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Electrical separation device for aircraft

A technology for electrical separation and aircraft, applied in the aerospace field, can solve the problems of aircraft damage, difficulty in installation, and large size, and achieve the effects of protective structure, friendly structure, and novel separation methods

Active Publication Date: 2016-05-11
中国航天科工动力技术研究院 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of the above-mentioned problems in the prior art, the present invention provides an electrical separation device for aircraft launch, which solves the problems of the existing electrical separation device, such as large volume, difficulty in installation, and great damage to the aircraft, and realizes missiles, rockets and unmanned vehicles. Aircraft such as man-machines are electrically separated from ground equipment during launch

Method used

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Embodiment Construction

[0021] The present invention improves the separation method of the existing aircraft electrical appliances, that is, the separation method that converts the parallel sliding motion into a vertical motion when the electrical separation devices are separated, and the specific implementation method is as follows:

[0022] Such as image 3 As shown, the electrical separation device includes an electrical socket 2 , an electrical plug 3 , and a plug base 4 . The electrical socket 2 is fixed on the aircraft 1, the plug base 4 is installed on the aircraft launcher or launch tube, and the electrical plug 3 can be inserted into the plug base 4 and inserted into the electrical socket 2. Wherein, the electrical socket 2 includes 20 jacks.

[0023] Such as Figure 4 As shown, the electrical plug 3 is an "I"-shaped plug, including a plug board 7 and a ferrule 8. The plug board 7 is provided with a mating plane 5 and a mating slope 6, of which there are 20 ferrules 8 in total. The plug b...

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Abstract

The invention belongs to the field of aerospace technology research, in particular relates to an electrical separation device for an aircraft. The electrical separation device comprises a plug base, an electrical plug and an electrical socket, wherein the plug base is fixed on an aircraft launching rack or launching cylinder, the electrical socket is fixed on the aircraft, the electrical plug is arranged in the socket base and inserted into the electrical socket, and an electrical plug installation inclined surface is inserted into the electrical socket by a plug base inclined surface. The electrical separation device is novel in separation mode, the aircraft and the structure of the separation device are protected, the aerodynamic performance cannot be affected by the device part on the aircraft, and the structure is user friendly.

Description

technical field [0001] The invention belongs to the field of aerospace technology research, in particular to an electrical separation device for aircraft. Background technique [0002] When missiles, rockets and unmanned aerial vehicles are launched, they need to exchange information with the ground launch control device. Therefore, there is a set of electrical separation devices between the aircraft and the launch control device to realize information interaction and electrical separation functions and complete launch control tasks. . [0003] The existing electrical separation methods mainly include the following two types, such as figure 1 and figure 2 Shown: (1) longitudinal parallel separation method, that is, the separation direction of socket 2 and plug 3 is parallel to the course of aircraft 1, and the plug is fixed on the launching device 4; (2) oblique insertion separation method, separation of socket 2 and plug 3 The direction forms a certain angle with the he...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01R24/00H01R13/46H01R13/633
CPCH01R13/46H01R13/633H01R24/00
Inventor 李经玮李永盛罗占飞张娜张书会权维利魏雄波杨振华张钰安清华
Owner 中国航天科工动力技术研究院
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