Spatial comprehensive environment in-situ and semi-in-situ test shielding device and test shielding method thereof

A technology of in-situ testing and comprehensive environment, applied in the direction of measuring devices, instruments, scientific instruments, etc., can solve the problems of staying, unable to meet the requirements of in-situ/semi-in-situ testing, and the work of instruments and equipment.

Pending Publication Date: 2022-08-05
HARBIN INST OF TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

Moreover, the current tests for this aspect are still mainly in the laboratory state, and the instruments and equipment are all working in a conventional environment, which cannot meet the in-situ / semi-in-situ test requirements

Method used

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  • Spatial comprehensive environment in-situ and semi-in-situ test shielding device and test shielding method thereof
  • Spatial comprehensive environment in-situ and semi-in-situ test shielding device and test shielding method thereof
  • Spatial comprehensive environment in-situ and semi-in-situ test shielding device and test shielding method thereof

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specific Embodiment 1

[0030] according to Figure 1 to Figure 4 As shown, the specific optimized technical solution adopted by the present invention to solve the above technical problems is as follows: the present invention relates to an in-situ and semi-in-situ testing shielding device and a testing shielding method for a comprehensive space environment.

[0031] A space integrated environment in-situ and semi-in-situ testing shielding device, the device includes: testing equipment, a driving mechanism and a remote control system 10, the driving mechanism is equipped with a testing equipment, and the remote control system controls the driving mechanism;

[0032] The test equipment includes a test equipment host 2, a test equipment probe 3 and a test equipment cabin cable 4, and the test equipment cabin cable 4 is connected to the test equipment host 2 and the test equipment probe 3; the test equipment host 2 is located in the integrated cabin container. , a radiation protection structure 7 is arra...

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Abstract

The invention relates to an in-situ and semi-in-situ test shielding device for a space comprehensive environment and a test shielding method thereof. The invention relates to the technical field of space environment simulation and testing, the device comprises a testing device, a driving mechanism and a remote control system, the testing device is carried on the driving mechanism, and the remote control system controls the driving mechanism; the test equipment comprises a test equipment host, a test equipment probe and a test equipment cabin-penetrating cable, and the test equipment cabin-penetrating cable is connected with the test equipment host and the test equipment probe; the test equipment host is located in the comprehensive cabin container, and a radiation protection structure is arranged on the periphery of the test equipment host; in-situ and semi-in-situ tests can be carried out on a sample in a test according to space extreme environment factors such as vacuum, high and low temperature, solar radiation, ultraviolet radiation and charged particle radiation which are simulated on the ground.

Description

technical field [0001] The invention relates to the technical field of space environment simulation and testing, and relates to a space comprehensive environment in-situ and semi-in-situ testing shielding device and a testing shielding method. Background technique [0002] In order to timely and accurately grasp the evolution law of materials, devices and system components in extreme comprehensive environments such as vacuum, high and low temperature, irradiation (sun, ultraviolet, charged particles, etc.) position) and variable position, unchanged environmental state (semi-in-situ) for test analysis. Moreover, the current tests for this aspect are mainly still in the laboratory state, and the instruments and equipment work in a conventional environment, which cannot meet the in-situ / semi-in-situ testing requirements. SUMMARY OF THE INVENTION [0003] The invention is oriented to the extreme environment factors in space such as vacuum, high and low temperature, solar irra...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N17/00G01D21/02
CPCG01N17/00G01N17/004G01D21/02
Inventor 闫继宏陈化智唐术锋吕良星琚丹丹李云龙
Owner HARBIN INST OF TECH
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