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Synchronously following type aircraft forced landing platform

A platform and aircraft technology, applied in the field of synchronous follow-up aircraft forced landing platform, can solve the problems of low success rate, forced landing failure, and the aircraft will be damaged or destroyed, and achieve the effect of increasing friction and ensuring safety.

Inactive Publication Date: 2014-01-08
滕世进
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the aircraft needs to make an emergency landing due to the failure of the landing gear, the only measure that can be taken is to use the resistance generated by the grounding of the aircraft belly and the ground friction to force the aircraft to slow down and stop. The forced landing failed due to the uncontrollable situation, and the aircraft was either damaged or destroyed

Method used

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  • Synchronously following type aircraft forced landing platform

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Embodiment Construction

[0009] Below in conjunction with accompanying drawing and embodiment the present invention is further described:

[0010] A buffering retardation layer (3) is installed on the forced landing platform base (4), and when the forced landing aircraft (1) landed on the forced landing platform (2), the buffering retardation layer (3) promptly buffered the impact on the forced landing aircraft when landing The impact force of the forced landing platform (2) avoids the damage caused by the deformation of the belly of the aircraft due to the impact force when the aircraft lands, and increases the friction between the forced landing aircraft (1) and the platform base (4) of the forced landing, avoiding the impact caused by the forced landing. When the platform (2) decelerates on the runway, the forced landing aircraft (1) slides forward relative to the forced landing platform (2) on the forced landing platform (2) due to inertia, thereby ensuring the safety of the entire forced landing p...

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Abstract

The invention relates to a synchronously following type aircraft forced landing platform, which is auxiliary equipment for forced landing due to the failure of an aircraft landing gear. The synchronously following type aircraft forced landing platform can move ahead on a runway at the speed which is equal to the horizontal instant speed of a forced landing aircraft which is about to land to synchronously follow the forced landing aircraft to move, so that the forced landing aircraft can land on the forced landing platform safely with zero impulse force in a horizontal direction. The forced landing platform can also carry the forced landing aircraft to reduce the speed by braking on the runway to consume the kinetic energy of the forced landing aircraft, so that the safe aircraft brake is realized; and a buffering retardant layer is arranged on the platform, so that the comprehensive impact force generated when the forced landing aircraft lands on the platform is buffered to prevent the aircraft belly from being damaged due to deformation, and the frictional force between the aircraft and the platform is increased to prevent the aircraft from generating sliding movement on the platform due to inertia when the aircraft is decelerated on the runway of the platform, and thus the safety of the integral forced landing process is ensured.

Description

[0001] Field [0002] The invention relates to an aircraft forced landing platform, in particular to a synchronous following type aircraft forced landing platform. technical background [0003] Existing airports have very advanced facilities for ensuring the normal take-off and landing of aircraft, but there is no special auxiliary equipment for the forced landing of aircraft due to aircraft landing gear failure. When the aircraft needs to make an emergency landing due to the failure of the landing gear, the only measure that can be taken is to use the resistance generated by the grounding of the aircraft belly and the ground friction to force the aircraft to slow down and stop. Uncontrollable, the forced landing failed, and the aircraft was either damaged or destroyed. Contents of the invention [0004] In order to overcome the above-mentioned defects, the present invention proposes a design of a synchronous follow-up aircraft forced landing platform, which assists the air...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F1/02
Inventor 苏青刘祥泽滕世进
Owner 滕世进
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