CN102126557A - Aerial emergency life saving system for passenger plane - Google Patents
Aerial emergency life saving system for passenger plane Download PDFInfo
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- CN102126557A CN102126557A CN2011100095582A CN201110009558A CN102126557A CN 102126557 A CN102126557 A CN 102126557A CN 2011100095582 A CN2011100095582 A CN 2011100095582A CN 201110009558 A CN201110009558 A CN 201110009558A CN 102126557 A CN102126557 A CN 102126557A
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- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 4
- 239000001301 oxygen Substances 0.000 claims description 4
- 229910052760 oxygen Inorganic materials 0.000 claims description 4
- 230000029058 respiratory gaseous exchange Effects 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 4
- 238000009434 installation Methods 0.000 claims description 3
- 230000001012 protector Effects 0.000 claims description 3
- 230000003111 delayed effect Effects 0.000 claims description 2
- 230000000994 depressogenic effect Effects 0.000 claims description 2
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- 241000272525 Anas platyrhynchos Species 0.000 abstract 2
- 230000000694 effects Effects 0.000 description 3
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 description 2
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- 230000032258 transport Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000009194 climbing Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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- 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
- B64D25/12—Ejectable capsules
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- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
- Motorcycle And Bicycle Frame (AREA)
Abstract
The invention relates to an aerial emergency life saving system for a passenger plane and belongs to the field of aviation. The invention aims to ensure that a passenger can escape safely during the emergency of the passenger plane, and the aerial emergency life saving system is dual-use. The technical scheme adopted by the invention is that: the conventional chicken beak-shaped tail of the passenger plane is changed into a duck bill-shaped tail or a dovetailed tail; the conventional single vertical fin is changed into two vertical fins; a life saving exit is formed at the proper position above the duck bill-shaped tail or in the middle of the dovetailed tail; a plurality of I-shaped tracks which have teeth and are parallel to each other are arranged in the machinery room of the passenger plane; the conventional two rows or three rows of seats are combined into a row of seats; and two sides are provided with aisles; multi-functional life saving seats are connected in parallel by taking rows as a unit, fixed on the track through a large pulley, a gear and a positioner, and triggered and started through a trigger and get out of the plane, and a parachute is opened for escape.
Description
Technical field: the present invention relates to aviation field, be used for large-scale passenger aeroplane inflight emergency life saving system.
Background technology: at present known big-and-middle-sized passenger aeroplane has become people's requisite vehicle rapidly and efficiently of going on a journey, higher relatively than other vehicle safety factor, yet air crash also happens occasionally, aircraft is not method once the something unexpected happened consequence is very miserable up to also having actv. to solve at present.
Summary of the invention: the objective of the invention is to be passenger aeroplane 1 design one cover actv. life saving system, when emergency situation takes place passenger aeroplane 1, make the passenger can safe escape, and can be dual-use.
The technical solution used in the present invention is: passenger aeroplane 1 traditional chicken mouth shape tail is designed to duckbill tail 2 or dovetail form tail 3, traditional single vertical fin (yaw rudder) is designed to twin vertical fin 4, promptly two at duckbill tail 2 or dovetail form tail 3 respectively establish one, just formed a Wheelchair Accessible in the centre of twin vertical fin 4 like this, lifesaving outlet 5 is offered in the centre of appropriate location or dovetail form tail 3 above duckbill tail 2, lifesaving door 6 is by electric liquid actuator 12 automatically retractable closures, in the cabin of passenger aeroplane 1, establish many parallel toothed I-shape tracks 14 arranged side by side, from the straight-through lifesaving outlet 5 of cockpit, become one to be listed as the cabin middle part of putting side by side the form of two traditional row or three row seats with passenger aeroplane 1, both sides are made as aisle 13, multifunctional lifesaving seat 23 is that unit is connected in parallel with row, be fixed on the track 14 by pulley 43 and gear 44 and steady arm 16, trigger to start by binary pair 22 and deliver from godown and the parachute-opening escape.
The triggering system and the installation method of multifunctional lifesaving seat 23 are: the end of the arm of force 18 that will reset is stuck on the hook of file protect 19, file protect 19 is attached on the binary pair 22 by flexible axle backguy 21, the binary pair 22 of passenger aeroplane 1 afterbody first row's multifunctional lifesaving seat 23 is installed to the appropriate location of lifesaving outlet 5, so that lifesaving door 6 triggers first row's Lifesaving chair 23 when opening, the binary pair 22 of second series multifunctional lifesaving seat 23 is installed to first row 1.5 meters, multifunctional lifesaving seat 23 back, the binary pair 22 of the 3rd row's multifunctional lifesaving seat 23 is installed in steady arm shell 15 fronts of first row's multifunctional lifesaving seat 23, by that analogy all binary pairs 22 are installed, multifunctional lifesaving seat 23 with regard to energy and last row draws back a safety distance after each row's multifunctional lifesaving seat 23 starts like this, and the multifunctional lifesaving seat 23 top steady arm shells 15 that the binary pair 22 of front one row's multifunctional lifesaving seat 23 is arranged by back one trigger.
Lifesaving outlet 5 is designed to oblong, and be provided with the groove that can play airtight effect, the size of lifesaving outlet 5 is can easily being advisable by row's multifunctional lifesaving seat 23, on the inwall of lifesaving outlet 5, a plurality of file protects 8 are installed, each file protect 8 closely links to each other by connecting rod 10 and is attached on the electric liquid actuator 12, the master cock of electricity liquid actuator 12 is located on the operator's station of chaufeur, when chaufeur is opened master cock, electricity liquid actuator 12 can be opened file protect 8, lifesaving door 6 just can be opened, appropriate location in lifesaving outlet 5 is equipped with binary pair 22, and when lifesaving door 6 was opened, binary pair 22 just can be triggered.Multifunctional lifesaving seat 23 is started at once.
Triggering system is made up of binary pair 22, flexible axle backguy 21, file protect 19, the arm of force 18 that resets, steady arm 16, steady arm shell 15, starting switch 17.Wherein binary pair 22, flexible axle backguy 21, file protect 19 are fixed on the track 14, and file protect 19 then is the parts that can control the arm of force 18 that resets of 14 two on track simultaneously; The arm of force 18 that resets be by retracing spring work done device on multifunctional lifesaving seat 23; Steady arm 16 and starting switch 17 devices are in steady arm shell 15,17 devices of starting switch are below steady arm 16, steady arm shell 15 devices are on multifunctional lifesaving seat 23, the arm of force of steady arm 16 is stuck in the draw-in groove of the arm of force 18 that resets, the end of the arm of force 18 of resetting is stuck on the hook of file protect 19, and file protect 19 is attached on the binary pair 22 by flexible axle backguy 21; Binary pair 22 is once be triggered and just can spur file protect 19 and separate with the arm of force 18 that resets, the arm of force 18 that resets is depressed steady arm 16 at once and is dropped on above the starting switch 17, make starting switch 17 energisings and starter motor 53 is started, multifunctional lifesaving seat 23 separates with track 14 simultaneously.
The power supply of starting switch 17 is attached at above the high ferro cell group 55, the other end is attached at above the close switch 52, the other end of close switch 52 is attached at above the starter motor 53, close switch 52 and controller 51 devices are on the underframe 24 of multifunctional lifesaving seat 23, controller 51 is made up of the arm of force, pulley and retracing spring, pulley action is on track 14, once the pulley of controller 51 and track 14 break away from, controller 51 just can be by action of reset spring on close switch 52, the power supply of close switch 52 is disconnected, make starter motor 53 stalls.
Leg pressing then is installed in the handrail on underframe 24 both sides protects frame 28, it is the Safety protectors that manually draw back auto-closing by teeth steady arm and retracing spring that frame 28 is protected in leg pressing, which is provided with control handle 29, the effect that frame 28 is protected in leg pressing is to make the passenger be unlikely to be thrown out of multifunctional lifesaving seat 23 when the unexpected something unexpected happened of passenger aeroplane 1; Air bag 38, high ferro cell group 55, intelligent charger 54 and starter motor 53 are installed in the bottom of underframe 24, wherein starter motor 53 is installed near track 14 first, can start automatically and the charger of disconnection and constant pressure and flow and intelligent charger 54 is one, and be installed in power lead on the track 14 by latch and socket UNICOM; The long handrail upper end first of underframe 24 is provided with a retractable pallet 27, front end is provided with big hinge 25, underframe 24 connects together by big hinge 25, and can opening and closing, the teeth steady arm 26 of a band retracing spring is housed in the bottom of big hinge 25, can makes and open automatically between the underframe 24 and locate.
Bayonet lock carriage 45 and bayonet lock 47 are installed in the rear end of the handrail that big hinge 25 is installed, bayonet lock carriage 45 is installed on first the handrail, tied up stabilizing spring on the bayonet lock 47 and be installed on the bayonet lock carriage 45, hook 48 is installed on the handrail of opposite side, two underframe 24 just had been connected in parallel on together when hook 48 passed from bayonet lock carriage 45 and blocked by bayonet lock 47, bayonet lock 47 will be linked up with 48 two underframe 24 when decontroling and just can open automatically and block by big hinge 25 and teeth steady arm 26, bayonet lock carriage 45 and bayonet lock 47 and link up with 48 and respectively adorn a cover up and down, bayonet lock 47 is attached on the file protect 49 that is contained in the handrail nock by flexible axle backguy 21, the other end of file protect 49 is attached on the umbrella rope 40, when the 40 stressed tensions of umbrella rope, file protect 49 just can will link up with 48 releases with bayonet lock 47 pulling by flexible axle backguy 21, and underframe 24 just can open automatically and locatees by Da He page or leaf 25 and teeth steady arm 26.
Every row's multifunctional lifesaving seat 23 is divided into two groups, every group by big hinge 25 and bayonet lock carriage 45 bayonet locks 47 and link up with 48 and be connected in parallel, binding between two groups is solid with same method binding and pin, and bayonet lock 47 is attached at above the file protect 49 by flexible axle backguy 21.Multifunctional lifesaving seat 23 also can be designed to other pattern under the situation that function does not subtract, power also can adopt other power, as adopting high-pressure gas cylinder and pneumatics starter motor etc.; When being installed to multifunctional lifesaving seat 23 on the track 14, should keep certain distance, in case multifunctional lifesaving seat 23 is having on because of the floor article influence normally not pass through after the startup with the floor; Multifunctional lifesaving seat 23 is that unit one goes out a row with row when startup is delivered from godown; other followed by rushing out as domino; whole passengers that approximately need about 30 seconds large-scale passenger aeroplanes 1 and aviator's the lifesaving process that delivers from godown just can be finished; when the escape parachute 39 of each row's multifunctional lifesaving seat 23 is opened; each row's multifunctional lifesaving seat 23 promptly can be by device at the bayonet lock carriage 45 and the bayonet lock 47 of midway location and link up with 48 and separately become two groups; every group of multifunctional lifesaving seat 23 opens automatically by big hinge 25 and teeth steady arm 26 and locatees; so just make every group of multifunctional lifesaving seat 23 be encircled into a cast aloft automatically; the device thereon air bag 38 will the success the safety guard-safeguard effect of playing; anticollision floats safely in water on land.
The life saving system operation of this passenger aeroplane 1 is very simple, when passenger aeroplane 1 aloft is in an emergency, as long as the aviator is the starting switch on the push platform, the electric liquid actuator 12 of device on lifesaving outlet 5 and lifesaving door 6 just can start, lifesaving door 6 just can be opened and the binary pair 22 of flip flop equipment on lifesaving door 5, and binary pair 22 just can be opened file protect 19 by flexible axle backguy 21 multifunctional lifesaving seat 23 is started; And the passenger need only protect frame 32 and press leg is fixed consolidating leg, buckles safety strap 35 and safty shield 36 left behind and put on oxygen breathing apparatus and get final product.This life saving system all can effectively be implemented at basic, normal, high sky.
The life saving system of passenger aeroplane 1 of the present invention possesses two kinds of functions of civil and military simultaneously, promptly can emergency survival when civilian passenger flight, can transport the parachutist in army's time spent, also can be designed to different patterns and function according to different purposes, as: multifunctional lifesaving seat 23 is designed to shelf transports and throw in goods and materials, or be designed to the bomb fixed mount and load onto aerial bomb and use as bomber.When throwing in parachutist or goods and materials or bomb in army's time spent, passenger aeroplane 1 can be done 45 simultaneously and spend the action of climbing, whole like this launch process just can easily beautiful finishing, and so just makes large-scale passenger aeroplane 1 become military transportation airplane, the bomber of safeguarding without military expenditure.
The invention has the beneficial effects as follows: make people safer when taking advantage of aircraft, can save writing for national defense construction simultaneously and open money.
Description of drawings:
Fig. 1 is the afterbody sectional side elevation that front view Fig. 2 of the present invention is Fig. 1
Fig. 3 is that section plan Fig. 4 of Fig. 1 is a dovetail form passenger aeroplane of the present invention
Fig. 5 is that lateral plan Fig. 6 of lifesaving outlet and lifesaving door is the planar view of Fig. 5
Fig. 7 is that track and triggering system view Fig. 8 are the multifunctional lifesaving seats
Fig. 9 is that back view Figure 10 of Fig. 8 is Fig. 8's and connect method
Figure 11 is that lateral plan Figure 12 of Figure 10 is the front section view of Fig. 8
Figure 13 is that sectional side view Figure 14 of Fig. 8 is that triggering system is installed view
Figure 15 is that embodiments of the invention 1 Figure 16 is embodiments of the invention 2
Among the figure: the 1st, passenger aeroplane, the 2nd, the duckbill tail, the 3rd, the dovetail form tail, the 4th, twin vertical fin, the 5th, the lifesaving outlet, the 6th, the lifesaving door, the 7th, hinge, the 8th, file protect, 9 is enlarged drawings of 8, the 10th, connecting rod, the 11st, hook, the 12nd, electric liquid actuator, the 13rd, the aisle, the 14th, track, the 15th, the steady arm shell, the 16th, steady arm, the 17th, starting switch, the 18th, the arm of force resets, the 19th, file protect, 20 is front elevations of 19, the 21st, the flexible axle backguy, the 22nd, binary pair, the 23rd, the multifunctional lifesaving seat, the 24th, underframe, the 25th, big hinge, the 26th, the teeth steady arm, the 27th, pallet, the 28th, frame is protected in leg pressing, the 29th, the control handle, the 30th, carriage, the 31st, stretcher, the 32nd, solid leg protects frame, the 33rd, the control handle, the 34th, seat cushion, the 35th, safety strap, the 36th, safty shield, the 37th, the teeth steady arm, the 38th, air bag, the 39th, escape parachute, the 40th, the umbrella rope, the 41st, link, the 42nd, throw the umbrella rifle, the 43rd, pulley, the 44th, gear, the 45th, the bayonet lock carriage, 46 is enlarged drawings of 45, the 47th, bayonet lock, the 48th, hook, the 49th, file protect, the 50th, starting switch, the 51st, controller, the 52nd, close switch, the 53rd, starter motor, the 54th, intelligent charger, the 55th, the high ferro cell group.
Specific implementation method: embodiment 1, as Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, Fig. 7, Figure 15, the first step, at first the chicken mouth shape tail with passenger aeroplane 1 is designed to duckbill tail 2 or dovetail form tail 3, and yaw rudder is set in the both sides of duckbill tail 2 or dovetail form tail 3, it is twin vertical fin 4, offer lifesaving outlet 5 and lifesaving door 6 in the appropriate location, top of duckbill tail 2 or the centre of dovetail form tail 3, so just make multifunctional lifesaving seat 23 when promptly delivering from godown parachute-opening unblocked with toothed I-shape track 14 according to need quantity at interval suitably distance be installed in parallel in the cabin middle part of passenger aeroplane 1 side by side, both sides are set to aisle 13, and two tracks 14 of centre are communicated with cockpits, the end of track 14 is designed to corresponding shape and is communicated with the lifesaving outlet 5. starting switch device appropriate locations on the operator's station of cockpit with electric liquid actuator 12 according to the concrete structure of duckbill tail 2 or dovetail form tail 3.
Second step, as Fig. 8, Fig. 9, Figure 10, Figure 11, Figure 12, Figure 13, Figure 15, with the multifunctional lifesaving seat 23 that assembles by big hinge 25 and bayonet lock carriage 45 bayonet locks 47 and link up with 48 and be parallel to together, removing controller 51 row's multifunctional lifesaving seat 23 that parallel connection is good with hand then penetrates from the end of track 14, and multifunctional lifesaving seat 23 is shifted onto the position of pre-installation, by that analogy, each row's multifunctional lifesaving seat 23 all is through on the track 14.
The 3rd step, as Fig. 5, Fig. 6, Fig. 7, Figure 10, Figure 11, Figure 12, Figure 14,19 flexible axle backguys 21 of erection insurance device and binary pair 22, the end that is installed in the arm of force 18 that resets on multifunctional lifesaving seat 23 underframe 24 is stuck on the hook of file protect 19, make like this reset the arm of force 18 with steady arm 16 lever up with track 14 on teeth withstand on together, thereby multifunctional lifesaving seat 23 is fixed on the track 14, the binary pair 22 of passenger aeroplane 1 last row's multifunctional lifesaving seat 23 is installed in the appropriate location of lifesaving outlet, when being opened, the lifesaving door is triggered, power supply with starting switch 17 and starting switch 50 is attached on the Wiring terminal of high ferro cell group 55 at last, and the latch of intelligent charger 54 is inserted device on the battery socket on the track 14.
Embodiment 2: as Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, Fig. 7, Fig. 8, Fig. 9, Figure 10, Figure 11, Figure 12, Figure 14, Figure 15, Figure 16, when passenger aeroplane 1 aloft is in an emergency, because leg pressing is protected frame 28 and the passenger is pressed in above the multifunctional lifesaving seat 23 can be thrown out of, need only want the passenger will consolidate leg with hand protects frame 32 and presses the leg fixed bit, safety strap 35 is fastened, again safty shield 36 is left behind and put on oxygen breathing apparatus, chaufeur is pressed lifesaving door 6 with starting switch and just is opened at once and touches binary pair 22 multifunctional lifesaving seat 23 is started, multifunctional lifesaving seat 23 is rushed out by the order of setting, when the controller 51 on the underframe 24 of device at multifunctional lifesaving seat 23 de-orbits 14 the time, controller 51 just can be pressed on the starting switch 50, throw simultaneously umbrella rifle 42 just can switch on the outburst escape parachute 39 is pulled out, and air bag 38 also can be switched on and delay time and broken out in two seconds, the bayonet lock 47 that installs simultaneously at row's multifunctional lifesaving seat 23 middle parts also can discharge hook 48, make row's Lifesaving chair 23 be divided into two groups and surround two casts automatically from the centre by big hinge page or leaf 25 and teeth steady arm 26, simultaneously controller 51 also can de-orbit and 14 impact make starter motor 53 outage and stalls on close switch 52. multifunctional lifesaving seat 23 subsequently just can by safety drop to ground or waterborne, dress signal projector thereon just can send an SOS by frequency preset.
This life saving system is applicable to the individual layer passenger aeroplane, also is applicable to double-deck passenger aeroplane simultaneously.
Claims (7)
1. passenger aeroplane inflight emergency life saving system, it is characterized in that passenger aeroplane 1 traditional chicken mouth shape tail is designed to duckbill tail 2 or dovetail form tail 3, traditional single vertical fin (yaw rudder) is designed to twin vertical fin 4, promptly respectively establish one in the both sides of duckbill tail 2 or dovetail form tail 3, lifesaving outlet 5 is offered in the centre of appropriate location or dovetail form tail 3 above duckbill tail 2, lifesaving door 6 is by electric liquid actuator 12 automatically retractable closures, in the cabin of passenger aeroplane 1, establish many parallel toothed I-shape tracks 14 arranged side by side, from the straight-through lifesaving outlet 5 of cockpit, become one to be listed as the cabin middle part of putting side by side the form of two traditional row or three row seats with passenger aeroplane 1, both sides are made as aisle 13, multifunctional lifesaving seat 23 is that unit is connected in parallel with row, be fixed on the track 14 by pulley 43 and gear 44 and steady arm 16, start the also parachute-opening escape of delivering from godown by binary pair 22 triggerings, multifunctional lifesaving seat 23 also can be designed to different patterns and function according to different purposes.
2. according to claim 1 described a kind of passenger aeroplane inflight emergency life saving system, the installation method that it is characterized in that binary pair 22 is, the end of the arm of force 18 of will resetting is stuck on the hook of file protect 19, file protect 19 is attached on the binary pair 22 by flexible axle backguy 21, the binary pair 22 of passenger aeroplane 1 afterbody first row's multifunctional lifesaving seat 23 is installed to the appropriate location of lifesaving outlet 5, the binary pair 22 of second series multifunctional lifesaving seat 23 is installed to first row 1.5 meters, multifunctional lifesaving seat 23 back, the binary pair 22 of the 3rd row's multifunctional lifesaving seat 23 is installed in steady arm shell 15 fronts of first row's multifunctional lifesaving seat 23, by that analogy all binary pairs 22 are installed, multifunctional lifesaving seat 23 with regard to energy and last row draws back a safety distance after each row's multifunctional lifesaving seat 23 starts like this, and the multifunctional lifesaving seat 23 top steady arm shells 15 that the binary pair 22 of front one row's multifunctional lifesaving seat 23 is arranged by back one trigger.
3. according to claim 1 described a kind of passenger aeroplane inflight emergency life saving system, the triggering system that it is characterized in that binary pair 22 is by binary pair 22, flexible axle backguy 21, file protect 19, the arm of force 18 resets, steady arm 16, steady arm shell 15, starting switch 17 is formed, wherein binary pair 22, flexible axle backguy 21, file protect 19 is fixed on the track 14, file protect 19 then is the parts that can control the arm of force 18 that resets of 14 two on track simultaneously, the arm of force 18 that resets be by retracing spring work done device on multifunctional lifesaving seat 23, steady arm 16 and starting switch 17 devices are in steady arm shell 15,17 devices of starting switch are below steady arm 16, steady arm shell 15 devices are on multifunctional lifesaving seat 23, the arm of force of steady arm 16 is stuck in the draw-in groove of the arm of force 18 that resets, the end of the arm of force 18 of resetting is stuck on the hook of file protect 19, file protect 19 is attached on the binary pair 22 by flexible axle backguy 21, binary pair 22 is once be triggered and just can spur file protect 19 and separate with the arm of force 18 that resets, the arm of force 18 that resets is depressed steady arm 16 at once and is dropped on above the starting switch 17, makes starting switch 17 energisings and starter motor 58 is started.
4. according to claim 1 described a kind of passenger aeroplane inflight emergency life saving system, the method that it is characterized in that starter motor 53 outages of multifunctional lifesaving seat 23 is, the power supply of starting switch 17 is attached at above the high ferro cell group 55, the other end is attached at above the close switch 52, the other end of close switch 52 is attached at above the starter motor 53, close switch 52 and controller 51 devices are on the underframe 24 of multifunctional lifesaving seat 23, controller 51 is by the arm of force, pulley and retracing spring are formed, pulley action is on track 14, once the pulley of controller 51 and track 14 break away from, controller 51 just can be by action of reset spring on close switch 52, the power supply of close switch 52 is disconnected, make starter motor 53 stalls.
5. according to claim 1 described a kind of passenger aeroplane inflight emergency life saving system, it is characterized in that multifunctional lifesaving seat 23 is one and adopts high ferro cell group 55 and starter motor 53 to be the buoyant apparatus of power, its keystone configuration is divided into seat 23 and underframe 24 two large divisions, escape parachute 39 is installed above the seat 23, throw umbrella rifle 42, safty shield 36, safety strap 35, air bag 38, carriage 30, stretcher 31, in safty shield 36, be provided with oxygen breathing apparatus, and signal projector is installed on the top of backrest, two of carriage 30 solid leg is installed and protects frame 32, leg pressing then is installed in the handrail on underframe 24 both sides protects frame 28, it is the Safety protectors that manually draw back auto-closing by teeth steady arm and retracing spring that frame 28 is protected in leg pressing, which is provided with control handle 29, in the bottom of underframe 24 air bag 38 is installed, high ferro cell group 55, intelligent charger 54 and starter motor 53, the long handrail upper end first of underframe 24 is provided with a retractable pallet 27, front end is provided with big hinge 25, underframe 24 connects together by big hinge 25, the teeth steady arm 26 of a band retracing spring is housed in the bottom of big hinge 25, can make and open automatically between the underframe 24 and locate, the power of multifunctional lifesaving seat 23 also can adopt high-pressure gas cylinder and pneumatics starter motor.
6. according to claim 1 described a kind of passenger aeroplane inflight emergency life saving system, it is characterized in that, the also linked method of multifunctional lifesaving seat 23 is, bayonet lock carriage 45 and bayonet lock 47 are installed in the rear end of the handrail that big hinge 25 is installed, bayonet lock carriage 45 is installed on first the handrail, tied up stabilizing spring on the bayonet lock 47 and be installed on the bayonet lock carriage 45, hook 48 is installed on the handrail of opposite side, two underframe 24 just had been connected in parallel on together when hook 48 passed from bayonet lock carriage 45 and blocked by bayonet lock 47, bayonet lock 47 will be linked up with 48 two underframe 24 when decontroling and just can open automatically and block by big hinge 25 and teeth steady arm 26, bayonet lock carriage 45 and bayonet lock 47 and link up with 48 and respectively adorn a cover up and down, bayonet lock 47 is attached on the file protect 49 that is contained in the handrail nock by flexible axle backguy 21, and the other end of file protect 49 is attached on the umbrella rope 40.
7. according to claim 1 described a kind of passenger aeroplane inflight emergency life saving system, it is characterized in that, the parachute deployment means of multifunctional lifesaving seat 23 is, controller 51 is installed on the handrail of underframe 24, the appropriate location is equipped with starting switch 50 above controller 51, the pulley action of controller 51 is on track 14, when the pulley of controller 51 once de-orbit 14, controller 51 just can impact on starting switch 50, the power supply of starting switch 50 is attached on the high ferro cell group 55, the other end is attached at the electronics of throwing umbrella rifle 42 and draws on the core and the electronics of air bag 38 draws on the core and on the signal projector, it is that the electronics that broke out in two seconds of can delaying time draws core that the electronics of air bag 38 draws core, throwing umbrella rifle 42 just can break out at once escape parachute 39 is pulled out when starting switch 50 starts, air bag 38 also can be delayed time and be opened in two seconds simultaneously, and signal projector just can send an SOS.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110009558 CN102126557B (en) | 2011-01-05 | 2011-01-05 | Aerial emergency life saving system for passenger plane |
| PCT/CN2011/084947 WO2012092826A1 (en) | 2011-01-05 | 2011-12-29 | Aerial emergency life saving system for passenger plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110009558 CN102126557B (en) | 2011-01-05 | 2011-01-05 | Aerial emergency life saving system for passenger plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102126557A true CN102126557A (en) | 2011-07-20 |
| CN102126557B CN102126557B (en) | 2013-12-25 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201110009558 Expired - Fee Related CN102126557B (en) | 2011-01-05 | 2011-01-05 | Aerial emergency life saving system for passenger plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN102126557B (en) |
| WO (1) | WO2012092826A1 (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2012092826A1 (en) * | 2011-01-05 | 2012-07-12 | Zhang Peixia | Aerial emergency life saving system for passenger plane |
| CN104512550A (en) * | 2013-10-08 | 2015-04-15 | 北京科实医学图像技术研究所 | Paradropper |
| CN104590564A (en) * | 2014-11-27 | 2015-05-06 | 北京空间机电研究所 | Buffering airbag active exhaust system low delay detonating control device |
| CN105882982A (en) * | 2014-09-13 | 2016-08-24 | 杨宗福 | A safe airplane |
| CN106680528A (en) * | 2016-12-14 | 2017-05-17 | 中国航空救生研究所 | Method of determining ejection speed of man-seat system |
| CN106828943A (en) * | 2017-03-24 | 2017-06-13 | 蒋昊维 | High altitude escape seat |
| CN106927053A (en) * | 2017-03-24 | 2017-07-07 | 蒋昊维 | Passenger plane high altitude escape system |
| CN107499521A (en) * | 2017-08-23 | 2017-12-22 | 芜湖超源力工业设计有限公司 | A kind of pilot's safety guard |
| CN109018396A (en) * | 2018-07-27 | 2018-12-18 | 宁波光舟通信技术有限公司 | Airborne intelligent system and data processing method thereof |
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Cited By (10)
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| WO2012092826A1 (en) * | 2011-01-05 | 2012-07-12 | Zhang Peixia | Aerial emergency life saving system for passenger plane |
| CN104512550A (en) * | 2013-10-08 | 2015-04-15 | 北京科实医学图像技术研究所 | Paradropper |
| CN105882982A (en) * | 2014-09-13 | 2016-08-24 | 杨宗福 | A safe airplane |
| CN104590564A (en) * | 2014-11-27 | 2015-05-06 | 北京空间机电研究所 | Buffering airbag active exhaust system low delay detonating control device |
| CN106680528A (en) * | 2016-12-14 | 2017-05-17 | 中国航空救生研究所 | Method of determining ejection speed of man-seat system |
| CN106680528B (en) * | 2016-12-14 | 2019-08-13 | 中国航空救生研究所 | A method of judging human seat model ejection speed |
| CN106828943A (en) * | 2017-03-24 | 2017-06-13 | 蒋昊维 | High altitude escape seat |
| CN106927053A (en) * | 2017-03-24 | 2017-07-07 | 蒋昊维 | Passenger plane high altitude escape system |
| CN107499521A (en) * | 2017-08-23 | 2017-12-22 | 芜湖超源力工业设计有限公司 | A kind of pilot's safety guard |
| CN109018396A (en) * | 2018-07-27 | 2018-12-18 | 宁波光舟通信技术有限公司 | Airborne intelligent system and data processing method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102126557B (en) | 2013-12-25 |
| WO2012092826A1 (en) | 2012-07-12 |
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