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Electric connector device easy to disassemble in orbit

A technology of electrical connectors and ratchets, which is applied to parts of connecting devices, devices for preventing wrong connections, connections, etc., can solve problems such as poor ergonomics evaluation, large volume of electric tools, complicated operation, etc., and achieve optimal results. Effects of on-orbit visibility and operational convenience, reduced functional requirements, and enhanced reliability

Active Publication Date: 2020-12-15
SHANGHAI AEROSPACE SYST ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] In terms of maintenance tools, most electrical connectors are disassembled by electric tools at present. There are problems such as large volume, heavy weight, complicated operation and difficult operation of electric tools, and the evaluation of ergonomics is not good.

Method used

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  • Electric connector device easy to disassemble in orbit
  • Electric connector device easy to disassemble in orbit
  • Electric connector device easy to disassemble in orbit

Examples

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Embodiment Construction

[0040] The following will combine Figure 1 to Figure 18 The electric connector device which is easy to be disassembled on rail of the present invention is further described in detail.

[0041] The preferred embodiment of the present invention takes the J599 electrical connector as an example to describe in detail the electrical connector device that is easy to be disassembled on rail in the present invention. The present invention is also applicable to other rotary electrical connectors.

[0042] figure 1 A schematic diagram of the J599 electrical connector plug is shown; figure 2 A schematic diagram of the J599 electrical connector receptacle is shown.

[0043] see figure 1 and figure 2, The J599 electrical connector includes a plug 1 and a socket 2, and the plug 1 and the socket 2 are threadedly connected. Specifically, the shell 1-1 of the plug 1 has an internal thread, the socket 2 has an external thread 2-1, and the number of thread engagement circles is 1, and t...

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PUM

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Abstract

The invention discloses an electric connector device easy to disassemble in an orbit. The electric connector device comprises an electric connector, wherein the electric connector comprises a plug anda socket, the socket is fixedly installed on the aircraft and serves as a non-on-orbit detachable part; the ratchet wheel and ratchet mechanism is used as a plug accessory to be integrated with the plug to be used as an on-track detachable part; and the ratchet mechanism swings back and forth around the shaft of the electric connector, so that the plug is screwed out of the socket. According to the electric connector device easy to disassemble on the orbit, the ratchet mechanism of the ratchet wheel and the plug of the electric connector are integrated, so that the one-way rotating action ofseparation and disassembly of the electric connector is converted into small-range reciprocating swing motion, an astronaut can conveniently operate by using a simple manual tool, and the requirementson a maintenance tool and the operation capability of the astronaut are reduced.

Description

technical field [0001] The invention relates to an electrical connector, in particular to an electrical connector device that is easy to be disassembled on rails. Background technique [0002] Maintainability, as one of the important ways to improve the working life of space mechanism, has been widely adopted in the design of space mechanism, that is, maintainability design. [0003] Large-scale space agencies are composed of many small-scale agencies, and quite a few of these small-scale agencies are single-point links. Whether this part of the agency can work normally will directly affect the life of the entire large-scale space agency. Therefore, in the design of the mechanism, fully consider the maintainability design, and adopt the on-orbit replaceable design for some components, that is, when a failure of a component is detected, the astronauts can replace it in the out-of-orbit cabin. [0004] In terms of functional design, limited by the current level of research an...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01R13/633H01R13/64
CPCH01R13/633H01R13/64
Inventor 杨德财李长江陈欢马超马志飞钱志源王治易
Owner SHANGHAI AEROSPACE SYST ENG INST
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