CN1483633A

CN1483633A - Injection and parachute linked self-escape apparatus capable of avoiding air disaster

Info

Publication number: CN1483633A
Application number: CNA02142389XA
Authority: CN
Inventors: 严忠武
Original assignee: Individual
Current assignee: Individual
Priority date: 2002-09-17
Filing date: 2002-09-17
Publication date: 2004-03-24

Abstract

The present invention relates to a parachute coupling self-saving equipment capable of avoiding air catastrophe. Said invention is implemented by utilizing a series of technical measures on the equipment, its parachute-opener is a key component, it can ensure that the parachute also can be opened in low altitute so as to make airplane implement sat soft landing.

Description

Can avoid the parachute linked self-escape apparatus of airplane crash

An airplane crash! Countless people's fresh and alive life has been forfeited in the again and again generation of airplane crash.The aircraft flame-out in flight, fighter plane is not bad, and the aviator can abandoning machine and parachute jumping; The passenger plane flame-out in flight, all occupants can only perish together with aircraft, and are can the survivor also rare.

The present invention---the self-saving equipment for airplane that can avoid airplane crash to take place is realized by installing a series of technical measures, makes aircraft realize safe soft landing aloft.

Fig. 1 is a major part structure of the present invention, and Fig. 1-1 is a towing rocket; Fig. 1-2 is a booster umbrella; Fig. 1-3 is main force's umbrellas.In addition, Fig. 6 is a parachute opening device, also is vitals.

Fig. 9 is a summary diagram of the present invention.

The present invention is achieved like this, and according to the size of airframe, default " the skylight window " that has plug hatch more than two at its back is as Fig. 2-1,2; Fig. 3 is the self-saving equipment for airplane scheme drawing that beneath window is ready.Fig. 3-1 is a storage umbrella tube; Fig. 3-2 is booster umbrellas; Fig. 3-3 is trailing cables; Fig. 3-4 is platforms; Fig. 3-5 is towing rockets; Fig. 3-6 is rocket cylinders.

Fig. 4 is a booster umbrella, and Fig. 4-1 is the umbrella body of handling through fireproof agent; Fig. 4-2 is parachute opening devices; Fig. 4-3 is umbrella ropes.

Fig. 5 is a parachute opening device work scheme drawing, and parachute opening device is a critical component, it can guarantee that umbrella also can in time open and design-calculated in the low latitude, when towing rocket is run away, lights a fire simultaneously at the mouse bullet of parachute opening device end, with umbrella to around draw back, to reach the purpose of parachute-opening; In main force's umbrella, also be provided with this device.

Fig. 6 is a parachute-opening mouth scheme drawing.Fig. 6-1 is the mouse bullet; Fig. 6-2 is lashings; Fig. 6-3 is Ignition Modules; Fig. 6-4 is rocket socket of parachute opening device.

The present invention is performed such work:

Fig. 7, when aero-engine was flame-out, the aviator pressed the Self-saving equipment for airplane button immediately, and the self-help apparatus hatchcover is opened, and towing rocket Fig. 7-1 igniting automatically penetrates, and extracts booster umbrella Fig. 7-3 simultaneously; Fig. 7-2 is the control cords that separate towing rocket and booster umbrella, and this rope is slightly shorter than the umbrella rope of booster umbrella bottom, and electromagnetic bolt is being controlled in its upper end, as shown in figure 10.

Fig. 8, towing rocket is with when booster umbrella Fig. 8-1 separates, and parachute opening device Fig. 8-2 works immediately, and the umbrella body is opened.When booster umbrella was opened, booster umbrella was extracted huge umbrella Fig. 8-3 of the main force thereupon.

Fig. 9-1,2 is huge main force umbrellas, and main force's umbrella is in time opened under the help of parachute opening device.Under the help of self-saving equipment for airplane, can make the aircraft that runs out of steam realize safe soft landing aloft.

The present invention is specially adapted to saving oneself of all kinds of fighter planes, passenger plane and flying instrument in the air.

Claims

Its principal right requires:

1, every group of self-saving equipment for airplane has a towing rocket, Fig. 1-1, and its effect is that booster umbrella is extracted;
2, every group of self-saving equipment for airplane has a booster umbrella, Fig. 1-2, and its effect is to utilize it to extract the huge umbrella of the main force;
3, every group of self-saving equipment for airplane has a huge main force umbrella, Fig. 1-3, its effect be with machine on similar parachute kit is collaborative that aircraft is pulled off a soft landing.
4, there are the parachute opening device an of cross-shaped symmetrical (or M shape symmetry), Fig. 6 in the booster umbrella of every group of self-saving equipment for airplane and main force umbrella umbrella body lower end.
5, every group of self-saving equipment for airplane has a rope control or automatically controlled separation bolt, Figure 10.