CN101468719A - Avigation passenger transport life saving method - Google Patents
Avigation passenger transport life saving method Download PDFInfo
- Publication number
- CN101468719A CN101468719A CNA2007103072514A CN200710307251A CN101468719A CN 101468719 A CN101468719 A CN 101468719A CN A2007103072514 A CNA2007103072514 A CN A2007103072514A CN 200710307251 A CN200710307251 A CN 200710307251A CN 101468719 A CN101468719 A CN 101468719A
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- China
- Prior art keywords
- survival capsule
- plane
- life saving
- avigation
- lifesaving
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Abstract
The invention provides a rescue solution for the crew of a plane. According to the solution, the plane is designed with two parts which are closely connected and can be manually separated, wherein the two parts are a rescue capsule and other parts of the plane. When the plane is in danger, a worker starts rescue and the rescue capsule is released. At the same time, a deceleration parachute arranged on the rescue capsule separates the rescue capsule from the body of the plane and decelerate the plane.
Description
Technical field
The present invention relates to a kind of method for preventing the passenger plane accident all occupants to be carried out lifesaving.
Background technology
The situation of its security fields of current air passenger traffic industry is that in case occur irresistible fault in the passenger traffic, persons on board are difficult to survive, though aircraft is equipped with parachute can for every occupant, reason has some, and the chutist will have certain fitness, also will be through training; Even if everybody does some training very often, narrow and small hatch door also can't allow so much people escape at short notice; And maximum problem is, when aircraft is all out of control, and the health who can also draw oneself up?
Summary of the invention
In order to overcome the difficult problem that the people is difficult to survive in the aircraft accident, the invention provides a kind of brand new air passenger traffic lifesaving scheme, this scheme can make everyone obtain lifesaving.
The scheme of a technical solution difficult problem of the present invention is, do not changing the aircraft outer shape, the change of inner structure under the situation that does not influence original control system of aircraft and flight quality in essence, is set up one and can be separated from airframe, carry the survival capsule of deceleration parachute.Its scope comprises the space between main cabin and main cabin and the driving compartment, and its subject is personnel on the aircraft, and its control system is independent of outside original flight control system, and the deceleration parachute that it carries plays deceleration effort to self.
When aircraft is out of control, start lifesaving by the aviator, personnel are retracted survival capsule by the passage that connects survival capsule by mechanical force together with its seat in the driving compartment, porthole sealing then; Then, the device of original leak-tight joint survival capsule and body discharges survival capsule rapidly, and the deceleration parachute that bury at the survival capsule top launches, and opens the pulling force of back generation survival capsule is separated from body, and make the survival capsule deceleration and keep balance.
The beneficial effect of this programme is, everyone is escaped together by survival capsule on the aircraft, and deceleration parachute is without the bigger heavy burden of bearing ratio survival capsule.
Description of drawings
Further specify with regard to specific embodiments of the present invention below in conjunction with accompanying drawing.
Fig. 1 is the aircraft lateral plan.
Fig. 2 is the survival capsule birds-eye view.
Dotted line is survival capsule and the separable joint portion of body among Fig. 1.As shown in Figure 1, the survival capsule rear design becomes an inclined-plane, the resistance when separating to reduce, and the contact surface design carriage and the cooling material of survival capsule and body prevent that friction from producing high temperature; Install shockproof facility simultaneously additional, alleviate the bump of landing and contingent airplane tail group normal limb; Consider ditching, survival capsule is designed to watertight type.
Point among Fig. 2 is the deceleration parachute that is imbedded under the survival capsule upper surface.
When the aviator started lifesaving, flight deck crew was retracted survival capsule by mechanical force from the passage that connects driving compartment and survival capsule by seat, porthole sealing then; Then, the survival capsule of leak-tight joint on body is released, and four jiaos of deceleration parachutes that bury of survival capsule eject, and survival capsule risen from body separate and deceleration effort.Several in addition auxiliary parachutes that are that bury a little are by staff's control in the survival capsule.
Claims (2)
1. air passenger traffic lifesaving scheme, all occupants are subject with aircraft, set up a survival capsule that carries deceleration parachute, it is characterized in that: life saving system is independent of outside other flight control system, can be separated from body by staff's control.
2. the lifesaving scheme according to right 1, deceleration parachute evenly buries under the survival capsule upper surface, ejects the back whole survival capsule is play a part to separate and slow down from body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2007103072514A CN101468719A (en) | 2007-12-29 | 2007-12-29 | Avigation passenger transport life saving method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2007103072514A CN101468719A (en) | 2007-12-29 | 2007-12-29 | Avigation passenger transport life saving method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101468719A true CN101468719A (en) | 2009-07-01 |
Family
ID=40826584
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2007103072514A Pending CN101468719A (en) | 2007-12-29 | 2007-12-29 | Avigation passenger transport life saving method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101468719A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102162369A (en) * | 2011-01-30 | 2011-08-24 | 三一重型装备有限公司 | Elevating rescue capsule used for mine accidents |
| CN106081126A (en) * | 2016-06-13 | 2016-11-09 | 王晨 | Bionical cellular active safety escape compartment embeds application and the design of aviation aircraft |
| CN110606185A (en) * | 2019-10-11 | 2019-12-24 | 王彪 | Safety airplane with combined structure |
-
2007
- 2007-12-29 CN CNA2007103072514A patent/CN101468719A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102162369A (en) * | 2011-01-30 | 2011-08-24 | 三一重型装备有限公司 | Elevating rescue capsule used for mine accidents |
| CN102162369B (en) * | 2011-01-30 | 2013-04-03 | 三一重型装备有限公司 | Elevating rescue capsule used for mine accidents |
| CN106081126A (en) * | 2016-06-13 | 2016-11-09 | 王晨 | Bionical cellular active safety escape compartment embeds application and the design of aviation aircraft |
| CN110606185A (en) * | 2019-10-11 | 2019-12-24 | 王彪 | Safety airplane with combined structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Open date: 20090701 |