CN1102163A - Life-saving passenger cabin for civil airplane - Google Patents
Life-saving passenger cabin for civil airplane Download PDFInfo
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- CN1102163A CN1102163A CN 93119356 CN93119356A CN1102163A CN 1102163 A CN1102163 A CN 1102163A CN 93119356 CN93119356 CN 93119356 CN 93119356 A CN93119356 A CN 93119356A CN 1102163 A CN1102163 A CN 1102163A
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- passenger cabin
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- saving passenger
- cabin
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Abstract
The present invention discloses a life-saving passenger cabin for civil airplane, relating to an emergency equipment or device used in airplane. It consists of airplane fuselage (2) and control system (1). Its main improvement is as follows: the life-saving passenger cabin (4) is installed on the bellyhold (14), behind the control cabin (15) in the case shell (10) of the airplane, and the life-saving passenger cabin consists of parachute (3) mounted on its top, and ari bag (5), convex track (11) and its correspondent concave track (12), front sealed cabin door (6) and rear sealed cabin door (13) installed on its bottom, and four hydraulic landing gears installed on four corners of the case shell (17) of the passenger cabin, so that when the airplane runs into an accident, it can ensure the life-saving passenger cabin for safe landing.
Description
The present invention relates to be used for to break away from the emergency serving unit or the device of aircraft main frame, especially belong to life-saving passenger cabin for civil airplane when emergency chute.
On the existing aircraft survival capsule is not set generally, therefore the driving technique that can only rely on the aviator to have by oneself when aircraft meets accident is turned danger into safety, yet for the so passenger plane and the unpredictable rough weather of bulky complex, the aviator is helpless, so just be doomed aircraft in case accident is the fatal crass, caused painful air crash.Chinese patent by retrieval, the patent application of application number " 88108189.2 " " lifesaving control system of civil aircraft " is arranged, this application is to be bondsman, machine safe falling design-calculated, there is not disconnecting gear again owing to structure is numerous and jumbled, and be difficult to prevent generation such as burning and blast, cause the blast of catching fire if run into aero-engine, this control system can not work fully so, also the purpose of out of reach people, machine safe falling.
The objective of the invention is to: provide a kind of when aircraft meets accident accident aloft, can be with several independent separately before whole airplane crashes, life is perfect, and escape danger life-saving passenger cabin and aircraft main frame breaks away from fully, and make the device that the life-saving passenger cabin of escaping danger after escaping danger can stable landing, to reach the purpose that the passenger and crew is survived.
The technical solution used in the present invention is: it is by airframe 2, control system 1 is formed, its improvements are: the life-saving passenger cabin 4 of escaping danger is to be contained in airplane skin 10 the insides, after the driving compartment 15, on the cargo hold 14, and life-saving passenger cabin 4 tops of escaping danger are equipped with parachute 3, and the bottom is equipped with airbag 5, protruding rail 11 and cooresponding recessed rail 12, nose capsule door 6, back seal hatch door 13 and on four angles of main cabin shell 17 four hydraulic pressure landing gears 34 be housed to be formed.
The invention has the advantages that: (1) the present invention when the aircraft normal flight can steadily firmly connect together into as a whole with aircraft itself, accident and in case aircraft meets accident, the present invention just can break away from the aircraft that is about to crash rapidly safely, thereby gives the chance of passenger and crew to survive.(2) when having an accident suddenly in take-off process, aircraft guns off the runway to fly up the time, the present invention can be before aircraft smashes under computer control, the self-opening life saving system of escaping danger, location door bolt is opened and is lighted the projector life-saving passenger cabin of will escaping danger and penetrates, meanwhile before does not also land in the main cabin, self-filler in the main cabin forms the recoil damping part to three groups of airbag qi of chong channel ascending adversely of the bilge rapidly, makes every joint life-saving passenger cabin all finish the purpose that same instruction reaches soft landing.When (3) gunning off the runway its thing of bump for some reason when airfield approach lands, the present invention also can make the soft landing safely of every joint life-saving passenger cabin with the method in (2) point.(4) the present invention designs eight tops or more parachute, and they stagger mutually and maximally utilise large-area parachute, increase the speed that resistance slows down the main cabin tenesmus, make the main cabin reduce to nadir to the impulse force of ground bump.(5) escape danger life-saving passenger cabin size, joint number how much be the weight in main cabin, the limit of bearing of impulsive contact force to be come design-calculated according to parachute, airbag and three parts of landing gear, it can be three joints, also can be more than three joints.(6) airbag as the 3rd recoil damping part is design-calculated by inner bag, middle bag and outer bag, when promptly being subjected to impact effect, inner bag is broken earlier, after be that middle bag breaks, and outer bag is designed and can not be broken, this advantage is when bag go up to be done to collide repeatedly up and down outside again and again in the main cabin, the main cabin all the time not directly and the ground striking, thereby make the main cabin reduce to zero point to ground-surface impactization.(7) as second the recoil damping part four hydraulic pressure landing gears, they contact to earth the end be the hook type, one circular airbag is arranged therebetween, this airbag breaks when recoiling the damping part pressurized as first, the haptic element of hook type can support the main cabin reposefully, under computer monitor control, can guarantee that every landing gear is stressed equal and according to the big minor adjustment of terrain slope each pillar that stretches, the balance main cabin is unlikely rolls.(8) every joint life-saving passenger cabin all has the same perfect life of escaping danger, and has the sanitary accomodation that non-drinkable water storage cabinet is wherein arranged; Food, first-aid medicine and drinkable water storeroom are arranged; Electrical generator and self-filler are arranged; Have between the depositing of oil plant, oxygen canister, communication equipment and lifesaving instrument etc.
The present invention is described in further detail below in conjunction with accompanying drawing.
Fig. 1 is the life-saving passenger cabin for civil airplane schematic diagram
Fig. 2 is the A-A view of Fig. 1
Fig. 3 is the life distribution graph of escaping danger
Fig. 4 is the structure and the schematic diagram of position fixing system
Fig. 5 is protruding rail and recessed rail constructional drawing
Fig. 6 is the escape danger structure principle chart of life-saving passenger cabin of a joint
Fig. 7 is that the B of Fig. 6 is to view
Fig. 8 is the distribution graph of parachute
Fig. 9 is the constructional drawing of airbag
Wherein 1. control systems, 2. airframes, 3. parachutes 4. escape danger life-saving passenger cabin 5. airbags 6. nose capsule doors 7. transmitters 8. protruding rails location door bolt 9. recessed rails location door bolts 10. airplane skins 11. protruding rails 12. recessed rail 13. rear sealing hatch door 14. cargo holds 15. driving cabins 16. hide 19. water inlet drainage pipeline elastic interfaces, 20. air-conditioning pipeline elastic interfaces, 21. increase and decrease air-pressure duct elastic interfaces, 22. power supply touch panel elastic interfaces, 23. instruction touch panel elastic interfaces, 24. toilets, 17. life-saving passenger cabin shells storage bag chambers 18., umbrella chamber, non-drinkable water storage cabinet 25. communication apparatus oil plants and oxygen lifesaving instrument deposit between bag 38. inner bags in 26. food, first-aid medicine and drinkable water storeroom 27. generators and self-filler 28. passageway elastic outer wall devices 29. hatch door entrances 30. protruding rail motors 31. gears 32. recessed rail motor 33. portholes 34. hydraulic pressure landing gears 35. circular airbag 36. outer bags 37..
Be illustrated in figure 1 as the life-saving passenger cabin for civil airplane schematic diagram: it promptly is independent of outside airframe 2, driving compartment 15 and the cargo hold 14, again can be by five on airplane skin 10 inwalls recessed rail 12 combine with five protruding rails 11 on life-saving passenger cabin shell 17 walls, firmly be arranged on airplane skin 10 the insides, after the driving compartment 15, on the cargo hold 14, the perfect life-saving passenger cabin 4(that escape danger of such life of independently escaping danger is hereinafter to be referred as main cabin 4).Its inner various parts that reach itself all adopt a kind of composite material to make, the not only tough and tensile own wt of this material but also light, main cabin 4 can be divided into a joint, two joints, more than three joints or three save, nose capsule door 6 and back sealing hatch door 13 are opened when the aircraft normal flight, and joint main cabin 4, front and back is connected as a single entity and forms a complete big main cabin, and when having an accident, one first aid control system 1 is arranged in the driving compartment 15, the startup earlier of unlatching control system 1 back seals hatch door by the tail main cabin 4 interior life saving systems of escaping danger promptly and is closed, protruding rail location door bolt 8 and recessed rail location door bolt 9 are open, light projector 7 simultaneously, airframe 2 is penetrated along protruding rail 11 recessed rails 12 in main cabin 4, the top in the main cabin 4 after the disengaging releases a parachute 3 automatically, and 4 bottoms, main cabin have airbag 5 to be inflated and to place the bottom in main cabin 4 then.
Be illustrated in figure 2 as the A-A figure of Fig. 1: have one to hide umbrella chamber 16 at the top of every joint life-saving passenger cabin shell 17, the bag of Tibetan chamber 18 is arranged between 4 floors, main cabin and protruding rail 11, five corresponding recessed rails 12 and protruding rail 11 are arranged on life-saving passenger cabin shell 17 outer walls and airplane skin 10 inwalls, these five recessed rails 12 and protruding rail 11 can make the main cabin steadily firmly install on airframe 2 in 40 minutes, seat support strut 43 in the main cabin 4 is designed to fluid pressure type, is that cargo hold 14 is formed below main cabin 4.
Be illustrated in figure 3 as the life distribution graph of escaping danger: all be provided with into water drainage pipeline elastic interface 19 in the front in each main cabin 4, changes in temperature feed channel elastic interface 20, increase and decrease air-pressure duct elastic interface 21, power supply touch panel elastic interface 22, instruction touch panel elastic interface 23; Have sanitary accomodation 24 that non-drinkable water storage cabinet is arranged within it on 4 inner four angles, main cabin, this back that is used to escape danger is standby.Have communication equipment 25, oil plant, oxygen and lifesaving instrument deposit between 25, this usefulness such as contact first-aid organ etc. that is used to send an SOS.Food, first-aid medicine and drinkable water storeroom 26, this is used to allow the passenger that the necessity of existence is arranged.Electrical generator and self-filler 27, this is that be used to the to escape danger power supply of life saving system is supplied with.Passageway elastic outer wall device 28 is to connect during as normal flight to form the single-piece device between the main cabin.Hatch door inlet 29.Nose capsule door 6, sealing hatch door 13 in back is not intake big in the sea even if they close the back positive confinement yet.Projector 7 is equipped with at left and right corner place, below, the front in main cabin 4, and it can be the gunpowder formula, no matter main cabin 4 can both be penetrated outside the airframes 2 at high-altitude flight, this projector 7 that takes off or have an accident when landing.
Be illustrated in figure 4 as the structure and the schematic diagram of position fixing system: on the both sides of every joint main cabin 4 bottom protruding rails 11 and recessed rail 12, the rear and front end all is provided with position fixing system, and protruding rail motor 30 protruding rails location door bolt 8 is housed on protruding rail 11; When control system 1 is sent when instruction of escaping danger, electrical generator is also opened protruding rails location door bolt 8 by motor 30 in the starting cabin, power supply on the aircraft also can start the recessed rail motor 32 on the recessed rail 12 that is contained on the cargo hold top and open recessed rail by gear 31 and locate door bolt 9 simultaneously, and the life-saving passenger cabin 4 of escaping danger so just can penetrate smoothly.
Be illustrated in figure 5 as protruding rail and recessed rail constructional drawing: the life-saving passenger cabin shell is equipped with protruding rail 11 on 17 bottoms, and airplane skin 10 the inside cargo holds are equipped with recessed rail 12 on 14 tops, in the middle of recessed rail 12 and protruding rail 11 one group of rolling body 121 is housed and forms.
Be illustrated in figure 6 as a joint the escape danger structure and schematic diagram of life-saving passenger cabin: one group of parachute 3 it have six tops the same high equally big and two push up the high parachute of the same big ratio six top umbrellas, they stagger mutually, main cabin 4 the right and lefts have porthole 33, on four angles of main cabin shell 17 four hydraulic pressure landing gears 34 are arranged, hydraulic pressure push pull maneuver tube 341 is released hydraulic pressure landing gear 34 after the life saving system of escaping danger starts, the end that contacts to earth of hydraulic pressure landing gear 34 is shapes of hook type 342, one circular airbag 35 is arranged therebetween as first damping part, 4 bottoms, main cabin have three groups of airbags 5 to constitute.
The B that is illustrated in figure 7 as Fig. 6 is to view: the area after the right and left of protruding rail 11 respectively has one group of airbag 5, their inflations is bigger than life-saving passenger cabin shell 17, also have its two of one group of airbag 5 wideer than life-saving passenger cabin shell 17 in the centre of protruding rail 11, so that 4 bottoms, main cabin are at when landing direct colliding surface not, guarantee safety, the outside is that four hydraulic pressure landing gears 34 are formed on four angles of airbag 5.
Be illustrated in figure 8 as the parachute distribution graph: if during parachute 3 usefulness eight top, can be divided into four and hide umbrella chamber 16 and hide umbrella chamber at each and 16 li two top parachutes 3 are housed all, distribution is in order to increase resistance most effectively like this, also parachute-opening the most successfully and not being stuck.
Be illustrated in figure 9 as air bag structure figure: the structure of airbag 5 is made up of bag 37 and inner bag 38 in the outer bag 36, bag 37 during the impulse force that bears after inner bag 38 inflations is lower than, the impulse force that middle bag bears is lower than outer bag 36 again, like this in that to be subjected under the momentum effect inner bag broken earlier, bag 37 also breaks then, and outer bag 36 is designed to be difficult for breaking, and can allow main cabin 4 have on the bag 36 outside like this and more shake the leeway that subtracts bob power with change up and down, thereby reach the purpose of safe soft landing.
Its principle of work is: when the aircraft normal flight except that the rear door in main cabin, tail place 4 is closed, other sealing hatch door that respectively saves main cabin 4 is all opened by passageway elastic outer wall device 28 each main cabin 4 is linked to be a complete big main cabin, the same with the function in main cabin on the existing aircraft, when having only the fault that to save when the aircraft generation, emergency escape lifesaving control system 1 in the driving compartment 15 is by emergency escape computer system locking on the aircraft, can only after receiving aircraft signal out of control, the emergency escape computer system light by red light, just can open control system 1 makes instruction start the life saving system of escaping danger in main cabin 4 by instruction touch panel elastic interface 23, the stewardess makes nose capsule door 6 SELF CL after on your marks, protruding rail location door bolt 8 and recessed rail location door bolt 9 are opened, left and right sides projector 7 light and with main cabin 4 penetrate from airframe 2 and then second the joint, the 3rd joint, the escape danger program-disengaging airframe 2 same with first segment main cabin 4 finished in main cabin 4 successively, simultaneously positive co-pilot utilizes the emergency escape computer system to automatically lock head is entered to be inclined upwardly and enters rapidly near in the main cabin 4 of driving compartment behind the mission program, and hatch door is closed immediately before and after making, the door bolt unlatching left and right sides, convex-concave location projector 7 is lighted and is adorned main cabin 4 and penetrates the body 2 of disembarking, make main cabin 4 break away from the airframe 2 of being about to crash fully, the top in the main cabin 4 after escaping danger is abandoned covering automatically and is released a parachute 3, this moment is because the resistance that increases, add 4 bottoms, main cabin and also abandon 27 unlatchings of covering self-filler and main cabin 4 is held in 5 inflations of three groups of airbags and expansion, the life-saving passenger cabin (4) after escaping danger so just slowly descends slowly and lightly.Push pull maneuver tube 341 is released hydraulic pressure landing gear 34 and is formed trapezoid support on 17 4 angles of main cabin shell then, and hydraulic pressure landing gear 34 stretches out fully, and hook type 342 contacts to earth to hold and struts, and soft landings are prepared in circular airbag 35 inflations.Contact to earth earlier as the circular airbag 35 of the first bumper and absorbing shock parts in the moment of contacting to earth and to break, hold main cabin 4 tightly as the hook type 342 of the end that contacts to earth of the hydraulic pressure landing gear 34 of the second bumper and absorbing shock parts then, and carry out bumper and absorbing shock again by hydraulic pressure landing support function, when being hit when being pressed onto to a certain degree pillar, hydraulic pressure landing gear 34 pillars slowly withdraw, allow the 3rd bumper and absorbing shock parts airbag 5 finish the action of last change danger damping, 5 while of three groups of airbags this moment pressurized, so their inner bags 38 separately are broken earlier, bag 37 breaks then, last main cabin 4 is alleviated the bob power in the main cabin 4 that descends slowly and lightly on the outer bag 36 that is difficult for breaking further again, and then the hydraulic pressure landing gear 34 under computer monitor control stretches out pillar again according to the size of terrain slope, support the effect of main cabin 4 reposefully owing to hydraulic prop 43 and a whole set of life saving system of escaping danger under the seat in the cabin, all passengers and crew are escaped danger to survive.
Claims (8)
1, life-saving passenger cabin for civil airplane, by airframe (2), control system (1) is formed, it is characterized in that: the life-saving passenger cabin of escaping danger (4) is at airplane skin (10) the inside, driving compartment (15) afterwards, on the cargo hold (14), and be equipped with parachute (3) at the life-saving passenger cabin of escaping danger (4) top, airbag (5), protruding rail (11) and cooresponding recessed rail (12), nose capsule door (6) are equipped with in the bottom, and the back seals hatch door (13) and on four angles of main cabin shell (17) four hydraulic pressure landing gears (34) is housed to be formed.
2, life-saving passenger cabin according to claim 1 is characterized in that: the joint number of the life-saving passenger cabin of escaping danger (4) be one the joint, two the joint, three the joint or three the joint more than.
3, life-saving passenger cabin according to claim 1 and 2 is characterized in that: parachute (3) quantity that the top of the life-saving passenger cabin of escaping danger (4) is equipped with is one, more than two or two, is preferably eight.
4, life-saving passenger cabin according to claim 1 and 2 is characterized in that: the seat support strut (43) in the life-saving passenger cabin of escaping danger (4) is for fluid control.
5, life-saving passenger cabin according to claim 1 and 2 is characterized in that: the life-saving passenger cabin of escaping danger (4) the fwd lower left corner and the lower right corner are equipped with projector (7) and are formed.
6, life-saving passenger cabin according to claim 1 and 2, it is characterized in that: two protruding rails (11) are arranged at main cabin shell (17) bottom of the life-saving passenger cabin of escaping danger (4), a protruding rail (11) is respectively arranged at the right and left and top, five recessed rails (12) are arranged on the corresponding with it position, and between recessed rail (12) and protruding rail (11), rolling body (121) is housed and forms.
7, life-saving passenger cabin according to claim 1 and 2 is characterized in that: the end that contacts to earth of hydraulic pressure landing gear (34) is hook type (342), has a circular airbag (35) to form in the middle of hook type (342).
8, life-saving passenger cabin according to claim 1 and 2 is characterized in that: airbag (5) quantity of the life-saving passenger cabin of escaping danger (4) bottom is three groups, and airbag (5) is by inner bag (38), and middle bag (37) and outer bag (36) are formed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 93119356 CN1102163A (en) | 1993-10-27 | 1993-10-27 | Life-saving passenger cabin for civil airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 93119356 CN1102163A (en) | 1993-10-27 | 1993-10-27 | Life-saving passenger cabin for civil airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1102163A true CN1102163A (en) | 1995-05-03 |
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ID=4992873
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 93119356 Pending CN1102163A (en) | 1993-10-27 | 1993-10-27 | Life-saving passenger cabin for civil airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1102163A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1077063C (en) * | 1998-04-15 | 2002-01-02 | 王俊峰 | Automatic safety escaping danger system for aircraft distress personnel |
| CN103085964A (en) * | 2013-02-27 | 2013-05-08 | 王愐荣 | Method for manufacturing safe passenger plane |
| CN104309808A (en) * | 2014-09-25 | 2015-01-28 | 安徽科耀智能科技有限公司 | Safety collision device for unmanned aerial vehicle |
| CN104554730A (en) * | 2013-10-11 | 2015-04-29 | 天津得瑞丰凯新材料科技有限公司 | Passenger plane parachute bay collective escape device |
| CN106081126A (en) * | 2016-06-13 | 2016-11-09 | 王晨 | Bionical cellular active safety escape compartment embeds application and the design of aviation aircraft |
| 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 |
| CN108910056A (en) * | 2018-08-09 | 2018-11-30 | 雷子墨 | A kind of aircraft with separable pressurized cabin |
| CN111076625A (en) * | 2019-12-09 | 2020-04-28 | 中国兵器装备研究院 | Rocket device for throwing in materials |
| RU2750340C1 (en) * | 2020-03-02 | 2021-06-28 | Андрей Анатольевич Саприн | High security aircraft |
| EP4098558A1 (en) * | 2021-06-02 | 2022-12-07 | Du, Di | Aircraft safety lifesaving system |
-
1993
- 1993-10-27 CN CN 93119356 patent/CN1102163A/en active Pending
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1077063C (en) * | 1998-04-15 | 2002-01-02 | 王俊峰 | Automatic safety escaping danger system for aircraft distress personnel |
| CN103085964A (en) * | 2013-02-27 | 2013-05-08 | 王愐荣 | Method for manufacturing safe passenger plane |
| CN104554730A (en) * | 2013-10-11 | 2015-04-29 | 天津得瑞丰凯新材料科技有限公司 | Passenger plane parachute bay collective escape device |
| CN104309808A (en) * | 2014-09-25 | 2015-01-28 | 安徽科耀智能科技有限公司 | Safety collision device for unmanned aerial vehicle |
| CN106081126A (en) * | 2016-06-13 | 2016-11-09 | 王晨 | Bionical cellular active safety escape compartment embeds application and the design of aviation aircraft |
| 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 |
| CN108910056A (en) * | 2018-08-09 | 2018-11-30 | 雷子墨 | A kind of aircraft with separable pressurized cabin |
| CN111076625A (en) * | 2019-12-09 | 2020-04-28 | 中国兵器装备研究院 | Rocket device for throwing in materials |
| RU2750340C1 (en) * | 2020-03-02 | 2021-06-28 | Андрей Анатольевич Саприн | High security aircraft |
| EP4098558A1 (en) * | 2021-06-02 | 2022-12-07 | Du, Di | Aircraft safety lifesaving system |
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