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Flexible tool for assembling row-line chuck type wall board

A flexible tooling and suction cup technology, applied in the direction of manufacturing tools, workpiece clamping devices, etc., can solve the problems of lack of versatility, reduce the number of tooling, poor reconfiguration, etc., achieve strong flexibility and versatility, ensure safety, and high The effect of positioning accuracy

Inactive Publication Date: 2013-02-27
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide a flexible tooling for assembly of row and column suction cup wall panels to overcome the problems of poor reconfiguration, lack of versatility and low positioning accuracy of the current assembly tooling for aircraft panel components. The tooling is precisely adjusted through the motor control program The position of each vacuum suction cup in the space and the tooling suction cup can form different lattices, so as to realize a tooling system to complete the digital positioning and drilling and riveting assembly of various wall panel components, reduce the number of tooling, shorten the production preparation cycle, and improve positioning accuracy

Method used

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  • Flexible tool for assembling row-line chuck type wall board
  • Flexible tool for assembling row-line chuck type wall board
  • Flexible tool for assembling row-line chuck type wall board

Examples

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Embodiment Construction

[0034] The present invention is a flexible tool for assembling row and column suction cup type wall panels, such as figure 1 , 2 As shown, it mainly includes guide rail base 1, X-direction drive unit 2 and column shape adjustment assembly 3 units. The rail base 1 is fixedly connected to the ground, the column shape-adjusting assembly unit 3 is installed on the two X-direction linear guide rails 6 of the guide rail base 1, and can move along the X-direction linear guide rails 6, and the X-direction drive unit 2 is located in the column shape-adjusting assembly unit Between the bottom of 3 and the guide rail base 1, it is fixedly connected with the guide rail base 1, and is connected with the bottom of the column shape-adjusting assembly unit 3.

[0035] The guide rail base 1 is composed of a base 5, an X-direction linear guide rail 6, an X-direction ball screw fixing seat 7 and an X-direction movement limiting seat 8. X-direction linear guide rail 6, X-direction ball screw fi...

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Abstract

A flexible tool for assembling a row-line chuck type wall board comprises a guide rail base, an X-direction driving unit and an upright post shape-adjusting assembly unit, wherein the guide rail base is fixedly connected to the ground; the upright post shape-adjusting assembly unit is arranged on two X-direction linear guide rails of the guide rail base and can move along the X-direction linear guide rails; and the X-direction driving unit is positioned between the bottom of the upright post shape-adjusting assembly unit and the guide rail base, is fixedly connected with the guide rail base and is connected with the bottom of the upright post shape-adjusting assembly unit. According to the flexible tool disclosed by the invention, aircraft panel assemblies are adsorbed, clamped and digitally positioned by a dot matrix vacuum chuck and stability and reliability in clamping and positioning and high positioning precision are obtained; and the digitalized positioning and drilling and riveting assembly of different wall board assemblies can be realized by reconfiguration through the dot matrix chuck of the tool. The flexible tool has higher practical value and broad application prospect in the fields of mechanical engineering / aircraft assembly.

Description

Technical field: [0001] The invention relates to a flexible tooling for assembling row-column sucker-type wallboards, which belongs to the field of mechanical engineering / aircraft assembly. Background technique: [0002] Panel components are the main structural parts constituting the aerodynamic shape of the aircraft. They are numerous in number, complex in shape, and weak in rigidity. The assembly process mainly includes positioning, clamping, hole making, connection and so on. The assembly accuracy of the panel assembly directly affects the assembly quality of the subsequent fuselage, wing components and final assembly, and is the basis for ensuring the assembly accuracy of the aircraft. [0003] At present, the domestic aviation industry still adopts the traditional rigid tooling in the form of "one aircraft, one use" in the assembly of panel components, which has a low degree of modularization, poor reconfigurability, and lack of versatility. A set of assembly jigs has...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B25B11/00
Inventor 李东升翟雨农王亮罗红宇
Owner BEIHANG UNIV
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