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An aircraft wiring machine clamping device

A wiring machine, aircraft technology

Active Publication Date: 2021-08-06
山东同其数字技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, during the wiring process of the current aircraft wiring machine, because the wire ends cannot be fixed, it is easy to cause the cable to slide on the wiring machine, resulting in accidental rupture of the insulation layer, which is inconvenient to use and is not conducive to popularization.

Method used

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  • An aircraft wiring machine clamping device
  • An aircraft wiring machine clamping device
  • An aircraft wiring machine clamping device

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Embodiment Construction

[0033] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0034] see figure 1 , figure 2 , image 3 As shown, the present invention provides a technical solution: a wire clamping device for an aircraft wiring machine, characterized in that it includes a chuck 1;

[0035] The upper surface of the chuck 1 is provided with a chassis 7, and the front side of the upper surface of the chassis 7 is sequentially fixedly connected with a front left bracket 101 and a front right bracket 102; the rear side of the upper surfa...

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Abstract

The invention discloses a wire clamping device for an aircraft wiring machine, which comprises a chuck, the upper surface of the chuck is provided with a chassis, and the front side of the upper surface of the chassis is fixedly connected with a front left bracket and a front right bracket in sequence from left to right. The clamping device of the aircraft wiring machine can only rotate the right conveyor belt counterclockwise by setting the ratchet and the drive lever, so as to prevent the cable from falling off due to the reverse rotation of the conveyor belt during the cable holding process. By setting the left conveyor belt and the right conveyor belt The rotating connection between the cables can drive the cables into them when they enter the left conveyor belt and the right conveyor belt, so as to realize the function of cable clamping. Through the set pressure plate a and pressure plate b, when there are wires of different sizes When the cable enters the clamp, the pressure plate a and the pressure plate b will push the fit between the left conveyor belt and the right conveyor belt, so as to adapt to cables of different sizes.

Description

technical field [0001] The invention relates to the technical field of aerospace automation, in particular to a wire clamping device for an aircraft wiring machine. Background technique [0002] With the rapid development of the aviation industry, the number of aircraft manufactured is also increasing. In the assembly process of the aircraft, especially the arrangement of the cables, due to the material requirements of the aviation wires, the insulation layer of the cables must not be used during the arrangement process. Friction with external objects prevents accidental rupture of the insulation layer, so the aircraft wiring machine was born. [0003] However, during the wiring process of the current aircraft wiring machine, because the wire ends cannot be fixed, it is easy to cause the cable to slide on the wiring machine, resulting in accidental rupture of the insulation layer, which is inconvenient to use and is not conducive to popularization and use. Contents of the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B65H51/18
CPCB65H51/18
Inventor 宋宝焱王风友
Owner 山东同其数字技术有限公司