An aircraft crash emergency method

A technology of aircraft and air crashes, applied in the field of aircraft, can solve problems such as aircraft crashes and fatalities, inability to separate humans from machines, and adverse political influences

Inactive Publication Date: 2018-12-11
张延林
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Aiming at unforeseen natural disasters and man-made disasters that lead to air crashes, because the body is one body, it is impossible to separate the man-machine in a short time, causing major economic losses such as machine crashes and human deaths, as well as the defects of adverse political influence

Method used

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  • An aircraft crash emergency method

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Embodiment Construction

[0029] The following embodiments will further illustrate the present invention in conjunction with the accompanying drawings.

[0030] see figure 1 , the embodiment of the present invention includes the following steps:

[0031] One step: the aircraft is provided with a cabin 1, a front satellite parachute 2, a rear satellite parachute 3, an Osprey propeller 4, a front aluminum alloy telescopic spring tube 5 and a rear aluminum alloy telescopic spring tube 6; the cabin 1 is a buoyancy cabin, and the cabin 1 is located at the bottom of the aircraft cabin A; the front satellite parachute 2 is located at the top front of the aircraft cabin A, the rear satellite parachute 3 is located at the top rear of the aircraft cabin A, and the front satellite parachute 2 is provided with a front satellite parachute The parachute cabin roof 21 is provided with a rear satellite parachute cabin roof 31 on the top of the rear satellite parachute 3; the top of the Osprey propeller 4 is provided ...

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PUM

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Abstract

An aircraft crash emergency method relates to an aircraft. The aircraft is equipped with cabins, forward and aft satellite parachutes, osprey propellers, forward and rear telescopic spring tubes; thecabin is located at the bottom of the aircraft cabin; the front and rear satellite parachutes are arranged at the top of the aircraft cabin, and the top of the front and rear satellite parachute is provided with a front and rear satellite parachute cabin cover; The propeller is provided with a top cover of the engine room; The front and rear telescopic spring tubes are arranged on the front and rear sides of the aircraft cabin front tires; A left, right, upper and low groove is provided in that windshield of the aircraft; Place multiple filter plates in the spare luggage compartment; The bottom of the cabin is provided with I-shaped beams, the left and right sides of the I-shaped beams are respectively provided with tyres, the periphery of the cabin is covered by a frame, the frame is provided with lifting hydraulic rods, and the cabin is sealed; When the air crash occurs at an altitude of 3000m, the main fuel tank is discarded in turn, the backup landing fuel tank is activated, the satellite parachute and propeller are opened and the landing gear in the abdominal cabin of the aircraft is opened automatically.

Description

technical field [0001] The invention relates to an aircraft, in particular to an emergency method for an aircraft accident. Background technique [0002] The main causes of aircraft crashes are the inhalation of flying objects such as birds into the engine, terrorist attacks, human factors, and failures of aircraft circuit system equipment. [0003] When the existing aircraft air disaster took place, there were many related emergency measures. [0004] Chinese patent CN104648677A discloses an escape device for aircraft passengers. Unforeseen natural disasters and man-made disasters have led to air crashes. Due to the fact that the airframe is one body, it is impossible to separate the man-machine in a short time, resulting in major economic losses such as aircraft crashes and fatalities, as well as adverse political effects. In the invention, the engine room bottom plate is connected with a sealing rubber pad and a locking mechanism, and the safety chair in the engine room...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/54B64D45/06B64D17/80B64C1/14B64D25/00B64D25/18
CPCB64C1/1476B64C25/54B64D17/80B64D25/00B64D25/18B64D45/06
Inventor 张延林
Owner 张延林
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