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Undercarriage mounting vehicle

A landing gear and installation vehicle technology, applied in lifting gear, hoisting device, aircraft assembly, etc., can solve problems such as unsatisfactory use requirements, hidden safety hazards, and high physical energy consumption, so as to reduce operational safety risks, improve safety, and alleviate The effect of labor intensity

Pending Publication Date: 2022-03-08
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The installation, maintenance and disassembly of the landing gear of the aircraft requires frequent handling and disassembly. The weight of a single landing gear is about 200kg. And there are certain security risks
At the same time, due to the special way of installing the landing gear, it needs to be installed on the belly of the aircraft, and the control position and attitude of the landing gear need to be flexibly changed to align with the installation holes. Therefore, general-purpose handling or lifting mechanical equipment cannot meet the use requirements.

Method used

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  • Undercarriage mounting vehicle

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Embodiment Construction

[0014] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific illustrations.

[0015] see figure 1 A landing gear installation vehicle, comprising a mecanum wheel traveling mechanism 1, a vehicle frame 2, a parallel four-bar linkage lifting mechanism 3, a connecting pin 4, a hydraulic pump 5, a lifting adjustment cylinder 6, a pitch adjustment cylinder 7, Tooling trolley hanging plate 8, tooling trolley 9, fine-tuning mechanism 10 and landing gear 11, wherein, the bottom of the vehicle frame 2 is provided with four sets of mecanum wheel running mechanism 1, and the use of mecanum wheels makes the vehicle have Omnidirectional movement function, that is: forward and backward movement, left and right movement and in-situ steering movement, the front end of the frame 2 is provided with a parallel four-bar linkage lifting mecha...

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PUM

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Abstract

According to the undercarriage installation vehicle, four Mecanum wheel walking mechanisms are arranged at the bottom of a vehicle frame, a parallel four-connecting-rod lifting mechanism is arranged at the front end of the vehicle frame, one end of a lifting adjusting oil cylinder is installed on the vehicle frame, and the other end of the lifting adjusting oil cylinder is installed on the parallel four-connecting-rod lifting mechanism; one end of the pitching adjusting oil cylinder is installed on the frame, and the other end of the pitching adjusting oil cylinder is installed on the parallel four-connecting-rod lifting mechanism. The hydraulic pump is installed on the frame and connected with the lifting adjusting oil cylinder and the pitching adjusting oil cylinder at the same time. The tool cart is connected with the parallel four-connecting-rod lifting mechanism through a tool cart hanging plate. The fine adjustment mechanism is installed on the tool cart, and the undercarriage is placed on the tool cart. By means of the method, the aircraft landing gear can be installed in a mechanical mode, the labor intensity of operators in the landing gear installation process is greatly relieved, meanwhile, the operation safety risk is reduced, and the landing gear installation efficiency and the safety of the whole process are improved.

Description

technical field [0001] The invention relates to the technical field of aircraft installation equipment, in particular to a landing gear installation vehicle. Background technique [0002] The installation, maintenance and disassembly of the landing gear of the aircraft requires frequent handling and disassembly. The weight of a single landing gear is about 200kg. And there are certain security risks. At the same time, due to the special installation method of the landing gear, it needs to be installed on the belly of the aircraft, and the control position and attitude of the landing gear need to be flexibly changed to align with the installation holes. Therefore, general-purpose handling or lifting mechanical equipment cannot meet the use requirements. Contents of the invention [0003] The technical problem solved by the present invention is to provide a landing gear installation vehicle to solve the above-mentioned problems in the background technology. [0004] The te...

Claims

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Application Information

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IPC IPC(8): B66F7/06B66F7/08B66F7/28B64F5/40B64F5/10
CPCB66F7/0641B66F7/08B66F7/0625B66F7/28B64F5/40B64F5/10
Inventor 罗炜陈林杰裴立明许倩张如玉吴文渊
Owner JIANGXI HONGDU AVIATION IND GRP
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