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Method and equipment for removing skin margin of large aircraft parts

A technology for process equipment and large parts is applied in the field of removing the skin allowance of large parts of aircraft, which can solve the problems of long cutting time, scrapped skin, and low end face cutting quality, etc., and achieve the effect of simple operation and stable cutting quality.

Active Publication Date: 2018-08-24
SHAANXI AIRCRAFT CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Assembling parts without allowance puts forward more stringent requirements on tooling, it is difficult to achieve the expected process assembly effect, often resulting in scrapped skins; when manual cutting is used, due to the limitation of the space on the frame, the construction of the operator is very difficult Large size, low cutting quality of the end face, too long cutting time, prolonging the assembly cycle of parts

Method used

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  • Method and equipment for removing skin margin of large aircraft parts
  • Method and equipment for removing skin margin of large aircraft parts
  • Method and equipment for removing skin margin of large aircraft parts

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Embodiment Construction

[0024] The specific embodiments of the present invention will be further described below in conjunction with the accompanying drawings.

[0025] See Figure 1~4 , a process equipment for removing the skin margin of large aircraft parts. After the upper frame 1 and the lower frame 2 are spliced, an annular flat plate 3 is installed in the front. 7's installation datum. The ring-shaped guide rail 4 is positioned and connected with the corresponding holes on the plate 3 through the positioning holes and bolt holes that have been processed in the manufacturing process; the ring-shaped support assembly 5 is connected to the plate 3 with bolts through the support 7 backwards, and the support assembly 5 is screwed forward with the skin clamping assembly 8, and the skin clamping assembly 8 clamps the skin from the outer periphery; 11 sets of evenly distributed tension joint locators 6 The rear end is screwed with the flat plate 3, and the tension joint locators 6. The front end is s...

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Abstract

The invention belongs to the field of aviation, and relates to a method and technological device for removing skin allowance of a big component of an airplane. The method for removing the skin allowance of the big component of the airplane comprises the steps that firstly, all assemblies constituting the big component of the airplane are positioned, clamped and connected on an assembling tool; secondly, a redundant portion of the component is clamped through a skin clamping assembly 8 on a flat plate assembly; thirdly, special cutting equipment is mounted on a flat plate assembly guide rail 4 through four clamping wheels 91; fourthly, the special cutting equipment 9 is corrected through a tool setting block 10; and fifthly, an air source control valve and a tool rotation control valve of the special cutting equipment 9 are opened in sequence, then the cutting depth of a cutting tool is adjusted to be 8-10 mm through a manual adjustment handle, and finally a cutting device crawling control valve is opened, so that the special cutting equipment 9 is made to clockwise cut the skin allowance of the component on the guide rail 4. By the adoption of the method and technological device for removing the skin allowance of the big component of the airplane, the labor intensity of workers can be relieved, and the working efficiency and the working quality can be improved.

Description

technical field [0001] The invention relates to a method and technological equipment for removing the skin margin of large aircraft parts. Background technique [0002] The butt joints of large aircraft parts have high quality requirements. To achieve this purpose, the end face margins need to be accurately removed after the assembly of large parts is completed. Due to the high precision of the removal, the difficulty of removing the margin increases, and at the same time, the assembly cycle of the aircraft is seriously affected. [0003] At present, two methods are generally used in the industry to ensure the quality of the butt joint. The first type: remove the skin of the small parts before the large parts are assembled, that is, the large parts are assembled without margin; the second type: after the parts are assembled, use the scriber on the assembly tool to mark the product on the end surface of the part The edge line is then cut off manually. Both methods have the...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23D79/00
Inventor 王铁练尹富成卢文权左铁强郭相如张睿
Owner SHAANXI AIRCRAFT CORPORATION