CN1754778A - Civil aviation passenger aeroplane emergency survival capsule - Google Patents
Civil aviation passenger aeroplane emergency survival capsule Download PDFInfo
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- CN1754778A CN1754778A CN 200410050516 CN200410050516A CN1754778A CN 1754778 A CN1754778 A CN 1754778A CN 200410050516 CN200410050516 CN 200410050516 CN 200410050516 A CN200410050516 A CN 200410050516A CN 1754778 A CN1754778 A CN 1754778A
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Abstract
This invention relates to social and aviation industry manufacture part ad provides one life saving device for emergency, which adds one organic component on current plane and spends less money without changing current plane gas distribution and power characteristics to fulfill device studying work. The emergency life saving cabin can fulfill aviation saving and can realize emergent play and landing. The design emphasis is put on earth environment with accident record with more than seventy percent on earth.
Description
Affiliated technical field
The present invention provides a kind of to aircraft industry circle, when unfortunate generation " airplane crash " accident. big, the medium-sized passenger of civil aviaton aircraft, a kind of " airplane crash " emergency survival cabin of enabling rapidly. it can make passenger and crew hightail dangerous situation, safety is survived, the loss of disaster is reduced to Min.. this emergency survival cabin technical scheme, can start the beginning of " airplane crash " lifesaving, make the i.e. quick safety again of modern air travel.
Background technology
Civil aviaton's passenger's aircraft is a kind of modern vehicle, the flying method that it is high-speed, changed people's trip way, shortened simultaneously the space-time distance between two places on the earth greatly, make each place, the world all become genuine " global village ", entered since this century, because the develop rapidly of science and technology, the passenger of civil aviaton aircraft just promptly flies De Genggao to " higher ", and " faster " speed is faster, the farther and large scale development of " farther " flying distance, maturation day by day along with flight control technology, people have proposed exacting requirements more to this aircraft of aircarrier aircraft, have expressed bigger hope.
Thing is many-sided, and people also have " airplane crash " accident to take place again and again enjoying modernization simultaneously easily constantly, and " Lockerbie airplane crash " " 9,11 aircraft impact World Trade Organization building incident " makes all tongues of world's thorax order, talks " flying " look and becomes, the personage that carries weight estimation; In several years from now on, along with the maximization of aircraft, the development of high speed, the occurrence frequency of airplane crash will rise significantly, even may reach weekly degree together.Will people not only ask? modern science and technology are so flourishing, why to this " airplane crash " accident that life-and-death matter, but have no idea to solve! Do " crux " of problem go out there actually?
The modern passenger of civil aviaton aircraft, general employing air-jet eddy-current Duct-Burning Turbofan is a power, flying speed is fast, can reach 0,75-1, (M claims Mach between the 5M, the aerial propagation speed of representative voice), in order to improve the speed of a ship or plane, reduce the flight resistance of aircraft, fuel saving consumes, the flying height of aircraft is generally all in 10000 to 20000 meters high-altitudes, and at this height, bar pressure has only 1/tens of surface air pressure, rarefaction of air, air themperature drops to below the negative 60C degree, environment so, and the people can't survive, so, closed cabin is all made in the seat cabin of modern aircarrier aircraft, keeps apart with the external world, artificially makes in sitting the cabin, manage to keep the pressure that needed by human body is wanted, various conditions such as oxygen and temperature.So,, do not open because of the passenger cabin door sealing in the high-altitude, be not possibly with conventional parachute jumping escape, this is a factor that can not be ignored.A tree name relevant department adds up in addition, the generation of aircraft " airplane crash " accident, about is to occur in ground more than 70%, the taking off of aircraft, in the landing, because the cabin is airtight, personnel can't break away from aircraft, in case alighting gear breaks down, engine off, fuel leakage, blast on fire will cause personnel's heavy casualties.
Summary of the invention
Comprehensively various " airplane crash " accident, " crux " of problem is when " airplane crash " accident of generation, personnel can't hightail aircraft, as long as find the reliable way that breaks away from aircraft, the rescue of " airplane crash " just becomes possibility, I am from modern space technology, gain enlightenment in the multistage booster space disengaging technology, in domestic application more " Boeing ", the short distance aircarrier aircraft is a source, invent, designed the lifesaving scheme in a kind of passenger of civil aviaton aircraft " airplane crash " emergency survival cabin.In conjunction with the imagination design drawing, specifically set forth this design plan now.
Description of drawings
Accompanying drawing 1; The passenger of civil aviaton aircraft " airplane crash " emergency survival cabin structure figure
Accompanying drawing 2; The emergency survival cabin scheme drawing of escaping in the air
Accompanying drawing 3; Ground, emergency survival cabin escape scheme drawing
Among the figure; Shock-absorption air bag (10) seat (11) radio beacon emitter and sea coloring agent (12) oxygen of the stable landing of Aircraft Main main cabin (1) wing (2) multiple spot blasting bolt (3) pack (4) main force's landing pack (5) rocket nozzle (6) sled shape slide plate (7) damping spring application cylinder (8) solid fuel retro-rocket or high pressure air cylinder (9) nitrogen, the airtight hatch door of nitrogen cylinder (13) emergency survival cabin body (14) rudder (15) tailplane (16) vertical tail (17) cabin door (18) hinge (19) (20) airbag filling device (21) steel wire twisted rope (22) column type airbag (23).
Emergency survival of the present invention cabin body (14) is actually one of aircraft sealing main cabin independently part, Account for 1/3rd of aircraft sealing main cabin. Be connected 1 with the Aircraft Main main cabin at ordinary times) closely connect airtight hatch door (20) The same construction in personnel channel and host and guest cabin one and surface pressure, the closed environment that the oxygen concentration temperature is suitable, In the emergency survival cabin, except the conventional facilities such as arrangement seat (11) cabin door (18), also need an in addition standby cover Pressure and air handling system, the oxygen of right quantity, nitrogen cylinder (13), airbag filling device (21) calculates Rocket firing and the Parachute Opening controller of machine control, radio beacon emitter and sea coloring agent (12) etc. Buoyant apparatus. Use in the time of in order to emergency survival, the main body load-bearing roof beam structure of emergency survival cabin and aircraft, quick-fried with multiple spot Fried bolt (3) connects suspension, and between covering, it is anti-that two pieces of solid fuels are housed under floor, emergency survival cabin and under the aircraft Push away rocket or high pressure air tube (9), rocket nozzle (6) is towards the aircraft direction of advance, and six damping springs are done Supporting two sled shape slide plates (7) with tube (8), remainder has filled up the shock-absorption air bag (10) that has been full of nitrogen, Two outsides, emergency survival cabin are equipped with column type airbag (23) tail to be filled and lower covering centre joint place settles some blasts Bolt (3) (is annotated; B point and line are settles the blasting bolt place) on the ceiling of emergency survival cabin and on the aircraft Between covering, install 4-6 compact stabilized landing pack (4), 4 large-scale main force landing packs (5). Among the figure its His part; Aircraft wing on the aircraft body (2) vertical tail (17) tailplane (16) rudder (15) The equipment such as hinge (19) steel wire twisted rope (22).
Concrete implementing method
The imagination of system works is such, when the passenger of civil aviaton aircraft aloft flies, as run into aircraft and cataphoretic failure occurs, as engine sudden parking, aircraft stall, flying height sharply descends, and can't trouble-shooting the time, the crew organizes the passenger to enter the emergency survival cabin, close airtight hatch door, the aviator starts aerial emergency survival program, connects survival capsule and body, the each point explosive bolt at tail and following covering centre joint place, detonate simultaneously, survival capsule and aircraft main body break away from, by gravity, and covering is opened around hinge under the aircraft, survival capsule leaves aircraft, stable parachute is opened immediately, keeps the survival capsule horizontality, does not roll, under the computer program control of main force's parachute radio altimeter in the parachute-opening controller, guarantee that main parachute opens automatically when the 7000-5000 rice of distance ground, meanwhile open the airbag filling device, for tying up the column type air bag inflated with nitrogen that is attached to both sides, emergency survival cabin; If survival capsule drops to the ocean, the inside, lake, this column type air bag and survival capsule bottom air bag, will play provides buoyancy and keeps survival capsule stable, the effect of not toppling, the radio beacon emitter is worked automatically in the landing process, for ground rescue provides geographic orientation, as drop in the water and can use sea coloring agent, illuminating lamp etc., for the aerospace plane search provides orientation, accompanying drawing two are its scheme drawings.
Be equipped with on the aircraft of abort escape system, should be before taking off or landing, with the concentrated emergency survival cabin that enters of passenger, close airtight hatch door, rising of aircraft, in falling if emergency, the aviator starts ground emergency survival program, makes to connect survival capsule and body, the explosive bolt at tail and following covering centre joint place, detonate simultaneously, survival capsule and body break away from, by gravity, and covering is opened around hinge under the aircraft, survival capsule leaves aircraft and drops to ground, at this moment survival capsule will continue to advance, in order to hightail aircraft owing to the powerful inertia that advances along with aircraft, computer program will be lighted two pieces of solid fuel retro-rockets or high pressure air tube, antagonistic force is promoting survival capsule and body breaks away from fast, and survival capsule and ground have more than two meters high, the shock-absorption air bag of nitrogen, the synergy of six damping spring application cylinders can alleviate the personal injury of inertia impact to the passenger.Accompanying drawing three is its scheme drawings.
Aircraft aloft, finish after the survival capsule disengaging, if aircraft still has under the situation of part power, can be covering under the aircraft of opening is closed again with twisted rope, keep the pneumatic substantially external form of aircraft, because aircraft has alleviated weight, can be with gliding and other measures, operating aircraft lands in an emergency, if must abandon machine, the aviator can in time start individual ejection-seat, breaks away from aircraft.
This Design of device thought is being followed following several departure point and is being carried out; 1, in the statistics of existing air crash, the probability that ground has an accident is more than 70%, and emphasis prevents ground accident, is the factor that preferentially will consider, this emergency survival cabin is placed on airplane tail group 1/3 place, consider emergency survival cabin when having an accident exactly, can hightail aircraft, and again away from flammable and explosive substances such as aircraft fuel fuel tanks, though some drawbacks of center of gravity of airplane out-of-position are arranged, the aviator can solve by the operate lifting rudder face, is a kind of technical scheme of the best, 2, adopting small-sized solid fuel rocket or high pressure air tube, is because it is in light weight, easy and simple to handle, dependable performance, match with sledge runner, the power that hightails aircraft is provided, promptly can on airstrip, slide race, also can on soil and lawn, slide, 3, use in the employing aircraft in the controller, radio altimeter and automatic computer combine, the opening altitude of automatic guidance main force parachute is to reduce the airborne period of survival capsule as far as possible.Owing to adopt automatic computer control, can work out in the air, the two kinds of automatic control programs in ground are implemented automatically, in case of necessity, also can manually artificial parachute-opening and rocket firing.4, reduce destruction to the external form of original shape aircraft as far as possible, keep the original airworthiness of original shape aircraft.Reduce exploitation and development cost.5, the airtight measure in emergency survival cabin must be the same with aircraft cockpit tight, and intensity will suitably strengthen, to adapt in the emergency survival inclement weather environmental concerns.
I am an amateurish aviation, the fan of space technology to aeronautical technology, has a smattering of, have half knowledge, owing to technical reason economically, can't implement this technical scheme with individual strength, if aircraft industry department at all, adopt this technical scheme, domestic to thorough change, so the public security situation of world's civil aircraft, will play positive impetus.Be a good job that promotes the well-being of mankind, promptly will produce long-term, immeasurable, good economic benefit and social benefit.
Claims (3)
1, a kind of passenger of civil aviaton aircraft provided by the invention " airplane crash " emergency survival cabin is characterized in that; Emergency survival cabin body (14) is the independently component part in aircraft sealing main cabin.At ordinary times with aircraft host and guest cabin (1) leak-tight joint, airtight hatch door (20) is the personnel channel, with the same construction in host and guest cabin one and surface pressure, the closed environment that the oxygen concentration temperature is suitable, in the emergency survival cabin, except settling seat (11) cabin door conventional facilities such as (18), to be equipped with a cover pressure and an air conditioner system in addition, and the oxygen of right quantity, nitrogen gas cylinder (13), airbag filling device (21), the controller of computer-controlled rocket firing and parachute parachute-opening, with radio beacon emitter sea coloring agent buoyant apparatus such as (12), the main body load-bearing roof beam structure of emergency survival cabin and aircraft, connect suspension with multiple spot explosive bolt (3), under floor, emergency survival cabin and under the aircraft between covering, two pieces of solid fuel retro-rockets or compressed-air cylinder (9) are housed, rocket nozzle (6), damping spring application cylinder (8) is being supported sled shape slide plate (7), and all the other have filled up shock-absorption air bag (10), two outsides, emergency survival cabin are equipped with column type airbag (23) tail to be filled and following covering centre joint place settles some explosive bolts (3), between covering, install compact stabilized landing pack (4) on the top ceiling of emergency survival cabin and on the aircraft, large-scale main force landing pack (5).
2, it is characterized in that according to a kind of passenger of civil aviaton aircraft " airplane crash " emergency survival cabin of claim one; In the navigation of high-altitude " airplane crash " takes place, start aerial lifesaving electronic program, adopt the bottom air bag of main parachute and survival capsule, the method that the column type airbag combines can guarantee the emergency survival cabin, the safe landing or the landing water surface.
3, it is characterized in that according to a kind of passenger of civil aviaton aircraft " airplane crash " emergency survival cabin of claim one; When the take-off and landing of ground, take place " airplane crash ", start ground lifesaving electronic program, adopt shock-absorption air bag, the damping spring application cylinder, solid fuel retro-rocket or compressed-air cylinder and the synergy of sled shape slide plate can alleviate the personal injury of inertia impact to the passenger., the survival capsule reversing sense is pushed away aircraft, away from flammable and explosive substances such as Fuel Tanks, guarantee the lifesaving success.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200410050516 CN1754778A (en) | 2004-09-27 | 2004-09-27 | Civil aviation passenger aeroplane emergency survival capsule |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200410050516 CN1754778A (en) | 2004-09-27 | 2004-09-27 | Civil aviation passenger aeroplane emergency survival capsule |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1754778A true CN1754778A (en) | 2006-04-05 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200410050516 Pending CN1754778A (en) | 2004-09-27 | 2004-09-27 | Civil aviation passenger aeroplane emergency survival capsule |
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| CN (1) | CN1754778A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292497A (en) * | 2015-10-28 | 2016-02-03 | 吴然 | Automatic escape seat for passenger planes |
| CN106828938A (en) * | 2017-02-16 | 2017-06-13 | 佛山市三水区希望火炬教育科技有限公司 | A kind of military big aircraft life-saving device for being exclusively used in transporting leatherneck |
| CN113165466A (en) * | 2018-11-21 | 2021-07-23 | 北极星工业有限公司 | Vehicle with adjustable compression and rebound damping |
-
2004
- 2004-09-27 CN CN 200410050516 patent/CN1754778A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292497A (en) * | 2015-10-28 | 2016-02-03 | 吴然 | Automatic escape seat for passenger planes |
| CN106828938A (en) * | 2017-02-16 | 2017-06-13 | 佛山市三水区希望火炬教育科技有限公司 | A kind of military big aircraft life-saving device for being exclusively used in transporting leatherneck |
| CN113165466A (en) * | 2018-11-21 | 2021-07-23 | 北极星工业有限公司 | Vehicle with adjustable compression and rebound damping |
| CN113165466B (en) * | 2018-11-21 | 2024-05-28 | 北极星工业有限公司 | Vehicle with adjustable compression damping and rebound damping |
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