CN101391654A - Safety lifesaving airplane - Google Patents
Safety lifesaving airplane Download PDFInfo
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- CN101391654A CN101391654A CNA2007101545299A CN200710154529A CN101391654A CN 101391654 A CN101391654 A CN 101391654A CN A2007101545299 A CNA2007101545299 A CN A2007101545299A CN 200710154529 A CN200710154529 A CN 200710154529A CN 101391654 A CN101391654 A CN 101391654A
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- tail
- airplane
- fuselage
- parachute
- wing
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
- B64D25/12—Ejectable capsules
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
Abstract
The invention discloses a safety rescuing airplane, which is applicable to large-scale, medium-scale and small-scale airplanes including fixed wing airplanes and rotor wing airplanes, a passenger cabin of the large-scale and medium-scale airplanes adopts at least two layers of channel-shaped floors, when the airplane runs into an inevitable air crash, the airplane can ignite exploding bolts that are used for fixing airplane wings, an airplane tail and a front undercarriage, and cut off an operating connection rod, a cable or an electric cable that are led into the airplane wings, the airplane tail and the front undercarriage, thus abandoning the airplane wings, the airplane tail and the front undercarriage, simultaneously opening parachutes on the top of an airplane body and at the airplane tail, motivating the charging of two air bags in the bottom and at the lower two sides of the airplane body, and leading the airplane body to land or stop smoothly, slowly and safely under the actions of the parachutes and the air bags. The fixed wing airplane can omit the abandoning of the front undercarriage and the abandoning of the airplane tail in a ground sliding process; and the lightweight fixed wing airplane also can omit the abandoning of the airplane tail.
Description
One, technical field
The present invention relates to a kind of aircraft, particularly relate to a kind of safety lifesaving airplane, it belongs to the airplane design field.
Two, background technology
Along with economic development, social progress, aircraft is more and more, and air crash is also more and more, fatal crass mostly when airplane crash takes place, driver and crew's mortality is a hundred per cent almost.People are wanting to design a kind of aircraft that can safe life-saving always for these years, but have only the light-duty full machine parachuting aircraft of all the people present of U.S. a company research and development partly to be suitable for up to now, also there is fatal shortcoming in but this full machine parachuting aircraft, though that is exactly a parachute aircraft landing speed is slowed down, but still there is risk of explosion behind the fuel tank colliding surface, so to bigger a little again aircraft, this full machine parachute landing system is just powerless: this in addition full machine parachuting aircraft is inapplicable to fuel fire and explosion accident take place.
Three, summary of the invention
(1) the technical problem to be solved in the present invention is for overcoming weak point of the prior art, design a kind of simple, advanced, practical, economical, high reliability, be suitable for all large, medium and small aircrafts, comprise fixed wing aircraft and autogiro, big-and-middle-sized aircraft passenger compartment adopts two-layer at least channel shape floor, seat can laterally be put, also can vertically put, when the aircraft distress airplane crash is inevitable, start abort escape system, abandon wing, tail and nose-gear, release a parachute and air bag, excite the rocket launching of heligyro fuselage bottom, thus the safety lifesaving airplane that makes the steadily slow safe falling of fuselage or stop; Fixed wing aircraft also can not abandoned nose-gear, do not abandon tail in the middle of ground taxi; Light fixed-wing aircraft also can not abandoned tail.
(2) technical scheme
The aircraft element comprises body, maneuvering system, engine installation and airborne equipment etc.Safety lifesaving airplane of the present invention is formed by wing, tail, nose-gear, fuselage, parachute, air bag, manipulation, eight principal character system in combination such as electric, and other system is the same with conventional airplane.
The wing system: it is characterized in that comprising explosive bolt, cable cutter, driving engine and the fuel tank of precaution device, emergency survival button, signal transmssion line, wing control connecting rod, vertical wall joint in wing spar, preceding vertical wall and back and fuselage trusses or stringer and reinforcement bulkhead or common bulkhead infall joint are fixed with explosive bolt.
Tail system: it is characterized in that comprising explosive bolt, the umbrella cabin of tail afterbody, the explosive bolt of empennage control link, cable cutter that precaution device, emergency survival button, signal transmssion line, tail and fuselage are fixing.The heligyro engine installation constitutes one at fuselage top and tail, and fuel tank is installed in tail.If aircraft is abandoned tail in the middle of ground taxi, fuselage has hindered tail and has slided forward, exists tail to smash the fuselage risk, so aircraft is not abandoned tail in the middle of ground taxi, abandons tail aloft.Because a top parachute has enough been used for aviette, so light fixed-wing aircraft of the present invention can be abandoned tail, also can not abandon tail.
Nose-gear system: it is characterized in that comprising precaution device, emergency survival button, signal transmssion line, fixedly nose-gear and the explosive bolt of fuselage, the fixing explosive bolt of explosive bolt, cable cutter, nose-gear hatchcover and fuselage of nose-gear control link.Because nose-gear weight is not very big, so fixed wing aircraft of the present invention can be abandoned nose-gear, also can not abandon nose-gear, the present invention is distilled off as example simultaneously with nose-gear and wing summary of the invention is described.
The fuselage system: it is characterized in that comprising precaution device, emergency survival button, signal transmssion line, driving compartment, main cabin, storage battery, umbrella cabin, fuselage top, fuselage bottom and two side lower part air bag cabins, the heligyro fuselage bottom also is provided with rocket.Establish a plurality of sealings and close on the fuselage bulkhead, control link or cable and electrical cable are from sealing suitable mistake; Fuselage afterbody is established hatch door and is led to deck store, and the high-altitude flight aircraft is established airtight hatch door, and low-flying aircraft is established common hatch door.Also can use the parachute safe life-saving when making big-and-middle-sized aircraft distress airplane crash inevitable, also reduce simultaneously fuel oil consumption and cost, the present invention adopts two-layer at least channel shape floor to big-and-middle-sized aircraft passenger compartment, two-layer seating capacity is increased to the twice of original one deck seating capacity, main cabin length reduces half, main cabin weight saving near half; Three layers of seating capacity is increased to nearly three times of original one deck seating capacity, and it is nearly 2/3rds that main cabin length reduces, and main cabin weight saving is nearly 2/3rds, and seat can be by laterally putting, also can be by vertically putting, and the outside, both sides, upper strata be a child seat.Like this same seat figure place aircraft of the present invention than existing conventional airplane weight saving many, this has created condition with regard to carrying out safe life-saving for big-and-middle-sized aircraft utilization parachute and air bag.CAAC's regulation airline carriers of passengers is blimp below 100, and the 100-200 seat is a Medium Plane, is large aircraft more than 200.
Parachute system: it is characterized in that comprising precaution device, emergency survival button, signal transmssion line, umbrella cabin, rocket, parachute sleeve, parachute, umbrella rope, suspension ring.Parachute comprises fuselage top parachute and tail parachute, and its umbrella cabin is designed to streamline contour.At the trusses at fuselage top or stringer or itself and the infall of strengthening bulkhead or common bulkhead suspension ring are set, the umbrella rope ties up to tension and semifixed at the fuselage top on the suspension ring, and the other end places in the umbrella cabin.Parachute places in the parachute sleeve, and parachute sleeve links to each other with rocket, and parachute sleeve and rocket are installed in the umbrella cabin.Precaution device and emergency survival button are installed in series in driving compartment, and link to each other with rocket by signal transmssion line.According to aircraft size fuselage top at least one top and one deck parachute at least are installed, parachute is opened from back to front successively, opens the pull power of moment to aircraft to cushion parachute.1 quadrature parachute can bear 20 kilogram weights, and China's Shenzhou spacecraft has 1200 squares with the parachute area, and 90 kilogram weights can be used for 24 tons heavy aircrafts.
Gas-bag system: the explosive bolt that it is characterized in that comprising precaution device, emergency survival button, signal transmssion line, air bag cabin, air bag, fixation balloon hatchcover.Air bag comprises fuselage bottom air bag and two side lower part air bags.Can use high pressure gas, gunpowder explosion or chemical reaction etc. to airbag aeration.Air bag can adopt the buffer air bag that install the tank bottom when aircraft is jettisoninged tank.
Maneuvering system: it is characterized in that fighter plane of new generation all adopts fly-by-wire, novel aircarrier aircraft also progressively adopts fly-by-wire, and some type airplane also adopt mechanical manoeuvring system.Mechanical manoeuvring system comprises jociey stick, cable wire or rod member, pneumatic rudder face; Fly-by-wire comprises mini manipulation bar, sensor, cable, signal processor, steering wheel, pneumatic rudder face.The cable of the cable wire of mechanical manoeuvring system or rod member or fly-by-wire from driving compartment through main cabin bulkhead sealing close towards the wing cabin, tail cabin, noselanding gear well.
Electric system: it is characterized in that the aircraft electrical equipment comprises power equipment supply and various consumer.Power equipment supply comprises electrical generator, voltage regulator, reverse rent cutout, storage battery, DC booster, umformer.Consumer comprises: flight control, engine control, aviation electronics, motor machine, life support, illumination and signal, Thermal Anti-ice, passenger's service for life etc.The electric system cable leads to wing cabin, tail cabin, noselanding gear well, air bag cabin, parachute compartment and heligyro bottom rocket from main cabin bulkhead seal box.
According to above elaboration to each system, the present invention adopts two-layer channel shape floor to Medium Plane, and under the same situation of main cabin length, seating capacity is increased to the twice of common one deck aircraft seat number; If seating capacity is identical, then the two-layer aircraft of the present invention has reduced half than common one deck aircraft passenger compartment length, main cabin weight saving near half.Seat can be by laterally putting, also can be by vertically putting, and the outside, both sides, upper strata is a child seat, pillar is used to support upper floor.Same seat figure place aircraft weight of the present invention can alleviate manyly than existing conventional airplane like this, and this just also can use parachute and air bag to carry out safe life-saving to have created condition for Medium Plane, has also reduced fuel oil consumption and cost simultaneously.
The present invention adopts three layers of channel shape floor to large aircraft, and under the same situation of main cabin length, seating capacity is increased to nearly three times of common one deck aircraft seat number; If seating capacity is identical, then three layers of aircraft of the present invention reduced than common one deck aircraft passenger compartment length nearly 2/3rds, main cabin weight saving nearly 2/3rds.Seat can be by laterally putting, also can be by vertically putting, and the outside, both sides, upper strata is a child seat, pillar is used to support upper floor.Same seat figure place aircraft weight of the present invention can alleviate manyly than existing conventional airplane like this, and this has also created condition for large aircraft can use parachute and air bag to carry out safe life-saving, has also reduced fuel oil consumption and cost simultaneously.
Mechanical manoeuvring system fixed wing aircraft of the present invention is when aloft getting into danger, the precaution device that is installed in the driving compartment is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed aerial lifesaving button, start abort escape system, signal leads to wing through signal transmssion line transmission and control, tail, the explosive bolt of the control link of nose-gear and wing, tail, nose-gear, fuselage top parachute hatchcover, tail parachute hatchcover, fuselage bottom air bag hatchcover, the explosive bolt blast of fuselage side lower part air bag hatchcover, moment is opened hatchcover, excite airbag aeration simultaneously, the rocket launching of fuselage top parachute compartment and tail parachute compartment, air bag has sufficient intensity that it can not risen brokenly after the inflation of high-altitude, each cutter cuts off wing respectively behind the time-delay 1s, tail, the cable of nose-gear, so abandon wing, tail, nose-gear, parachute launches rapidly, the resistance that produces is evenly distributed by the umbrella rope on the suspension ring that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage is the steadily slow safe landing or the landing water surface under parachute and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.
Mechanical manoeuvring system fixed wing aircraft of the present invention is in danger when in ground taxi, the precaution device that is installed in the driving compartment is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed ground lifesaving button, start abort escape system, signal leads to wing through signal transmssion line transmission and control, the explosive bolt of the control link of nose-gear and wing, nose-gear, fuselage top parachute hatchcover, tail parachute hatchcover, fuselage bottom air bag hatchcover, the explosive bolt blast of fuselage side lower part air bag hatchcover, moment is opened hatchcover, excite airbag aeration simultaneously, the rocket launching of fuselage top parachute compartment and tail parachute compartment, air bag has sufficient intensity that it can not risen brokenly after the inflation of high-altitude, each cutter cuts off wing respectively behind the time-delay 1s, the cable of nose-gear, so abandon wing, nose-gear, parachute launches rapidly, the resistance that produces is evenly distributed by the umbrella rope on the suspension ring that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage steadily slowly stops safely under parachute and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.In this ground safe life-saving system because the iris action of unidirectional transmission unit such as optic coupler, diode etc., signal can not transfer to " blast of empennage control link explosive bolt, the blast of tail explosive bolt, time-delay 1s cutting machine pigtail ", so these three instructions can not be carried out, tail can be abandoned.
Fly-by-wire fixed wing aircraft of the present invention is when aloft getting into danger, the precaution device that is installed in the driving compartment is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed aerial lifesaving button, start abort escape system, signal is through signal transmssion line transmission and control wing, tail, nose-gear, fuselage top parachute hatchcover, tail parachute hatchcover, fuselage bottom air bag hatchcover, the explosive bolt blast of fuselage side lower part air bag hatchcover, moment is opened hatchcover, excite airbag aeration simultaneously, the rocket launching of fuselage top parachute compartment and tail parachute compartment, air bag has sufficient intensity that it can not risen brokenly after the inflation of high-altitude, each cutter cuts off wing respectively behind the time-delay 1s, tail, the cable of nose-gear, so abandon wing, tail, nose-gear, parachute launches rapidly, the resistance that produces is evenly distributed by the umbrella rope on the suspension ring that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage is the steadily slow safe landing or the landing water surface under parachute and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.
Fly-by-wire fixed wing aircraft of the present invention is in danger when in ground taxi, the precaution device that is installed in the driving compartment is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed ground lifesaving button, start abort escape system, signal is through signal transmssion line transmission and control wing, nose-gear, fuselage top parachute hatchcover, tail parachute hatchcover, fuselage bottom air bag hatchcover, the explosive bolt blast of fuselage side lower part air bag hatchcover, moment is opened hatchcover, excite airbag aeration simultaneously, the rocket launching of fuselage top parachute compartment and tail parachute compartment, each cutter cuts off nose-gear respectively behind the time-delay 1s, the cable of wing, so abandon wing, nose-gear, parachute launches rapidly, the resistance that produces is evenly distributed by the umbrella rope on the suspension ring that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage steadily slowly stops safely under parachute and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.In this ground safe life-saving system because the iris action of unidirectional transmission unit such as optic coupler, diode etc., signal can not transfer to " blast of tail explosive bolt, time-delay 1s cutting machine pigtail ", so these two instructions can not be carried out, tail can be abandoned.
Mechanical manoeuvring system heligyro of the present invention is when aloft getting into danger, the precaution device that is installed in the driving compartment is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed aerial lifesaving button, start abort escape system, signal leads to the explosive bolt of tail and control link thereof through signal transmssion line transmission and control, fuselage bottom air bag hatchcover, the explosive bolt blast of fuselage side lower part air bag hatchcover, moment is opened hatchcover, excite airbag aeration, cutter cuts off the cable of tail behind the time-delay 1s, excite the fuselage bottom rocket launching simultaneously, time-delay 2s excites the rocket launching of fuselage top parachute compartment, comprises fuselage top driving engine and the screw propeller that constitutes one with tail so abandon tail, and fuselage hightails tail, parachute can not got to by screw propeller, parachute launches rapidly, and the resistance of generation is evenly distributed by the umbrella rope on the suspension ring that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage is the steadily slow safe landing or the landing water surface under parachute and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.
Fly-by-wire heligyro of the present invention is when aloft getting into danger, the precaution device that is installed in the driving compartment is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed aerial lifesaving button, start abort escape system, signal is through signal transmssion line transmission and control tail, fuselage bottom air bag hatchcover, the explosive bolt blast of fuselage side lower part air bag hatchcover, moment is opened hatchcover, excite airbag aeration, cutter cuts off the cable of tail behind the time-delay 1s, excite the fuselage bottom rocket launching simultaneously, time-delay 2s excites the rocket launching of fuselage top parachute compartment, comprises fuselage top driving engine and the screw propeller that constitutes one with tail so abandon tail, and fuselage hightails tail, parachute can not got to by screw propeller, parachute launches rapidly, and the resistance of generation is evenly distributed by the umbrella rope on the suspension ring that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage is the steadily slow safe landing or the landing water surface under parachute and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.
(3) beneficial effect
The present invention is wing; tail; nose-gear is designed to and can separates the form of abandoning fully with fuselage; the medium or large passenger plane main cabin is designed to two-layer at least channel shape floor; body weight has been alleviated greatly; be suitable for all large, medium and small aircrafts; comprise fixed wing aircraft and autogiro; fuselage top and tail are provided with parachute; fuselage bottom and two side lower parts are provided with air bag; the heligyro fuselage bottom is provided with rocket; fuselage steady slowly safe falling or stop under parachute and air bag effect; air bag can also make fuselage float on the water surface; so just make driver and crew thoroughly break away from fuel fire and blast threat, effectively ensure driver and crew's safety, can effectively protect fuselage in addition; some valuable equipments can be utilized again, even fuselage also can utilize again.
Four, description of drawings
Fig. 1 is an aircraft lateral plan of the present invention;
Fig. 2 is an aircraft birds-eye view of the present invention;
Fig. 3 is a fuselage top parachute compartment lateral plan;
Fig. 4 is the two-layer main cabin of a present invention cross sectional drawing;
Fig. 5 is three layers of main cabin cross sectional drawing of the present invention;
Fig. 6 is a heligyro lateral plan of the present invention;
Fig. 7 is a mechanical manoeuvring system fixed wing aircraft abort escape system order drawing of the present invention;
Fig. 8 is a fly-by-wire fixed wing aircraft abort escape system order drawing of the present invention;
Fig. 9 is a mechanical manoeuvring system heligyro abort escape system order drawing of the present invention;
Figure 10 is a fly-by-wire heligyro abort escape system order drawing of the present invention.
Among the figure: 1, precaution device, 2, the emergency survival button, 3, signal transmssion line, 4, wing, 5, alighting gear, 6, tail, 7, fuselage top parachute compartment, 8, the tail parachute compartment, 9, the main cabin, 10, driving compartment, 11, fuselage bottom air bag cabin, 12, fuselage side lower part air bag cabin, 13, explosive bolt, 14, fuselage top suspension ring, 15, the umbrella rope, 16, driving engine, 17, helicopter fuselage top parachute compartment, 18, rocket, 19, parachute sleeve, 20, parachute, 21, the main cabin bulkhead, 22, the seat, 23, pillar, 24, the floor, 25, the aisle, 26, unidirectional transmission unit.
Five, the specific embodiment
The two-layer channel shape of embodiment 1 Medium Plane floor:
According to Fig. 4, the present invention adopts two-layer channel shape floor (24) to Medium Plane, and under the same situation of main cabin (9) length, seating capacity is increased to the twice of common one deck aircraft seat number; If seating capacity is identical, then the two-layer aircraft of the present invention has reduced half than common one deck aircraft passenger compartment (9) length, main cabin (9) weight saving near half.Seat (22) can be by laterally putting, also can be by vertically putting, and the outside, both sides, upper strata is a child seat, pillar (23) is used to support upper floor (24).Same seat figure place aircraft weight of the present invention can alleviate manyly than existing conventional airplane like this, and this just also can use parachute (20) and air bag to carry out safe life-saving to have created condition for Medium Plane, has also reduced fuel oil consumption and cost simultaneously.
Three layers of channel shape of embodiment 2 large aircrafts floor:
According to Fig. 5, the present invention adopts three layers of channel shape floor (24) to large aircraft, and under the same situation of main cabin (9) length, seating capacity is increased to nearly three times of common one deck aircraft seat number; If seating capacity is identical, then three layers of aircraft of the present invention reduced than common one deck aircraft passenger compartment (9) length nearly 2/3rds, main cabin (9) weight saving nearly 2/3rds.Seat (22) can be by laterally putting, also can be by vertically putting, and the outside, both sides, upper strata is a child seat, pillar (23) is used to support upper floor (24).Same seat figure place aircraft weight of the present invention can alleviate manyly than existing conventional airplane like this, and this also also can use parachute (20) and air bag to carry out safe life-saving to have created condition for large aircraft, has also reduced fuel oil consumption and cost simultaneously.
According to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, shown in Figure 7, mechanical manoeuvring system fixed wing aircraft of the present invention is when aloft getting into danger, the precaution device (1) that is installed in the driving compartment (10) is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed aerial lifesaving button (2), start abort escape system, signal leads to wing (4) through signal transmssion line (3) transmission and control, tail (6), the explosive bolt of the control link of nose-gear (5) and wing (4), tail (6), nose-gear (5), fuselage top parachute compartment (7) hatchcover, tail parachute compartment (8) hatchcover, fuselage bottom air bag cabin (11) hatchcover, the explosive bolt blast of fuselage side lower part air bag cabin (12) hatchcover, moment is opened hatchcover, excite airbag aeration simultaneously, the rocket launching of fuselage top parachute compartment (7) and tail parachute compartment (8), each cutter cuts off wing (4) respectively behind the time-delay 1s, tail (6), the cable of nose-gear (5), so abandon wing (4), tail (6), nose-gear (5), parachute (20) launches rapidly, the resistance that produces is evenly distributed by the umbrella rope (15) on the suspension ring (14) that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage is the steadily slow safe landing or the landing water surface under parachute (20) and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.Fixed wing aircraft also can not abandoned nose-gear (5); Light fixed-wing aircraft also can not abandoned tail (6).
According to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, shown in Figure 7, mechanical manoeuvring system fixed wing aircraft of the present invention is in danger when in ground taxi, the precaution device (1) that is installed in the driving compartment (10) is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed ground lifesaving button (2), start abort escape system, signal leads to wing (4) through signal transmssion line (3) transmission and control, the explosive bolt of the control link of nose-gear (5) and wing (4), nose-gear (5), fuselage top parachute compartment (7) hatchcover, tail parachute compartment (8) hatchcover, fuselage bottom air bag cabin (11) hatchcover, the explosive bolt blast of fuselage side lower part air bag cabin (12) hatchcover, moment is opened hatchcover, excite airbag aeration simultaneously, fuselage top parachute compartment (7), the rocket launching of tail parachute compartment (8), each cutter cuts off wing (4) respectively behind the time-delay 1s, the cable of nose-gear (5), so abandon wing (4), nose-gear (5), parachute (20) launches rapidly, the resistance that produces is evenly distributed by the umbrella rope (15) on the suspension ring (14) that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage steadily slowly stops safely under parachute (20) and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.Fixed wing aircraft also can not abandoned nose-gear (5).
According to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, shown in Figure 8, fly-by-wire fixed wing aircraft of the present invention is when aloft getting into danger, the precaution device (1) that is installed in the driving compartment (10) is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed aerial lifesaving button (2), start abort escape system, signal is through signal transmssion line (3) transmission and control wing (4), tail (6), nose-gear (5), fuselage top parachute compartment (7) hatchcover, tail parachute compartment (8) hatchcover, fuselage bottom air bag cabin (11) hatchcover, the explosive bolt blast of fuselage side lower part air bag cabin (12) hatchcover, moment is opened hatchcover, excite airbag aeration simultaneously, the rocket launching of fuselage top parachute compartment (7) and tail parachute compartment (8), each cutter cuts off wing (4) respectively behind the time-delay 1s, tail (6), the cable of nose-gear (5), so abandon wing (4), tail (6), nose-gear (5), parachute (20) launches rapidly, the resistance that produces is evenly distributed by the umbrella rope (15) on the suspension ring (14) that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage is the steadily slow safe landing or the landing water surface under parachute (20) and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.Fixed wing aircraft also can not abandoned nose-gear (5); Light fixed-wing aircraft also can not abandoned tail (6).
According to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, shown in Figure 8, fly-by-wire fixed wing aircraft of the present invention is in danger when in ground taxi, the precaution device (1) that is installed in the driving compartment (10) is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed ground lifesaving button (2), start abort escape system, signal is through signal transmssion line (3) transmission and control wing (4), nose-gear (5), fuselage top parachute compartment (7) hatchcover, tail parachute compartment (8) hatchcover, fuselage bottom air bag cabin (11) hatchcover, the explosive bolt blast of fuselage side lower part air bag cabin (12) hatchcover, moment is opened hatchcover, excite airbag aeration simultaneously, the rocket launching of fuselage top parachute compartment (7) and tail parachute compartment (8), each cutter cuts off wing (4) respectively behind the time-delay 1s, the cable of nose-gear (5), so abandon wing (4), nose-gear (5), parachute (20) launches rapidly, the resistance that produces is evenly distributed by the umbrella rope (15) on the suspension ring (14) that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage steadily slowly stops safely under parachute and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.Fixed wing aircraft also can not abandoned nose-gear (5).
Embodiment 7 mechanical manoeuvring system heligyroes:
According to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, shown in Figure 9, mechanical manoeuvring system heligyro of the present invention is when aloft getting into danger, the precaution device (1) that is installed in the driving compartment (10) is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed aerial lifesaving button (2), start abort escape system, signal leads to the explosive bolt of tail (6) and control link thereof through signal transmssion line (3) transmission and control, fuselage bottom air bag (11) hatchcover, the explosive bolt blast of fuselage side lower part air bag cabin (12) hatchcover, moment is opened hatchcover, excite airbag aeration, cutter cuts off the cable of tail (6) behind the time-delay 1s, excite fuselage bottom retro-rocket (18) emission simultaneously, time-delay 2s excites the rocket launching of fuselage top parachute compartment (17), comprise fuselage top driving engine and the screw propeller that constitutes one with tail (6) so abandon tail (6), fuselage hightails tail (6), parachute can not got to by screw propeller, parachute (20) launches rapidly, at this moment parachute can not got to by screw propeller, the resistance that produces is evenly distributed by the umbrella rope (15) on the suspension ring (14) that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage is the steadily slow safe landing or the landing water surface under parachute (20) and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.
According to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, shown in Figure 10, fly-by-wire heligyro of the present invention is when aloft getting into danger, the precaution device (1) that is installed in the driving compartment (10) is reported to the police, chaufeur is examined and is judged dangerous situation, if airplane crash is inevitable, chaufeur is just pressed aerial lifesaving button (2), start abort escape system, signal is through signal transmssion line (3) transmission and control tail (6), fuselage bottom air bag cabin (11) hatchcover, the explosive bolt blast of fuselage side lower part air bag cabin (12) hatchcover, moment is opened hatchcover, excite airbag aeration, cutter cuts off the cable of tail (6) behind the time-delay 1s, excite fuselage bottom retro-rocket (18) emission simultaneously, time-delay 2s excites the rocket launching of fuselage top parachute compartment (17), comprises fuselage top driving engine and the screw propeller that constitutes one with tail so abandon tail (6), and fuselage hightails tail (6), parachute can not got to by screw propeller, parachute (20) launches rapidly, and the resistance of generation is evenly distributed by the umbrella rope (15) on the suspension ring (14) that are fixed on the fuselage different parts, makes the stable deceleration of fuselage.Fuselage is the steadily slow safe landing or the landing water surface under parachute (20) and air bag effect, thereby reaches the safe life-saving purpose, effectively ensures driver and crew and fuselage safety.
Claims (2)
1, safety lifesaving airplane, it is characterized in that forming by wing (4), tail (6), nose-gear (5), parachute (20), fuselage, air bag, manipulation, eight system in combination such as electric, big-and-middle-sized aircraft passenger compartment (9) adopts two-layer at least channel shape floor (24), seat (22) can laterally be put, also can vertically put, other system is the same with conventional airplane, is suitable for large, medium and small aircraft, comprises fixed wing aircraft and autogiro.Press aerial lifesaving button when the aircraft distress airplane crash is inevitable aloft, press ground lifesaving button on ground, leading to wing (4), tail (6), the explosive bolt (13) of the control link of nose-gear (5), be used for fixing wing (4), tail (6), nose-gear (5), fuselage top parachute compartment (7) hatchcover, tail parachute compartment (8) hatchcover, fuselage bottom air bag cabin (11) hatchcover, the explosive bolt (13) of fuselage side lower part air bag cabin (12) hatchcover is ignited, leading to wing (4), tail (6), the cable cutting of nose-gear (5), excite airbag aeration, the rocket (18) of fuselage top parachute compartment (7) and tail parachute compartment (8), heligyro fuselage bottom rocket (18) emission, so just abandoned wing (4), tail (6), nose-gear (5), fuselage steady slowly safe falling or stop under parachute (20) and air bag effect effectively ensures driver and crew and fuselage safety.Fixed wing aircraft also can not abandoned nose-gear (5), do not abandon tail (6) in the middle of ground taxi; Light fixed-wing aircraft also can not abandoned tail (6).
2, safety lifesaving airplane according to claim 1, it is characterized in that aerial lifesaving button is in parallel with ground lifesaving button, and be provided with unidirectional transmission unit (26) between instruction on signal transmssion line " blast of tail explosive bolt, time-delay 1s cutting machine pigtail; the mechanical manoeuvring system fixed wing aircraft comprises the blast of empennage control link explosive bolt " and other instruction, signal can only pass to other instruction from above instruction, can not reverse transfer, after guaranteeing the starting ground life saving system, do not abandon tail (6).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2007101545299A CN101391654A (en) | 2007-09-21 | 2007-09-21 | Safety lifesaving airplane |
| PCT/CN2008/072448 WO2009039787A1 (en) | 2007-09-21 | 2008-09-22 | Safety rescue aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2007101545299A CN101391654A (en) | 2007-09-21 | 2007-09-21 | Safety lifesaving airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101391654A true CN101391654A (en) | 2009-03-25 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2007101545299A Pending CN101391654A (en) | 2007-09-21 | 2007-09-21 | Safety lifesaving airplane |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN101391654A (en) |
| WO (1) | WO2009039787A1 (en) |
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| GR1003755B (en) * | 2000-03-31 | 2002-01-15 | Aircraft with detachable cabin equipped with shock-absorbing parachutes-airbags-seats and conventional aircraft equipped with said safety systems | |
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