WO2012054002A1 - Procédé d'évacuation collective d'urgence de passagers d'un moyen de transport aérien et avion doté d'un équipement pour porter secours à des passagers dans une situation d'urgence - Google Patents

Procédé d'évacuation collective d'urgence de passagers d'un moyen de transport aérien et avion doté d'un équipement pour porter secours à des passagers dans une situation d'urgence Download PDF

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Publication number
WO2012054002A1
WO2012054002A1 PCT/UA2011/000005 UA2011000005W WO2012054002A1 WO 2012054002 A1 WO2012054002 A1 WO 2012054002A1 UA 2011000005 W UA2011000005 W UA 2011000005W WO 2012054002 A1 WO2012054002 A1 WO 2012054002A1
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WO
WIPO (PCT)
Prior art keywords
capsule
passengers
capsules
hatch
fuselage
Prior art date
Application number
PCT/UA2011/000005
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English (en)
Russian (ru)
Inventor
Тэтяна Иванивна ДЭМЭНЧУК
Original Assignee
Demenchuk Tetyana Ivanivna
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 Demenchuk Tetyana Ivanivna filed Critical Demenchuk Tetyana Ivanivna
Publication of WO2012054002A1 publication Critical patent/WO2012054002A1/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 invention relates to aviation, and in particular to methods for rescuing passengers from an aircraft.
  • a known method for emergency evacuation of a rescue capsule from a helicopter comprising a propeller with blades and a fuselage, consisting of a bow with a cockpit, a central and aft parts, where the passenger compartment is located in the central part, made in the form of an autonomous rescue capsule with doorways and a parachute.
  • the fuselage along its body and circumferentially between the nose part with the cockpit ", the central part with an autonomous capsule and the tail part and in the place of fastening screws to the fuselage disposed elongated shaped charges.
  • SUBSTITUTE SHEET (RULE 26) parts and lining of the fuselage, open the parachute (see RF patent N ° 2207301, IPC B64C27 / 04, B64C1 / 32, B64D17 / 80, publ. 06/27/2003).
  • the disadvantage of this method is that the use of explosive cutting of the fuselage is not safe for passengers, also the claimed method does not provide a safe landing of the rescue capsule on the ground, on the water and the capsule is not equipped with life support equipment for passengers, landed or splashed before the rescuers arrived.
  • the aircraft includes a fuselage with hatches for the entry and exit of passengers and crew members with a pilot's cabin, equipped with an on-board computer and a device for delivering electrical commands in the necessary sequence for implementation rescue program, which, in the case of a decision to evacuate passengers, can be turned on by an on-board computer, pilot or from the Earth; wings; tail unit; engines; chassis; emergency hatch in the rear of the fuselage, made with the possibility of its automatic opening, and passenger seats Also, the aircraft is equipped with at least one rigid inflatable landing container located inside the fuselage, inside of which passengers and crew seats are installed in the longitudinal direction;
  • upper and lower guides are installed, configured to interact with them of the corresponding container elements and are means for fixing the said container in a stationary state
  • the aircraft is also equipped with a means for automatically closing the emergency hatch after the container is pulled out of the fuselage
  • the container is equipped with:
  • SUBSTITUTE SHEET (RULE 26) a device for moving the container along the fuselage, in the direction of the emergency hatch;
  • shock-absorbing cylinders mainly those that are filled with gas, with the possibility of automatically opening these hatches, automatically inflating these cylinders according to the altimeter signal and installing them before landing or bringing below the lower overall surface of the container on set value;
  • an on-board computer capable of controlling the orientation of the container in space, the speed of descent, the distance to the surface of the Earth or water;
  • compartment of on-board automation and measuring equipment including a device for determining the location of the container
  • the task to be solved by the first invention of the group and the technical result achieved are to create a method for mass emergency evacuation of passengers from air transport, in which due to the use of new equipment and a new sequence of actions, the range of emergency situations will be achieved in which safe mass rescue of passengers from air transport is achieved.
  • the passenger cabin is made in the form of separate sealed autonomous rescue capsules with parachutes, which consists in throwing sealed autonomous rescue capsules with passengers from the cabin
  • the passage of the capsule is sealed with shutters, unhooked intercapsular connecting junctions are opened, after which passengers are automatically fixed in passenger seats with the help of restraining furniture equipment and airbags, and the release of autonomous rescue capsules occurs while opening the hatches designed specifically for each capsule, and the capsule, which is previously placed rigidly on the tube guides, which are rigidly fixed on flexible supports, slides along tubular directions under the influence of its weight and pneumatic accumulator barking, and then the external airbags of the capsule are deployed and the capsule's parachute is further automatically opened.
  • a feature of this method is that the opening of the hatch occurs with a rigid fixation of the hatch until the capsule completely drops out, so that some planning of the flight of the air transport is provided and resistance to air flow is achieved in order to slow down the speed of the falling air transport.
  • Another feature is that, if necessary, after throwing out just one capsule, the hatch is closed and the fuselage is sealed.
  • the aircraft body is divided into separate compartments that contain a carousel mechanism in which the capsules are located on different tiers and are lowered in a circle down to the lower hatch.
  • the invention is also based on the task of improving the design of an aircraft with equipment for saving passengers in an emergency, in which by changing its design and the introduction of additional equipment, an extension of the range of emergency situations is achieved, which ensures safe mass disposal of passengers from air transport.
  • the specified technical result is achieved by the fact that in a well-known aircraft with equipment for rescuing passengers in an emergency, including: a fuselage containing a pilot's cabin, equipped with an on-board computer and a device for delivering electronic commands in the necessary sequence for the implementation of the evacuation program, wings; tail; engines chassis; at least one emergency hatch in,
  • SUBSTITUTE SHEET (RULE 26) the fuselage, made with the possibility of automatic opening, it introduced at least one sealed autonomous rescue capsule in which passengers are located, and it is equipped with:
  • compartments with hinged hatches for placement of brake parachutes in them, and hatches are made with the possibility of their automatic opening, and parachutes with the possibility of automatically putting them into action;
  • Figure 1 General view of the aircraft with the layout of the capsules in the fuselage (top view);
  • Figure 2 diagram of the opening of the lower hatches of the fuselage
  • Fig.Z is a diagram of the loss of rescue capsules through the lower hatches of the fuselage
  • Figure 5 section of the fuselage with the capsule in a calm (non-emergency) situation, section aa in figure 2;
  • 'A is a side view
  • B is a top view
  • Fig.9 the mechanism for opening the lower hatch, put into operation
  • Figure 10 the ejection of rescue capsules through the upper hatches of the fuselage with the previous shooting of the tail;
  • Fig. 16 is a section of a multi-tier aircraft with a carousel mechanism for dropping capsules through the lower hatch;
  • 17 is a section of a multi-tiered aircraft with a carousel mechanism for dropping capsules through the lower hatch.
  • An airplane with a device for rescuing passengers in an emergency contains a fuselage 1 with a pilot cabin 2, wings 3, tail unit 4, engines 5, a chassis (not shown), passenger seats 16.
  • Figure 2 and Figure 3 shows the opening scheme of the lower fuselage hatches, where the fuselage 1, hatch 6, rescue capsule 7, portholes 9, caps support 15, axis of rotation of the hatch 18, axis of rotation of the capsule 19, belt of airbags of the capsules 20.
  • Figure 4 shows the capsule of the aircraft 7 with portholes 9 and belts of airbags capsules 20.
  • Figure 5 shows a section of the fuselage with the capsule in a calm (non-emergency) environment, where the fuselage 1, hatch 6, rescue capsule 7, portholes 9, life support system 10, luggage compartment 11, tubular guides 12, locks for opening the hatch 13, ejection mechanism 14 , capsule supports 15, passenger seats 16, parachute system 17.
  • Figure 6 shows the placement of the capsule on the tubular guides of the lower hatch
  • A is a side view
  • B is a top view where the hatch 6, the rescue capsule 7, the tubular guides 12, the eject mechanism 14, the caps support 15, the piston of the eject mechanism 27.
  • Figure 7 shows the sliding of the capsule 7 along the tubular guides 12, where the hatch 6, the ejection mechanism 14, the capsule supports 15.
  • Fig. 8 shows the emergency hatch opening mechanism at the bottom of the fuselage, where the fuselage 1, hatch 6, rescue capsule 7, portholes 9, eject mechanism 14, capsule supports 15, axis of rotation of the hatch 18, axis
  • Figure 9 shows the emergency hatch opening mechanism at the bottom of the fuselage, put into operation, where the fuselage 1, hatch 6, rescue capsule 7, portholes 9, eject mechanism 14, capsule supports 15, hatch axis of rotation 18, capsule rotation axis 19, capsule air bag belts 20, movable beam 24, hatch opening lever 25, mount the movable beam to the fuselage 26.
  • Figure 10 and figure 11 shows the ejection of the rescue capsules 7 through the hatches in the upper part of the fuselage 21 with the previous firing of the tail unit 4, where the fuselage 1, the transition between the capsules 8, portholes 9, the parachute system 17, the axis of rotation of the hatch 18, axis rotation of the capsule 19.
  • Figure 12 shows the ejection of the rescue capsules 7 through the hatch 22 in the rear of the fuselage 1 with the preliminary firing of the tail unit 4, where the windows 9, the tubular guides 12.
  • Figure 13 shows the ejection of rescue capsules 7 through the hatch 22 in the rear of the fuselage 1, where portholes 9, tubular guides 12, parachute system 17.
  • FIG shows the location of the capsules 7 in the fuselage 1 when they are thrown out through the lower hatches 6 along the vertical guides of the capsule descent 23, where the fuselage 1, the pilot cabin 2, the tail unit 4, the transition between capsules 8, the guide for the movement of capsules "in a circle "29.
  • FIG shows the ejection of the capsules 7 through the lower hatches 6 of the fuselage 1 along the vertical rails 23, where the tail unit 4, the transition between the capsules 8, portholes 9, the parachute system 17, the belt of the airbags of the capsules 20.
  • FIG. 16 and FIG. 17 shows a section of a multi-tier airplane with a carousel mechanism for dropping capsules through the lower hatch 6, where the fuselage 1, the capsule 7, the vertical guides for lowering the capsules 23, rigid supports
  • SUBSTITUTE SHEET (RULE 26) carousel on the fuselage 28, the guide for the movement of capsules "in a circle” 29.
  • the proposed aircraft comprises a fuselage 1 containing a pilot's cabin 2, equipped with an on-board computer and a device for delivering electronic commands in the necessary sequence for implementing the evacuation program, wings 3, tail unit 4, engines 5, chassis (not shown).
  • wings 3, tail unit 4, engines 5, chassis (not shown).
  • chassis (not shown).
  • four emergency hatches 6, made with the possibility of automatic opening ( Figure 1 and Figure 2).
  • Pilot cockpit 2 is equipped with all the usual controls for a passenger cockpit, as well as a device for sending electronic commands in the necessary sequence for implementing the method of mass emergency evacuation of passengers.
  • this device can be powered by an on-board computer, pilot, flight attendant or a signal from the Earth.
  • the passenger compartment is made in the form of four separate sealed autonomous rescue capsules 7, which are separated from each other by narrow passages 8.
  • Each capsule 7 is designed for 4-12 passengers. In a calm, non-emergency situation, during normal operation of the air transport, the capsule 7 is connected by transitions 8 to each other, and therefore only functions as a compartment (compartment). It also allows you to divide the cabin into classes and levels of comfort. If the aircraft is a private vehicle, then the capsules 7 become separate rooms, with the appropriate furniture for them. Capsules are attached to each other using rubber gaskets-suction cups (not shown), which act as stabilizers for the position of the capsules in the fuselage.
  • SUBSTITUTE SHEET (RULE 26) capsule retention mechanism in the fuselage.
  • Each capsule contains. portholes 9, located opposite the side portholes of the fuselage, passenger seats 17, which are equipped with individual means of fixation to ensure the safety of passengers and crew (not shown).
  • a life support system 10 which includes the necessary supply of food, water, medicines and things that are necessary for the survival of passengers after landing or splashing the capsule.
  • the capsule 7 has a luggage compartment 11, and in the upper part of the capsule there is a compartment with hinged hatches, in which brake parachutes 17 are placed, and the hatches are made with the possibility of their automatic opening, and parachutes with the possibility of automatically putting them into action.
  • capsule 7 there is a device for moving the capsule 7 along the fuselage 1, consisting of tubular guides 12 located in the lower part of the fuselage 1, the opening locks of the hatch 13, the ejection mechanism 14 and the capsule support 15 (Fig. 5 and Fig. 6). Also in capsule 7 there are devices for controlling flight planning and parachute slings, a passenger safety system for capsule 7 falling out, which is carried out using furniture equipment, individual means for depreciation in the seats of passengers and crew at the time of capsule falling out and destabilization of the capsule’s position, and also at the time of landing or splashdown (not shown). Externally, the capsule, on the sides and bottom, there are airbag belts 20 ( Figure 4).
  • each hatch 6 In the lower part of the fuselage there are four hatches 6, which automatically open in case of emergency. Above them, along the fuselage 1, are placed capsules 7, standing on flexible supports 15, which are rigidly fixed on the inner wall of the hatches 6. The length of each hatch 6 is elongated by an amount selected taking into account the size of the capsule 7 so that the capsule 7 when turning and falling out passed without contact with open hatch 6 and other parts of the fuselage 1. Also, the axis of rotation
  • SUBSTITUTE SHEET (RULE 26) capsule 19 is offset relative to the axis of the hatch 18 in height.
  • Such an arrangement in the presence of flexible supports 15, such as stabilizers of the parallelism position of the capsule 7 relative to the hatch 6, makes it possible to discard the capsule 7 with minimal cost of the side space.
  • the movable beam 24 passes.
  • the beam 24 is attached to the inside of the fuselage 1 by means of a fastening 26 at a level between the upper edge of the hatch 6 and the windows 9 and is brought into horizontal movement by means of a pneumatic accumulator (not shown).
  • a rotary lever for opening the hatch 25 is attached to the beam 24 from the side of the pneumatic accumulator.
  • the other end is attached rigidly to the inner surface of the hatch 6.
  • the horizontal beam 24 will move the edge of the lever 25 horizontally, which, under the action of pressure, will open the hatch cover 6.
  • the hatch 6 and the capsule 7 rotate in a circle, respectively, for their axes 18 and 19, and flexible resistances 15 support the capsule 7 parallel to the hatch 6.
  • the proposed method for emergency evacuation of passengers from air transport is as follows.
  • a signal is received about the implementation of the evacuation program from the on-board computer or from the pilot, or from the flight attendant, or
  • the capsule has the ability to be controlled from the inside. It is equipped with devices for flight planning and sling management, which is important when falling out in mountainous regions.
  • Hatchways 6 are the lower hinged part of the fuselage, located directly under the capsule 7.
  • the locks of the hatches 13 are opened using hydraulic devices or pneumatic ejection mechanisms 14.
  • the capsules 7 are pushed out of the hatches 6 under the action of their weight and the pneumatic accumulator, slide along the tubular guides 12.
  • the airbags 20 are opened on the outer capsule body, which are located on the sides and bottom of the capsule and after which the first parachute from the parachute system automatically opens
  • SUBSTITUTE SHEET (RULE 26) 17 which after a fraction of a second, as it moves away from the aircraft, draws out the main parachute.
  • Airbags are indispensable when landing capsules 7 on water, and also serve as shock absorbers when landing on land.
  • the tail 4 is first shot, the vertical hatches 21 are opened, then the capsules are ejected using compressed air along the vertical guides of the capsule descent 23.
  • the airbags 20 immediately open on each capsule 7 and the first parachute opens automatically from the parachute system 17, which, after a fraction of a second, as it moves away from the aircraft, draws out the main parachute, which makes it possible to sharply increase the distance of the capsule 7 from the aircraft (to come off).
  • a rail chain evacuation mechanism is used, in which all the capsules 7 are evacuated sequentially: one after the other through the hatch in the rear of the fuselage 22.
  • the structure inside the body is equipped with solid axes that tighten stiffness, and also solid guides 12, on which capsules 7 are fixed, with the possibility of slipping on them.
  • the tail is shot first.
  • the air stream that will be directed in the direction opposite to the crash will take out capsules 7, each following the previous one, while automatically opening the first parachute from the parachute system 17, which after a split second, as you move away from the plane, pulls the main parachute.
  • the aircraft body When evacuating capsule 7 from large two-tier aircraft, the aircraft body is divided into separate compartments, which include a carousel mechanism in which the capsules are located on different tiers and descend in a circle down to the lower hatch 6. Having reached an adjacent position with the lower hatch 6 in the fuselage 1, the capsule with the guide "in a circle” 29 slides along
  • SUBSTITUTE SHEET (RULE 26) vertical rails 23 down through a previously opened hatch 6. Having released its lower position, other capsules 7 descend in turn to the place of the previous capsule 7 and similarly leave the plane.

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

Abstract

L'invention concerne l'aviation, en particulier des procédés visant à porter secours à des passagers d'un moyen de transport aérien. Le procédé d'évacuation d'urgence de passagers de moyen de transport aérien est basé sur l'utilisation d'un salon se présentant sous la forme de capsules hermétiques séparées dotées de parachutes. Le moyen de transport aérien utilisé comporte des passages entre les capsules et est équipé de trappes en lien direct avec chaque capsule, de guides tubulaires qui sont fixés sur des supports flexibles et de batteries pneumatiques. Dans une situation d'urgence, les passages de liaison entre les capsules sont détachés, et les passagers sont automatiquement immobilisés sur des sièges passagers de la capsule. Les capsules sont éjectées lors de l'ouverture des trappes. Des coussins externes de sécurité de la capsule se déploient lors de l'ouverture automatique du parachute. L'invention concerne également un avion doté d'un équipement pour porter secours à des passagers et comprenant une trappe de secours dans le fuselage et des capsules. Chaque capsule est équipée de dispositifs en vue d'un déplacement le long du fuselage dans la direction de la trappe de secours, de freins parachutes, de dispositifs d'amortissement et de moyens individuels pour la survie des passagers, de dispositifs de commande de vol plané, au cours du vol, et de commande des suspentes du parachute. Ces inventions concernent également l'élargissement de la plage de situations d'urgence dans lesquelles s'effectue le sauvetage collectif de passagers.
PCT/UA2011/000005 2010-10-20 2011-01-28 Procédé d'évacuation collective d'urgence de passagers d'un moyen de transport aérien et avion doté d'un équipement pour porter secours à des passagers dans une situation d'urgence WO2012054002A1 (fr)

Applications Claiming Priority (2)

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UA2010012397 2010-10-20
UAA201012397 2010-10-20

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WO2012054002A1 true WO2012054002A1 (fr) 2012-04-26

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102826226A (zh) * 2011-06-14 2012-12-19 凌春林 民航机的安全装置
WO2017033033A1 (fr) * 2015-08-26 2017-03-02 Dunai Nándor Système de sécurité pour des aéronefs
RU186459U1 (ru) * 2018-10-31 2019-01-21 Евгений Станиславович Фокин 1 безопасный самолёт фокина
RU188465U1 (ru) * 2018-11-15 2019-04-15 Евгений Станиславович Фокин 1 спасательное кресло фокина для летательных аппаратов

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1798137A (en) * 1927-12-15 1931-03-31 Peter A Beck Load-discharging means for airplanes
RU2039680C1 (ru) * 1993-06-08 1995-07-20 Центральный научно-исследовательский институт химии и механики Управляемая парашютная система для доставки грузов
RU2085095C1 (ru) * 1993-11-15 1997-07-27 Камелия Вениаминовна Князева Каска с подшлемником
RU2096261C1 (ru) * 1993-11-12 1997-11-20 Владимир Павлович Жигунов Универсальный корпус летательного аппарата
RU7656U1 (ru) * 1997-10-15 1998-09-16 Государственный космический научно-производственный центр им.М.В.Хруничева Площадка для группового десантирования с легкого самолета
US5921504A (en) * 1997-08-17 1999-07-13 Elizondo; Joey P. Aircraft passenger extraction system
US6554227B2 (en) * 1999-03-01 2003-04-29 Dietmar Wolter Flight apparatus
RU2260548C2 (ru) * 1999-12-20 2005-09-20 Чуй-Вен ЧЮ Самолет с разделяемым корпусом и независимыми пассажирскими салонами
RU2270787C2 (ru) * 2004-04-12 2006-02-27 Ефремов Владимир Анатольевич Способ эвакуации людей из объекта их большого скопления
RU2304547C2 (ru) * 2003-06-25 2007-08-20 Валерий Ильич Сметанников Устройство для размещения грузов на летательном аппарате и их десантирования с него
RU80430U1 (ru) * 2008-08-04 2009-02-10 Владимир Степанович Лекарев Устройство для спасения авиапассажиров
UA52936U (uk) * 2010-05-27 2010-09-10 Владимир Николаевич Татаренко Літак із пристроєм для порятунку пасажирів при аварійній ситуації

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1798137A (en) * 1927-12-15 1931-03-31 Peter A Beck Load-discharging means for airplanes
RU2039680C1 (ru) * 1993-06-08 1995-07-20 Центральный научно-исследовательский институт химии и механики Управляемая парашютная система для доставки грузов
RU2096261C1 (ru) * 1993-11-12 1997-11-20 Владимир Павлович Жигунов Универсальный корпус летательного аппарата
RU2085095C1 (ru) * 1993-11-15 1997-07-27 Камелия Вениаминовна Князева Каска с подшлемником
US5921504A (en) * 1997-08-17 1999-07-13 Elizondo; Joey P. Aircraft passenger extraction system
RU7656U1 (ru) * 1997-10-15 1998-09-16 Государственный космический научно-производственный центр им.М.В.Хруничева Площадка для группового десантирования с легкого самолета
US6554227B2 (en) * 1999-03-01 2003-04-29 Dietmar Wolter Flight apparatus
RU2260548C2 (ru) * 1999-12-20 2005-09-20 Чуй-Вен ЧЮ Самолет с разделяемым корпусом и независимыми пассажирскими салонами
RU2304547C2 (ru) * 2003-06-25 2007-08-20 Валерий Ильич Сметанников Устройство для размещения грузов на летательном аппарате и их десантирования с него
RU2270787C2 (ru) * 2004-04-12 2006-02-27 Ефремов Владимир Анатольевич Способ эвакуации людей из объекта их большого скопления
RU80430U1 (ru) * 2008-08-04 2009-02-10 Владимир Степанович Лекарев Устройство для спасения авиапассажиров
UA52936U (uk) * 2010-05-27 2010-09-10 Владимир Николаевич Татаренко Літак із пристроєм для порятунку пасажирів при аварійній ситуації

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102826226A (zh) * 2011-06-14 2012-12-19 凌春林 民航机的安全装置
WO2017033033A1 (fr) * 2015-08-26 2017-03-02 Dunai Nándor Système de sécurité pour des aéronefs
RU186459U1 (ru) * 2018-10-31 2019-01-21 Евгений Станиславович Фокин 1 безопасный самолёт фокина
RU188465U1 (ru) * 2018-11-15 2019-04-15 Евгений Станиславович Фокин 1 спасательное кресло фокина для летательных аппаратов

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