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Safety landing aid and rescue system for aircraft landing gear failure

A technology of aircraft landing gear and aircraft, which is applied in the field of safety assistance and rescue systems, can solve problems such as difficulty in grasping direction, easy rollover of aircraft landing, and crash of aircraft, so as to achieve the effect of ensuring stability and safety

Active Publication Date: 2019-08-09
蓝宁
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, it is difficult to grasp the directionality of the faulty plane when it is forced to land and taxi, and it is difficult to control the landing attitude of the faulty plane when it is forced to land. , often causing huge property losses due to aircraft crashes

Method used

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  • Safety landing aid and rescue system for aircraft landing gear failure
  • Safety landing aid and rescue system for aircraft landing gear failure
  • Safety landing aid and rescue system for aircraft landing gear failure

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Embodiment Construction

[0026]The present invention will be further elaborated below in conjunction with accompanying drawing, wherein, the direction of the present invention is with figure 1 as standard.

[0027] like Figure 1 to Figure 5 As shown, a kind of safe landing assistance rescue system for aircraft landing gear failure of the present invention comprises aircraft landing assistance vehicle 1, forced landing platform system 2, lifting tray system 3, positioning system 4, power supply 5 and control system 6, and aircraft assistance system The landing vehicle 1 is used to place, carry and transport all the mechanisms, devices and systems of the rescue system of the present invention, and keep consistent with the speed and direction when the forced landing aircraft is about to land on the airport runway, so as to present the aircraft landing aid vehicle 1 and the forced landing vehicle 1. The synchronous following state of the aircraft; the forced landing platform system 2 is used to carry th...

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Abstract

The present invention disclosed a safety assistance system for the fault of the aircraft landing frame.The aircraft's forced landing platform system, the hydraulic tray for the lift of the gesture tube lift when the aircraft is adjusted when the aircraft landed, and the vehicle control system and the positioning system.And the real -time monitored fault aircraft flight status information information is fed back to the control system, the control system controls the power driving system, lifting tray system and forced landing platform system to control the faulty aircraft according to the fault aircraft flight status information informationIt effectively solves the difficulty of grasping the direction of the faulty aircraft when it is forced to drop and the body's posture is difficult to control when landing, resulting in the problem of rolling aircraft prone to rolling aircraft when landing.

Description

technical field [0001] The present invention relates to the technical field of emergency rescue of a malfunctioning aircraft, in particular to a safety landing assistance and rescue system for aircraft landing gear failure with a self-contained positioning system, height adjustable tray height, greater versatility and simple structure . Background technique [0002] At present, there are more than ten thousand times of aircraft flying in the sky every day in the world, and the accident rate of aircraft failure is one in a million. However, up to 90 percent of those one-in-a-million accidents are caused by aircraft landing gear failures. Because the structure of the aircraft landing gear is affected by the number of take-offs and landings, the fatigue of the steel, the hydraulic oil seal, the wheel hub and other factors, it is prone to failure. Especially in the harsh atmospheric environment, when the wheels are deformed or the landing gear system fails, the landing gear ca...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F1/02B60G17/015G05D1/12
CPCG05D1/12B60G17/015B60G2400/252B60G2600/21B60G2800/914B64F1/0297
Inventor 蓝宁
Owner 蓝宁
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