WO2012092826A1 - 一种载客飞机空中紧急情况救生系统 - Google Patents

一种载客飞机空中紧急情况救生系统 Download PDF

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Publication number
WO2012092826A1
WO2012092826A1 PCT/CN2011/084947 CN2011084947W WO2012092826A1 WO 2012092826 A1 WO2012092826 A1 WO 2012092826A1 CN 2011084947 W CN2011084947 W CN 2011084947W WO 2012092826 A1 WO2012092826 A1 WO 2012092826A1
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WIPO (PCT)
Prior art keywords
tail
trigger
life
seat
rescue
Prior art date
Application number
PCT/CN2011/084947
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English (en)
French (fr)
Inventor
张培霞
Original Assignee
Zhang Peixia
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Filing date
Publication date
Application filed by Zhang Peixia filed Critical Zhang Peixia
Publication of WO2012092826A1 publication Critical patent/WO2012092826A1/zh

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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

Definitions

  • the invention relates to the field of aviation, and in particular relates to an airborne emergency rescue system for a passenger aircraft.
  • An airborne emergency rescue system for a passenger aircraft characterized in that:
  • the tail of the passenger aircraft is a duckbill tail or a dovetail tail;
  • the rudder is a double vertical tail;
  • the double vertical tails are respectively arranged on the sides of the duckbill tail or the dovetail tail;
  • the duckbill A life-saving exit and a rescue bin door are arranged in the middle of the tail of the machine or in the middle of the dovetail tail;
  • the life-saving door is telescopically closed by an electro-hydraulic actuator; and a plurality of parallel parallel teeth are arranged in the machine compartment of the passenger aircraft
  • the I-shaped track of the tooth; the I-shaped track passes through the life-saving exit from the driving compartment;
  • a row of multifunctional rescue seats is arranged in the middle of the passenger compartment of the passenger aircraft, and the two sides are arranged as a walkway;
  • the units are connected in parallel and fixed on the track by pulleys, gears and positioners, which can
  • the end of the resetting force arm is caught on the hook of the fuse, the fuse is connected to the trigger through the soft shaft cable, and the trigger of the first row of the multifunctional life seat at the tail of the passenger aircraft is installed in the rescue
  • the triggers of the second row of multi-function life-saving seats are installed 1.5 meters behind the first row of multi-function rescue seats
  • the triggers of the third row of multi-function life-saving seats are installed in the first row of multi-function rescue seats.
  • the front of the locator housing, and so on, all the triggers are installed.
  • Each row of multi-function rescue seats can be opened with a safe distance from the front row of multi-function rescue seats.
  • the trigger of the lifeguard seat is triggered by the locator housing above the multi-function rescue seat of the rear row.
  • the trigger system of the trigger is composed of a trigger, a soft shaft cable, a fuse, a reset force arm, a positioner, a positioner housing, and a start switch; the trigger, the soft shaft cable, and the insurance
  • the device is fixed on the track (on, the fuse can simultaneously control the two reset arms of the track, the reset force arm is set on the multifunctional rescue seat through the return spring, the positioner and the start switch are set in the positioner housing, and the start switch is set Below the positioner, the positioner housing is placed on the multifunctional rescue seat, the force arm of the positioner is stuck in the card slot of the reset force arm, the end of the reset force arm is stuck on the hook of the fuse, and the fuse passes through the soft
  • the shaft pull wire is connected to the trigger, and once the trigger is triggered, the fuse is separated from the reset force arm, and the reset force arm immediately drops the positioner on the start switch to energize the start switch and start the start motor.
  • the power source of the start switch is connected to the battery pack, the other end is connected to the closed switch, and the other end of the close switch is connected to the starter motor, and the close switch and the controller are disposed on the chassis of the multifunctional rescue seat;
  • the controller is composed of a force arm, a pulley and a return spring, and the pulley acts on the track; when the pulley of the controller is separated from the track, the controller controls the closing switch through the return spring, so that the power of the closed switch is disconnected, and the motor is stopped.
  • the multifunctional rescue seat is a life saver powered by a battery pack and a starter motor, and the main structure thereof is divided into a seat and a chassis, and the seat is mounted with a life saver and a throw.
  • Umbrella gun, safety shield, seat belt, air bag, bracket, foot pedal, An oxygen breathing apparatus is provided in the safety shield, and a signal transmitter is mounted on the top of the backrest.
  • Two leg brackets are mounted with a solid leg guard; a leg press guard is mounted on the inner side of the armrest on both sides of the chassis, and the leg leg guard is manually opened and automatically closed by a tooth positioner and a return spring, and is provided thereon.
  • the handle is controlled, and an air bag, a battery pack, a smart charger and a starter motor are installed at the bottom of the chassis.
  • the upper end of the armrest on the longer side of the chassis is provided with a retractable tray, and the front end is provided with a large hinge, and the chassis passes through
  • the hinges are connected together, and a tooth locator with a return spring is arranged at the bottom of the hinge to automatically open and position the chassis.
  • the power of the multifunctional rescue seat can also be stored under high pressure. Bottle and air compressor starter.
  • a bayonet bracket and a bayonet are mounted on the rear end of the armrest on which the large hinge is mounted, and the bayonet bracket is mounted on a handrail, and the bayonet is fastened with a stabilizer spring.
  • the hook is mounted on the armrest on the other side, and the two chassis are connected in parallel when the hook is jammed from the bayonet bracket by the latching pin; the latch pin releases the hook when the two are released
  • the chassis is opened and jammed by the large hinge and the tooth locator, and the bayonet bracket and the bayonet and the hook are respectively arranged one above the other, and the bayonet is connected by a soft shaft cable to the fuse mounted on the upper end of the front part of the armrest. The other end of the fuse is attached to the parachute.
  • the controller is mounted on the armrest of the chassis,
  • a start switch is arranged above the controller, and the pulley of the controller acts on the track; when the pulley of the controller is off track, the controller hits the start switch, the power of the start switch is connected to the battery pack, and the other end is connected
  • the electronic core of the parachute gun and the electronic core of the airbag and the signal transmitter is an electronic core that can be delayed for two seconds.
  • the start switch is started, the umbrella will burst and the umbrella will be pulled out. At the same time, the airbag will also open for two seconds, and the signal transmitter will send a distress signal.
  • the life-saving system of the passenger aircraft is very simple to operate.
  • the pilot simply presses the start switch on the console, and the electro-hydraulic actuator mounted on the life-saving exit and the rescue door will When activated, the life-saving door will open and trigger the trigger mounted on the life-saving door.
  • the trigger will open the fuse through the soft-shaft cable to activate the multi-function rescue seat.
  • the passenger only needs to press the solid-leg support. Lower the leg, buckle the seat belt and pull the safety shield down to wear the oxygen breathing apparatus.
  • the lifesaving system can be effectively implemented in low, medium and high altitudes.
  • the life-saving system of the passenger aircraft of the invention has both civil and military functions, that is, emergency rescue can be carried out during civil passenger flight, airborne troops can be transported during military use, and different styles and functions can be designed according to different purposes.
  • the multi-functional life-saving seat is designed to be transported and placed on the shelf, or it is designed to be used as a bomber for the bomb.
  • the passenger aircraft can perform a 45-degree climb at the same time, so that the entire delivery process can be easily and beautifully completed, thus making the large passenger aircraft become military without military maintenance.
  • the invention makes people safer when riding a plane, and can save a lot of money for national defense construction.
  • Fig. 1 is a front elevational view of the tail of Fig. 1; Fig. 3 is a schematic cross-sectional view of Fig. 1; Fig. 4 is a schematic view of a dovetail passenger aircraft of the present invention; And a side view of the rescue door;
  • Figure 6 is a plan view of Figure 5;
  • Figure 7 is a schematic diagram of the track and trigger system;
  • 8 is a schematic view of the multifunctional rescue seat;
  • FIG. 9 is a rear view of FIG. 8;
  • FIG. 10 is a schematic view of the parallel connection of FIG. 8; FIG.
  • Figure 13 is a side cross-sectional view of Figure 8;
  • Figure 14 is a schematic view of the trigger system installation;
  • 1 is a passenger aircraft
  • 2 is a duckbill tail
  • 3 is a dovetail tail
  • 4 is a double tail
  • 5 is a life-saving exit
  • 6 is a life-saving door
  • 7 is a hinge
  • 8 is a fuse 9 is an enlarged view of 8
  • 10 is a connecting rod
  • 11 is a hook
  • 12 is an electro-hydraulic actuator
  • 13 is a walkway
  • 14 is a rail
  • 15 is a positioner housing
  • 16 is a positioner
  • 17 is a start switch
  • 18 It is a resetting force arm
  • 19 is a fuse
  • 20 is a front view of 19
  • 21 is a soft shaft cable
  • 22 is a trigger
  • 23 is a multifunctional rescue seat
  • 24 is a chassis
  • 25 is a large hinge
  • 26 is a tooth
  • 27 is a tray
  • 28 is a leg press guard
  • 29 is a control handle
  • 30 is a bracket
  • the first step is to design the traditional chicken mouth of the passenger aircraft 1 into a duckbill machine.
  • Tail 2 or dovetail tail 3 and set the rudder on both sides of the duckbill tail 2 or the dovetail tail 3, that is, the double vertical tail 4, in the upper position of the duckbill tail 2 or the dovetail machine
  • the life-saving exit 5 and the life-saving door 6 are opened in the middle of the tail 3, so that the multifunctional life-saving seat 23 is unobstructed when the emergency exit is opened.
  • the I-shaped rails 14 with teeth are installed in parallel in the middle of the cabin of the passenger aircraft 1 at an appropriate distance, and the two sides are arranged as a walkway 13 and the two rails 14 in the middle are connected to the cockpit.
  • the end of 14 is designed in a corresponding shape according to the specific structure of the duckbill tail 2 or the dovetail tail 3 and communicates with the lifesaving outlet 5.
  • the start switch of the electro-hydraulic actuator 12 is mounted at an appropriate position on the console of the cockpit.
  • the assembled multifunctional rescue seat 23 passes through the large hinge 25 and the bayonet bracket 45 , The bayonet 47 and the hook 48 are connected in parallel, and then a parallel row of multifunctional rescue seats 23 are inserted from the end of the rail 14, and the multifunctional rescue seat 23 is placed in a pre-installed position, and so on.
  • Each row of multifunctional life-saving seats 23 is worn on the track 14.
  • the fuse 19 the soft shaft cable 21 and the trigger 22 are mounted, and the utility model is installed in the multifunctional rescue seat. 23.
  • the end of the restoring force arm 18 on the chassis 24 is caught on the hook of the fuse 19, such that the resetting force arm 18 picks up the positioner 16 and the teeth on the track 14 together, thereby enabling the multifunctional lifesaving
  • the seat 23 is fixed to the rail 14, and the trigger 22 of the last row of the multi-function rescue seat 23 of the passenger aircraft 1 is installed at an appropriate position of the life-saving exit, so that the rescue door is triggered when it is opened, and finally the switch 17 is activated.
  • the power source of the start switch 50 is coupled to the terminal of the high-iron battery pack 55, and the latch of the smart charger 54 is inserted into the power socket disposed on the track 14. .
  • the first step is to design the traditional chicken mouth of the passenger aircraft 1 into a duckbill machine.
  • Tail 2 or dovetail tail 3 and set the rudder on both sides of the duckbill tail 2 or the dovetail tail 3, that is, the double vertical tail 4, in the upper position of the duckbill tail 2 or the dovetail machine
  • the life-saving exit 5 and the life-saving door 6 are opened in the middle of the tail 3, so that the multifunctional life-saving seat 23 is unobstructed when the emergency exit is opened.
  • the I-shaped rails 14 with teeth are installed in parallel in the middle of the cabin of the passenger aircraft 1 at an appropriate distance, and the two sides are arranged as a walkway 13 and the two rails 14 in the middle are connected to the cockpit.
  • the end of 14 is designed in a corresponding shape according to the specific structure of the duckbill tail 2 or the dovetail tail 3 and communicates with the lifesaving outlet 5.
  • the start switch of the electro-hydraulic actuator 12 is mounted at an appropriate position on the console of the cockpit.
  • the assembled multifunctional rescue seat 23 passes through the large hinge 25 and the bayonet bracket 45 , The bayonet 47 and the hook 48 are connected in parallel, and then a parallel row of multifunctional rescue seats 23 are inserted from the end of the rail 14, and the multifunctional rescue seat 23 is placed in a pre-installed position, and so on.
  • Each row of multifunctional life-saving seats 23 is worn on the track 14.
  • the fuse 19 the soft shaft cable 21 and the trigger 22 are mounted, and the utility model is installed in the multifunctional rescue seat. 23.
  • the end of the restoring force arm 18 on the chassis 24 is caught on the hook of the fuse 19, such that the resetting force arm 18 picks up the positioner 16 and the teeth on the track 14 together, thereby enabling the multifunctional lifesaving
  • the seat 23 is fixed to the rail 14, and the trigger 22 of the last row of the multi-function rescue seat 23 of the passenger aircraft 1 is installed at an appropriate position of the life-saving exit, so that the rescue door is triggered when it is opened, and finally the switch 17 is activated.
  • the power source of the start switch 50 is coupled to the terminal of the high-iron battery pack 55, and the latch of the smart charger 54 is inserted into the power socket disposed on the track 14. .
  • the traditional chicken-shaped tail of the passenger aircraft 1 is designed as a duckbill tail 2 or a dovetail tail 3, and the traditional single tail (rudder) is designed as a double tail 4, that is, at the tail of the duckbill 2 or one of the two tails of the dovetail tail 3, so that a barrier-free passage is formed in the middle of the double vertical tail 4, which is opened at the appropriate position above the duckbill tail 2 or in the middle of the dovetail tail 3
  • the life-saving exit 5, the life-saving door 6 can be automatically telescopically closed by the electro-hydraulic actuator 12, and a plurality of parallel-shaped I-shaped rails 14 with parallel teeth are arranged in the machine compartment of the passenger aircraft 1 to directly pass the life-saving exit from the driving compartment.
  • the traditional two-row or three-row seats are juxtaposed in a row with the middle of the machine compartment of the passenger aircraft 1, and the two sides are set as the walkway 13, and the multifunctional rescue seats 23 are connected in parallel by the row.
  • the pulley 43 and the gear 44 and the positioner 16 are fixed to the rail 14, and the trigger 22 is used to trigger the start of the exit and the escape of the umbrella.
  • the triggering system and the mounting method of the multifunctional rescue seat 23 are: the end of the resetting force arm 18 is caught on the hook of the fuse 19, and the fuse 19 is coupled to the trigger 22 through the flexible shaft cable 21 to carry the passenger aircraft 1
  • the trigger 22 of the first row of multifunctional rescue seats 23 of the tail is mounted to the appropriate position of the life-saving exit 5 so that the first row of life-saving seats 23 is triggered when the life-saving door 6 is opened, and the second row of the multi-function life-saving seats 23 is
  • the trigger 22 is mounted 1.5 meters behind the first row of multi-function rescue seats 23, and the triggers 22 of the third row of multi-function rescue seats 23 are mounted in front of the positioner housing 15 of the first row of multi-function rescue seats 23.
  • all the triggers 22 are installed, so that after each row of the multifunctional life-saving seats 23 is activated, a safe distance can be opened from the front row of the multifunctional life-saving seats 23, and the front row is more
  • the trigger 22 of the functional rescue seat 23 is triggered by the locator housing 15 above the multi-function rescue seat 23 of the rear row.
  • the life-saving outlet 5 is designed to be rectangular and has a groove that can be air-tight.
  • the life-saving outlet 5 is sized to easily pass through a row of multifunctional life-saving seats 23, and a plurality of inner walls of the life-saving outlet 5 are mounted.
  • a fuse 8 each fuse 8 is closely connected by a connecting rod 10 and coupled to the electro-hydraulic actuator 12, and the control switch of the electro-hydraulic actuator 12 is provided on the driver's console, when the driver turns on the control switch At this time, the electro-hydraulic actuator 12 can open the fuse 8 and the life-saving door 6 can be opened.
  • a trigger 22 is mounted at a suitable position of the life-saving outlet 5, and when the rescue door 6 is opened, the trigger 22 is Triggered to enable the multifunctional rescue seat 23 to be activated immediately.
  • the life-saving door 6 is designed in the form of a telescopic fold, which is fixed on the life-saving exit 5 by a hinge 7, and a hook 11 is provided at the edge of the life-saving door 6, and when the life-saving door 6 and the life-saving exit 5 are closed, the fuse is The card arm of 8 snaps into the hook 11 and is tightened to ensure airtight compression, and the life-saving door 6 is automatically closed by the electro-hydraulic actuator 12.
  • the trigger system is composed of a trigger 22, a soft shaft cable 21, a fuse 19, a resetting force arm 18, a positioner 16, a positioner housing 15, and a start switch 17.
  • the trigger 22, the soft shaft cable 21 and the fuse 19 are fixed on the rail 14, and the fuse 19 is a component of the resetting force arm 18 which can simultaneously control the two rails 14; the restoring force arm 18 is made by the return spring.
  • the utility model is disposed above the multifunctional rescue seat 23; the positioner 16 and the start switch 17 are disposed in the positioner housing 15, the start switch 17 is disposed under the positioner 16, and the positioner housing 15 is disposed in the multifunctional rescue seat 23, the force arm of the positioner 16 is stuck in the card slot of the resetting force arm 18, the end of the resetting force arm 18 is caught on the hook of the fuse 19, and the fuse 19 is coupled to the trigger 22 through the flexible shaft cable 21; Once the trigger 22 is triggered, the fuse 19 is pulled apart from the resetting force arm 18, and the resetting force arm 18 immediately drops the positioner 16 onto the starting switch 17, energizing the starting switch 17 and starting the starting motor 53 while simultaneously The multifunctional rescue seat 23 is separated from the track 14.
  • the power source of the start switch 17 is coupled to the upper surface of the high-iron battery pack 55, the other end of which is coupled to the close switch 52, and the other end of the close switch 52 is coupled to the starter motor 53.
  • the close switch 52 and the controller 51 are disposed in the multi-function rescue seat 23.
  • the controller 51 is composed of a force arm, a pulley and a return spring. The pulley acts on the rail 14, and once the pulley of the controller 51 is disengaged from the rail 14, the controller 51 is closed by the return spring. On the switch 52, the power of the closing switch 52 is turned off, and the starting motor 53 is stopped.
  • the multi-function life-saving seat 23 is a life-saving device powered by a battery pack and a starter motor 53.
  • the battery pack of the present invention uses a high-iron battery pack 55, that is, a battery pack used on a high-speed rail; the main structure is divided into a seat 23 and The chassis 24 has two major parts.
  • the seat 23 is mounted with a life saver 39, an umbrella 8 , a safety shield 36 , a safety belt 35 , an air bag 38 , a bracket 30 , and a foot pedal 31 ;
  • the umbrella rope 40 of the life saver 39 is respectively fixed to the multifunctional seat
  • an airbag 38 is mounted on the lower side of the lifeguard 39 and the middle of the backrest and the bottom of the bottom frame 24;
  • each of the parabolic guns 42 can be connected to two or
  • a multi-purpose umbrella 39 is provided;
  • the safety shield 36 can be retracted up and down by the tooth positioner 37, and an oxygen breathing apparatus is disposed in the safety shield 36.
  • the safety belt 35 is mounted on the backrest of the seat 23, and is on the backrest.
  • the top end is equipped with a signal transmitter;
  • the seat cushion 34 is designed as a pneumatic bag type,
  • the bracket 30 is mounted on the seat 23 and can be retracted, and two of the brackets 30 are mounted with a solid leg guard 32, and the solid leg guard 32
  • It is a manually operated brace with a tooth positioner, and a control handle 33 is mounted thereon;
  • the foot pedal 31 is mounted on the bracket 30, and the bracket 30 can be controlled by the toe pedal 31. .
  • a pressure leg guard 28 is mounted on the armrests on both sides of the chassis 24, and the leg press guard 28 is a safety guard that is manually opened and automatically closed by a tooth positioner and a return spring, and a control handle 29 is disposed thereon.
  • the function of the leg press guard 28 is to prevent the passenger from being pulled out of the multifunctional rescue seat 23 when the passenger aircraft 1 suddenly has an unexpected situation; the air bag 38, the high-iron battery pack 55, and the smart charging are installed at the bottom of the chassis 24
  • a starter motor 53 wherein the starter motor 53 is mounted adjacent to the track 14, and the smart charger 54 is a charger that can automatically start and disconnect and constant voltage and constant current, and is connected through the pin and the socket.
  • a tooth positioning device 26 with a return spring is mounted at the bottom of the large hinge 25 to automatically open and position the chassis 24.
  • a bayonet bracket 45 and a bayonet 47 are mounted on the rear end of the armrest on which the large hinge 25 is mounted, and the bayonet bracket 45 is mounted on a handrail, and the bayonet 47 is attached with a stabilizer spring and mounted on the bayonet pin.
  • the hook 48 is mounted on the armrest on the other side, and the hook 48 is from the bayonet bracket When the middle of the 45 is caught by the bayonet 47, the two chassis 24 are connected in parallel. When the bayonet 47 releases the hook 48, the two chassis 24 pass through the large hinge 25 and the tooth locator 26 automatically.
  • the bayonet bracket 45 and the bayonet 47 and the hook 48 are respectively mounted one above the other, and the bayonet 47 is coupled to the fuse 49 mounted on the upper end of the front portion of the armrest through the flexible shaft cable 21, the fuse 49 The other end is connected to the umbrella rope 40.
  • the fuse 49 pulls the bayonet 47 through the soft shaft cable 21 to release the hook 48, and the chassis 24 passes through the page 25 and The tooth locator 26 is automatically opened and positioned.
  • the controller 51 is composed of a return spring, a control arm and a pulley and is mounted on the armrest of the chassis 24.
  • a start switch 50 is mounted at an appropriate position above the controller 51.
  • the pulley of the controller 51 acts on the track 14. When the pulley of the controller 51 is released from the track 14, the controller 51 will strike the start switch 50.
  • the power source of the start switch 50 is coupled to the high-iron battery pack 55, and the other end is coupled to the electronic core of the parabolic gun 42 and to the electronic core of the air bag 38 and to the signal transmitter.
  • the electronic core of the air bag 38 is a deferrable When the electronic core is broken in two seconds, when the start switch 50 is started, the umbrella 42 will immediately erupt and pull out the life-saving umbrella 39, and the air bag 38 will also be delayed for two seconds to open, and the signal transmitter will send a distress signal.
  • Each row of multifunctional life-saving seats 23 is divided into two groups, each group is connected in parallel by a large hinge 25 and a bayonet bracket 45, a latch 47 and a hook 48.
  • the connection between the two groups is connected and sold in the same way.
  • the bayonet 47 is coupled to the upper portion of the fuse 49 via a flexible shaft cable 21.
  • the multifunctional rescue seat 23 can also be designed in other styles without any function, and the power can also be powered by other powers, such as using a high-pressure gas cylinder and an air compressor, etc.;
  • the track 14 should be kept at a certain distance from the floor to prevent the multifunctional life-saving seat 23 from passing normally after being activated due to the influence of items on the floor; the multi-function life-saving seat 23 is discharged in units of the row when starting the warehouse. In a row, the other ones follow the dominoes, and it takes about 30 seconds for all the passengers of a large passenger aircraft 1 and the pilot's life-saving warehouse to complete, in each row of multi-function lifeguards.
  • each row of the multi-function life-saving seats 23 is separated into two groups by a bayonet bracket 45 and a bayonet 47 and a hook 48 disposed at an intermediate position, each group of multi-function lifeguards
  • the chair 23 is automatically opened and positioned by the large hinge 25 and the tooth locator 26, so that each set of the multifunctional rescue seat 23 is automatically enclosed in a circle in the air, and the airbag 38 disposed thereon is successful. Safeguarding, in land The anti-collision, floating in the water security.
  • the first step is to design the traditional chicken mouth of the passenger aircraft 1 into a duckbill machine.
  • Tail 2 or dovetail tail 3 and set the rudder on both sides of the duckbill tail 2 or the dovetail tail 3, that is, the double vertical tail 4, in the upper position of the duckbill tail 2 or the dovetail machine
  • the life-saving exit 5 and the life-saving door 6 are opened in the middle of the tail 3, so that the multifunctional life-saving seat 23 is unobstructed when the emergency exit is opened.
  • the I-shaped rails 14 with teeth are installed in parallel in the middle of the cabin of the passenger aircraft 1 at an appropriate distance, and the two sides are arranged as a walkway 13 and the two rails 14 in the middle are connected to the cockpit.
  • the end of 14 is designed in a corresponding shape according to the specific structure of the duckbill tail 2 or the dovetail tail 3 and communicates with the lifesaving outlet 5.
  • the start switch of the electro-hydraulic actuator 12 is mounted at an appropriate position on the console of the cockpit.
  • the assembled multifunctional rescue seat 23 passes through the large hinge 25 and the bayonet bracket 45 , The bayonet 47 and the hook 48 are connected in parallel, and then a parallel row of multifunctional rescue seats 23 are inserted from the end of the rail 14, and the multifunctional rescue seat 23 is placed in a pre-installed position, and so on.
  • Each row of multifunctional life-saving seats 23 is worn on the track 14.
  • the fuse 19 the soft shaft cable 21 and the trigger 22 are mounted, and the utility model is installed in the multifunctional rescue seat. 23.
  • the end of the restoring force arm 18 on the chassis 24 is caught on the hook of the fuse 19, such that the resetting force arm 18 picks up the positioner 16 and the teeth on the track 14 together, thereby enabling the multifunctional lifesaving
  • the seat 23 is fixed to the rail 14, and the trigger 22 of the last row of the multi-function rescue seat 23 of the passenger aircraft 1 is installed at an appropriate position of the life-saving exit, so that the rescue door is triggered when it is opened, and finally the switch 17 is activated.
  • the power source of the start switch 50 is coupled to the terminal of the high-iron battery pack 55, and the latch of the smart charger 54 is inserted into the power socket disposed on the track 14. .
  • leg press guard 28 presses the passenger on the multifunctional rescue seat 23, it will not be pulled out, and only the passenger needs to press the solid leg protector 32 by hand. Fix it, buckle the seat belt 35, then pull down the safety shield 36 and put on the oxygen breathing apparatus. The driver will activate the switch and press the rescue door 6 to be opened immediately and touch the trigger 22 to use the multi-function lifeguard.
  • the chair 23 is activated to cause the multi-function rescue seat 23 to flow out in a set order, and when the controller 51 provided on the chassis 24 of the multi-function rescue seat 23 is disengaged from the rail 14, the controller 51 is pressed
  • the switch 50 When the switch 50 is activated, the parachute gun 42 will be energized to eject the life-saving umbrella 39, and the air bag 38 will be energized and erupted for two seconds, while the bayonet 47 disposed in the middle of the row of multi-function rescue seats 23 is provided.
  • the hooks 48 are also released, so that a row of life-saving seats 23 are divided into two groups from the middle and automatically encircled into two loops by the hinge table 25 and the tooth locator 26, while the controller 51 is also disengaged from the track 14
  • the hitting switch 52 is used to de-energize the starter motor 53 and stop.
  • the multi-function rescue seat 23 is then safely Landing on the ground or water, which is mounted on the signal transmitter will send a distress signal by a predetermined frequency.
  • This rescue system is suitable for single-deck passenger aircraft and also for double-deck passenger aircraft.
  • the invention designs an effective life-saving system for the passenger aircraft, which enables the passenger to escape safely in the event of an emergency in the passenger aircraft, and has industrial applicability.

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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)

Description

一种载客飞机空中紧急情况救生系统 技术领域
本发明涉及航空领域,具体涉及一种载客飞机空中紧急情况救生系统。
 背景技术
目前公知的大中型载客飞机已成为人们出行必不可少的快速高效的交通工具,较其它交通工具而言安全系数相对较高,然而空难事故也时有发生,飞机一但发生意外情况后果十分惨烈,直到目前还没有有效的解决办法。
技术问题
本发明的目的是提供一种载客飞机空中紧急情况救生系统，为载客飞机设计一套有效的救生系统,在载客飞机发生紧急情况时使乘客可以安全逃生。
技术解决方案
一种载客飞机空中紧急情况救生系统,其特征在于： 载客飞机的机尾为鸭嘴形机尾或燕尾形机尾；方向舵为双垂尾；所述双垂尾分别设置于所述鸭嘴形机尾或燕尾形机尾的两侧；鸭嘴形机尾的上方或燕尾形机尾的中间设有救生出口及救生仓门；所述救生仓门通过电液作动器伸缩闭合；载客飞机的机仓内设多条并列平行的带齿牙的工字形轨道；所述工字形轨道从驾驶仓直通救生出口；载客飞机的机仓中部设置有一列多功能救生座椅，两侧设为走道；所述多功能救生座椅以排为单位并联在一起，通过滑轮、齿轮及定位器固定在轨道上，能够通过触发器触发启动出仓并开伞逃生。
本发明的优选方案是，复位力臂的末端卡在保险器的挂钩上，保险器通过软轴拉线连接在触发器上，载客飞机尾部第一排多功能救生座椅的触发器安装在救生出口上，第二排多功能救生座椅的触发器安装在第一排多功能救生座椅后面1.5米处，第三排多功能救生座椅的触发器安装在第一排多功能救生座椅的定位器外壳前面,以此类推，将所有的触发器安装好，每一排多功能救生座椅启动后能够和前一排的多功能救生座椅拉开一个安全距离,前面一排多功能救生座椅的触发器由后一排的多功能救生座椅上面的定位器外壳触发。
本发明的又一优选方案是，触发器的触发系统由触发器、软轴拉线、保险器、复位力臂、定位器、定位器外壳、启动开关组成；所述触发器、软轴拉线、保险器固定在轨道(上,保险器可以同时控制轨道两则的复位力臂,复位力臂通过复位弹簧设置在多功能救生座椅上,定位器和启动开关设置在定位器外壳内,启动开关设置在定位器的下方,定位器外壳设置在多功能救生座椅上,定位器的力臂卡在复位力臂的卡槽中,复位力臂的末端卡在保险器的挂钩上,保险器通过软轴拉线连接在触发器上,触发器一但被触发便会拉动保险器与复位力臂分离,复位力臂即刻将定位器压下落在启动开关上面,使启动开关通电并使启动电机启动。
本发明的又一优选方案是，启动开关的电源连接电池组,另一端连接在闭合开关,闭合开关的另一端连接启动电机,闭合开关和控制器设置在多功能救生座椅的底架上；所述控制器由力臂、滑轮和复位弹簧组成,滑轮作用在轨道上；控制器的滑轮与轨道脱离时,控制器通过复位弹簧控制闭合开关,使闭合开关的电源断开,启动电机停转。
本发明的又一优选方案是，所述多功能救生座椅是一个采用电池组和启动电机为动力的救生器,其主要结构分为座椅和底架,座椅上面安装有救生伞、抛伞枪、安全防护罩、安全带、气囊、托架、脚踏板, 在安全防护罩内设有氧气呼吸器, 并在靠背的顶端安装有信号发射器, 在托架的两则安装有固腿护架；在底架两边的扶手内侧安装有压腿护架,压腿护架通过齿牙定位器和复位弹簧进行手动拉开自动闭合,其上设有控制拉手,在底架的底部安装有气囊、电池组、智能充电器和启动电机,底架较长一侧的扶手上端设有一个可收放的托盘,前端设有大合页,底架通过大合页连在一起,在大合页的底部装有一个带复位弹簧的齿牙定位器,可以使底架之间自动张开并定位,多功能救生座椅的动力也可以采用高压储气瓶和空压启动机。
本发明的另一优选方案是，在安装有大合页的扶手的后端安装有卡销托架和卡销,卡销托架安装在一则的扶手上,卡销上缚有稳定弹簧并安装在卡销托架上,挂钩安装在另一侧的扶手上,挂钩从卡销托架中穿过被卡销卡住时两个底架并联在一起；卡销将挂钩放开时两个底架通过大合页和齿牙定位器张开并卡住,卡销托架和卡销及挂钩上下各装一套,卡销通过软轴拉线连接在装在扶手前部上端的保险器上,保险器的另一端连接在伞绳上。
本发明的再一优选方案是，所述控制器安装在底架的扶手上, 在控制器的上方设置有启动开关，控制器的滑轮作用在轨道上；当控制器的滑轮脱离轨道,控制器击打在启动开关上,启动开关的电源连接在电池组上,另一端连接在抛伞枪的电子引芯和气囊的电子引芯以及信号发射器,气囊的电子引芯是一个可以延时两秒爆发的电子引芯,在启动开关启动时抛伞枪即刻爆发将救生伞拉出,同时气囊也会延时两秒打开,信号发射器便会发出求救信号。
 有益效果
本载客飞机的救生系统操作非常简单,当载客飞机在空中出现紧急情况时,飞行员只要按下操作台上的启动开关,安装在救生出口和救生仓门上的电液作动器便会启动,救生仓门便会打开并触发安装在救生仓门上的触发器,触发器便会通过软轴拉线将保险器打开使多功能救生座椅启动；而乘客只需要将固腿护架按下将腿固定住,扣上安全带并将安全防护罩拉下戴上氧气呼吸器即可。本救生系统在低、中、高空均可有效实施。
本发明的载客飞机的救生系统同时具备民用和军用两种功能,即在民用载客飞行时可以紧急救生,在军用时可以运输空降兵,也可以根据不同的用途设计成不同的样式和功能,如:将多功能救生座椅设计成货架运送并投放物资,或设计成航弹固定架装上航空炸弹作为轰炸机用。在军用时投放空降兵或物资或航弹时,载客飞机可以同时作45度爬升动作,这样整个投放过程便会轻松漂亮的完成,这样就使大型载客飞机变成了不用军费维护的军用运输机、轰炸机。本发明使人们在乘座飞机时更加安全,同时可以为国防建设节约大笔资金。
 附图说明
图1是本发明的主视示意图；图2是图1的尾部纵剖示意图；图3是图1的平面剖视示意图；图4是本发明的燕尾形载客飞机示意图；图5是救生出口和救生仓门的侧视示意图； 图6是图5的平面示意图；图7是轨道和触发系统示意图； 图8是多功能救生座椅示意图；图9是图8的后视示意图；图10是图8的并连方法示意图；图11是图10的侧视示意图；图12是图8的正面剖视示意图；图13是图8的侧面剖示示意图；图14是触发系统安装示意图；图15是本发明的实施例 1的示意图；图16 是本发明的实施例2的示意图。
图中：1是载客飞机、2是鸭嘴形机尾、3是燕尾形机尾、4是双垂尾、5是救生出口、6是救生仓门、7是合页、8是保险器、9是8的放大图、10是连杆、11是挂钩、12是电液作动器、13是走道、14是轨道、15是定位器外壳、16是定位器、17是启动开关、18是复位力臂、19是保险器、20是19的正视图、21是软轴拉线、22是触发器、23是多功能救生座椅、24是底架、25是大合页、26是齿牙定位器、27是托盘、28是压腿护架、29是控制拉手、30是托架、31是脚踏板、32是固腿护架、33是控制拉手、34是座垫、35是安全带、36是安全防护罩、37是齿牙定位器、38是气囊、39是救生伞、40是伞绳、41是挂环、42是抛伞枪、43是滑轮、44是齿轮、45是卡销托架、46是45的放大图、47是卡销、48是挂钩、49是保险器、50是启动开关、51是控制器、52是闭合开关、53是启动电机、54是智能充电器、55是高铁电池组。
 本发明的最佳实施方式
如图1、图2、图3、图4、图5、图6、图7、图15所示，第一步,首先将载客飞机1传统的鸡嘴形机尾设计成鸭嘴形机尾2或燕尾形机尾3,并在鸭嘴形机尾2或燕尾形机尾3的两侧设置方向舵,即双垂尾4,在鸭嘴形机尾2的上部适当位置或燕尾形机尾3的中间开设救生出口5和救生仓门6,这样就使多功能救生座椅23在紧急出仓开伞时畅通无阻。将带齿牙的工字形轨道14按照所需要的数量间隔适当距离并列平行安装在载客飞机1的机仓中部,两侧设置为走道13,并将中间的两条轨道14连通驾驶仓,轨道14的末端根据鸭嘴形机尾2或燕尾形机尾3的具体结构设计成相应的形状并连通救生出口5。将电液作动器12的启动开关安装在驾驶仓的操作台上适当位置。
第二步,如图8、图9、图10、图11、图12、图13、图15所示,将组装好的多功能救生座椅23通过大合页25和卡销托架45、卡销47及挂钩48并联到一起,然后将并联好的一排多功能救生座椅23从轨道14的末端穿入,并将多功能救生座椅23放到预安装的位置,以此类推,将每一排多功能救生座椅23都穿在轨道14上。
第三步,如图5、图6、图7、图10、图11、图12、图14所示,安装保险器19、软轴拉线21和触发器22,将安装在多功能救生座椅23、底架24上的复位力臂18的末端卡在保险器19的挂钩上,这样使复位力臂18将定位器16撬起和轨道14上的齿牙顶在一起,从而使多功能救生座椅23固定在轨道14上,将载客飞机1最后一排多功能救生座椅23的触发器22安装在救生出口的适当位置,使救生仓门开启时即被触发,最后将启动开关17和启动开关50的电源连结在高铁电池组55的接线柱上,将智能充电器54的插销插入设置在轨道14上的电源插座上 。
 本发明的实施方式
如图1、图2、图3、图4、图5、图6、图7、图15所示，第一步,首先将载客飞机1传统的鸡嘴形机尾设计成鸭嘴形机尾2或燕尾形机尾3,并在鸭嘴形机尾2或燕尾形机尾3的两侧设置方向舵,即双垂尾4,在鸭嘴形机尾2的上部适当位置或燕尾形机尾3的中间开设救生出口5和救生仓门6,这样就使多功能救生座椅23在紧急出仓开伞时畅通无阻。将带齿牙的工字形轨道14按照所需要的数量间隔适当距离并列平行安装在载客飞机1的机仓中部,两侧设置为走道13,并将中间的两条轨道14连通驾驶仓,轨道14的末端根据鸭嘴形机尾2或燕尾形机尾3的具体结构设计成相应的形状并连通救生出口5。将电液作动器12的启动开关安装在驾驶仓的操作台上适当位置。
第二步,如图8、图9、图10、图11、图12、图13、图15所示,将组装好的多功能救生座椅23通过大合页25和卡销托架45、卡销47及挂钩48并联到一起,然后将并联好的一排多功能救生座椅23从轨道14的末端穿入,并将多功能救生座椅23放到预安装的位置,以此类推,将每一排多功能救生座椅23都穿在轨道14上。
第三步,如图5、图6、图7、图10、图11、图12、图14所示,安装保险器19、软轴拉线21和触发器22,将安装在多功能救生座椅23、底架24上的复位力臂18的末端卡在保险器19的挂钩上,这样使复位力臂18将定位器16撬起和轨道14上的齿牙顶在一起,从而使多功能救生座椅23固定在轨道14上,将载客飞机1最后一排多功能救生座椅23的触发器22安装在救生出口的适当位置,使救生仓门开启时即被触发,最后将启动开关17和启动开关50的电源连结在高铁电池组55的接线柱上,将智能充电器54的插销插入设置在轨道14上的电源插座上 。
如图1、图2、图3、图4、图5、图6、图7、图8、图9、图10、图11、图12、图13、图14、图15、图16所示， 将载客飞机1传统的鸡嘴形机尾设计成鸭嘴形机尾2或燕尾形机尾3,将传统的单垂尾(方向舵)设计成双垂尾4,即在鸭嘴形机尾2或燕尾形机尾3的两则各设一个,这样在双垂尾4的中间就形成了一个无障碍通道,在鸭嘴形机尾2的上方适当位置或燕尾形机尾3的中间开设救生出口5,救生仓门6通过电液作动器12可自动伸缩闭合,在载客飞机1的机仓内设多条并列平行的带齿牙的工字形轨道14,从驾驶仓直通救生出口5,将传统的两列或三列座椅的形式并列成一列置与载客飞机1的机仓中部,两侧设为走道13,多功能救生座椅23以排为单位并联在一起,通过滑轮43和齿轮44及定位器16固定在轨道14上，通过触发器22触发启动出仓并开伞逃生。
多功能救生座椅23的触发系统及安装方法是：将复位力臂18的末端卡在保险器19的挂钩上，保险器19通过软轴拉线21连结在触发器22上，将载客飞机1尾部第一排多功能救生座椅23的触发器22安装到救生出口5的适当位置,以便救生仓门6开启时触发第一排救生座椅23,将第二排多功能救生座椅23的触发器22安装到第一排多功能救生座椅23后面1.5米处，将第三排多功能救生座椅23的触发器22安装在第一排多功能救生座椅23的定位器外壳15前面,以此类推将所有的触发器22安装好,这样在每一排多功能救生座椅23启动后就能和前一排的多功能救生座椅23拉开一个安全距离,而前面一排多功能救生座椅23的触发器22由后一排的多功能救生座椅23上面的定位器外壳15来触发。
救生出口5设计为长方形，并设有可以起气密作用的凹槽,救生出口5的尺寸以可轻松通过一排多功能救生座椅23为宜,在救生出口5的内壁上安装有多个保险器8,每个保险器8通过连杆10紧密相连并连结在电液作动器12上,电液作动器12的控制开关设在驾驶员的操作台上,当驾驶员打开控制开关时,电液作动器12即可将保险器8打开,救生仓门6便可开启,在救生出口5的适当位置安装有触发器22,在救生仓门6开启时,触发器22便会被触发，使多功能救生座椅23即刻启动。
救生仓门6设计为可伸缩折叠的形式,通过合页7固定在救生出口5上,在救生仓门6的边缘设有挂钩11,当救生仓门6与救生出口5闭合时,将保险器8的卡臂卡入挂钩11中并顶紧,以保证能够气密受压,救生仓门6通过电液作动器12可自动闭合。
触发系统由触发器22、软轴拉线21、保险器19、复位力臂18、定位器16、定位器外壳15、启动开关17组成。其中触发器22、软轴拉线21、保险器19固定在轨道14上,而保险器19则是一个可以同时控制轨道14两则的复位力臂18的部件;复位力臂18是通过复位弹簧作功而设置在多功能救生座椅23上面；定位器16和启动开关17设置在定位器外壳15内,启动开关17则设置在定位器16的下方,定位器外壳15设置在多功能救生座椅23上面,定位器16的力臂卡在复位力臂18的卡槽中,复位力臂18的末端卡在保险器19的挂钩上,保险器19通过软轴拉线21连结在触发器22上；触发器22一但被触发便会拉动保险器19与复位力臂18分离,复位力臂18即刻将定位器16压下落在启动开关17上面,使启动开关17通电并使启动电机53启动,同时多功能救生座椅23与轨道14分离。
启动开关17的电源连结在高铁电池组55上面,另一端连结在闭合开关52上面,闭合开关52的另一端连结在启动电机53上面,闭合开关52和控制器51设置在多功能救生座椅23的底架24上面,控制器51是由力臂、滑轮和复位弹簧组成,滑轮作用在轨道14上,一但控制器51的滑轮与轨道14脱离,控制器51便会通过复位弹簧作用在闭合开关52上,使闭合开关52的电源断开,使启动电机53停转。
多功能救生座椅23是一个采用电池组和启动电机53为动力的救生器,本发明的电池组采用高铁电池组55，即在高铁上使用的电池组；其主要结构分为座椅23和底架24两大部分。座椅23上面安装有救生伞39、抛伞枪42、安全防护罩36、安全带35、气囊38、托架30、脚踏板31；救生伞39的伞绳40分别固定在多功能座椅23的靠背上和扶手前端的挂环41上及保险器49上,在救生伞39的下边和靠背的中部及底架24的底部安装有气囊38；每具抛伞枪42可连结两具或多具救生伞39;安全防护罩36通过齿牙定位器37可以上下收放,并在安全防护罩36内设有氧气呼吸器,安全带35装在座椅23的靠背上,并在靠背的顶端安装有信号发射器；座垫34设计为充气包式,托架30安装在座椅23上并且可以收放,在托架30的两则安装有固腿护架32,固腿护架32是一个装有齿牙定位器的通过手动操作的护具,其上装有控制拉手33；脚踏板31安装在托架30上面,并且可通过脚尖挑动脚踏板31控制托架30进行收放。
在底架24两边的扶手内则安装有压腿护架28,压腿护架28是通过齿牙定位器和复位弹簧进行手动拉开自动闭合的安全护具,其上设有控制拉手29,压腿护架28的作用是在载客飞机1突然发生意外情况时使乘客不至于被甩出多功能救生座椅23;在底架24的底部安装有气囊38、高铁电池组55、智能充电器54和启动电机53,其中启动电机53安装在靠近轨道14的一则,而智能充电器54是一个可以自动启动和断开并且恒压恒流的充电器,并通过插销和插座联通安装在轨道14上的电源线；底架24较长一则的扶手上端设有一个可收放的托盘27,前端设有大合页25,底架24通过大合页25连在一起,并且可以张合,在大合页25的底部装有一个带复位弹簧的齿牙定位器26,可以使底架24之间自动张开并定位。
在安装有大合页25的扶手的后端安装有卡销托架45和卡销47,卡销托架45安装在一则的扶手上,卡销47上缚有稳定弹簧并安装在卡销托架45上,挂钩48安装在另一侧的扶手上,挂钩48从卡销托架 45中穿过被卡销47卡住时两个底架24便并联在了一起,卡销47将挂钩48放开时两个底架24便会通过大合叶25和齿牙定位器26自动张开并卡住,卡销托架45和卡销47及挂钩48上下各装一套,卡销47通过软轴拉线21连结在装在扶手前部上端的保险器49上,保险器49的另一端连结在伞绳40上,在伞绳40受力拉紧时,保险器49便会通过软轴拉线21将卡销47拉动将挂钩48释放,底架24便会通过大何页25及齿牙定位器26自动张开并定位。
控制器51是由复位弹簧、控制臂及滑轮组成并安装在底架24的扶手上, 在控制器51的上方适当位置安装有启动开关50,控制器51的滑轮作用在轨道14上,当控制器51的滑轮一但脱离轨道14，控制器51便会击打在启动开关50上,启动开关50的电源连结在高铁电池组55上,另一端连结在抛伞枪42的电子引芯上和气囊38的电子引芯上以及信号发射器上,气囊38的电子引芯是一个可以延时两秒爆发的电子引芯,在启动开关50启动时抛伞枪42便会即刻爆发将救生伞39拉出,同时气囊38也会延时两秒打开,信号发射器便会发出求救信号。
每排多功能救生座椅23分为两组,每组通过大合页25和卡销托架45卡销47及挂钩48并联在一起,两组之间的连结是以同样的方法连结并销固,卡销47通过软轴拉线21连结在保险器49上面。多功能救生座椅23在功能不减的情况下也可以设计成其它样式,动力也可以采用其它动力,如采用高压储气瓶和空压启动机等;在将多功能救生座椅23安装到轨道14上时应当与地板保持一定距离,以防多功能救生座椅23在启动后因地板上有物品影响而不能正常通过；多功能救生座椅23在启动出仓时以排为单位一出一排,其它的紧跟着象多米诺骨牌一样鱼贯而出,大约须要30秒左右一架大型载客飞机1的全部乘客和飞行员的救生出仓过程便可完成,在每一排多功能救生座椅23的救生伞39打开的同时,每一排多功能救生座椅23即会通过设置在中间位置的卡销托架45和卡销47及挂钩48分开成为两组,每组多功能救生座椅23通过大合页25和齿牙定位器26自动张开并定位,这样就使每组多功能救生座椅23在空中自动合围成一个圈形,设置在其上的气囊38就会成功的起到安全保护作用,在陆地上防碰撞,在水中安全飘浮。
实施例1：
如图1、图2、图3、图4、图5、图6、图7、图15所示，第一步,首先将载客飞机1传统的鸡嘴形机尾设计成鸭嘴形机尾2或燕尾形机尾3,并在鸭嘴形机尾2或燕尾形机尾3的两侧设置方向舵,即双垂尾4,在鸭嘴形机尾2的上部适当位置或燕尾形机尾3的中间开设救生出口5和救生仓门6,这样就使多功能救生座椅23在紧急出仓开伞时畅通无阻。将带齿牙的工字形轨道14按照所需要的数量间隔适当距离并列平行安装在载客飞机1的机仓中部,两侧设置为走道13,并将中间的两条轨道14连通驾驶仓,轨道14的末端根据鸭嘴形机尾2或燕尾形机尾3的具体结构设计成相应的形状并连通救生出口5。将电液作动器12的启动开关安装在驾驶仓的操作台上适当位置。
第二步,如图8、图9、图10、图11、图12、图13、图15所示,将组装好的多功能救生座椅23通过大合页25和卡销托架45、卡销47及挂钩48并联到一起,然后将并联好的一排多功能救生座椅23从轨道14的末端穿入,并将多功能救生座椅23放到预安装的位置,以此类推,将每一排多功能救生座椅23都穿在轨道14上。
第三步,如图5、图6、图7、图10、图11、图12、图14所示,安装保险器19、软轴拉线21和触发器22,将安装在多功能救生座椅23、底架24上的复位力臂18的末端卡在保险器19的挂钩上,这样使复位力臂18将定位器16撬起和轨道14上的齿牙顶在一起,从而使多功能救生座椅23固定在轨道14上,将载客飞机1最后一排多功能救生座椅23的触发器22安装在救生出口的适当位置,使救生仓门开启时即被触发,最后将启动开关17和启动开关50的电源连结在高铁电池组55的接线柱上,将智能充电器54的插销插入设置在轨道14上的电源插座上 。
实施例2：
如图1、图2、图3、图4、图5、图6、图7、图8、图9、图10、图11、图12、图14、图15、图16所示， 当载客飞机1在空中出现紧急情况时,由于压腿护架28将乘客压在多功能救生座椅23上面不会被甩出去,只需要乘客用手将固腿护架32按下将腿固定住,将安全带35扣住,再将安全防护罩36拉下并戴上氧气呼吸器,驾驶员将启动开关按下救生仓门6便即刻被打开并触动触发器22将多功能救生座椅23启动,使多功能救生座椅23按设定的顺序鱼贯而出,当设置在多功能救生座椅23的底架24上的控制器51脱离轨道14时,控制器51便会压在启动开关50上,同时抛伞枪42便会通电爆发将救生伞39拉出,而气囊38也会通电并延时两秒爆发,同时设置在一排多功能救生座椅23中部的卡销47也会将挂钩48释放,使一排救生座椅23从中间分为两组并通过大合叶页25和齿牙定位器26自动围成两个圈形,同时控制器51也会脱离轨道14击打在闭合开关52上使启动电机53断电并停转.多功能救生座椅23随后便会被安全的降落在地面或水上,装在其上的信号发射器便会按预设的频率发出求救信号。
本救生系统适用于单层载客飞机,同时也适用于双层载客飞机。
 工业实用性
本发明为载客飞机设计一套有效的救生系统，在载客飞机发生紧急情况时使乘客可以安全逃生，具有工业实用性。

Claims (7)

  1. 一种载客飞机空中紧急情况救生系统,其特征在于： 载客飞机（1）的机尾为鸭嘴形机尾（2）或燕尾形机尾（3）；方向舵为双垂尾（4）；所述双垂尾（4）分别设置于所述鸭嘴形机尾（2）或燕尾形机尾（3）的两侧；鸭嘴形机尾（2）的上方或燕尾形机尾（3）的中间设有救生出口(5)及救生仓门（6）；所述救生仓门（6）通过电液作动器(12)伸缩闭合；载客飞机(1)的机仓内设多条并列平行的带齿牙的工字形轨道(14)；所述工字形轨道(14)从驾驶仓直通救生出口（5）；载客飞机（1）的机仓中部设置有一列多功能救生座椅（23），两侧设为走道（13）；所述多功能救生座椅（23）以排为单位并联在一起，通过滑轮（43）、齿轮（44）及定位器（16）固定在轨道（14）上，能够通过触发器（22）触发启动出仓并开伞逃生。
  2. 根据权利要求1所述的一种载客飞机空中紧急情况救生系统,其特征在于：复位力臂（18）的末端卡在保险器（19）的挂钩上，保险器（19）通过软轴拉线（21）连接在触发器（22）上，载客飞机（1）尾部第一排多功能救生座椅（23）的触发器（22）安装在救生出口（5）上，第二排多功能救生座椅（23）的触发器（22）安装在第一排多功能救生座椅（23）后面1.5米处，第三排多功能救生座椅（23）的触发器（22）安装在第一排多功能救生座椅（23）的定位器外壳（15）前面,以此类推，将所有的触发器（22）安装好，每一排多功能救生座椅（23）启动后能够和前一排的多功能救生座椅（23）拉开一个安全距离,前面一排多功能救生座椅（23）的触发器（22）由后一排的多功能救生座椅（23）上面的定位器外壳（15）触发。
  3. 根据权利要求1所述的一种载客飞机空中紧急情况救生系统，其特征在于：触发器（22）的触发系统由触发器（22）、软轴拉线（21）、保险器（19）、复位力臂（18）、定位器（16）、定位器外壳（15）、启动开关（17）组成；所述触发器（22）、软轴拉线（21）、保险器(19)固定在轨道(14)上,保险器(19)可以同时控制轨道（14）两则的复位力臂(18),复位力臂(18)通过复位弹簧设置在多功能救生座椅(23)上,定位器(16)和启动开关(17)设置在定位器外壳(15)内,启动开关（17）设置在定位器（16）的下方,定位器外壳（15）设置在多功能救生座椅（23）上,定位器（16）的力臂卡在复位力臂（18）的卡槽中,复位力臂（18）的末端卡在保险器(19)的挂钩上,保险器(19)通过软轴拉线(21)连接在触发器(22)上,触发器(22)一但被触发便会拉动保险器(19)与复位力臂(18)分离,复位力臂(18)即刻将定位器(16)压下落在启动开关(17)上面,使启动开关(17)通电并使启动电机（58）启动。
  4. 根据权利要求1所述的一种载客飞机空中紧急情况救生系统,其特征在于：启动开关（17）的电源连接电池组,另一端连接在闭合开关（52）,闭合开关（52）的另一端连接启动电机（53）,闭合开关（52）和控制器（51）设置在多功能救生座椅（23）的底架（24）上；所述控制器（51）由力臂、滑轮和复位弹簧组成,滑轮作用在轨道（14）上；控制器（51）的滑轮与轨道（14）脱离时,控制器（51）通过复位弹簧控制闭合开关（52）,使闭合开关（52）的电源断开,启动电机（53）停转。
  5. 根据权利要求1所述的一种载客飞机空中紧急情况救生系统,其特征在于：所述多功能救生座椅（23）是一个采用电池组和启动电机（53）为动力的救生器,其主要结构分为座椅（23）和底架（24）,座椅(23)上面安装有救生伞(39)、抛伞枪(42)、安全防护罩（36）、安全带（35）、气囊（38）、托架（30）、脚踏板（31）, 在安全防护罩（36）内设有氧气呼吸器, 并在靠背的顶端安装有信号发射器, 在托架（30）的两则安装有固腿护架（32）；在底架（24）两边的扶手内侧安装有压腿护架（28）,压腿护架（28）通过齿牙定位器和复位弹簧进行手动拉开自动闭合,其上设有控制拉手（29）,在底架（24）的底部安装有气囊（38）、电池组、智能充电器（54）和启动电机（53）,底架（24）较长一侧的扶手上端设有一个可收放的托盘（27）,前端设有大合页（25）,底架（24）通过大合页（25）连在一起,在大合页（25）的底部装有一个带复位弹簧的齿牙定位器（26）,可以使底架（24）之间自动张开并定位,多功能救生座椅（23）的动力也可以采用高压储气瓶和空压启动机。
  6. 根据权利要求1所述的一种载客飞机空中紧急情况救生系统,其特征在于：在安装有大合页（25）的扶手的后端安装有卡销托架(45)和卡销(47),卡销托架(45)安装在一则的扶手上,卡销（47）上缚有稳定弹簧并安装在卡销托架（45）上,挂钩（48）安装在另一侧的扶手上,挂钩（48）从卡销托架（45）中穿过被卡销（47）卡住时两个底架（24）并联在一起；卡销（47）将挂钩（48）放开时两个底架（24）通过大合页（25）和齿牙定位器（26）张开并卡住,卡销托架（45）和卡销（47）及挂钩（48）上下各装一套,卡销（47）通过软轴拉线（21）连接在装在扶手前部上端的保险器（49）上,保险器（49）的另一端连接在伞绳（40）上。
  7. 根据权利要求1所述的一种载客飞机空中紧急情况救生系统,其特征在于：所述控制器（51）安装在底架（24）的扶手上, 在控制器（51）的上方设置有启动开关（50）,控制器（51）的滑轮作用在轨道（14）上；当控制器（51）的滑轮脱离轨道（14）,控制器（51）击打在启动开关（50）上,启动开关（50）的电源连接在电池组上,另一端连接在抛伞枪（42）的电子引芯和气囊（38）的电子引芯以及信号发射器,气囊（38）的电子引芯是一个可以延时两秒爆发的电子引芯,在启动开关（50）启动时抛伞枪（42）即刻爆发将救生伞（39）拉出,同时气囊（38）也会延时两秒打开,信号发射器便会发出求救信号。
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