CN109927913A - A kind of aircraft intelligent escape seat - Google Patents
A kind of aircraft intelligent escape seat Download PDFInfo
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- CN109927913A CN109927913A CN201910345374.XA CN201910345374A CN109927913A CN 109927913 A CN109927913 A CN 109927913A CN 201910345374 A CN201910345374 A CN 201910345374A CN 109927913 A CN109927913 A CN 109927913A
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- opening
- pedestal
- backrest
- host
- intelligent escape
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The present embodiments relate to a kind of aircraft intelligent escape seats, comprising: pedestal opens up jet port, switch opening and control opening；Backrest opens up propeller opening, air-conditioning opening and oxygen opening；Containing tube；Power supply；Host is electrically connected to a power source；Driving motor；Propeller, including shaft, lantern ring and blade, shaft rod upper sleeve are equipped with support ring, and shaft is connect with driving motor；Electric pushrod is installed in support ring, connect with lantern ring；Jet-propelled ejector, corresponding jet port；Control switch is installed in switch opening；Control panel is installed in control opening；Shield covers at intelligent escape seat.The intelligent escape seat aircraft occur dangerous situation and it is out of control in the state of, cabin is flown away from controllable intelligent escape seat fire, protects personal personal safety.
Description
Technical field
The invention belongs to aircraft seat design fields, and in particular to a kind of aircraft intelligent escape seat.
Background technique
Airplane crash refers to that aircraft etc. awing breaks down, meets with disaster caused by natural calamity or other contingencies.
Refer to as a consequence of an irresistible cause or aviation accident caused by human factor, and the thus casualties and property of bringing on a disaster property
Loss.
There are also " airplane falling event " or " aviation accidents " for vocabulary usually identical with " airplane crash " meaning.To various in Chinese
Aircraft include various manned aviation aircrafts take off, fly or descent in, due to human factor or irresistible
Catastrophic loss caused by reason is referred to as airplane crash to such event.
After aircraft generation accident, how to escape, become the problem of general public more pays close attention to.In this regard, in the prior art
A kind of modular ejector seat is provided and is related to escape device, and it is an object of the present invention to provide one kind can be fast comprising its escape aircraft
Speed assists passenger to be detached from the modular ejector seat of cabin and the escape aircraft comprising it.Provided modular ejector-seat
Chair includes: seat body and catapult-launching gear；The seat body and the ejection end of the catapult-launching gear fit, and in the bullet
Lower its of ejection effect of injection device can be separated with the catapult-launching gear.Provided escape includes: fuselage, escape window and above-mentioned
Modular ejector seat；The escape window is set on the fuselage；The relatively described escape window fixation of the catapult-launching gear is set
It sets；The seat body is opposite with the escape window just, and the seat body can under the ejection effect of the catapult-launching gear
The fuselage is completely disengaged by the escape window.However, ejector seat and escape device that the prior art provides, are being popped up
Further rescue behave is had no after aircraft, it is difficult to guarantee that passenger's bullet is rescued safely after getting off the plane.
Summary of the invention
The embodiment of the present invention is designed to provide a kind of aircraft intelligent escape seat, solves current escape seat and is detached from machine
Subsequent rescue problem behind cabin.
To achieve the goals above, the embodiment of the present invention provides the following technical solutions:
According to a first aspect of the embodiments of the present invention, a kind of aircraft intelligent escape seat, the intelligent escape seat installing
In in aircraft cabin, the intelligent escape seat includes: pedestal, and shape is cabinet, and the pedestal is placed horizontally at aircraft cabin
Interior, bottom surface, which is spaced apart, is equipped with several jet ports, and the base upper surface offers switch opening and controls opening, under base front surface
Portion is convexly equipped with a foot pedal；Backrest, shape are cabinet, are vertically arranged at base upper surface far from foot pedal one end, the backrest
It is connected on the inside of bottom surface and pedestal, the backrest upper surface middle part offers propeller opening；Containing tube is vertically arranged at backrest
Inside, on the inside of the corresponding pedestal of the containing tube upper port and propeller open communication, lower port；Power supply is installed in described
On the inside of pedestal；Host, be installed on the inside of the pedestal and with the power electric connection, the host internal processor；Driving electricity
Machine, is installed on the inside of the pedestal, and the driving motor is electrically connected to a power source and connect with main-machine communication；Propeller, including it is perpendicular
The lantern ring and be provided at circumferentially spaced along lantern ring and be connected to lantern ring with may be reversed that shaft, the sliding sleeve being directly arranged are set on shaft
The blade of upper surface, the shaft rod upper sleeve below lantern ring are equipped with a support ring, and the shaft upper end extend out to propeller opening
Top, shaft lower end and the driving motor output end are drivingly connected；At least one electric pushrod is installed in the support vertically
Ring upper surface, the output end of electric push rod and lantern ring are drivingly connected, and the electric pushrod is electrically connected to a power source and leads to host
Letter connection；Jet-propelled ejector, is installed in the pedestal inside bottom surface, and ejection end corresponds to the jet port of the pedestal, the spray
Gas formula ejector is electrically connected to a power source and connect with main-machine communication；Control switch is installed in the pedestal switch opening, the control
System switch is electrically connected to a power source, and forms the control being opened and closed to power supply；Control panel is installed in the pedestal control opening, described
Control panel is connect with main-machine communication；Shield, shape are an arc transparent casing, are covered on the intelligent escape seat,
The shield upper end rotation is connected to backrest upper surface；The aircraft cabin cabin top is retractable structure, is formed and is escaped for intelligence
The ejection opening of cabin is flown away from raw seat fire.
Further, backrest front side, which is from top to bottom spaced apart, is equipped with air-conditioning opening and oxygen opening；Accordingly,
The backrest inside upper part is installed with an air-conditioning, and air-conditioner air outlet corresponds to the air-conditioning opening, and the air-conditioning is electrically connected to a power source
And it is connect with the main-machine communication；The backrest middle inside is installed with an oxygenerator, and the oxygen outlet of the oxygenerator is corresponding
The oxygen opening, the oxygenerator are electrically connected to a power source and connect with the main-machine communication.
Further, aircraft cabin ground location is provided with guide rail along cabin length direction, accordingly, the base end face
It is convexly equipped with the pulley matched with the guide rail, forms sliding setting of the intelligent escape seat in cabin.
Further, the shaft is telescopically inserted in containing tube, accordingly, the bottom of corresponding containing tube lower open end
Seat inside bottom surface is installed with a lifting platform, and the driving motor is installed in lifting platform upper surface, and the lifting platform passes through lifting air
Cylinder driving rises or falls, and the lifting cylinder is electrically connected to a power source and connect with main-machine communication；The lantern ring sliding sleeve is set to
Shaft outer wall above support ring, the blade are resisted against accommodating inside pipe wall far from lantern ring one end；Cabin cabin, which opens, opens, institute
It states control panel and jet-propelled ejector starting is controlled by host, aircraft is flown away from the injection of intelligent escape seat, and control panel passes through
Host controls lifting cylinder driving lifting platform and rises, and lifting platform rising drives the shaft upper end for being connected to driving motor to extend out to and leans on
Propeller open outer side is carried on the back, control panel controls electric pushrod by host and lantern ring is driven to move to shaft top, paddle along shaft
Leaf extend out on the outside of containing tube and by blade self weight turning unfolding, and control panel passes through host and controls driving motor driving shaft
It rotates and is driven blade rotation, so that intelligent escape seat hovers above in the air.
Further, pedestal opposing sidewalls lower part offers bar shaped lifebuoy opening, lifebuoy opening respectively
Inside it is installed with inflatable marine life ring, the marine life ring inflating port is towards on the inside of pedestal；Accordingly, on the inside of the pedestal
The position of corresponding marine life ring is installed with an inflator pump, and the inflator pump is electrically connected to a power source and connect with main-machine communication, institute
Inflator pump outlet side is stated to be connected to marine life ring inflating port；Control panel controls inflator pump by host and opens, inflator pump pair
Marine life ring inflation, the marine life ring pop-up lifebuoy opening after inflation, forms to the intelligent escape seat at sea
The support of floating.
Further, backrest upper surface side offers parachute opening, accordingly, the backrest inboard, upright
It is provided with parachute export conduit, the parachute export conduit upper open end and parachute open communication；Pack is installed in
On the inside of the backrest below parachute export conduit lower open end, the corresponding parachute of extractor parachute opening of pack is led
Pipe lower open end；The position that the backrest front corresponds to pack parachute opener offers a parachute-opening mouth, the parachute-opening dress of the pack
It sets and backrest front outside is extend out to by parachute-opening mouth；Passenger's pull parachute opener, extractor parachute drive the main chute in pack by parachute
Export conduit extend out to above backrest upper surface and is unfolded, and forms the support floated in the sky to the intelligent escape seat.
Further, the position that base upper surface corresponds to the control opening is installed with supply case, the control panel lid
Set on supply box opening, the supply case is provided with supply；The supply includes but is not limited to water, food and drug；The bottom
Seat upper surface offers solar panel opening, and accordingly, the position of corresponding solar panel opening is installed with solar panel on the inside of the pedestal
Slot is arranged at intervals with several solar panels in the battery board slot, and several solar panels are filled with power supply respectively
Power port electrical connection, forms the charging to power supply.
Further, pedestal two lateral walls top offers camera shooting opening respectively, accordingly, in camera shooting opening
It is installed with camera, the camera is electrically connected to a power source and connect with main-machine communication, is formed to scape outside intelligent escape seat
The shooting of elephant.
Further, the backrest upper surface offers several distress lights and opens along backrest is circumferentially-spaced close to the position of outer rim
Mouthful, distress light is installed in several distress light openings respectively, the distress light is electrically connected to a power source and connects with main-machine communication
It connects；The distress light is LED distress light；It is installed with the GPS positioning module connecting respectively with processor communication in the host, deposits
Store up module and navigation module.
Further, shield is the heat-insulated bulletproof glass cover of tempering, and the shield end face is with pedestal and by back contacts position
Install and be equipped with sealing ring, accordingly, the pedestal and backrest be provided with shield contact position matched with sealing ring it is close
Sealing groove.
The beneficial effect of the embodiment of the present invention is:
By the matching design of host and injector, in conjunction with the retractable structure on aircraft cabin top, aircraft occur dangerous situation and
In the state of out of control, passenger can control intelligent escape seat fire to fly away from cabin, cooperate the power of propeller, so that intelligent escape
Seat flees from cabin, and can control the safe landing of intelligent escape seat by control panel, can more comprehensively protect individual
Personal safety；
The calcination of dense smoke and high fever is isolated in the design of shield when passenger may make to encounter dense smoke fire behavior, while in safety
Offer is quieter when flight comfortably seizes the opportunity environment, not by noise in cabin, the infringement of peculiar smell and bacterial virus；
The design of air-conditioning and oxygenerator is improved and is relaxed so that the passenger being located in shield is in the air environment of safety
Appropriateness.
Detailed description of the invention
It, below will be to embodiment party in order to illustrate more clearly of embodiments of the present invention or technical solution in the prior art
Formula or attached drawing needed to be used in the description of the prior art are briefly described.It should be evident that the accompanying drawings in the following description is only
It is merely exemplary, it for those of ordinary skill in the art, without creative efforts, can also basis
The attached drawing of offer, which is extended, obtains other implementation attached drawings.
Structure depicted in this specification, ratio, size etc., only to cooperate the revealed content of specification, for
Those skilled in the art understands and reads, and is not intended to limit the invention enforceable qualifications, therefore does not have technical
Essential meaning, the modification of any structure, the change of proportionate relationship or the adjustment of size are not influencing the function of the invention that can be generated
Under effect and the purpose that can reach, should all still it fall in the range of disclosed technology contents obtain and can cover.
Fig. 1 is a kind of structural schematic diagram of aircraft intelligent escape seat provided by the embodiment of the present invention 1；
Fig. 2 stretches for the shaft and blade of propeller in a kind of aircraft intelligent escape seat provided by the embodiment of the present invention 1
Out to the structural schematic diagram above backrest；
Fig. 3 is the schematic diagram of internal structure of backrest in a kind of aircraft intelligent escape seat provided by the embodiment of the present invention 1；
Fig. 4 is that the shaft of propeller and blade extend out to the structural schematic diagram above backrest in Fig. 3；
Fig. 5 is the schematic diagram of internal structure of pedestal in a kind of aircraft intelligent escape seat provided by the embodiment of the present invention 1；
Fig. 6 is extend out to above backrest for parachute in a kind of aircraft intelligent escape seat provided by the embodiment of the present invention 4
Structural schematic diagram；
Fig. 7 is the control planning schematic diagram in a kind of aircraft intelligent escape seat provided by the embodiment of the present invention 1；
Wherein, 1, pedestal, 11, jet port, 12, switch opening, 13, control opening, 14, foot pedal, 15, lifebuoy opens
Mouthful, 16, solar panel opening；
2, backrest, 21, propeller opening, 22, air-conditioning opening, 23, oxygen opening, 24, parachute opening, 25, parachute
Export conduit, 26, parachute-opening mouth, 27, distress light opening, 271, distress light；
3, containing tube；
4, power supply；
5, host, 51, processor, 52, GPS positioning module, 53, memory module, 54, navigation module；
6, driving motor；
7, propeller, 71, shaft, 72, lantern ring, 73, blade, 74, support ring, 75, electric pushrod；
8, jet-propelled ejector；
9, control switch；
10, control panel；
20, shield；
30, air-conditioning；
40, oxygenerator；
50, lifting platform, 501, lifting cylinder；
60, inflator pump；
70, pack, 701, parachute opener, 702, main chute；
80, supply case；
90, battery board slot, 901, solar panel；
91, camera shooting opening, 92, camera.
Specific embodiment
Embodiments of the present invention are illustrated by particular specific embodiment below, those skilled in the art can be by this explanation
Content disclosed by book is understood other advantages and efficacy of the present invention easily.
It should be clear that this specification structure depicted in this specification institute accompanying drawings, ratio, size etc., only to cooperate specification to be taken off
The content shown is not intended to limit the invention enforceable qualifications so that those skilled in the art understands and reads, therefore
Do not have technical essential meaning, the modification of any structure, the change of proportionate relationship or the adjustment of size are not influencing the present invention
Under the effect of can be generated and the purpose that can reach, it should all still fall in disclosed technology contents and obtain the model that can cover
In enclosing.Meanwhile in this specification cited such as "upper", "lower", "left", "right", " centre " term, be merely convenient to chat
That states is illustrated, rather than to limit the scope of the invention, relativeness is altered or modified, and is changing skill without essence
It is held in art, when being also considered as the enforceable scope of the present invention.
Embodiment 1
Referring to FIG. 1 to FIG. 5 and Fig. 7, a kind of aircraft intelligent escape seat provided by the present invention, the intelligent escape seat
Chair is installed in aircraft cabin, and the intelligent escape seat includes: pedestal 1, and shape is cabinet, and the pedestal 1 is placed horizontally at
In aircraft cabin (not shown), 1 bottom surface of pedestal, which is spaced apart, is equipped with several jet ports 11, and 1 upper surface of pedestal offers
Switch opening 12 and control opening 13, the positive lower part of the pedestal 1 are convexly equipped with a foot pedal 14；Backrest 2, shape are cabinet, are erected
1 upper surface of pedestal is directly set to far from 14 one end of foot pedal, is connected on the inside of 2 bottom surface of backrest and pedestal 1, on the backrest 2
Surface middle part offers propeller opening 21；Containing tube 3, is vertically arranged at the inside of backrest 2,3 upper port of containing tube with
21 connection of propeller opening, lower port correspond to 1 inside of pedestal；Power supply 4 is installed in 1 inside of pedestal；Host 5, installing
It is electrically connected in 1 inside of pedestal and with the power supply 4,5 internal processor 51 of host；Driving motor 6 is installed in described
1 inside of pedestal, the driving motor 6 are electrically connected with power supply 4 and communicate to connect with host 5；Propeller 7, including what is be vertically arranged
It lantern ring 72 that shaft 71, sliding sleeve are set on shaft 71 and is provided at circumferentially spaced along lantern ring 72 and turnable is connected to lantern ring
The blade 73 of 72 upper surfaces, is arranged with a support ring 74 on the shaft 71 of 72 lower section of lantern ring, and 71 upper end of shaft is stretched out
To 21 top of propeller opening, 71 lower end of shaft and 6 output end of driving motor are drivingly connected；At least one electric pushrod
75, it is installed in 74 upper surface of support ring vertically, 75 output end of electric pushrod and lantern ring 72 are drivingly connected, described electronic
Push rod 75 is electrically connected with power supply 4 and communicates to connect with host 5；Jet-propelled ejector 8 is installed in 1 inside bottom surface of pedestal, spray
The jet port 11 of the corresponding pedestal 1 in end is penetrated, the jet-propelled ejector 8 is electrically connected with power supply 4 and communicates to connect with host 5；
Control switch 9 is installed in the switch of pedestal 1 opening 12, and the control switch 9 is electrically connected with power supply 4, and power supply 4 is opened in formation
The control closed；Control panel 10 is installed in the control of pedestal 1 opening 13, and the control panel 10 is communicated to connect with host 5；
Shield 20, shape are an arc transparent casing, are covered on the intelligent escape seat, and 20 upper end of the shield rotation connects
It is connected to 2 upper surface of backrest；The aircraft cabin cabin top is retractable structure, is formed and flies away from cabin for intelligent escape seat fire
Ejection opening.
Wherein, 72 sliding sleeve of lantern ring is set to 71 outer wall of shaft for being located at 74 top of support ring, and the blade 73 is separate
72 one end of lantern ring is resisted against 3 inner wall of containing tube.
Further, the position that 1 upper surface of pedestal corresponds to the control opening 13 is installed with supply case 80, the control plane
Plate 10 is covered on the opening of supply case 80, and the supply case 80 is provided with supply；The supply includes but is not limited to water, food and medicine
Product；1 upper surface of pedestal offers solar panel opening 16, accordingly, the position of solar panel opening 16 is corresponded on the inside of the pedestal 1
It sets and is installed with battery board slot 90, several solar panels 901, several sun are arranged at intervals in the battery board slot 90
Energy solar panel 901 is electrically connected with 4 charge port of power supply respectively, forms the charging to power supply 4.
Further, the 1 two lateral walls top of pedestal offers camera shooting opening 91 respectively, and accordingly, camera shooting is opened
Camera 92 is installed in mouth 91, the camera 92 is electrically connected with power supply 4 and communicates to connect with host 5, formed and escaped to intelligence
The shooting of raw seat external sights.
Further, 2 upper surface of backrest offers several distress lights along backrest 2 is circumferentially-spaced close to the position of outer rim
Opening 27 is installed with distress light 271 in several distress lights opening 27 respectively, and the distress light 271 is electrically connected simultaneously with power supply 4
It is communicated to connect with host 5；The distress light 271 is LED distress light；It is installed in the host 5 and is communicated respectively with processor 51
GPS positioning module 52, memory module 53 and the navigation module 54 of connection.
Further, shield 20 is the heat-insulated bulletproof glass cover of tempering, 20 end face of shield and pedestal 1 and backrest 2
Contact position is provided with sealing ring (not shown), and accordingly, the pedestal 1 and backrest 2 are provided with 20 contact position of shield
The seal groove (not shown) matched with sealing ring.
A kind of usage mode of aircraft intelligent escape seat provided by the present invention is as follows:
Aviation accident or it is out of control when, cabin cabin, which opens, opens, and control panel 10 is controlled jet-propelled ejector 8 and opened by host 5
Dynamic, the injection of intelligent escape seat flies away from aircraft to aerial, and control panel 10 controls electric pushrod 75 by host 5 and drives lantern ring 72
71 top of shaft is moved to along shaft 71, blade 73 extend out to 3 outside of containing tube and by the self weight turning unfolding of blade 73, control
Panel 10 is controlled driving motor 6 and driven shaft 71 to rotate and be driven blade 73 by host 5 to be rotated, so that intelligent escape seat disc
It is threaded onto aerial.
The intelligent escape seat, by the matching design of host 5 and jet-propelled ejector 8, in conjunction with aircraft cabin top can
Opening structure, aircraft occur dangerous situation and it is out of control in the state of, passenger can control intelligent escape seat fire fly away from cabin, cooperate
The power of propeller 7 so that intelligent escape seat flees from cabin, and can control intelligent escape seat safety by control panel 10
It lands, can more comprehensively protect personal personal safety；
The design of shield 20, is isolated the calcination of dense smoke and high fever when passenger may make to encounter dense smoke fire behavior, while pacifying
Offer is quieter when full flight comfortably seizes the opportunity environment, not by noise in cabin, the infringement of peculiar smell and bacterial virus；
The design of supply case 80, may make passenger after aircraft is left in ejection, sufficiently be fed, and win longer rescue
Help the time.
Embodiment 2
Aircraft cabin ground location is provided with guide rail (not shown) along cabin length direction, accordingly, 1 bottom surface of pedestal
It is convexly equipped with the pulley (not shown) matched with the guide rail, forms sliding setting of the intelligent escape seat in cabin.
The matching design of intelligent escape seat pulley and guide rail may make intelligent escape seat to keep fire away, and be moved to peace
Aircraft is left in ejection after all positon, guarantees safety pop-up.
Remaining is the same as embodiment 1.
Embodiment 3
The positive side of the backrest 2, which is from top to bottom spaced apart, is equipped with air-conditioning opening 22 and oxygen opening 23；Accordingly, described
2 inside upper part of backrest is installed with an air-conditioning 30, and 30 air outlet of air-conditioning corresponds to the air-conditioning opening 22, the air-conditioning 30 and power supply 4
It is electrically connected and is communicated to connect with the host 5；2 middle inside of backrest is installed with an oxygenerator 40, the oxygenerator 40
Oxygen outlet corresponds to the oxygen opening 23, and the oxygenerator 40 is electrically connected with power supply 4 and communicates to connect with the host 5.
The design of air-conditioning 30 and oxygenerator 40 mentions so that the passenger being located in shield is in the air environment of safety
High degree of comfort.
Remaining is the same as embodiment 1.
Embodiment 4
The 1 opposing sidewalls lower part of pedestal offers bar shaped lifebuoy opening 15 respectively, and lifebuoy opening 15 is built-in
Equipped with inflatable marine life ring (not shown), the marine life ring inflating port is towards the inside of pedestal 1；Accordingly, the bottom
The position of the corresponding marine life ring in 1 inside of seat is installed with an inflator pump 60, and the inflator pump 60 is electrically connected with power supply 4 and and host
5 communication connections, 60 outlet side of inflator pump is connected to marine life ring inflating port；Control panel 10 is filled by the control of host 5
Air pump 60 is opened, and inflator pump 60 inflates marine life ring, the marine life ring pop-up lifebuoy opening 15 after inflation, formation pair
The support that the intelligent escape seat at sea floats.
The design of marine life ring realizes floating, it is ensured that the safety of escape when intelligent escape seat may make to drop into the sea
Property.
Remaining is the same as embodiment 1.
Embodiment 5
The shaft 71 is telescopically inserted in containing tube 43, accordingly, the pedestal 1 of corresponding 3 lower open end of containing tube
Inside bottom surface is installed with a lifting platform 50, and the driving motor 6 is installed in 50 upper surface of lifting platform, and the lifting platform 50 passes through liter
The driving of sending down abnormally ascending cylinder 501 rises or falls, and the lifting cylinder 501 is electrically connected with power supply 4 and communicates to connect with host 5；
Cabin cabin, which opens, opens, and the control panel 10 controls jet-propelled ejector 8 by host 5 and starts, intelligent escape seat
Aircraft is flown away from chair injection, and control panel 10 controls lifting cylinder 501 by host 5 and lifting platform 50 is driven to rise, on lifting platform 50
It rises and 71 upper end of shaft for being connected to driving motor 6 is driven to extend out to 2 propeller of backrest opening, 21 outside, control panel 10 passes through master
Machine 5 controls electric pushrod 75 and lantern ring 72 is driven to move to 71 top of shaft along shaft 71, and blade 73 extend out to 3 outside of containing tube simultaneously
By the self weight turning unfolding of blade 73, control panel 10 controls driving shaft 71 rotation of driving motor 6 by host 5 and is driven paddle
Leaf 73 rotates, so that intelligent escape seat hovers above in the air.
The design of lifting platform 50 may make propeller 7 to be integrally located at 2 inside of backrest, in use, just driving shaft 71 stretches out
To 21 outside of propeller opening, to guarantee the aesthetic measure of intelligent escape seat entirety, degree easy to use.
Remaining is the same as embodiment 1.
Embodiment 6
Referring to Fig. 3 and Fig. 6, the 2 upper surface side of backrest offers parachute opening 24, accordingly, the backrest 2
Inboard, upright is provided with parachute export conduit 25, and parachute export 25 upper open end of conduit and parachute opening 24 connect
It is logical；Pack 70, is installed in 2 inside of backrest below parachute export 25 lower open end of conduit, and the extractor parachute of pack 70 is opened
The mouth corresponding parachute (not shown) exports 25 lower open end of conduit；Corresponding 70 parachute opener 701 of pack in 2 front of backrest
Position offer a parachute-opening mouth 26, the parachute opener 701 of the pack 70 extend out to 2 front outside of backrest by parachute-opening mouth 26；
Passenger's pull parachute opener 701, the extractor parachute main chute 702 (not shown) driven in pack are extend out to by parachute export conduit 25
Above 2 upper surface of backrest and it is unfolded, forms the support floated in the sky to the intelligent escape seat.
The design of pack 70, the substitution or standby that can be used as propeller 7 use, it is ensured that intelligent escape seat safe falling.
Remaining is the same as embodiment 1.
Although above having used general explanation and specific embodiment, the present invention is described in detail, at this
On the basis of invention, it can be made some modifications or improvements, or some functional module is deleted, this is to those skilled in the art
It is obvious for member.Therefore, it these modifications or improvements or deletes without departing from theon the basis of the spirit of the present invention,
It falls within the scope of the claimed invention.
Claims (10)
1. a kind of aircraft intelligent escape seat, which is characterized in that the intelligent escape seat is installed in aircraft cabin, the intelligence
Can escape seat include:
Pedestal (1), shape are cabinet, are placed horizontally in aircraft cabin, and the pedestal (1) is equipped with dry-spray if bottom surface is spaced apart
Mouth (11), pedestal (1) upper surface offer switch opening (12) and control opening (13), the positive lower part projection of pedestal (1)
There are a foot pedal (14)；
Backrest (2), shape are cabinet, are vertically arranged at pedestal (1) upper surface far from foot pedal (14) one end, the backrest (2)
It is connected on the inside of bottom surface and pedestal (1), backrest (2) upper surface middle part offers propeller opening (21)；
Containing tube (3) is vertically arranged on the inside of backrest (2), containing tube (3) upper port and propeller be open (21) be connected to,
Lower port corresponds on the inside of the pedestal (1)；
Power supply (4) is installed on the inside of the pedestal (1)；
Host (5) is installed on the inside of the pedestal (1) and is electrically connected with the power supply (4), host (5) internal processor
(51)；
Driving motor (6) is installed on the inside of the pedestal (1), and the driving motor (6) is electrically connected with power supply (4) and and host
(5) it communicates to connect；
Propeller (7), including be vertically arranged shaft (71), sliding sleeve be set to shaft (71) on lantern ring (72) and along lantern ring
(72) it is provided at circumferentially spaced and turnable the blade (73) for being connected to lantern ring (72) upper surface, the axis being located at below lantern ring (72)
It is arranged on bar (71) support ring (74), shaft (71) upper end is extend out to above propeller opening (21), shaft (71)
Lower end and the driving motor (6) output end are drivingly connected；At least one electric pushrod (75), is installed in the support ring vertically
(74) upper surface, electric pushrod (75) output end and lantern ring (72) are drivingly connected the electric pushrod (75) and power supply (4)
It is electrically connected and is communicated to connect with host (5)；
Jet-propelled ejector (8), is installed in the pedestal (1) inside bottom surface, and ejection end corresponds to the jet port of the pedestal (1)
(11), the jet-propelled ejector (8) is electrically connected with power supply (4) and communicates to connect with host (5)；
Control switch (9) is installed in the pedestal (1) switch opening (12), and the control switch (9) is electrically connected with power supply (4),
Form the control being opened and closed to power supply (4)；
Control panel (10), is installed in the pedestal (1) control opening (13), and the control panel (10) communicates with host (5)
Connection；
Shield (20), shape are an arc transparent casing, are covered on the intelligent escape seat, on the shield (20)
End rotation is connected to backrest (2) upper surface；
The aircraft cabin cabin top is retractable structure, forms the ejection for flying away from cabin for intelligent escape seat fire and is open.
2. aircraft intelligent escape seat according to claim 1, which is characterized in that the positive side of the backrest (2) is by upper
Air-conditioning opening (22) and oxygen opening (23) are equipped with to lower be spaced apart；
Accordingly, backrest (2) inside upper part is installed with an air-conditioning (30), and air-conditioning (30) air outlet corresponds to the air-conditioning opening
(22), the air-conditioning (30) is electrically connected with power supply (4) and communicates to connect with the host (5)；
Backrest (2) middle inside is installed with an oxygenerator (40), and the oxygen outlet of the oxygenerator (40) corresponds to the oxygen
Gas is open (23), and the oxygenerator (40) is electrically connected with power supply (4) and communicates to connect with the host (5).
3. aircraft intelligent escape seat according to claim 1, which is characterized in that aircraft cabin ground location is long along cabin
Degree direction is provided with guide rail, and accordingly, the base end face is convexly equipped with the pulley matched with the guide rail, forms the intelligence
Sliding setting of the escape seat in cabin.
4. aircraft intelligent escape seat according to claim 1, which is characterized in that the shaft (71) telescopically plugs
In containing tube (3), accordingly, pedestal (1) inside bottom surface of corresponding containing tube (3) lower open end is installed with a lifting platform
(50), the driving motor (6) is installed in lifting platform (50) upper surface, and the lifting platform (50) is driven by lifting cylinder (501)
Dynamic to rise or fall, the lifting cylinder (501) is electrically connected with power supply (4) and communicates to connect with host (5)；
Lantern ring (72) sliding sleeve is set to shaft (71) outer wall being located above support ring (74), and the blade (73) is far from set
Ring (72) one end is resisted against containing tube (3) inner wall；
Cabin cabin, which opens, opens, and the control panel (10) controls jet-propelled ejector (8) starting, intelligent escape by host (5)
Aircraft is flown away from seat injection, and control panel (10) is risen by host (5) control lifting cylinder (501) driving lifting platform (50),
Lifting platform (50), which rises, drives shaft (71) upper end for being connected to driving motor (6) to extend out to backrest (2) propeller opening (21)
Outside, control panel (10) move to shaft along shaft (71) by host (5) control electric pushrod (75) driving lantern ring (72)
(71) top, blade (73) extend out on the outside of containing tube (3) and by blade (73) self weight turning unfoldings, and control panel (10) is logical
It crosses host (5) control driving motor (6) driving shaft (71) to rotate and be driven blade (73) rotation, so that intelligent escape seat disc
It is threaded onto aerial.
5. aircraft intelligent escape seat according to claim 1, which is characterized in that pedestal (1) the opposing sidewalls lower part
Bar shaped lifebuoy opening (15) is offered respectively, is installed with inflatable marine life ring in lifebuoy opening (15), it is described
Marine life ring inflating port is towards on the inside of pedestal (1)；
Accordingly, the position of corresponding marine life ring is installed with an inflator pump (60), the inflator pump on the inside of the pedestal (1)
(60) it is electrically connected and is communicated to connect with host (5), inflator pump (60) outlet side and marine life ring inflating port with power supply (4)
Connection；
Control panel (10) is opened by host (5) control inflator pump (60), and inflator pump (60) inflates marine life ring, inflation
Marine life ring pop-up lifebuoy opening (15) afterwards, forms the support at sea floated to the intelligent escape seat.
6. aircraft intelligent escape seat according to claim 1, which is characterized in that open backrest (2) the upper surface side
It is open (24) equipped with a parachute, accordingly, backrest (2) inboard, upright is provided with parachute export conduit (25), institute
Parachute export conduit (25) upper open end is stated to be connected to parachute opening (24)；
Pack (70) is installed on the inside of the backrest (2) below parachute export conduit (25) lower open end, pack (70)
The corresponding parachute of extractor parachute opening exports conduit (25) lower open end；Described corresponding pack (70) parachute-opening in backrest (2) front
The position of device (701) offers a parachute-opening mouth (26), and the parachute opener (701) of the pack (70) is stretched out by parachute-opening mouth (26)
To backrest (2) front outside；
Passenger's pull parachute opener (701), extractor parachute drive the main chute (702) in pack to be stretched out by parachute export conduit (25)
Above to backrest (2) upper surface and it is unfolded, forms the support floated in the sky to the intelligent escape seat.
7. aircraft intelligent escape seat according to claim 1, which is characterized in that pedestal (1) upper surface corresponds to the control
The position of system opening (13) is installed with supply case (80), and the control panel (10) is covered on supply case (80) opening, the benefit
Supply is provided with to case (80)；
The supply includes but is not limited to water, food and drug；
Pedestal (1) upper surface offers solar panel opening (16), and accordingly, corresponding solar panel is opened on the inside of the pedestal (1)
The position of mouth (16) is installed with battery board slot (90), is arranged at intervals with several solar panels in the battery board slot (90)
(901), several solar panels (901) are electrically connected with power supply (4) charge port respectively, form the charging to power supply (4).
8. aircraft intelligent escape seat according to claim 1, which is characterized in that in pedestal (1) two lateral walls
Portion offers camera shooting opening (91) respectively, accordingly, is installed with camera (92), the camera in camera shooting opening (91)
(92) it is electrically connected with power supply (4) and is communicated to connect with host (5), form the shooting to intelligent escape seat external sights.
9. aircraft intelligent escape seat according to claim 1, which is characterized in that backrest (2) upper surface is close to outer
The position of edge offers several distress lights opening (27) along backrest (2) is circumferentially-spaced, in several distress lights openings (27) point
It is not installed with distress light (271), the distress light (271) is electrically connected with power supply (4) and communicates to connect with host (5)；
The distress light (271) is LED distress light；
GPS positioning module (52), the memory module (53) respectively with processor (51) communication connection are installed in the host (5)
And navigation module (54).
10. aircraft intelligent escape seat according to claim 1, which is characterized in that shield (20) is that tempering is heat-insulated anti-
Cloche is played, shield (20) end face and pedestal (1) and backrest (2) contact position are provided with sealing ring, accordingly, described
Pedestal (1) and backrest (2) are provided with the seal groove matched with sealing ring with shield (20) contact position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910345374.XA CN109927913B (en) | 2019-04-26 | 2019-04-26 | Intelligent escape seat for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910345374.XA CN109927913B (en) | 2019-04-26 | 2019-04-26 | Intelligent escape seat for airplane |
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| Publication Number | Publication Date |
|---|---|
| CN109927913A true CN109927913A (en) | 2019-06-25 |
| CN109927913B CN109927913B (en) | 2023-03-24 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910345374.XA Active CN109927913B (en) | 2019-04-26 | 2019-04-26 | Intelligent escape seat for airplane |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112249060A (en) * | 2020-09-11 | 2021-01-22 | 中车工业研究院有限公司 | Intelligent protection isolation barrier device |
| CN114506459A (en) * | 2020-06-02 | 2022-05-17 | 赵润生 | Sideslip type ejection suspension seat of armed helicopter |
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| RU2010114360A (en) * | 2010-04-13 | 2011-10-20 | Открытое акционерное общество "Научно-производственное предприятие "Звезда" имени академика Г.И. Северина" (RU) | EMERGENCY RESCUE METHOD FOR A PLANE CREW MEMBER AND SYSTEM FOR ITS IMPLEMENTATION |
| KR20110131379A (en) * | 2010-05-31 | 2011-12-07 | 변상복 | A device of emergency escape for aircraft |
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| RU186459U1 (en) * | 2018-10-31 | 2019-01-21 | Евгений Станиславович Фокин | 1 FOKIN SAFE PLANE |
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|---|---|---|---|---|
| US3662978A (en) * | 1970-10-22 | 1972-05-16 | Kaman Aerospace Corp | Aircraft ejection seat vehicle stowed rotor |
| EP0200630A2 (en) * | 1985-04-26 | 1986-11-05 | Pierre Delajoud | Central canopy buckle for an ejection seat |
| RU2010114360A (en) * | 2010-04-13 | 2011-10-20 | Открытое акционерное общество "Научно-производственное предприятие "Звезда" имени академика Г.И. Северина" (RU) | EMERGENCY RESCUE METHOD FOR A PLANE CREW MEMBER AND SYSTEM FOR ITS IMPLEMENTATION |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114506459A (en) * | 2020-06-02 | 2022-05-17 | 赵润生 | Sideslip type ejection suspension seat of armed helicopter |
| CN112249060A (en) * | 2020-09-11 | 2021-01-22 | 中车工业研究院有限公司 | Intelligent protection isolation barrier device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109927913B (en) | 2023-03-24 |
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