CN201033634Y - Civil aircraft safety escaping armchair - Google Patents
Civil aircraft safety escaping armchair Download PDFInfo
- Publication number
- CN201033634Y CN201033634Y CNU2007201015813U CN200720101581U CN201033634Y CN 201033634 Y CN201033634 Y CN 201033634Y CN U2007201015813 U CNU2007201015813 U CN U2007201015813U CN 200720101581 U CN200720101581 U CN 200720101581U CN 201033634 Y CN201033634 Y CN 201033634Y
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- plate
- side handrail
- board
- seat
- front apron
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Abstract
The utility model relates to an escape seat, which is used for passengers of civil aircrafts for safe escaping in case of an emergency situation, comprising an inner backrest board, an outer backrest board, a base plate, an outer side plate of the lateral handrail, and an inner side plate of the lateral handrail. The inner backrest board, the outer backrest board, the base plate, the outer side plate of the lateral handrail, and the inner side plate of the lateral handrail form a backrest-type seat. A deckhead push-up cylinder and a roof are arranged in the hollow cavity between the inner backrest board and the outer backrest board; a pneumatic cylinder of the lateral handrail and an inner lifting plate of the lateral handrail are arranged in the hollow cavity between the outer side plate of the lateral handrail and the inner side plate of the lateral handrail; a GPS positioning device, an oxygen cylinder and nourishing water are arranged between the base plate and the clapboard; an upper plate of front baffle and a lower plate of front baffle are arranged below the seat body; a bottom outer gasbag and a parachute are arranged from top to bottom in the seat cavity between the upper plate of front baffle and the clapboard; the gasbags are arranged on the whole plated surface. The utility model has the advantages of convenience and safety for escape under emergent situations in civil aviation.
Description
One, technical field:
The utility model relates to a kind of safe escape seat, is a kind of civil aircraft passenger safe escape seat in case of emergency that is applicable to.
Two, background technology
At present, both at home and abroad the seat of civil aircraft all installs and fixes together with body, passenger's difficulty of escaping during the generation airplane crash, and mortality almost is a hundred per cent.Though current also have a lot of experts and scholar in the research of being engaged in the civil aviation escape, all do not accomplish to coordinate in technology and economic aspect, still be a blank at civil aviation escape technical elements.
Three, summary of the invention
The purpose of this utility model is to overcome the deficiencies in the prior art, the civil aircraft safe escape seat that provides a kind of passenger in case of emergency to escape convenience, safety.
The purpose of this utility model can realize by following technical measures:
Civil aircraft safe escape seat, by interior back board, outer back board, seat board, the side handrail outer panel, the side handrail interior plate is formed, interior back board, outer back board, seat board, side handrail outer panel and side handrail inner panel side plate are formed the seat of backrest type, it is characterized in that: interior back board and outer back board are formed backrest, interior back board and outside be the cavity of hollow between the back board, be provided with the top board bearing of taking blame for others in the bottom of hollow cavity, top board is taken blame for others, and hinge joint has top board to take blame for others on the bearing, the take blame for others bearing hinge joint of inferior part of the cylinder block that top board is taken blame for others and top board, the take blame for others following hook hinge joint of hook-type link span of the top of cylinder bar and square of top board, the other end of hook-type link span is connected with the bottom of the top board that is loaded on the backrest hollow cavity, be provided with the mouth that top board protrudes upward on the top of backrest hollow cavity, air bag in the top board is housed on the front face of top board, on the back plate face of top board, air bag outside the top board is housed, air bag in the seat chair is housed on the front face of interior back board, the outer air bag of backrest is housed on the back plate face of back board outside, the handrail of the left and right sides is made up of side handrail outer panel and side handrail inner panel side plate, between side handrail outer panel and the side handrail inner panel side plate is the inner chamber of hollow, inner chamber in two side handrail hollows is equipped with lifter plate in the side handrail, inner chamber in two side handrail hollows is equipped with the side handrail air cylinder that vertical is provided with, the cylinder body of side handrail air cylinder links to each other with lifter plate in the side handrail with the side handrail outer panel respectively with the cylinder bar, the extending port that lifter plate in the side handrail is arranged on the top of side handrail, between the handrail inner panel side plate of the left and right sides, seat board and dividing plate are installed, it between seat board and the dividing plate storage chamber of hollow, the GPS registration device is housed in the storage chamber, oxygen bottle and nutritive water, the length of seat board and dividing plate is less than the length of side handrail, shrouding before seat board is equipped with in the front portion of seat board and dividing plate, stretcher is arranged at the bottom of shrouding before the plate, the seat body of stretcher bottom is the cavity of the door font of open front, in the cavity of door font, be provided with the chute that front apron lower plate and front apron upper plate vertically skid off, there is front apron to take blame for others at the rear portion of door font cavity by the front apron bearing hinge joint of taking blame for others, cylinder bar that front apron is taken blame for others and front apron lower plate are by resupinate torque spring hinge joint, the front portion of front apron lower plate and front apron upper plate is by resupinate torque spring hinge joint, air bag and parachute outside the bottom is housed in the seat cavity between front apron upper plate and dividing plate from top to bottom, pulley and strong magnet are installed on the sidewall of seat bottom, the upper board face of front apron upper plate is provided with the outer air bag of front apron inner panel, the inboard air bag of overhead gage before the lower panel face of front apron upper plate is provided with, air bag in the lower baffle plate inboard before the upper board face of front apron lower plate is provided with, the lower panel face of front apron upper plate is provided with front apron outside air bag, the external plates face of side handrail outer panel is provided with side handrail outside plate outside air bag, the inner panel face of side handrail interior plate is provided with side handrail interior plate air bag, is respectively arranged with the inboard air bag of side handrail inner panel outside air bag and side handrail inner panel in side handrail on the external plates face of lifter plate and the inner panel face.
The purpose of this utility model can also realize by following technical measures:
There is the emboss pit that is bonded with each other on the upper top of lifter plate and the limit, the left and right sides of top board in the side handrail, there is the emboss pit that is bonded with each other on the upper top of lifter plate and the limit, the left and right sides of top board in the side handrail, and there is the emboss pit that is bonded with each other with front apron lower plate and front apron upper plate the front portion of side handrail outer panel and side handrail inner panel side plate.
The utility model compared with prior art has following advantage:
1, the existing technology of utilization and overcome the shortcoming of economic problems, the passenger in case of emergency escapes conveniently, the advantage of safety, and has filled up the blank of civil aviation escape.
2, two kinds of escape modes integrally combine, both high-altitude protections of fleeing from and force-land.
3, adopt the fire-fighting quipment insulation.Adopt the external capsule azide to ignite, capsula interna pressure regulation inflation.Shorten the time of fleeing from and increase the safety and comfort performance.Make and design hommization more.
4, protection cabin quick make, and in conjunction with the linear electric motors track, make and flee from more rapidly effectively.
5, launch the life security that multiple protective that parachute combines with protective cover and inside and outside air bag effectively guarantees the passenger automatically.6, the eye-catching color of GPS positioning combination is convenient to receive and is rescued personnel's quick lock in target.7, in conjunction with prior art, cost economic is reasonable.
Four, description of drawings
Fig. 1 is a civil aircraft safe escape seat front view (analysing and observe)
Fig. 2 is a civil aircraft safe escape seat lateral plan (analysing and observe)
Five, the specific embodiment
Fig. 1---shown in 2: civil aircraft safe escape seat, be made up of interior back board 2, outer back board 6, seat board 24, side handrail outer panel 25, side handrail interior plate 30, interior back board 2, outer back board 6, seat board 24, side handrail outer panel 25 and side handrail inner panel side plate 30 are formed the seat of backrest type.Interior back board 2 and outer back board 6 are formed backrest, interior back board 2 and outside be the cavity of hollow between the back board 6, be provided with the top board bearing 17 of taking blame for others in the bottom of hollow cavity, top board is taken blame for others, and hinge joint has top board to take blame for others 16 on the bearing 17, top board 16 inferior part of the cylinder block and top board bearing 17 hinge joints of taking blame for others of taking blame for others, the take blame for others following hook hinge joint of hook-type link span of the top of 16 cylinder bars and square of top board, the other end of hook-type link span is connected with the bottom of the top board 4 that is loaded on the backrest hollow cavity, be provided with the mouth that top board 4 protrudes upward on the top of backrest hollow cavity, air bag 3 in the top board is housed on the front face of top board 4, on the back plate face of top board 4, air bag 5 outside the top board is housed, air bag 1 in the seat chair is housed on the front face of interior back board 2, the outer air bag 7 of backrest is housed on the back plate face of back board 6 outside, the handrail of the left and right sides is made up of side handrail outer panel 25 and side handrail inner panel side plate 30, between side handrail outer panel 25 and the side handrail inner panel side plate 30 is the inner chamber of hollow, inner chamber in two side handrail hollows is equipped with lifter plate 28 in the side handrail, inner chamber in two side handrail hollows is equipped with the side handrail air cylinder 9 that vertical is provided with, the cylinder body of side handrail air cylinder 9 links to each other with lifter plate 28 in the side handrail with side handrail outer panel 25 respectively with the cylinder bar, the extending port that lifter plate 28 in the side handrail is arranged on the top of side handrail, between left and right sides handrail inner panel side plate 30, seat board 24 and dividing plate 13 are installed, be the storage chamber of hollow between seat board 24 and the dividing plate 13, GPS registration device 8 is housed in the storage chamber, oxygen bottle 10 and nutritive water 12 have control cock 11 on oxygen bottle 10.The length of seat board 24 and dividing plate 13 is less than the length of side handrail, shrouding 42 before seat board is equipped with in the front portion of seat board 24 and dividing plate 13, stretcher 33 is arranged at the bottom of shrouding 42 before the seat board, the seat body of stretcher 33 bottoms is the cavity of the door font of open front, in the cavity of door font, be provided with the chute that front apron lower plate 18 and front apron upper plate 19 vertically skid off, there is front apron to take blame for others 41 at the rear portion of door font cavity by front apron bearing 23 hinge joints of taking blame for others, front apron is taken blame for others 41 cylinder bar and front apron lower plate 18 by resupinate torque spring 21 hinge joints, the front portion of front apron lower plate 18 and front apron upper plate 19 is by resupinate torque spring 21 hinge joints, air bag 14 and parachute 15 outside the bottom is housed in the seat cavity between front apron upper plate 19 and dividing plate 13 from top to bottom, pulley 20 and strong magnet 22 are installed on the sidewall of seat bottom, the upper board face of front apron upper plate 18 is provided with the outer air bag 38 of front apron inner panel, the inboard air bag 36 of overhead gage before the lower panel face of front apron upper plate 18 is provided with, air bag 34 in the lower baffle plate inboard before the upper board face of front apron lower plate 19 is provided with, the lower panel face of front apron upper plate 19 is provided with front apron outside air bag 40, the external plates face of side handrail outer panel 25 is provided with side handrail outside plate outside air bag 26, the inner panel face of side handrail interior plate 30 is provided with side handrail interior plate air bag 31, is respectively arranged with the inboard air bag 29 of side handrail inner panel outside air bag 27 and side handrail inner panel in side handrail on the external plates face of lifter plate 28 and the inner panel face.There is the emboss pit that is bonded with each other on the upper top of lifter plate 28 and the limit, the left and right sides of top board 4 in the side handrail, there is the emboss pit that is bonded with each other on the upper top of lifter plate 28 and the limit, the left and right sides of top board 4 in the side handrail, and there is the emboss pit that is bonded with each other with front apron lower plate 18 and front apron upper plate 19 front portion of side handrail outer panel 25 and side handrail inner panel side plate 30.
Principle of work of the present utility model is as follows:
1, escape in the high-altitude: start escape system when emergency situation takes place; seat two side shields eject, front apron ejects, top board ejects and closed seat, interior air bag begin inflation, (on the aircraft) linear electric motors start and with seat slide to the outlet of escaping, seat break away from body simultaneously the azide of outer air bag open the quick-fried parachute that launches automatically and open, form complete buffer protection system.
2, forced landing protection: when having little time to break away from body when emergency situation takes place.Start the forced landing protection system, the ejection of seat two side shields, front apron ejection, top board ejection and closed seat, interior air bag begin inflation.Outer air bag minor radius opens quick-fried simultaneously.Form complete insulation buffer protection system.
Claims (2)
1. civil aircraft safe escape seat, by interior back board (2), outer back board (6), seat board (24), side handrail outer panel (25), side handrail interior plate (30) is formed, interior back board (2), outer back board (6), seat board (24), side handrail outer panel (25) and side handrail inner panel side plate (30) are formed the seat of backrest type, it is characterized in that: interior back board (2) and outer back board (6) are formed backrest, interior back board (2) and outside be the cavity of hollow between the back board (6), be provided with the top board bearing (17) of taking blame for others in the bottom of hollow cavity, the top board bearing (17) of taking blame for others is gone up hinge joint top board take blame for others (16) is arranged, the top board inferior part of the cylinder block of (16) and top board bearing (17) hinge joint of taking blame for others of taking blame for others, the take blame for others following hook hinge joint of hook-type link span of the top of (16) cylinder bar and square of top board, the other end of hook-type link span is connected with the bottom of the top board that is loaded on the backrest hollow cavity (4), be provided with the mouth that top board (4) protrudes upward on the top of backrest hollow cavity, air bag in the top board (3) is housed on the front face of top board (4), on the back plate face of top board (4), air bag outside the top board (5) is housed, air bag in the seat chair (1) is housed on the front face of interior back board (2), the outer air bag (7) of backrest is housed on the back plate face of back board (6) outside, the handrail of the left and right sides is made up of side handrail outer panel (25) and side handrail inner panel side plate (30), between side handrail outer panel (25) and the side handrail inner panel side plate (30) is the inner chamber of hollow, inner chamber in two side handrail hollows is equipped with lifter plate in the side handrail (28), inner chamber in two side handrail hollows is equipped with the side handrail air cylinder (9) that vertical is provided with, the cylinder body of side handrail air cylinder (9) links to each other with lifter plate (28) in the side handrail with side handrail outer panel (25) respectively with the cylinder bar, the extending port that lifter plate in the side handrail (28) are arranged on the top of side handrail, seat board (24) and dividing plate (13) are installed between left and right sides handrail inner panel side plate (30), between seat board (24) and the dividing plate (13) is the storage chamber of hollow, GPS registration device (8) is housed in the storage chamber, oxygen bottle (10) and nutritive water (12), the length of seat board (24) and dividing plate (13) is less than the length of side handrail, shrouding (42) before seat board is equipped with in the front portion of seat board (24) and dividing plate (13), stretcher (33) is arranged at the bottom of shrouding (42) before the plate, the seat body of stretcher (33) bottom is the cavity of the door font of open front, in the cavity of door font, be provided with the chute that front apron lower plate (18) and front apron upper plate (19) vertically skid off, by front apron bearing (23) hinge joint of taking blame for others front apron take blame for others (41) is arranged at the rear portion of door font cavity, front apron is taken blame for others the cylinder bar of (41) and front apron lower plate (18) by resupinate torque spring (21) hinge joint, the front portion of front apron lower plate (18) and front apron upper plate (19) is by resupinate torque spring (21) hinge joint, air bag (14) and parachute (15) outside the bottom is housed in the seat cavity between front apron upper plate (19) and dividing plate (13) from top to bottom, pulley (20) and strong magnet (22) are installed on the sidewall of seat bottom, the upper board face of front apron upper plate (18) is provided with the outer air bag (38) of front apron inner panel, the inboard air bag (36) of overhead gage before the lower panel face of front apron upper plate (18) is provided with, air bag (34) in the lower baffle plate inboard before the upper board face of front apron lower plate (19) is provided with, the lower panel face of front apron upper plate (19) is provided with front apron outside air bag (40), the external plates face of side handrail outer panel (25) is provided with side handrail outside plate outside air bag (26), the inner panel face of side handrail interior plate (30) is provided with side handrail interior plate air bag (31), is respectively arranged with the inboard air bag (29) of side handrail inner panel outside air bag (27) and side handrail inner panel on the external plates face of lifter plate in side handrail (28) and the inner panel face.
2. civil aircraft safe escape seat according to claim 1, it is characterized in that: there is the emboss pit that is bonded with each other on the upper top of lifter plate (28) and the limit, the left and right sides of top board (4) in the side handrail, there is the emboss pit that is bonded with each other on the upper top of lifter plate (28) and the limit, the left and right sides of top board (4) in the side handrail, and there is the emboss pit that is bonded with each other with front apron lower plate (18) and front apron upper plate (19) front portion of side handrail outer panel (25) and side handrail inner panel side plate (30).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007201015813U CN201033634Y (en) | 2007-06-06 | 2007-06-06 | Civil aircraft safety escaping armchair |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007201015813U CN201033634Y (en) | 2007-06-06 | 2007-06-06 | Civil aircraft safety escaping armchair |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201033634Y true CN201033634Y (en) | 2008-03-12 |
Family
ID=39194526
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007201015813U Expired - Fee Related CN201033634Y (en) | 2007-06-06 | 2007-06-06 | Civil aircraft safety escaping armchair |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201033634Y (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101995323A (en) * | 2010-09-09 | 2011-03-30 | 北京航空航天大学 | Simulation device for air airflow tripping force experiments of arm |
| CN104071341A (en) * | 2014-05-21 | 2014-10-01 | 苏州标图高级座椅有限公司 | Intelligent control system for aircraft seat |
| CN104129505A (en) * | 2014-07-25 | 2014-11-05 | 沈阳兴华航空电器有限责任公司 | Travel switch |
| CN104163120A (en) * | 2013-12-10 | 2014-11-26 | 明光市浩淼消防科技发展有限公司 | Rotary and retractable seat device with air respirator |
| CN104276063A (en) * | 2013-07-11 | 2015-01-14 | 上海耀华大中新材料有限公司 | Seat private cover and machining method thereof |
| CN106828943A (en) * | 2017-03-24 | 2017-06-13 | 蒋昊维 | High altitude escape seat |
| CN106927053A (en) * | 2017-03-24 | 2017-07-07 | 蒋昊维 | Passenger plane high altitude escape system |
| CN108033035A (en) * | 2017-11-24 | 2018-05-15 | 航宇救生装备有限公司 | A kind of seat recovery system for ejection test |
| CN111232218A (en) * | 2020-04-13 | 2020-06-05 | 程建坤 | Safety seat for civil aircraft |
| CN111268139A (en) * | 2020-02-05 | 2020-06-12 | 绍兴裕铭机械科技有限公司 | External escape device on water of airborne vehicle |
| CN112829948A (en) * | 2021-01-29 | 2021-05-25 | 北京天创凯睿科技有限公司 | Military helicopter sliding seat with furling air bag |
-
2007
- 2007-06-06 CN CNU2007201015813U patent/CN201033634Y/en not_active Expired - Fee Related
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101995323B (en) * | 2010-09-09 | 2012-07-04 | 北京航空航天大学 | Simulation device for air airflow tripping force experiments of arm |
| CN101995323A (en) * | 2010-09-09 | 2011-03-30 | 北京航空航天大学 | Simulation device for air airflow tripping force experiments of arm |
| CN104276063A (en) * | 2013-07-11 | 2015-01-14 | 上海耀华大中新材料有限公司 | Seat private cover and machining method thereof |
| CN104163120A (en) * | 2013-12-10 | 2014-11-26 | 明光市浩淼消防科技发展有限公司 | Rotary and retractable seat device with air respirator |
| CN104071341A (en) * | 2014-05-21 | 2014-10-01 | 苏州标图高级座椅有限公司 | Intelligent control system for aircraft seat |
| CN104129505B (en) * | 2014-07-25 | 2016-04-27 | 沈阳兴华航空电器有限责任公司 | A kind of travel switch |
| CN104129505A (en) * | 2014-07-25 | 2014-11-05 | 沈阳兴华航空电器有限责任公司 | Travel switch |
| CN106828943A (en) * | 2017-03-24 | 2017-06-13 | 蒋昊维 | High altitude escape seat |
| CN106927053A (en) * | 2017-03-24 | 2017-07-07 | 蒋昊维 | Passenger plane high altitude escape system |
| CN108033035A (en) * | 2017-11-24 | 2018-05-15 | 航宇救生装备有限公司 | A kind of seat recovery system for ejection test |
| CN108033035B (en) * | 2017-11-24 | 2021-03-26 | 航宇救生装备有限公司 | Seat recovery system for ejection test |
| CN111268139A (en) * | 2020-02-05 | 2020-06-12 | 绍兴裕铭机械科技有限公司 | External escape device on water of airborne vehicle |
| CN111232218A (en) * | 2020-04-13 | 2020-06-05 | 程建坤 | Safety seat for civil aircraft |
| CN112829948A (en) * | 2021-01-29 | 2021-05-25 | 北京天创凯睿科技有限公司 | Military helicopter sliding seat with furling air bag |
| CN112829948B (en) * | 2021-01-29 | 2021-11-12 | 北京天创凯睿科技有限公司 | Military helicopter sliding seat with furling air bag |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |