WO2017181302A1 - Siège éjectable modulaire, détachable permettant l'évacuation d'un passager d'un aéronef - Google Patents

Siège éjectable modulaire, détachable permettant l'évacuation d'un passager d'un aéronef Download PDF

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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
Application number
PCT/CN2016/000211
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English (en)
Chinese (zh)
Inventor
刘继军
Original Assignee
刘继军
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 刘继军 filed Critical 刘继军
Priority to PCT/CN2016/000211 priority Critical patent/WO2017181302A1/fr
Publication of WO2017181302A1 publication Critical patent/WO2017181302A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D25/00—Emergency apparatus or devices, not otherwise provided for
    • B64D25/08—Ejecting or escaping means
    • B64D25/12—Ejectable capsules

Definitions

  • the 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.
  • 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.
  • 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.
  • Figure 2 illustrates that 1, 2, 3, 4... are sequential ejections as a whole.
  • 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
  • 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.
  • 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.

Landscapes

  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Lowering Means (AREA)
  • Seats For Vehicles (AREA)

Abstract

La présente invention concerne un siège éjectable modulaire, détachable permettant l'évacuation d'un passager d'un aéronef. Un siège de passager est construit sous la forme d'une entité modulaire et détachable unique, et sous la forme d'une unité modulaire unique combinée avec une fenêtre d'aéronef. L'unité modulaire est insérée dans un côté d'un aéronef, et peut être injectée dans la direction opposée de l'insertion, de façon à fournir un siège éjectable modulaire pour se détaché de l'aéronef.
PCT/CN2016/000211 2016-04-21 2016-04-21 Siège éjectable modulaire, détachable permettant l'évacuation d'un passager d'un aéronef WO2017181302A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/CN2016/000211 WO2017181302A1 (fr) 2016-04-21 2016-04-21 Siège éjectable modulaire, détachable permettant l'évacuation d'un passager d'un aéronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2016/000211 WO2017181302A1 (fr) 2016-04-21 2016-04-21 Siège éjectable modulaire, détachable permettant l'évacuation d'un passager d'un aéronef

Publications (1)

Publication Number Publication Date
WO2017181302A1 true WO2017181302A1 (fr) 2017-10-26

Family

ID=60116520

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2016/000211 WO2017181302A1 (fr) 2016-04-21 2016-04-21 Siège éjectable modulaire, détachable permettant l'évacuation d'un passager d'un aéronef

Country Status (1)

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WO (1) WO2017181302A1 (fr)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02133299A (ja) * 1988-11-11 1990-05-22 Toshio Ukaji 航空機の緊急脱出装置
WO2002068851A2 (fr) * 2001-02-28 2002-09-06 Anatoly Michailovich Chekaev Dispositif de transport d'un objet, recipient gonflable utilise avec ce dispositif et moyen de prevention des collisions de l'objet avec les elements d'un vehicule de transport aerien
CN1473739A (zh) * 2002-08-08 2004-02-11 孙则阳 民航客机枪式弹射救生系统
CN102030108A (zh) * 2010-11-23 2011-04-27 李家涛 一种飞机救生装置
US20110233341A1 (en) * 2010-03-26 2011-09-29 Monteforte Michael A Hybrid emergency ejection system
CN202400290U (zh) * 2011-10-14 2012-08-29 王晓进 一种飞机遇险分离式机舱逃生装置
CN102874411A (zh) * 2011-07-14 2013-01-16 郑冰 飞行器侧滑式弹射坐椅

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02133299A (ja) * 1988-11-11 1990-05-22 Toshio Ukaji 航空機の緊急脱出装置
WO2002068851A2 (fr) * 2001-02-28 2002-09-06 Anatoly Michailovich Chekaev Dispositif de transport d'un objet, recipient gonflable utilise avec ce dispositif et moyen de prevention des collisions de l'objet avec les elements d'un vehicule de transport aerien
CN1473739A (zh) * 2002-08-08 2004-02-11 孙则阳 民航客机枪式弹射救生系统
US20110233341A1 (en) * 2010-03-26 2011-09-29 Monteforte Michael A Hybrid emergency ejection system
CN102030108A (zh) * 2010-11-23 2011-04-27 李家涛 一种飞机救生装置
CN102874411A (zh) * 2011-07-14 2013-01-16 郑冰 飞行器侧滑式弹射坐椅
CN202400290U (zh) * 2011-10-14 2012-08-29 王晓进 一种飞机遇险分离式机舱逃生装置

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