CN2767324Y

CN2767324Y - Civil aviation airplane with self-rescue function

Info

Publication number: CN2767324Y
Application number: CN 200420111281
Authority: CN
Inventors: 余祖文
Original assignee: Individual
Current assignee: Individual
Priority date: 2004-11-09
Filing date: 2004-11-09
Publication date: 2006-03-29
Anticipated expiration: 2014-11-09

Abstract

The utility model relates to a civil aviation passenger airplane with a life-saving function. An airplane compartment is composed of three cambered plates, a compartment wall of a bottom compartment, and two symmetrical movable compartment walls of an upper compartment, wherein the movable compartment walls can be opened and closed, and electric hydraulic devices which are specially used for controlling the open and the closure of each movable compartment wall of the upper compartment are arranged in the bottom compartment and the upper compartment. Passenger seats in the airplane compartment are arranged in a protecting compartment, the protecting compartment is installed on a bottom plate of the airplane compartment through a seat disk of a rubber lattice, and a parachute is arranged on the protecting compartment. When the passenger airplane encounters an especially dangerous case, an operating button of the hydraulic device is pressed by a driver, the strong air pressure in an air storing barrel instantaneously passes through a bidirectional hydraulic cylinder, a pushing and pulling rod in a column type piston barrel is quickly pushed out through an air inlet pipe of a hydraulic pipe, and then, the open-close type compartment wall of the upper compartment can be opened; at this time, the parachute which is exposed on the top of the protecting compartment is instantaneously sucked to the air by the air flow, each protecting compartment which is inserted into the seat disk of the rubber lattice is integrally and quickly disengaged from an airplane body which quickly falls under the traction of large resistance of the parachute, and then, each protecting compartment which is used for carrying passengers can safely carry out soft landing. The utility model increases the safety of civil aviation passenger airplanes, and can be used for civil aviation passenger airplanes of various models.

Description

Airline carriers of passengers with the function of saving oneself

Technical field

The utility model relates to a kind of aircarrier aircraft, a kind of specifically airline carriers of passengers with the function of saving oneself.

Background technology

According to statistics, aircraft is the highest transportation means of safety factor in the public transport means (automobile, steamer and train), but because the structure in the airline carriers of passengers cabin of existing various models is the sealed type cylindrical shape, the lifesaving appliance of parachute class all can not be set, in a single day therefore dangerous situation aloft takes place, the possibility of surviving is just very remote.

Summary of the invention

The utility model purpose is to provide a kind of airline carriers of passengers with the function of saving oneself.

The technical scheme that the utility model solves the problems of the technologies described above is: a kind of airline carriers of passengers with the function of saving oneself, comprise the cabin, seat in the cabin and cabin base plate, the cabin is the O-ring tubular, cabin base plate in the cabin is divided into the hold of its below and the upper-deck cabin of its top with the cabin, it is characterized in that described cabin is by three arcs--but the upper-deck cabin detachable bulkhead of two symmetries of hold bulkhead and folding combines, the upper-deck cabin detachable bulkhead adopts loose-leaf structure to be connected with the junction of hold bulkhead, and the folding intersection of arc limit, two upper-deck cabin detachable bulkhead tops mouth adopts mutual connection rubber pad lamination mouth array mode; Be provided with the electro hydraulic gear of special control upper-deck cabin detachable bulkhead folding in hold and the upper-deck cabin; Passenger seat in the cabin all is contained in the protection cabin, and the protection cabin is installed on the base plate of cabin by rubber lattice attic base, and protection is equipped with parachute on the cabin; Driver's seat then directly is installed on the base plate of cabin by rubber lattice attic base, and the back of seat is provided with parachute; On each rubber lattice attic base bottom surface supply hub is arranged, there are one and the cooresponding attaching plug of supply hub in each protection bilge portion.

Described electro hydraulic gear by high-energy accumulator jar (electrical motor special use), air pressure convertible valve folding joystick, electrical motor, Air compressor, two-way hydraulic cylinder, hold device of air, hydraulic pressure air inlet pipe, hydraulic pressure muffler and pillar piston barrel and form; Accumulator jar and electrical motor link together, and the folding button of accumulator jar is contained on the interior operator's station of driving compartment; Electrical motor links to each other with Air compressor, and Air compressor is connected by the pneumatics pipeline with two-way hydraulic cylinder with air tank, air tank, and the air pressure convertible valve is housed between air tank and the two-way hydraulic cylinder; The air pressure convertible valve links to each other with air pressure convertible valve folding joystick; Two-way hydraulic cylinder is communicated with hydraulic pressure air inlet pipe and hydraulic pressure muffler; The pillar piston barrel by the hydraulic pressure air inlet bronchus that links to each other with the hydraulic pressure air inlet pipe be connected with two-way hydraulic cylinder with hydraulic pressure return-air bronchus that the hydraulic pressure muffler is communicated with; The pillar piston push-pull rod is housed in the pillar piston barrel, and pillar piston barrel and pillar pull bar thereof are fixed on the base plate of cabin by the pull bar pedestal, and the top of pillar pull bar is connected with the upper-deck cabin detachable bulkhead.

But cabin, described protection cabin body front end has the emissive plastic glazing of a folding, and the side is a hatch door; The foam balance block is equipped with in protection body lower end, cabin, cabin, and the semisphere elasticity bilge then is equipped with in its bottom; The parachute at body top, cabin has two: main chute and auxiliary parachute, wherein auxiliary parachute is being buckled with a belt that snap-fastener arranged through folding back and is being lain in the top, cabin, the other end of belt be draw ring pierce into by its top and protect in the cabin; Seat front end in the bulkhead is equipped with a folding oblong chain-wales.

Also be provided with lamps and lanterns, global positioning system, distress signal lamp in the described protection cabin.

The utility model has at first been broken existing all enclosed general layouts in airline carriers of passengers cabin both at home and abroad in the design in passenger plane cabin, engine room bulkhead is designed to opening and closing type, and airliner seat is arranged to have the protection cabin of parachute.During the aircraft standby for takeoff, the control button of chaufeur primer fluid pressure device, electrical motor running rapidly also drive the Air compressor running simultaneously, and input also stores in air tank the strong gas pressure that moment produced through air-pressure tube.When the passenger plane in the aerial flight of height runs into especially big dangerous situation; as long as chaufeur is pressed the control button of hydraulic efficiency gear; strong gas pressure moment in the air tank is by the operation of two-way hydraulic cylinder forward; apace the pull bar in the pillar piston barrel is released through the hydraulic pipe air inlet pipe; thereby opening and closing type upper-deck cabin bulkhead is opened; the parachute suction on the top, protection cabin that windstream moment of this moment just will expose is in the air; each is assigned into protection cabin in the rubber lattice attic base thereupon under the involving of parachute large drag forces, hightails with the animal economy formula of quick tenesmus.Failed in time to break away from the protection cabin in cabin even have at that time; as long as the passenger spurs the draw ring of standby parachute; this moment, huge standby parachute strengthened the resistance of air; heaving out the protection cabin breaks away from itself and cabin or the passenger plane that is reversed tenesmus is dished out out of my cabin fast; its parachute also can be opened in air flow automatically in upset, makes the soft landing of manned protection cabin energy safety.

The utility model has greatly increased the safety of airline carriers of passengers, can be widely used in the airline carriers of passengers of various models.

Description of drawings

Fig. 1 is the utility model integral structure scheme drawing

Fig. 2 is a cut-away view in the utility model upper-deck cabin

Fig. 3 opens scheme drawing for the utility model upper-deck cabin bulkhead

Fig. 4 is the utility model hydraulic piston pull bar and engine room bulkhead connection diagram

Fig. 5 arranges scheme drawing for the utility model protection cabin

Fig. 6 is the utility model protection cabin structure scheme drawing

Fig. 7 is the utility model driver's seat structure scheme drawing

Fig. 8 is the utility model electro hydraulic gear principle of work scheme drawing

The specific embodiment

As Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6 and shown in Figure 7, a kind of airline carriers of passengers with lifesaving function, bulkhead with integral seal cylindrical shape fuselage 1 both sides of existing airline carriers of passengers, is the movable axis point along wing top central longitudinal to axial location, with body upper circular arc top, longitudinally line of centers is cut into 2/2nds arcs of semicircle; Again with the central axis incision longitudinally of the bulkhead above the wing of fuselage both sides (position that cabin two walls will cut is the main cabin and controls the cabin), the columnar cabin of original sealed type has been become by three arc bulkheads 15,16 to combine, upper-deck cabin detachable bulkhead 15 adopts hinge axis 12 to be connected with the junction of hold bulkhead 16, the rubber spacer 14 of leakproof is equipped with in the folding intersection of arc limit, two upper-deck cabin detachable bulkhead 15 tops mouth, and bulkhead 15 can avoid the infiltration of rainwater etc. in the activity of fuselage after cutting out like this; Be provided with the electro hydraulic gear 4 of special control upper-deck cabin detachable bulkhead folding in the hold 5 of fuselage 1 and the upper-deck cabin 6; Passenger seat 31 in the upper-deck cabin 6 all is contained in the protection cabin 9, and protection cabin 9 is installed on the base plate of cabin by rubber lattice attic base 11; Protection is equipped with parachute 8 on the cabin 9; The 10th, the window on the detachable bulkhead 15; Driver's seat then directly is installed on the base plate of cabin by rubber lattice dish 11, and rubber lattice attic base 11 usefulness spiral nails are fixed on the cabin base plate 7; The back of driver's seat is provided with parachute 55; On each rubber lattice attic base 11 bottom surface supply hub 32 is arranged, one and supply hub 32 cooresponding attaching plugs 29 are arranged at each protection 9 bottom, cabin.

One under the utility model cabin base plate 7 is hold 5 bulkheads 16, two on the cabin base plate 7 is upper-deck cabin 6 detachable bulkheads 15 of symmetry, upper-deck cabin detachable bulkhead 15 adopts hinge axis 12 to be connected with the junction of hold 5 bulkheads 16, two upper-deck cabin bulkheads 15 are opening and closing type, and the folding intersection of its arc limit, top mouth adopts mutual connection rubber spacer 14 to press a mouthful array mode; The electro hydraulic gear 4 that 15 foldings of special control upper-deck cabin bulkhead are arranged in hold and the upper-deck cabin; Seat 31 in the upper-deck cabin 6 all is contained in the protection cabin 9, and protection cabin 9 is installed on the cabin base plate 7 by rubber lattice attic base 11, and protection is equipped with parachute 8 on the cabin 9; On each rubber lattice attic base 11 bottom surface supply hub 32 is arranged, there are one and supply hub 32 cooresponding attaching plugs 29 in each protection bilge portion.

By the control that is connected of a plurality of scalable hydraulic pressure pillar piston push-pull rod 17 of electro hydraulic gear 4, each telescopic pillar piston push-pull rod 17 is sleeved in the pillar piston barrel 42 and is fixed on the cabin base plate 7 by pull bar pedestal 20 respectively respectively in the folding of the detachable bulkhead 15 of fuselage 1 both sides.The various supply lines of nacelle top all adopt the circuit card form to be connected with modes such as docking slot.The utilization of this power supply mode is convenient to the fuselage detachable bulkhead and is not affected when opening and closing.

Start the button 3 of electro hydraulic gear when the person of controlling after, connect accumulator jar 35, electrical motor 37 rapid runnings also drive Air compressor (high pressure pump type) running simultaneously, and the strong gas pressure that moment produced is imported and stored in air tank through the pneumatics pipeline.When chaufeur need be opened the detachable bulkhead of fuselage, as long as press " opening " control button, the former strong gas pressure that stores in air tank moves by the two-way hydraulic cylinder forward, (shape and function class eject fast like jack "); like this; the detachable bulkhead of body upper both sides is pushed to both sides in application force following moment of pull bar, and at this moment nacelle top has just formed the spaces of 150 degree to make superpower air-flow turn to raft and hydraulic pressure air inlet pipe will be connected the pull bar of all pillar pistons of bulkhead through air pressure.

After chaufeur is pressed the Close button once more, the power system running drives the two-way hydraulic cylinder inverted running, strong gas pressure in the piston barrel will be extracted out by air pump, pull bar will be retracted in the piston barrel again, the detachable bulkhead that makes former two sides split into 150 degree gaps will be joined by pull-up again under the antagonistic force of pull bar, recovers original closed state.

As Fig. 2, shown in Figure 3, parachute 8 is contained in the top in protection cabin 9, the parachute 8 outer protective cases 13 that are with; The front portion in protection cabin 9 is an emissive plastic glazing 21, and protection cabin 9 is installed on the cabin base plate 7 by lattice attic base 11; Upper-deck cabin detachable bulkhead 15 is connected by hinge axis 12 with following cabin bulkhead 16; Rubber waterproof bed course 14 is equipped with at two fan detachable bulkhead junction surfaces.

As Fig. 5, shown in Figure 6, be the structural representation in protection cabin 9 and the distribution schematic diagram in the cabin thereof.Protection cabin 9 in the cabin is selected a large amount of pmma materials and light weight, wear-resisting for use as automobile bucket type driving compartment, and the alkali-free glass fibre combination of materials with anti-impact force is made, to increase the daylighting scope in protection cabin.Single formula is adopted in each protection cabin 9, arranges in order, and the order of its arrangement is two row longitudinally arranged side by side in the middle of the cabin; the walkway is respectively stayed on both sides; arrange delegation near the both sides, cabin, arrangement can make the door in each protection cabin can both be close to the walkway like this, is convenient to people's turnover.Between each protection cabin 9 and cabin base plate, fixing all around each 20 cm thick made from flexible materials such as rubber; 30 centimetres high square grid attic base 11; on the bottom surface in the middle of each lattice attic base 11 place's supply hub 32 is arranged; an attaching plug 29 is arranged at the bottom in each protection cabin; when the protection cabin is put in this square grid attic base; attaching plug 29 will inject in the supply hub 32 of cabin base plate; make its energized; do not influence the as usual work of electricity consumption facility in the protection cabin, make protection cabin 9 when the disengaging cabin, not be subjected to pullling of circuit to influence (sunflower seed that its principle does not also break away from floral disc in as the sunflower on the open country) again.The use of rubber lattice attic base 11 can be controlled at the place that needs arrangement with protection cabin 9 respectively, can not be moved taking off rising or landing ceiling board plane inclination on opportunity because of aircraft, simultaneously again can be convenient and swift, unaffected when breaking away from the cabin.

There is ornamental flexible foam protection bed course the inside in protection cabin 9; damping spring will be installed respectively by the foot rest bottom of each seat; the bottom in protection cabin 9 is equipped with the double-deck semisphere rubber bottom 34 that slows down impulsive force when landing; protection is equipped with the liquid crystal display shift knob 28 that illuminator lamp 22 and top, cabin signal lamp 25 are installed in foam balance block 30 cabins around 9 lower parts, cabin; the power supply of signal lamp 25 is the high-octane lithium celies of chargeable property, and a GPS (Global Position System) (EGNOS) 23 all is equipped with at the top in each protection cabin 9.On each seat 31 protection in front cabin inwall a folding oblong chain-wales 33 is installed, as having dinner etc.Chain-wales 33 top also is equipped with a direction compass, time clock, a track chart, but its wall is not close in the time spent pull-up.

The top in each protection cabin 9 respectively be one group of two parachute 8 (main chute, an auxiliary parachute) through having folded; the 24th, the parachute rope, the wide cut area of its parachute is enough to bear human body to add the moderate of total weight descending speed of protecting the cabin is standard to open the air resistance that produced of back at main chute.The other end that standby parachute is being buckled the top that lies in the protection cabin, belt through folding back with the belt of a band snap-fastener be draw ring pierce into by the top and protect in the cabin, be placed between the handrail of seat, control by passenger oneself.Protection all master cock buttons in the cabin all are installed on the handle 27 of the handrail 28 on limit, seat and Men Nei, so that can grasp control and use timely when any dangerous situation occurring in the flight way.Being placed on protection top, cabin at ordinary times is covered with by the parachute protective case 13 below the nacelle top through the parachute after folding; parachute will expose out thereupon after passenger plane is opened detachable bulkhead; be convenient to be inhaled in the air, thereby finish its peculiar mission given by air flow.

As shown in Figure 7; chaufeur can not be with protecting the cabin because of the restriction of its working space; but directly using special seat and rubber lattice attic base 11 devices, parachute 55 just is contained in the umbrella case 54 behind the chair back of spring 49 and spring springboard 48, and the foam balance block 50 with buoyancy has been installed around the seat.The control handle 52 of spring springboard 48 just is installed in below the handrail of seat.Distress signal lamp 46 and global position system 47 all are placed in the top of seat back, when chaufeur is prepared to abandon machine, as long as press the control handle 52 of lower spring springboard 48, the case lid 45 that just can go out umbrella case 54 upper ends ejected parachute 55 and opened 48 moments of spring springboard, after the detachable bulkhead in cabin is opened, thereby parachute is just taken chaufeur out of purpose that the cabin reaches escape together with seat.The 53rd, safety belt, the 51st, distress signal button.

As Fig. 8 and shown in Figure 4, be hydraulic efficiency gear of the present utility model, form by air pressure convertible valve folding joystick 2, high-energy accumulator jar 35, electrical motor 37, Air compressor 38, air tank 39, two-way hydraulic cylinder 41, hydraulic pressure air inlet pipe 43, hydraulic pressure muffler 44 and pillar piston barrel 42; Accumulator jar 35 and electrical motor 37 link together by electric wire, and the folding button 3 of accumulator jar is contained on the gauge panel in the driving compartment; Electrical motor 37 links to each other with Air compressor 38, and Air compressor 38 is connected by pneumatics pipeline 36 with two-way hydraulic cylinder 41 with air tank 39, air tank 39, between air tank 39 and the two-way hydraulic cylinder 41 air pressure convertible valve 40 is housed; Air pressure convertible valve folding joystick 2 is connected with air pressure convertible valve 40; Two-way hydraulic cylinder 41 is communicated with hydraulic pressure air inlet pipe 43 and hydraulic pressure muffler 44; Three pillar piston barrels 42 by the hydraulic pressure air intake branch 18 that is communicated with hydraulic pressure air inlet pipe 43 be connected with two-way hydraulic cylinder 41 with hydraulic pressure return-air arm 19 that hydraulic pressure muffler 44 is communicated with; Pillar piston push-pull rod 17 is housed in the pillar piston barrel 42, and pillar piston barrel 42 and pillar pull bar thereof are fixed on the cabin base plate 7 by pull bar pedestal 20, and the top of pillar pull bar 17 is connected with upper-deck cabin detachable bulkhead 15.

This cover special electric hydraulic efficiency gear of airline carriers of passengers is not subjected to the interference and the control of other hydraulic efficiency pressure system, has and overlaps independently operation procedure, works under the instruction of chaufeur.The purpose that designs this covering device is in order to make the high aerial passenger plane that flies when especially big dangerous situation takes place, fast and effeciently to start, open the detachable bulkhead of passenger plane, making the parachute band protection cabin fast speed and be out of danger.

Claims

1, a kind of airline carriers of passengers with the function of saving oneself, comprise seat and cabin base plate in cabin, the cabin, the cabin is the O-ring tubular, cabin base plate in the cabin is divided into the hold of its below and the upper-deck cabin of its top with the cabin, it is characterized in that but described cabin is combined by the upper-deck cabin detachable bulkhead of two symmetries of three arcs, one hold bulkhead and folding, the upper-deck cabin detachable bulkhead adopts loose-leaf structure to be connected with the junction of hold bulkhead, and the folding intersection of arc limit, two upper-deck cabin detachable bulkhead tops mouth adopts mutual connection rubber pad lamination mouth array mode; Be provided with the electro hydraulic gear of special control upper-deck cabin detachable bulkhead folding in hold and the upper-deck cabin; Passenger seat in the cabin all is contained in the protection cabin, and the protection cabin is installed on the base plate of cabin by rubber lattice attic base, and protection is equipped with parachute on the cabin; Driver's seat then directly is installed on the base plate of cabin by rubber lattice dish, and the back of seat is provided with parachute; On each rubber lattice attic base bottom surface supply hub is arranged, there are one and the cooresponding attaching plug of supply hub in each protection bilge portion.

2, airline carriers of passengers as claimed in claim 1, it is characterized in that described electro hydraulic gear by high-energy accumulator jar, air pressure convertible valve folding joystick, electrical motor, Air compressor, two-way hydraulic cylinder, hold device of air, hydraulic pressure air inlet pipe, hydraulic pressure muffler and pillar piston barrel and form; Accumulator jar and electrical motor link together, and the folding button of accumulator jar is contained on the interior operator's station of driving compartment; Electrical motor links to each other with Air compressor, and Air compressor is connected by the pneumatics pipeline with two-way hydraulic cylinder with air tank, air tank, and the air pressure convertible valve is housed between air tank and the two-way hydraulic cylinder; The air pressure convertible valve links to each other with air pressure convertible valve folding joystick; Two-way hydraulic cylinder is communicated with hydraulic pressure air inlet pipe and hydraulic pressure muffler; The pillar piston barrel by the hydraulic pressure air inlet bronchus that links to each other with the hydraulic pressure air inlet pipe be connected with two-way hydraulic cylinder with hydraulic pressure return-air bronchus that the hydraulic pressure muffler is communicated with; The pillar piston push-pull rod is housed in the pillar piston barrel, and pillar piston barrel and pillar pull bar thereof are fixed on the base plate of cabin by the pull bar pedestal, and the top of pillar pull bar is connected with the upper-deck cabin detachable bulkhead.

3, airline carriers of passengers as claimed in claim 1, but it is characterized in that cabin, described protection cabin body front end has the emissive plastic glazing of a folding, and the side is a hatch door; The foam balance block is equipped with in protection body bottom, cabin, cabin, and the semisphere elasticity bilge then is equipped with in its bottom; The parachute at body top, cabin has two: main chute and auxiliary parachute, wherein detaining a belt that snap-fastener is arranged on the Zhe Die auxiliary parachute, auxiliary parachute lies in cabin top, the other end of belt be draw ring pierce in the protection cabin by its top; Seat front end in the bulkhead is equipped with the folding oblong chain-wales of a people.

4, airline carriers of passengers as claimed in claim 3 is characterized in that also being provided with in the described protection cabin lamps and lanterns, global positioning system, distress signal lamp.