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Quick on-orbit integration system for high-integration-level electronic control information unit

An information unit and highly integrated technology, which is applied in the field of aerospace technology on-orbit integration, can solve the problems of manipulator dependence and other problems, and achieve the effect of large amplification ratio, light weight and easy installation

Inactive Publication Date: 2021-04-02
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problem in the prior art that the on-orbit maintenance of the large insertion force quick connection system depends on the mechanical arm, the present invention provides a fast on-orbit integration system for electronic control information units with high integration

Method used

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  • Quick on-orbit integration system for high-integration-level electronic control information unit
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  • Quick on-orbit integration system for high-integration-level electronic control information unit

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Embodiment Construction

[0016]CombineFigure 1 to 4In the present embodiment, a high intensive electronically controlled information unit is quickly in the rail integration system, including an electronically controlled information unit 1, including an electronically controlled information unit body 1-1 and an electronically control information unit connector. 1-2; also includes guides 2, multi-directional rolling slider 3, and boost mechanism 4; the electronically control information unit 1 is attached to the flash plug 5 of the electronically controlled information unit to install the substrate 5 -1 connection to achieve electrical signal transmission;

[0017]The boost mechanism 4 includes a power mechanism fulfill 4-1, a power mechanism lever 4-2, a power mechanism interface 4-3, and a power mechanism fixture 4-4;

[0018]The two ends of the guide rail 2 are connected to the power mechanism fulcrum 4-1 and the electronically controlled information unit mounting substrate 5, and the multi-directional rolling s...

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Abstract

The invention discloses a quick on-orbit integration system for a high-integration-level electronic control information unit, relates to an on-orbit maintenance system in the aerospace field, and aimsto solve the problem about quick on-orbit integration of the multi-contact, high-integration-level and large-insertion-and-extraction-force electronic control information unit. The system comprises the electronic control information unit; the electronic control information unit comprises an electronic control information unit body and an electronic control information unit connector; the system further comprises a guide rail, a multidirectional rolling sliding block and a power assisting mechanism; and the electronic control information unit is connected with an electronic control informationunit mounting substrate through the electronic control information unit connector to realize electric signal transmission. A power-assisted operating mechanism capable of being driven in the two directions is designed, the large-scale electronic control information unit can be quickly mounted and dismounted with relatively-small operating force, and astronauts can conveniently and quickly complete mounting and dismounting through just one-hand operation. The system has good universality and on-orbit operability, and is suitable for popularization and use in the field of on-orbit integration and on-orbit maintenance of similar functional modules.

Description

Technical field[0001]The present invention relates to aerospace technology in the field of rail integration, and more particularly to a high integrated electronically controlled information unit.Background technique[0002]With the rapid development of aerospace technology, space activities are more frequent, and the number of spacecraft in railway is increasing, the structure and composition of spacecraft are increasing, and the performance and technical levels are also increasing. However, due to the impact of the emission cost and objective environment, the spacecraft is rarely maintained, maintained, and upgraded, and the space environment is complicated, and the spacecraft often appears in its task. The situation in failure is huge. Therefore, how to ensure that the spacecraft lasts, stable operation in the space environment, is one of the problems that are now in urgent need. Therefore, it is especially important to carry out rail maintenance on the spacecraft.[0003]At present, ...

Claims

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Application Information

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IPC IPC(8): B25J5/02B25J18/00
CPCB25J5/02B25J18/00
Inventor 袁野王严刘伟赵伟国董吉洪徐抒岩
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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