Rapidly-assembled aircraft undercarriage assembly

A landing gear and aircraft technology, applied in the chassis and other directions, can solve the problems of cumbersome assembly process, inconvenient disassembly, etc., and achieve the effect of simple operation, fast installation, and realization of assembly connection

Pending Publication Date: 2017-12-01
深圳市科卫泰实业发展有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

With the rapid development of aircraft, it is widely used in civil and scientific research fields, and for the convenience of transportation, usually the fuselage and landing gear of the aircraft are separated

Method used

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  • Rapidly-assembled aircraft undercarriage assembly
  • Rapidly-assembled aircraft undercarriage assembly
  • Rapidly-assembled aircraft undercarriage assembly

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Embodiment Construction

[0024] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0025] In view of the cumbersome installation process and inconvenient disassembly of existing aircraft and landing gear, the purpose of the present invention is to provide an aircraft landing gear assembly that is easy to assemble and disassemble.

[0026] see figure 1 as shown, figure 1 It is a three-dimensional structural schematic diagram of the rapid assembly landing gear assembly of the present invention. The quick assembly landing gear assembly provided by the present invention is used to connect the landing gear 10 and the fuselage of the aircraft, which mainly includes the landing gear 1...

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Abstract

The invention provides a rapidly-assembled aircraft undercarriage assembly for connecting an undercarriage and an aircraft fuselage. The rapidly-assembled aircraft undercarriage assembly comprises the undercarriage and an aircraft connecting end mounted on an aircraft. The undercarriage comprises an undercarriage supporting end and an undercarriage connecting end, and the aircraft connecting end is connected with the undercarriage connecting end. A T-shaped fixing block arranged at the undercarriage connecting end is assembled in a T-shaped fixing groove of the aircraft connecting end, and when the T-shaped fixing block and the T-shaped fixing groove are completely assembled, a buckle body on an elastic buckle is inserted into an anti-falling groove in the T-shaped fixing groove in a corresponding mode so as to achieve rapid assembly of the undercarriage connecting end and the aircraft connection end. Compared with the prior art, quick assembling connection of an undercarriage movable end and an undercarriage fixed end can be achieved, and the advantages of quick mounting, easy operation and the like are achieved.

Description

technical field [0001] The invention belongs to connecting pieces, and in particular relates to a quick assembly component, which is mainly used to realize the quick connection between landing gear and aircraft fuselage. Background technique [0002] The landing gear is a device used to support the weight of the aircraft and bear the corresponding load when the aircraft is parked on the ground, taxiing, taking off and landing. The process of the aircraft taking off from the ground has a landing or recovery stage. With the rapid development of aircraft, it is widely used in civil and scientific research fields, and for the convenience of transportation, usually the fuselage and landing gear of the aircraft are separated, and the landing gear needs to be installed when in use, but most of the current Both the aircraft and the landing gear are fixed by screws. The assembly process is cumbersome and inconvenient to disassemble. Contents of the invention [0003] For this rea...

Claims

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Application Information

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IPC IPC(8): B64C25/02B64C25/06
CPCB64C25/02B64C25/06
Inventor 李明涛
Owner 深圳市科卫泰实业发展有限公司
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