly locked and released on the track, and automatically unfolded and closed. / experiment box

Method used

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  • A device for exposing materials outside the cabin
  • A device for exposing materials outside the cabin
  • A device for exposing materials outside the cabin

Examples

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Embodiment 1

[0043] Such as Figure 1-5 As shown, a device for exposing materials outside the cabin is installed on the outer platform of an orbiting spacecraft, including:

[0044] The base 21 is used for detachable installation on the outer platform of the orbiting spacecraft; the base 21 is a polygonal structure, and a gap 211 is reserved on one edge of the base 21;

[0045] Load center frame 25, the load center frame 25 is vertically fixedly installed at the center of the base 21;

[0046] The mounting bracket 22 is vertically fixedly installed on the base 21; each side of the mounting bracket 22 corresponding to the base 21 is respectively provided with at least one assembly port;

[0047] A number of test boxes 1, and a number of test boxes 1 are detachably installed in the assembly port;

[0048] The four-degree-of-freedom inspection robot arm 8, the four-degree-of-freedom inspection robot arm 8 is erected above the experimental box 1, and one end of the four-degree-of-freedom ins...

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Abstract

The invention relates to a device for exposing materials outside the cabin, which is installed on the outer platform of an orbiting spacecraft, including a base, a load center frame, a mounting bracket, several experimental boxes, and a four-degree-of-freedom inspection robot arm. A gap is left; the load center frame is vertically fixed and installed at the center of the base; each side of the base corresponding to the mounting bracket is provided with at least one assembly port; several test boxes are detachably installed in the assembly port; four degrees of freedom inspection One end of the robotic arm is rotatably connected to the top of the load center frame, and the other end is movable in the gap; an image acquisition device is slidably installed on the four-degree-of-freedom inspection robotic arm; where the other end of the four-degree-of-freedom inspection robotic arm moves out of the gap , the test box is opened, and the exposed surface of the test box is perpendicular to the base and parallel to the side of the corresponding base; the four-degree-of-freedom inspection robot arm drives the image acquisition device to rotate around the load center frame, and sequentially inspects the exposed surfaces of several test boxes. check.

Description

technical field [0001] The invention relates to the field related to the external exposure of space station materials, in particular to a material external exposure device. Background technique [0002] In order to meet the needs of future deep space exploration, it is of far-reaching significance to study the in-orbit service behavior of materials in the field of basic disciplines, and to study the in-orbit characteristics and changes of materials. During the missions of the former Soviet space station and the International Space Station, on-orbit exposure tests of metal and non-metal materials have been verified many times, and significant scientific research results have been achieved. However, my country is still in its infancy in terms of space material exposure. In order to meet the task requirements of material space exposure, it is urgent to involve a test system that can be repeatedly installed, repeatedly locked and released on the track, and automatically unfolded...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G4/00B64G1/66
CPCB64G1/66B64G4/00B64G2004/005
Inventor 王珂劳冠清吕宏宇杨鹏张聚乐李碘红
Owner TECH & ENG CENT FOR SPACE UTILIZATION CHINESE ACAD OF SCI
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