Undercarriage faulty airplane safe landing gear

A technology for safe landing and landing gear, applied in the direction of stopping devices, etc., can solve the problems of inconvenient popularization and application and high runway cost, and achieve the effect of improving safety and reliability, buffering impact force and friction force, and ensuring stability.

Inactive Publication Date: 2014-08-06
马新攀
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

With such a structure, when the aircraft that fails in flight achieves a soft landing, it can avoid violent collision with the ground when the aircraft lands, or cause casualties due to friction with the ground and cause fire and explosion, but the cost of laying the runway is relatively high, which is not convenient Promote application

Method used

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  • Undercarriage faulty airplane safe landing gear
  • Undercarriage faulty airplane safe landing gear
  • Undercarriage faulty airplane safe landing gear

Examples

Experimental program
Comparison scheme
Effect test

Embodiment approach 1

[0023] Such as figure 1 , image 3 , Figure 4 Shown: a safety landing device for an aircraft with a landing gear failure, including a landing plate 1 provided with a traction mechanism 9 and a sliding mechanism arranged under the landing plate 1, the sliding mechanism can adopt a universal wheel 4 with a shock absorber, The upper part of the landing plate 1 is provided with an elastic steel plate 5 with an “M”-shaped cross section, a flexible energy-dissipating layer 2 is arranged on the elastic steel plate 5, and a compensation airbag 3 is arranged in the cavity between the landing plate 1 and the elastic steel plate 5 , an automatic position correction device for the aircraft is set at the depression in the middle of the elastic steel plate 5 .

Embodiment approach 2

[0025] Such as figure 2 , image 3 Shown: a safety landing device for an aircraft with a landing gear failure, including a landing plate 1 provided with a traction mechanism 9 and a sliding mechanism arranged under the landing plate 1, the sliding mechanism can adopt a universal wheel 4 with a shock absorber, The upper part of the landing plate 1 is provided with an “M”-shaped elastic steel plate 5 in cross section, the landing plate 1 and the “M”-shaped elastic steel plate 5 are integrated, and a flexible energy-dissipating layer 2 is arranged on the elastic steel plate 5, A compensation airbag 3 is provided in the cavity between the landing plate 1 and the elastic steel plate 5 , and an automatic aircraft position correction device is installed in the depression in the middle of the elastic steel plate 5 . A distance fine-tuning mechanism is set between the landing plate 1 and the sliding mechanism. After a certain rear landing gear has a problem, the fine-tuning mechanism...

Embodiment approach 3

[0027] Such as figure 2 , image 3Shown: a safety landing device for an aircraft with a landing gear failure, including a landing plate 1 provided with a traction mechanism 9 and a sliding mechanism arranged under the landing plate 1, the sliding mechanism can adopt a universal wheel 4 with a shock absorber, The upper part of the landing plate 1 is provided with an “M”-shaped elastic steel plate 5 in cross section, the landing plate 1 and the “M”-shaped elastic steel plate 5 are integrated, and a flexible energy-dissipating layer 2 is arranged on the elastic steel plate 5, A compensation airbag 3 is provided in the cavity between the landing plate 1 and the elastic steel plate 5 , and an automatic aircraft position correction device is installed in the depression in the middle of the elastic steel plate 5 . A distance fine-tuning mechanism is set between the landing plate 1 and the sliding mechanism. After a certain rear landing gear has a problem, the fine-tuning mechanism ...

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PUM

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Abstract

The invention discloses an undercarriage faulty airplane safe landing gear. The undercarriage faulty airplane safe landing gear comprises a landing plate provided with a traction mechanism and a sliding mechanism arranged below the landing plate. An elastic steel sheet with the M-shaped cross section is arranged on the upper portion of the landing plate. A flexible energy relief layer is arranged on the elastic steel sheet. A compensation air bag is arranged in a cavity between the landing plate and the elastic steel sheet. An airplane position automatic correction device is arranged in a concave position in the middle of the elastic steel sheet. The undercarriage faulty airplane safe landing gear has the advantages of being high in anti-seismic buffering capacity, capable of accurately and conveniently conducting positioning, flexible and adjustable in airplane landing position, low in cost, and capable of being popularized and applied conveniently.

Description

technical field [0001] The invention belongs to the technical field of air transport facilities, and in particular relates to a safe landing device for an aircraft with landing gear failure. Background technique [0002] Since the invention of airplanes, airplanes have increasingly become an indispensable means of transportation for modern civilization, which has profoundly changed and influenced people's lives. Since the invention of airplanes, the time for human beings to travel around the world has been greatly shortened. The intricate air routes have connected countries all over the world, providing people with convenient and rapid passenger transportation. Airplanes closely connect people of different races and colors in different regions. Through continuous communication, people sow friendship, convey information, achieve mutual communication, mutual understanding and mutual promotion, and jointly promote human civilization. But, when aircraft provides convenience for...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/02
Inventor 马新攀
Owner 马新攀
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