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Device for enabling wall plates of wings to be automatically assembled onto and disassembled from frame

A siding and wing technology, which is applied in the field of the device for automatic upper and lower racking of wing siding, can solve problems such as difficulty in removing and dismounting the wing siding.

Active Publication Date: 2013-12-11
AVIC BEIJING AERONAUTICAL MFG TECH RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide a device for automatic loading and unloading of wing panels, so as to solve the difficulty of loading and unloading wing panels during wing assembly and realize automatic wing assembly. The device can realize rapid positioning of wings, Automatic attitude adjustment, accurate fit and other wing panel assembly work

Method used

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  • Device for enabling wall plates of wings to be automatically assembled onto and disassembled from frame
  • Device for enabling wall plates of wings to be automatically assembled onto and disassembled from frame
  • Device for enabling wall plates of wings to be automatically assembled onto and disassembled from frame

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Embodiment Construction

[0024] 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.

[0025] figure 1 Shown is a three-dimensional structural schematic diagram of a device 1 for automatically loading and unloading wing panels according to a specific embodiment of the present invention. The device 1 can be used for loading and unloading wing panels 100 during aircraft assembly, and can realize the assembly process The center wing panel 100 is automatically installed on the airfoil profile 200 . As shown in the figure, the device 1 includes a ba...

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Abstract

The invention discloses a device for enabling wall plates of wings to be automatically assembled onto and disassembled from a frame. The device comprises a base, a door-frame-shaped turning guide rail hinged to the base, a horizontally-moving frame arranged between two frame guide rails of the turning guide rail, an telescopic guide rail arranged in the horizontally-moving frame, and a swing posture adjusting assembly arranged at the tail end of the telescopic guide rail, wherein the wall plates of the wings can be arranged on the swing posture adjusting assembly. According to the device for enabling the wall plates of the wings to be automatically assembled onto and disassembled from the frame, the problem of enabling the wall plates of the wings to be assembled onto and disassembled from the frame in the wing assembly process can be solved, the wing assembly automation is achieved, and the wing wall plate assembly operation such as rapid positioning of the wings, automatic adjustment of the postures of the wings and accurate attaching of the wings can be achieved.

Description

technical field [0001] The invention relates to a device for automatic mounting and unloading of wing panels. The device can be used for the upper and lower shelves of aircraft assembly wing panels, and can realize the automatic installation of wing panels on the airfoil frame during the assembly process. , can greatly improve assembly efficiency and assembly quality. Background technique [0002] When assembling the wing panel of an aircraft, first install the skeleton including the wing root, titanium alloy beam and aluminum alloy beam on the fixed frame, and then install the whole wall including the wing skin, wall and long truss The plate and the skeleton are fitted together, and the position of interference is calibrated. After separation, the calibrated interference position is trimmed, and the interference position is checked and calibrated again, and the separation is repaired...until all the interference positions are trimmed, and the overall The wallboard and the ...

Claims

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Application Information

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IPC IPC(8): B23P19/00
Inventor 张书生王健李红英周万勇
Owner AVIC BEIJING AERONAUTICAL MFG TECH RES INST
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