WO2017181302A1 - Modular, detachable ejection seat allowing aircraft passenger escape - Google Patents
Modular, detachable ejection seat allowing aircraft passenger escape Download PDFInfo
- Publication number
- WO2017181302A1 WO2017181302A1 PCT/CN2016/000211 CN2016000211W WO2017181302A1 WO 2017181302 A1 WO2017181302 A1 WO 2017181302A1 CN 2016000211 W CN2016000211 W CN 2016000211W WO 2017181302 A1 WO2017181302 A1 WO 2017181302A1
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- WO
- WIPO (PCT)
- Prior art keywords
- aircraft
- modular
- seat
- unit
- passenger
- Prior art date
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/12—Ejectable capsules
Abstract
A modular, detachable ejection seat allowing aircraft passenger escape. A passenger seat is constructed as a single, modular and detachable entity, and as a single modular unit combined with an aircraft window. The modular unit is inserted into one side of an aircraft, and can be ejected away in the opposite direction of the insertion, thereby providing a modular ejection seat capable of detaching from the aircraft.
Description
技术领域:目前可查资料,全世界还没有把乘客的座椅做成模块化脱离式弹射座椅,乘客的生命安全,只能靠飞机任凭它支配,而客机乘客可逃生的模块化脱离式弹射座椅这种方案的设计无疑是一场现代客机安全的一种革命式的全新技术,带来的是具有划时代的安全新技术领域。Technical field: At present, the information can be checked. The passenger seat of the passenger has not been modularized and detached. The safety of passengers can only be borne by the aircraft, and the passengers can escape. The design of this type of ejection seat is undoubtedly a revolutionary new technology for the safety of modern passenger aircraft, bringing a new era of epoch-making safety technology.
背景资料:客机的事故率很低的,但是客机的死亡率是很高的,鉴于为客机上所有乘客的安全考虑,有必要实施一种“客机乘客可逃生的模块化脱离式弹射座椅”这种新的技术方案,否则是客机在出现事故过程中毫无求生的任何办法。Background information: The accident rate of passenger aircraft is very low, but the death rate of passenger aircraft is very high. In view of the safety considerations for all passengers on passenger aircraft, it is necessary to implement a modular decoupled ejection seat that allows passengers to escape. This new technical solution, otherwise, is no way for the passenger aircraft to survive in the event of an accident.
发明内容:客机乘客的座椅有两人一排,叁人一排,肆人一排的,把每排座椅做成模块式一个单元,每排是一个整体,(包括飞机的窗口及外侧)可单独向飞机外面弹射出去,弹出之后,每个整体都有降落伞,(可根据重量的大小来约束降落伞的大小)如果落在水中,座椅下面是救生衣,座椅下面可以做成封闭的箱体,可浮在水面,飞机出现事故,飞机窗口的一侧每个座椅的单元可有顺序往外弹射,完成了每一个单元座椅与飞机完全脱离,使得安全得到了保障。SUMMARY OF THE INVENTION: The passenger seat of a passenger aircraft has two rows of people, one row of people and one row of people. Each row of seats is made into a modular unit, each row is a whole, including the window and the outer side of the aircraft. ) can be ejected separately to the outside of the aircraft. After the pop-up, each of them has a parachute. (The size of the parachute can be restrained according to the weight.) If it falls in the water, the life jacket is under the seat, and the seat can be closed underneath. The cabinet can float on the water surface, and the aircraft has an accident. The units of each seat on one side of the aircraft window can be ejected in sequence, completing the complete separation of each unit seat from the aircraft, so that safety is guaranteed.
附图说明:图1说明:1、2、3、4……是每个座椅的单元,由飞机窗口部位嵌入飞机,每格单元制成弹射整体。BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 illustrates that 1, 2, 3, 4, ... are units of each seat, embedded in the aircraft by the window portion of the aircraft, and each unit is made into a projectile.
图2说明:1、2、3、4……是整体有顺序的弹射。Figure 2 illustrates that 1, 2, 3, 4... are sequential ejections as a whole.
具体实施方式:本实用新型就是在客机的每一个窗口的位置都是一个模块式的座椅单元,连同客机的窗口一起嵌入飞机整体内,也就是飞机是一个大的整体,大的框架,而座椅单元是一个个嵌入飞机的组成一个完整的飞机整体,单元是对应的,对应的单元座椅被例为一组,弹射飞机出去的也是同时对应向各自嵌入的反方向弹射出去,飞机座椅弹射的过程中,都是按照安全座椅带着窗口整体向着嵌入的反方向进行脱离式的弹射,达到单元座椅与飞机完全脱离,每一组单元座椅都是向着嵌入飞机的反方向进行弹射,飞机剩下的是整体的框架,而分离的却是每一个座椅的单元,有多少座椅单元,就有多少次的弹射,弹射装置设计在客机过道的下方,每一个单元座椅的下方与过道的下方是弹射装置的所在位置,是隐蔽在下方,看不见的一种装置,每一个单元座椅的弹射装置或是独立,或是连通每一个单元座椅的,弹射装置的牵动由自动和人工完成,弹射系统的启动也可用多人完成。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention is a modular seating unit at the position of each window of a passenger aircraft, which is embedded in the entire aircraft together with the window of the passenger aircraft, that is, the aircraft is a large whole, large frame, and The seat unit is a complete aircraft integrated into the aircraft, the unit is corresponding, the corresponding unit seats are exemplified as a group, and the ejection of the aircraft is also correspondingly ejected in the opposite direction of the respective embedded, the aircraft seat In the process of the catapult ejection, the safety seat is carried out with the window as a whole in the opposite direction of the embedded direction, so that the unit seat is completely separated from the aircraft, and each group of seats is oriented in the opposite direction of the embedded aircraft. For the ejection, the rest of the aircraft is the overall frame, and the separation is the unit of each seat, how many seat units, how many times of ejection, the ejection device is designed under the aisle of the passenger plane, each unit seat Below the chair and below the aisle is the location of the catapult, which is hidden underneath, a device that is invisible, each single Ejection apparatus or individual seats, or, each unit of the communication device ejection seat is done by automatic and manual affects completion, the system can also be used to start ejection people.
Claims (3)
- 一种客机每个窗口连同乘客的座椅做成可脱离模块化的单元整体①该整体连同飞机窗口一起由外向内嵌入飞机,并由锁定系统锁定②解锁时可以沿着嵌入的反方向弹射出去。A passenger aircraft, each window, together with a passenger's seat, is made of a unit that can be separated from the modular body. The whole body is embedded into the aircraft from the outside together with the aircraft window, and can be ejected in the opposite direction of the insertion when unlocked by the locking system. .
- 根据权利1所述单元整体,其特征在于①单元整体和客机整体达到分离自由②由自动或人工来控制分离②锁定和弹射由一个系统完成,先锁定,解锁必须弹射。The unit as a whole according to claim 1 is characterized in that the unit 1 and the passenger machine as a whole are separated freely. 2 The separation is controlled automatically or manually. 2 The locking and ejection are performed by a system, and the first locking and unlocking must be ejected.
- 根据权利1所述的可脱离小模块化的单元整体①脱离后降落伞自动打开②座椅下有封闭的箱体,入水后可浮在水面。 The detachable small modular unit 1 according to claim 1 is detached, and the parachute is automatically opened. The closed box under the seat 2 can be floated on the water surface after entering the water.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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PCT/CN2016/000211 WO2017181302A1 (en) | 2016-04-21 | 2016-04-21 | Modular, detachable ejection seat allowing aircraft passenger escape |
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Application Number | Priority Date | Filing Date | Title |
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PCT/CN2016/000211 WO2017181302A1 (en) | 2016-04-21 | 2016-04-21 | Modular, detachable ejection seat allowing aircraft passenger escape |
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PCT/CN2016/000211 WO2017181302A1 (en) | 2016-04-21 | 2016-04-21 | Modular, detachable ejection seat allowing aircraft passenger escape |
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Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02133299A (en) * | 1988-11-11 | 1990-05-22 | Toshio Ukaji | Emergency bail-out device for aircraft |
WO2002068851A2 (en) * | 2001-02-28 | 2002-09-06 | Anatoly Michailovich Chekaev | Device for transporting an object, an inflatable container used in said device and a means for preventing the collision of said object with elements of means of air transport |
CN1473739A (en) * | 2002-08-08 | 2004-02-11 | 孙则阳 | Gun type ejection life-saving system for civil air plane |
CN102030108A (en) * | 2010-11-23 | 2011-04-27 | 李家涛 | Aircraft lifesaving device |
US20110233341A1 (en) * | 2010-03-26 | 2011-09-29 | Monteforte Michael A | Hybrid emergency ejection system |
CN202400290U (en) * | 2011-10-14 | 2012-08-29 | 王晓进 | Plane distress separate cabin escape device |
CN102874411A (en) * | 2011-07-14 | 2013-01-16 | 郑冰 | Sideslip type catapult chair of air vehicle |
-
2016
- 2016-04-21 WO PCT/CN2016/000211 patent/WO2017181302A1/en active Application Filing
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02133299A (en) * | 1988-11-11 | 1990-05-22 | Toshio Ukaji | Emergency bail-out device for aircraft |
WO2002068851A2 (en) * | 2001-02-28 | 2002-09-06 | Anatoly Michailovich Chekaev | Device for transporting an object, an inflatable container used in said device and a means for preventing the collision of said object with elements of means of air transport |
CN1473739A (en) * | 2002-08-08 | 2004-02-11 | 孙则阳 | Gun type ejection life-saving system for civil air plane |
US20110233341A1 (en) * | 2010-03-26 | 2011-09-29 | Monteforte Michael A | Hybrid emergency ejection system |
CN102030108A (en) * | 2010-11-23 | 2011-04-27 | 李家涛 | Aircraft lifesaving device |
CN102874411A (en) * | 2011-07-14 | 2013-01-16 | 郑冰 | Sideslip type catapult chair of air vehicle |
CN202400290U (en) * | 2011-10-14 | 2012-08-29 | 王晓进 | Plane distress separate cabin escape device |
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