Aircraft engine insertion mounting device and mounting method

An aircraft engine and installation device technology, which is applied in aircraft assembly, electric vehicles, transportation and packaging, etc., can solve the problems of difficult engine installation, complex structure, and small installation space.

Active Publication Date: 2019-12-20
XIAN AIRCRAFT IND GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For the general situation that there is no guiding mechanism in the engine compartment, due to the characteristics of large volume, heavy weight, complex structure, various complex pipelines on the surface, and small installation space, it is diffi

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  • Aircraft engine insertion mounting device and mounting method
  • Aircraft engine insertion mounting device and mounting method
  • Aircraft engine insertion mounting device and mounting method

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Embodiment Construction

[0023] see figure 1 , 2 , 3, and 4, an aircraft engine plug-in installation device, including an AGV transport vehicle 1, a scissor fork lifting mechanism 2, an engine adjustment mechanism 3, an engine placement frame 5, a working platform 4, a laser positioning lamp 6, and an AGV transport vehicle 1 is located at the bottom of the aircraft engine plug-in installation device, and drives the entire device to move to the designated position. The working platform 4 is placed on the platform of the AGV transport vehicle 1, and the engine placement frame 5 is installed on the AGV transport vehicle 1 and is located in the middle of the working platform 4 , supporting the engine 8; the scissor-fork lifting mechanism 2 is installed on both sides of the AGV transport vehicle 1, the engine adjustment mechanism 3 is installed on the scissor-fork lifting mechanism 2, and can move up and down driven by the scissor-fork lifting mechanism 2; the laser positioning lamp 6 Installed on the rea...

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Abstract

The invention discloses an aircraft engine insertion mounting device and an aircraft engine insertion mounting method. The aircraft engine insertion mounting device comprises an AGV (automatic guidedvehicle) transport vehicle, a scissor fork lifting mechanism, an engine adjustment mechanism, an engine placing frame, a work platform and a laser positioning lamp, wherein the AGV transport vehicle drives the whole mounting device to move to a designated position, the work platform is placed on a table board of the AGV transport vehicle, the engine placing frame bears an engine, the engine adjustment mechanism is mounted on the scissor fork lifting mechanism, and can move up and down under drive of the scissor fork lifting mechanism, the laser positioning lamp is mounted at the rear end of the engine adjustment mechanism, the direction of laser beams sent by the laser positioning lamp guides the movement locus of the engine, and the engine adjustment mechanism hoists the engine, performsaccurate adjustment for the spatial position of the engine, and sends the engine to a mounting position in an engine mounting cabin.

Description

technical field [0001] The present application relates to the technical field of aircraft engine installation, in particular to an aircraft engine plug-in installation device and installation method. Background technique [0002] The installation of the aircraft engine is the last link of the aircraft assembly, and its installation quality will directly affect the dynamic performance of the entire aircraft, so the installation of the aircraft engine occupies a more important position in the aircraft assembly. At present, the common installation methods of aircraft engines mainly include three installation methods: hoisting installation, bracket installation and plug-in installation. The hoisting installation method is to use a large crane to hoist the aircraft engine to the installation position, and then connect and fix the aircraft and the engine. This method is suitable for the case where the aircraft engine has a large installation space or the aircraft engine compartmen...

Claims

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Application Information

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IPC IPC(8): B64F5/10
CPCB64F5/10Y02T90/14
Inventor 郭峰王新峰赵远鹏闫喜强
Owner XIAN AIRCRAFT IND GROUP
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