Spaceflight connector pit pulling device

A technology for extracting devices and connectors, which is applied in the direction of connecting/disconnecting the connecting devices, which can solve the problems of occupying space and difficulty in extracting, and achieve the effect of simple structure and limited space saving

CN103855593AInactive Publication Date: 2014-06-11CSSC SYST ENG RES INST +1
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Publication Date
2014-06-11
Estimated Expiration
Not applicable · inactive patent

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Abstract

The invention relates to a spaceflight connector pit pulling device. The spaceflight connector pit pulling device is a cylinder, wherein the cross section of the cylinder is in a C shape, a notch in the cylinder is a trunking groove, and the left end of the cylinder is provided with a boss which can be inserted into an open groove of a spaceflight plug. The spaceflight connector pit pulling device is simple in structure, and is used on the occasion where a spaceflight connector is pulled difficultly, and limited space of electronic equipment can be effectively saved.
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Description

technical field

[0001] The invention relates to a device for extracting a deep pit, which is especially suitable for use in occasions where aerospace connectors are difficult to extract from the deep pit. Background technique

[0002] Aerospace connectors are widely used in electronic equipment such as aerospace, navy, and army. Generally, aerospace connectors have long tails to seal and protect cables, which will take up limited space. Aerospace connectors are placed in electronic cases and cabinets. It will be difficult to extract in the deep pit. Contents of the invention

[0003] In order to overcome the disadvantages of the prior art, the present invention provides a device for extracting a deep pit of an aerospace connector, which has a simple structure, is sturdy and durable, and is easy to use, saving the limited space of electronic equipment.

[0004] The technical solution adopted by the present invention to solve the problems of the prior art is: it is a cylind...

Examples

Embodiment Construction

[0009] Such as figure 1 , 2 As shown, the present invention is a cylinder 1, the cross section of the cylinder 1 is "C" shape, the gap on it is the wire groove 2, the left end of the cylinder 1 has a boss 3, and the boss 3 can be inserted into an aerospace plug slotting.

[0010] There is a boss 3 at the right end of the cylinder 1 .

[0011] Bosses 3 are arranged at the left and right ends of the cylinder 1 .

[0012] The cross section of the boss 3 is square.

[0013] The cylinder 1 is a steel cylinder.

[0014] When inserting and pulling out the aerospace plug, the cable comes out from the wire slot 2, the boss 3 is aligned with the slot of the aerospace plug, and the plug can be inserted or pulled out by rotating the cylinder.