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Aircraft landing gear utilizing spring buckles

A technology of aircraft landing gear and spring clip is applied to aircraft landing gear, and the field of aircraft landing gear using spring clip can achieve the effects of slow contraction speed, increased stability and fast speed

Active Publication Date: 2018-09-14
桐乡乐维新材料有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the plane lands, there is generally an oil-air shock absorber to provide effective shock absorption, but they are generally affected by oil or gas and require regular maintenance. Therefore, we need a device that can replace the oil-air shock absorber

Method used

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  • Aircraft landing gear utilizing spring buckles
  • Aircraft landing gear utilizing spring buckles
  • Aircraft landing gear utilizing spring buckles

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0016] An aircraft landing gear utilizing a spring buckle is composed of a landing gear fixing device 1, a spring support rod I2, a landing gear support rod 3, a hydraulic rod I4, a landing gear moving device 5, a hydraulic rod II6 and a connecting rod with a rotating shaft 7, the landing gear fixing device 1 is composed of landing gear fixing plate 101, hydraulic rod III 102 and rotating shaft I 103, and the landing gear moving device 5 is composed of chassis 501, landing wheels 502, rotating shaft It consists of Ⅱ503, spring support rod Ⅱ504 and connecting shaft 505. It is characterized in that: spring support rod Ⅰ2 is installed on landing gear fixing device 1, hydraulic rod III102 is installed on landing gear fixing device 1, and one end of landing gear supporting rod 3 is fixed on The front end of the hydraulic rod III102, the middle point of the landing gear support rod 3 is fixed on the upper end of the spring support rod I2, the other end of the landing gear support rod...

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PUM

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Abstract

The invention discloses an aircraft landing gear utilizing spring buckles, and belongs to the field of aviation equipment. The aircraft landing gear consists of a landing gear fixing device, a springsupporting rod I, a landing gear supporting rod, a hydraulic rod I, landing gear moving devices, a hydraulic rod II and a rotating shaft with a rotating shaft connecting rod, wherein the spring supporting rod I is arranged on the landing gear fixing device; one end of the landing gear supporting rod is fixedly arranged on the front end of a hydraulic rod III, and the other end of the landing gearsupporting rod is fixedly arranged on the rotating shaft with the rotating shaft connecting rod; the rotating shaft with the rotating shaft connecting rod is fixedly arranged on the landing gear fixing device; one end of a rotating shaft II is fixedly arranged on the rotating shaft with the rotating shaft connecting rod, and the other end of the rotating shaft II is fixedly arranged on spring supporting rods II on the landing gear moving devices; one end of the hydraulic rod II is connected with the rotating shaft with the rotating shaft connecting rod, and the other end is fixedly arranged onthe landing gear supporting rod. The aircraft landing gear disclosed by the invention has the beneficial effects that the stretching and contracting speed of the hydraulic rods is controlled by utilizing the spring buckles, and the stability is enhanced.

Description

technical field [0001] The invention relates to an aircraft landing gear utilizing a spring buckle, in particular to an aircraft landing gear utilizing a spring buckle, and belongs to the field of aviation equipment. Background technique [0002] Landing gear is an accessory device used to support the aircraft and move on the ground (water surface) when the lower part of the aircraft is used for take-off and landing or ground (water surface) taxiing. The landing gear is the only part that supports the entire aircraft, so it is an integral part of the aircraft; without it, the aircraft cannot move on the ground. After the aircraft takes off, the landing gear can be retracted depending on the flight performance. Landing gear is an important load-bearing and manoeuvrable part of an aircraft, which plays an extremely important role in the safe take-off and landing of the aircraft. Landing gear is a necessary support system for aircraft takeoff, landing, taxiing, ground movemen...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/34B64C25/58B64C25/62
CPCB64C25/34B64C25/58B64C25/62B64C2025/345
Inventor 冯琴
Owner 桐乡乐维新材料有限公司
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