A semi-automatic strapping device

A semi-automatic, equipment-based technology, applied in the direction of electrical components, manufacturing wiring harnesses, circuits, etc., can solve the problems of uneven quality, low efficiency, and high labor intensity of binding, and achieve the effects of ensuring binding quality, improving efficiency, and saving labor.

Active Publication Date: 2018-01-12
CHANGCHUN UNIV OF SCI & TECH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a semi-automatic binding equipment, which can solve the problems of low efficiency, high labor intensity and uneven binding quality caused by the current domestic aircraft main engine factory using manual methods to make cables; Promoting the digital design and manufacturing transformation of aircraft cables and providing the equipment foundation are of great significance for promoting the upgrading of cable manufacturing technology in aviation manufacturing enterprises

Method used

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  • A semi-automatic strapping device
  • A semi-automatic strapping device
  • A semi-automatic strapping device

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Embodiment Construction

[0021] Embodiments of the present invention will be further described below in conjunction with the accompanying drawings.

[0022] like figure 1 As shown, the present invention provides a semi-automatic strapping device, which is mainly composed of a gear opening and closing pliers 101 , an openable gear 102 , a linear motor 103 and a servo motor 104 . The linear motor 103 is fixed on the base, the servo motor 104 is fixed on the gear opening and closing pliers 101, and the openable gear is connected on the gear opening and closing pliers 101.

[0023] like figure 2 , image 3 As shown, the gear opening and closing pliers 101 is composed of upper opening pliers 201, lower opening pliers 202, upper clamping plate I2031, upper clamping plate II2041, lower clamping plate I2032, lower clamping plate II2042, driven gear I205, pulley I206 , driving gear 207, driven gear II 208, driven gear III 209, pulley II 210, pulley III211, pulley IV 212. The upper opening pliers 201 and t...

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Abstract

The invention disclose semi-automatic bundling equipment for solving the problems of low efficiency, high labor intensity, and uneven bundling quality caused by manual cable bundling in an airplane main engine plant. The semi-automatic bundling equipment comprises a pair of gear opening-closing pliers, an openable gear, a linear motor and a servo motor, wherein the gear opening-closing pliers comprise an upper opening plier and a lower opening plier which are connected by pins; the upper opening plier is provided with a driving gear and a driven gear while the lower opening plier is provided with two driven gears; the servo motor is fixed on the upper opening plier and connected with the driving gear; the openable gear comprises an upper opening gear and a lower opening gear, one ends of which are hinged; the upper opening gear and the lower opening gear are mounted on the upper opening plier and the lower opening plier of the gear opening-closing pliers through tightening plates respectively, and meshed with the gears on the opening pliers; sliding ways are formed in the upper opening gear and the lower opening gear; the sliding ways are glidingly matched with pulleys on the upper opening plier and the lower opening plier respectively; the upper opening gear is also provided with a damping adjustment wheel; and the linear motor comprises a winding ring and a bayonet.

Description

technical field [0001] The invention relates to a wire harness bundling device, in particular to a semi-automatic bundling device used for bundling aircraft cable wire bundles, and belongs to the field of production technology and equipment of parts directly subordinate to aircraft general assembly. Background technique [0002] The aircraft cable is the central nervous system of the aircraft, which connects all aircraft control systems and avionics communication systems of the aircraft, transmits power sources for various functional components of the aircraft, and transmits the central control data of the aircraft to the control subsystems of the aircraft. With the continuous enrichment and improvement of aircraft functions, the electrical system of the aircraft has become more and more complex, resulting in a sharp increase in the number of cables on the aircraft. At present, the cables of the aircraft range from dozens to tens of thousands. At the same time, since each ca...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H01B13/012
CPCH01B13/01272
Inventor 曹国华陈雪梅孟宪宇乔晓利吕琼莹姜涛贾冰
Owner CHANGCHUN UNIV OF SCI & TECH
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