CN105752343A - Passenger plane high-altitude crash life-saving system and life-saving method - Google Patents
Passenger plane high-altitude crash life-saving system and life-saving method Download PDFInfo
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- CN105752343A CN105752343A CN201610114017.9A CN201610114017A CN105752343A CN 105752343 A CN105752343 A CN 105752343A CN 201610114017 A CN201610114017 A CN 201610114017A CN 105752343 A CN105752343 A CN 105752343A
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- 238000000034 method Methods 0.000 title claims description 12
- 230000007246 mechanism Effects 0.000 claims abstract description 32
- 238000007789 sealing Methods 0.000 claims abstract description 17
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims abstract description 10
- 239000001301 oxygen Substances 0.000 claims abstract description 10
- 229910052760 oxygen Inorganic materials 0.000 claims abstract description 10
- 239000002775 capsule Substances 0.000 claims description 125
- 230000004083 survival effect Effects 0.000 claims description 125
- 230000009471 action Effects 0.000 claims description 13
- 239000010410 layer Substances 0.000 claims description 13
- 239000007789 gas Substances 0.000 claims description 12
- 230000003028 elevating effect Effects 0.000 claims description 8
- 230000004044 response Effects 0.000 claims description 8
- 239000011229 interlayer Substances 0.000 claims description 7
- 238000006213 oxygenation reaction Methods 0.000 claims description 6
- 230000008602 contraction Effects 0.000 claims description 4
- 230000005012 migration Effects 0.000 claims description 3
- 238000013508 migration Methods 0.000 claims description 3
- 230000035945 sensitivity Effects 0.000 claims description 3
- 230000006378 damage Effects 0.000 abstract description 5
- 125000006850 spacer group Chemical group 0.000 abstract 1
- 238000009423 ventilation Methods 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 7
- 206010057071 Rectal tenesmus Diseases 0.000 description 3
- 208000027418 Wounds and injury Diseases 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 208000014674 injury Diseases 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 208000012271 tenesmus Diseases 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 235000013305 food Nutrition 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 239000003643 water by type Substances 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 235000012206 bottled water Nutrition 0.000 description 1
- 230000000739 chaotic effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 230000009191 jumping Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
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- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
The invention discloses a passenger plane high-altitude crash life-saving system which comprises a life-saving ball (14), life-saving ball loading equipment, life-saving ball launching equipment (7) and an automatic control system, wherein the life-saving ball comprises a fixed clamp (24), a lasso connecting device (21), soft handrails (19), an inner oxygen supply device (16), a spacer pull strap (13), a space inflation device (15), a pressure sensing ventilation valve (12) and a parachute; the life-saving ball loading equipment comprises a life-saving ball storage compartment (1) and a pre-opened life-saving ball loading compartment (5); a life-saving ball switching mechanism (2) is arranged in the life-saving ball storage compartment; a sealing mechanism (4) is arranged on the top of the pre-opened life-saving ball loading compartment; a lifting mechanism (8) is arranged on the side surface of the pre-opened life-saving ball loading compartment. By adopting the passenger plane high-altitude crash life-saving system, people can rapidly and safely leave off a plane, damage caused by temperature and pressure differences and falling collision to human bodies can be avoided, the situation that people in a passenger plane suffering from high-altitude plane crush cannot be saved by self can be changed, and high-altitude crush life-saving of passenger planes can be achieved.
Description
Technical field
The present invention relates to life saving system and lifesaving method, be related specifically to passenger plane high-altitude air accident rescue system and lifesaving method.
Background technology
Passenger plane is a kind of high speed manned means of transport efficiently, and it greatly reduces the consuming of time energy for people, creates huge economic benefit.And thus substantially increase passenger plane freight volume, promote the development of civil aviaton's cause.But simultaneously as manual operation is improper and the reason that takes place frequently etc. of equipment fault and climate change and extreme weather so that passenger plane airplane crash also gets more and more, and causes casualties and property loss is also increasing.
Passenger plane airplane crash is varied, and present people do not have a clear and definite classification and define.Discussing in order to convenient, the airplane crash that the passenger plane landing stage occurs for we is referred to as " low latitude airplane crash "；The airplane crash occurred during passenger plane normal flight is referred to as " high-altitude airplane crash ".According to investigations " low latitude airplane crash " had lifesaving technology and the equipment of relative maturity, so not discussing herein.On the contrary " high-altitude airplane crash " but there is no corresponding lifesaving technology and equipment or even blank out.As horse navigates MH370, horse boat QZ8501, the moral boat contour absolutely empty difficult matter part of 4U9525 once be exactly fatal crass.So, what be discussed herein primarily is exactly why up to now " high-altitude airplane crash " lifesaving technology and equipment remain blank out.It is considered that its reason has: 1, passenger plane is the seal of an accurate constant temperature and pressure；2, passenger plane is often in high-speed flight state upper and lower for 400km/h；3, passenger plane generally flies aerial at the height of 7000-13000M；4, passenger plane generally flies in the interval of low-temp low-pressure；The situations such as before 5, airplane crash occurs, passenger plane there will be tenesmus, jolts, rolling；6, before airplane crash occurs, persons on board there will be panic chaotic；7, it is likely to related personnel and cannot jump out self specialty limitation thus " high-altitude airplane crash " is lacked and integrally recognizes comprehensively；Etc. these reasons make problem become extremely complex, make us cannot take out a set of practical effective lifesaving technology and equipment, thus causing this blank.
It addition, the existence of this blank just, people have to promote the performance of passenger plane and maintain steadily to glide and force-land, thus prevention and avoid the generation of high-altitude airplane crash.While it is true, the generation of high-altitude airplane crash still cannot be stopped, and once occur, just necessarily cause great casualties and economic loss.This present situation, if in alien civilization, is exactly the joke of the mankind, grief simply.
Therefore, as why not by the made elbow of these challenges, opened new situation, it is achieved zero breakthrough of passenger plane high-altitude air accident rescue.Even if it is to say, airplane crash occurs passenger plane when high-altitude flight, persons on board implement self-help escape, no longer " packing is taken away " " living and diing together " such as through effective and feasible technology and equipment, here it is the problem that the present invention needs to solve.
Summary of the invention
The present invention is directed to passenger plane high-altitude air accident rescue blank, propose innovatively a kind of easy and simple to handle, rapidly and efficiently, the passenger plane high-altitude air accident rescue system of safe and feasible and lifesaving method.
It was found that when there is high-altitude airplane crash, except the instantaneous destruction situations such as blast, passenger plane always has the steady glide of quite a while.The lifesaving method of the present invention be exactly within the time of this section of steady glide the application of the invention innovation life saving system to organize and implement lifesaving.
The system that the present invention innovates is: passenger plane high-altitude air accident rescue system, and it includes survival capsule, survival capsule charging appliance, survival capsule dispensing device and automatic control system；Described survival capsule includes fixation clamp, lasso trick connecting device, soft handrail, internal layer, internal layer apparatus of oxygen supply, outer layer, interlayer pull strap, interlayer aerating device, air pressure sensing gas valve, parachute；Described survival capsule charging appliance includes between survival capsule storage, between pre-unlatching survival capsule loading, and described survival capsule is provided with survival capsule switching mechanism between storing, and between described pre-unlatching survival capsule loading, top is provided with enclosed mechanism, and side is provided with elevating mechanism；Described survival capsule dispensing device includes outlet valve, transporter, inlet valve；Described automatic control system includes triggering response and the timing control of various functions and action.
Further, described enclosed mechanism include being arranged on pre-open survival capsule load between sidewall accepting groove in screw-pinch circle, push-pull bar and the sealing rifle that is arranged on push-pull bar, described screw-pinch circle is provided with opening, and described push-pull bar is flexibly connected shrink-ring through sidewall and can promote the relatively inside and outside contraction in screw-pinch circle two ends.
The present invention has also innovated the lifesaving method of a kind of passenger plane high-altitude airplane crash: between the survival capsule of survival capsule charging appliance stores, control survival capsule switching mechanism according to instruction and be actuated for survival capsule switching, switch at survival capsule, passenger enters to trigger after interior lasso trick is plugged into the startup countdown of survival capsule automatic function, pre-unlatching between survival capsule loads starts, elevating mechanism is started working, enclosed mechanism drops to pre-unlatching at survival capsule and performs sealing between survival capsule loading after bottom position, and triggers survival capsule entrance survival capsule dispensing device further；Survival capsule is thrown in out passenger plane from survival capsule charging appliance by transporter migration by survival capsule dispensing device response survival capsule charging appliance；Depart from after passenger plane safe distance, countdown terminates to be sequentially completed inner space oxygenation, jacket space is inflated, release a parachute, drop to safe height above sea level and safe air pressure after trigger gas pressure sensitivity answer gas valve to open；Last survival capsule soft landing.
Beneficial effects of the present invention: the application of the invention, people can be made to depart from rapidly aircraft safely, and avoid temperature and pressure difference and tenesmus collision injury that human body is caused, change the passenger plane present situation that staff on board cannot save oneself when meeting with high-altitude airplane crash, it is achieved passenger plane high-altitude air accident rescue.
Accompanying drawing explanation
Fig. 1 is present invention installation site schematic diagram aboard,
Fig. 2 is the overall structure schematic diagram of the present invention,
Fig. 3 is survival capsule charging appliance and the survival capsule dispensing device fit structure schematic diagram of the present invention,
Fig. 4 is the survival capsule structural representation of the present invention,
The emergency exits that Fig. 5 is the present invention use position view,
Fig. 6 is the structure of a kind of enclosed mechanism of the present invention and uses view,
Fig. 7 is the flow chart of steps of lifesaving method of the present invention.
In the drawings, 1, survival capsule store between 2, survival capsule switching mechanism 3, emergency exits 4, enclosed mechanism 401, accepting groove 402, screw-pinch circle 403, push-pull bar 404, sealing rifle 405, opening 5, pre-open spheroid load between 6, base plate 7, survival capsule dispensing device 8, elevating mechanism 9, inlet valve 10, transporter 11, outlet valve 12, air pressure sensing gas valve 13, interlayer pull strap 14, survival capsule 15, jacket space aerating device 16, inner space inflation apparatus of oxygen supply 17, outer layer 18, internal layer 19, soft handrail 20, parachute 21, lasso trick connecting device 22, emergency start button 23, compressive state survival capsule 24, fixation clamp.
Detailed description of the invention
In order to make those skilled in the art be more fully understood that technical scheme, in conjunction with detailed description of the invention, the present invention is described in further detail below according to accompanying drawing.
As in figure 2 it is shown, described passenger plane high-altitude air accident rescue system, including survival capsule 14, survival capsule charging appliance, survival capsule dispensing device 7 and automatic control system, as shown in Figure 1, native system may be installed the tail position of aircraft, and passenger enters from main cabin afterbody and throws in, it is possible to selects other homes.
nullSuch as Fig. 4、Shown in 5，Described survival capsule has lasso trick connecting device 21 from inside to outside successively、Soft handrail 19、Inner space inflation apparatus of oxygen supply 16(ensures to drop to internal layer oxygen supply before safe altitude)、Internal layer 18(material needs airtight、Insulation、Thermal insulation、Elastic、The functions such as tension support，Such as spacesuit material)、Interlayer pull strap 13(keeps effective tensile force between ectonexine，Stablize human body sitting posture)、Jacket space aerating device 15(plays bumper and absorbing shock and gravity drop hammer effect，In order to reduce induction installation and sensitive time，Also can inflate apparatus of oxygen supply with inner space to unite two into one)、The same inner layer material of outer layer 17(，Power resistance strength is bigger)、Air pressure sensing gas valve 12、Between fixation clamp 24(and survival capsule loading, the draw-in groove (not shown in FIG.) of sidewall matches，For fixing compressive state survival capsule 23 " loaded " position and convenient switching，Unclamp after sealing)、Parachute 20.Wherein survival capsule disengaging aircraft safety terminates to be sequentially completed apart from rear response countdown: the inflation of jacket space and inner space oxygen supply action, with parachute opening action after passenger plane safe distance, after survival capsule drop to safe altitude substitute pressure ring border, air pressure sensing gas valve is opened to ensure contained life entity eupnea, preferably, including GPRS device, food, pocket knife etc., instrument all can be provided in lasso trick in advance, passenger is facilitated to depart from survival capsule after landing and wait for rescue (if on land, it is possible to depart from survival capsule；If on the waters surface such as Hu Hai, then can stay in survival capsule).
As shown in Figure 2,3, described survival capsule charging appliance includes shell, survival capsule store between 1, pre-open survival capsule load between 5, described survival capsule is provided with survival capsule switching mechanism 2 between storing, it is responsible for loading and switching survival capsule, described pre-unlatching lifesaving asks top between loading to be provided with enclosed mechanism 4, and side is provided with elevating mechanism 8.
Preferably, as shown in Figure 6, specifically a kind of enclosed mechanism include being arranged on pre-open spheroid load between sidewall accepting groove 401 in screw-pinch circle 402, push-pull bar and the similar tied silk rifle structure of the prior art of the sealing rifle 404(being arranged on push-pull bar 403, but precision and sealing property are higher), it is that opening two ends are not at a horizontal plane that described screw-pinch circle is provided with opening 405(effect, it is easy to the inside and outside contraction of screw-pinch circle, similar conveying worm blade construction), described push-pull bar is flexibly connected shrink-ring through sidewall and can promote the relatively inside and outside contraction in screw-pinch circle two ends.Specifically process is: lasso trick starts elevating mechanism work after plugging into, enclosed mechanism drops to pre-unlatching at survival capsule and performs sealing after bottom position between survival capsule loading, automatic system makes push-pull bar promote the relative direction motion in accepting groove of screw-pinch circle opening two ends, and the most at last survival capsule ball mouth draw in together, then sealing rifle performs sealing, having sealed rear automatic system makes push-pull bar pull screw-pinch circle opening two ends to initial position return, push-pull bar also returns to initial position, and trigger further and unclamp fixation clamp and base plate 6 and tilt to make survival capsule to enter dispensing device.
As it is shown on figure 3, described survival capsule dispensing device includes shell, inlet valve 9, transporter 10, outlet valve 11.Wherein inlet valve response charging appliance has sealed signal, manned pre-survival capsule of opening is transplanted on outlet valve place by transporter (such as transporter, angle of inclination should not be too steep, becomes about 30 ° with level), open outlet valve, manned survival capsule is thrown in out passenger plane.
Described survival capsule charging appliance realizes function: can store the survival capsule of q.s unaerated, and can transfer rapidly, switch and open described survival capsule in advance, can stablize in quickly people being loaded into further, can being quickly completed sealing action further, the triggering that can complete dispensing device further starts.
Described survival capsule dispensing device realizes function: can respond charging appliance and start, become cabin and outside excessive space, carrying pre-survival capsule of opening that is manned and that seal further and throw in out aircraft, the triggering that can complete half startup survival capsule residue function further starts.
Described survival capsule realizes function: can responding countdown after plugging in position of plugging into and start, complete internal layer oxygenation within disengaging passenger plane certain time further, interlayer is inflated, release a parachute etc. guarantees the injury that people is not collided in survival capsule by low-temp low-pressure and tenesmus；After falling to safe height above sea level and safe air pressure, safety air vavle is opened and is realized air exchange maintenance interal supplying oxygen further；Survival capsule soft landing further.
As shown in Figure 7, described passenger plane high-altitude air accident rescue method, the safe lasso trick being equipped with time before tissue escape in advance by boarding (possesses in prior art, can referring to mountain-climbing lasso trick and bungee jumping lasso trick, and the subsidiary tool kit of lasso trick, include cutter, compressed foods, GPRS positioner, bottled water etc..) dress, survival capsule charging appliance survival capsule controls survival capsule switching mechanism according to instruction (while opening emergency exits 3) between storing and is actuated for survival capsule switching, pre-unlatching between survival capsule loads has switched at survival capsule, passenger enters is fixed in survival capsule on connecting port by the safe lasso trick dressed in emergency exits 3 (now for compressive state survival capsule), lasso trick completes to plug into be simultaneously emitted by starting and performs signal, survival capsule starts automatic function on countdown, (under special circumstances, the emergency start button 22(on emergency exits also can press outdoors in escape personnel and establishment officer, in door), start elevating mechanism work, enclosed mechanism drops to pre-unlatching at survival capsule and performs sealing after bottom position between survival capsule loading, and unclamp fixation clamp further, survival capsule is dumped into survival capsule dispensing device with base plate 6；Survival capsule is thrown in out passenger plane from survival capsule charging appliance by transporter migration by survival capsule dispensing device response charging appliance；Depart from passenger plane safe distance countdown at survival capsule to terminate to be sequentially completed inner space oxygenation, jacket space inflation, release a parachute, after droping to safe height above sea level and safe air pressure, trigger gas pressure sensitivity answers gas valve to open, last soft landing also waits for rescue (can depart from survival capsule on land, continue to stay in survival capsule on the waters surface such as Hu Hai).
It is about 7000-13000M by passenger plane cruising altitude, often it is in high-speed flight state upper and lower for 400km/h, and the gliding ability of passenger plane can try to achieve, the time that passenger plane aloft glides is approximately in 20-40MIN, this is also the precondition that the present invention can implement, conservatively estimate, calculate with about 15S per capita from access arrangement to the system use departing from passenger plane is consuming time, often set escape system per minute can be escaped for 4 people, in the minimum coasting time of 20min, set of system is available for people's escape of about 4*20=80.With the basic 2-4 cover system of the carrying capacity of current passenger airplanes, enough everyone escapes at short notice.Additionally Free Falling Body in Upper Air spent time is about 60s ~ 80s formula is H=1/2 g t2, parachute open after drag acceleration be generally-2.2m/s2, namely will remain a constant speed after opening parachute about 4 ~ 5s landing, say, that survival capsule depart from after passenger plane be had sufficient time to oxygenation, inflated, a series of actions such as release a parachute.nullAdditionally need explanation，The automatic control system related in the air accident rescue system of described passenger plane high-altitude，Such as the survival capsule lifting action being directed to、Sealing action、Fixation clamp unclamps action、Base plate topples over action、Survival capsule transfer operation、Each valve opening and closing movement、Parachute opening action、The operation acts of inflation apparatus of oxygen supply，Also have the triggering between each action and response and time difference setting etc.，Order is: after lasso trick is plugged into or pressed startup button，Survival capsule function on countdown starts，Lowering or hoisting gear starts，It drop to pre-unlatching after bottom between survival capsule loading，Position sensor sends signal and controls enclosed mechanism work，Enclosed mechanism sends signal after completing sealing makes fixation clamp unclamp，Base plate is toppled over，Inlet valve is opened，Transporter starts，Outlet valve is opened，Calculate from after plugging into until outlet valve is opened required time and is set countdown and trigger the inner space oxygenation of survival capsule、Jacket space is inflated、Release a parachute，Air pressure sensing gas valve is opened，Pass through time timer、Position sensor、Air pressure induction apparatus、Performing processor etc. makes above-mentioned action complete to find in existing automatic control technology，Do not describe in detail one by one at this.
The key innovations of invention is in that:
1, passenger plane high-altitude air accident rescue system and lifesaving method are innovatively proposed.Zero breakthrough is realized in passenger plane airplane crash this field of saving oneself.Break passenger plane just to save oneself can only leave it to chance once meet accident, be close to the miserable situation of " zero survives ".
2, a kind of survival capsule charging appliance has been innovated, even if airplane crash occurs, as long as passenger plane has one section of state relatively smoothly, it is possible to organize and implement lifesaving.
3, innovated a kind of survival capsule dispensing device, made people can safely and effectively depart from the passenger plane of sealing in time, and without influence on the home within passenger plane, isolation temperature and pressure play the effect of transitional storehouse.
4, innovated a kind of survival capsule equipment, by use survival capsule, it is to avoid contained human body be subject to low-temp low-pressure and
The injury that land shock etc. causes, and no matter last drop point landform simply complexity is even landed in sea, can protect contained personal security so that it is be rescued and survive.
In description, not detailed description part all can be considered prior art; embodiment of above is only in order to illustrate technical scheme and unrestricted; although the present invention being described in detail with reference to specific embodiment; it will be understood by those within the art that; technical scheme can be modified or equivalent replacement; without deviating from the spirit and scope of technical solution of the present invention, it all should be encompassed in the middle of the scope of claim protection of the present invention.
Claims (3)
1. passenger plane high-altitude air accident rescue system, it is characterised in that: it includes survival capsule (14), survival capsule charging appliance, survival capsule dispensing device (7) and automatic control system；Described survival capsule includes fixation clamp (24), lasso trick connecting device (21), soft handrail (19), internal layer (18), internal layer apparatus of oxygen supply (16), outer layer (17), interlayer pull strap (13), interlayer aerating device (15), air pressure sensing gas valve (12), parachute, described survival capsule charging appliance includes between survival capsule storage (1), between pre-unlatching survival capsule loading (5), described survival capsule is provided with survival capsule switching mechanism (2) between storing, between described pre-unlatching survival capsule loads, top is provided with enclosed mechanism (4), side is provided with elevating mechanism (8), described survival capsule dispensing device includes outlet valve (11), transporter (10), inlet valve (9)；Described automatic control system includes triggering response and the timing control of various functions and action.
2. passenger plane high-altitude air accident rescue system according to claim 1, it is characterized in that: described enclosed mechanism include being arranged on pre-open survival capsule load between sidewall accepting groove (401) in screw-pinch circle (402), push-pull bar and the sealing rifle (404) that is arranged on push-pull bar (403), described screw-pinch circle is provided with opening (405), and described push-pull bar is flexibly connected shrink-ring through sidewall and can promote the relatively inside and outside contraction in screw-pinch circle two ends.
3. the lifesaving method of passenger plane high-altitude air accident rescue system described in a claim 1, it is characterized in that: the survival capsule of survival capsule charging appliance controls survival capsule switching mechanism according to instruction between storing and is actuated for survival capsule switching, pre-unlatching between survival capsule loads has switched at survival capsule, passenger enters to trigger after interior lasso trick is plugged into the countdown startup every automatic function of survival capsule, start elevating mechanism work, enclosed mechanism drops to pre-unlatching at survival capsule and performs sealing between survival capsule loading after bottom position, and triggers survival capsule entrance dispensing device further；Survival capsule is thrown in out passenger plane from survival capsule charging appliance by transporter migration by survival capsule dispensing device response charging appliance；Survival capsule departs from after passenger plane safe distance, countdown terminates to be sequentially completed inner space oxygenation, jacket space is inflated, release a parachute, drop to safe height above sea level and safe air pressure after trigger gas pressure sensitivity answer gas valve to open；Last survival capsule soft landing.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610114017.9A CN105752343B (en) | 2016-03-01 | 2016-03-01 | Passenger plane high-altitude air accident rescue system and lifesaving method |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201610114017.9A CN105752343B (en) | 2016-03-01 | 2016-03-01 | Passenger plane high-altitude air accident rescue system and lifesaving method |
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| CN105752343A true CN105752343A (en) | 2016-07-13 |
| CN105752343B CN105752343B (en) | 2017-12-19 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112141346A (en) * | 2019-06-28 | 2020-12-29 | 马建成 | Totally-enclosed foldable airliner air escape waiting device |
| CN113335535A (en) * | 2020-03-02 | 2021-09-03 | 中航西飞民用飞机有限责任公司 | Airplane air emergency parachute jumping slideway system and lifesaving method |
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| JPS5431760Y2 (en) * | 1975-07-23 | 1979-10-03 | ||
| JPH08164897A (en) * | 1994-12-13 | 1996-06-25 | Nakamura:Kk | Capsule for rescue |
| CN2296308Y (en) * | 1997-02-19 | 1998-11-04 | 朱信权 | Escaping ball device of craft |
| CN101817397A (en) * | 2010-04-29 | 2010-09-01 | 余坤朋 | Multifunctional wall-weather and all-region aerated lifesaving device and using method thereof |
| CN202541840U (en) * | 2012-03-28 | 2012-11-21 | 孙诺 | Intelligent safe emergency escape compartment |
| CN104015927A (en) * | 2014-04-29 | 2014-09-03 | 王翼 | High-altitude egg-shaped escape device |
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2016
- 2016-03-01 CN CN201610114017.9A patent/CN105752343B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5431760Y2 (en) * | 1975-07-23 | 1979-10-03 | ||
| JPH08164897A (en) * | 1994-12-13 | 1996-06-25 | Nakamura:Kk | Capsule for rescue |
| CN2296308Y (en) * | 1997-02-19 | 1998-11-04 | 朱信权 | Escaping ball device of craft |
| CN101817397A (en) * | 2010-04-29 | 2010-09-01 | 余坤朋 | Multifunctional wall-weather and all-region aerated lifesaving device and using method thereof |
| CN202541840U (en) * | 2012-03-28 | 2012-11-21 | 孙诺 | Intelligent safe emergency escape compartment |
| CN104015927A (en) * | 2014-04-29 | 2014-09-03 | 王翼 | High-altitude egg-shaped escape device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112141346A (en) * | 2019-06-28 | 2020-12-29 | 马建成 | Totally-enclosed foldable airliner air escape waiting device |
| CN113335535A (en) * | 2020-03-02 | 2021-09-03 | 中航西飞民用飞机有限责任公司 | Airplane air emergency parachute jumping slideway system and lifesaving method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105752343B (en) | 2017-12-19 |
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