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Mounting method of aircraft conduit bracket

A conduit bracket and aircraft technology, applied in the field of aviation assembly, can solve problems such as low installation efficiency, high labor intensity, and uncoordinated assembly

Inactive Publication Date: 2021-08-31
SHAANXI AIRCRAFT CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] In order to solve the above-mentioned problems, the present invention provides an installation method of an aircraft duct bracket, which alleviates that the installation of the existing duct bracket is carried out under the premise of precise installation of the ceiling frame, resulting in low installation efficiency, high labor intensity, and easy installation. There are problems such as inconsistency in assembly

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  • Mounting method of aircraft conduit bracket
  • Mounting method of aircraft conduit bracket

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Embodiment Construction

[0028] This part is the embodiment of the present invention, which is used to explain and illustrate the technical solution of the present invention.

[0029] figure 1 The schematic flow chart of the installation method of the aircraft duct support provided by the present invention, as figure 1 shown, including:

[0030] Step 1, install the aircraft roof skeleton on the aircraft middle part and the aircraft tail part respectively;

[0031] Step 2. Set tooling plates at the joints of the middle part of the aircraft and the tail part of the aircraft respectively. The tooling plate is parallel to the plane where the docking holes of the middle part of the aircraft and the tail part of the aircraft are located. The mounting holes for the laser pointer are arranged on the tooling plate ;

[0032] Step 3. Insert the laser transmitter into the mounting hole on the tooling plate, turn on the laser transmitter, and the laser light emitted by the laser transmitter is perpendicular to...

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Abstract

The invention discloses a mounting method of an airplane conduit bracket. The mounting method comprises the following steps: respectively mounting an airplane ceiling framework on an airplane middle section part and an airplane tail section part; arranging tool flat plates at the butt joint positions of the aircraft middle section component and the aircraft tail section component respectively, the tool flat plates being parallel to the plane where butt joint holes of the aircraft middle section component and the aircraft tail section component are located, and forming mounting holes of laser pens in the tool flat plates; inserting a laser emitter into the mounting hole in the tool flat plate, the laser emitter being turned on, and laser rays emitted by the laser emitter being perpendicular to the tool flat plate; installing guide pipe supports on ceiling frameworks of the aircraft middle section component and the aircraft tail section component according to laser rays emitted by the laser emitters, and the guide pipe supports being used for supporting guide pipes penetrating through the aircraft middle section component and the aircraft tail section component. And the conduit bracket can be quickly, simply, conveniently and accurately mounted.

Description

technical field [0001] The invention belongs to the technical field of aviation assembly, and relates to an installation method of an aircraft conduit bracket. Background technique [0002] In the process of aircraft development, users put forward more stringent requirements on the appearance and manufacturing quality of the aircraft, and at the same time realize the precise positioning and stress-free assembly of the duct. The conduits are mounted according to their brackets. Conduit installation decisions depend on the mounting accuracy of the bracket. [0003] There are two main installation methods for traditional aircraft duct brackets: [0004] 1) After the installation of the ceiling skeleton is completed, according to the design drawings, the workers shall draw the pipe brackets according to the size and draw lines based on the skeleton profiles and frame edges; [0005] 2) After the installation of the ceiling skeleton is completed, the process is based on the de...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/10
CPCB64F5/10
Inventor 叶阳杨毅范斌广伟刘卫东杨强韩波
Owner SHAANXI AIRCRAFT CORPORATION
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