WO2018190744A1 - Escape device for aircraft crew and passengers - Google Patents
Escape device for aircraft crew and passengers Download PDFInfo
- Publication number
- WO2018190744A1 WO2018190744A1 PCT/RU2017/000506 RU2017000506W WO2018190744A1 WO 2018190744 A1 WO2018190744 A1 WO 2018190744A1 RU 2017000506 W RU2017000506 W RU 2017000506W WO 2018190744 A1 WO2018190744 A1 WO 2018190744A1
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- WO
- WIPO (PCT)
- Prior art keywords
- aircraft
- passengers
- seat
- crew
- hatch
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- 230000004913 activation Effects 0.000 abstract 1
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
- B64D25/10—Ejector seats
Definitions
- the device is intended for the aviation industry, namely to save the crew and passengers of aircraft.
- the claimed device solves the problem of emergency rescue of the crew and passengers of such helicopters.
- This device can also be used for aircraft, where, in addition to saving the crew, it is necessary to save passengers.
- the device for saving the crew and passengers of aircraft contains seats for the crew and passengers, installed with the possibility of leaving the aircraft in emergency situations, while the seats with crew and passengers leave the aircraft through the lower hatches, while the opening of the lower hatches occurs using emergency pedals equipped with clamps with a ring, the very leaving the aircraft takes place along the guides installed in the cockpit at an angle to the lower hatch and parallel to the backs of the seats, in addition, the hinged lower hatches are fixed in the tilted state so that they and their guides form one plane with the guides for the seats along which the aircraft leaves.
- the second task, the invention is aimed at, is to increase the safety of leaving an emergency aircraft.
- This task is solved by the fact that the rescue chair is equipped with a march accelerate.
- FIG. 1 - the device is shown before the emergency, where 1 is the pilot's seat, 2 are the guides, 3 is the lower hatch, 4 is the location of the guides of the lower hatch.
- FIG. 2 FIG. 3, Fig. 4 - enlarged view shows the action of the emergency pedal - 5, with a pin - 6, with a latch - 7, retractable into the socket - 8.
- Fig. 5 and FIG. 6 pilot rescue (the design of the guides of the cockpit and the lower hatch is enlarged, see section A-A).
- FIG. 9 is a sectional view B - B in front showing the stages of leaving the emergency helicopter.
- the mid-flight accelerators — 9 are installed so that the seat with the person moves away from the emergency aircraft.
- the left seat is equipped with an accelerator on the right, and the right seat is on the left.
- the mid-flight accelerator turns on after 5 - 10 seconds. Opening the hatch under the right seat occurs after 5 - 10 seconds, and after another 5 - 10 seconds the marching accelerator of the right seat is turned on.
- FIG. 10 is a cross-sectional front view of an emergency aircraft with two rows of seats on the port side and port side.
- segments — 10, of the lower part of the skin of the aircraft are tilted, and then after 5 to 10 seconds the lower hatch opens, and only then the marching accelerator turns on.
- the mid-flight accelerators are installed on the right, and in the seats on the right, the mid-flight accelerators are installed on the left.
- the use of mid-flight accelerators in chairs allows avoiding a collision with the aircraft body, helicopter propeller, wings and aircraft engines.
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- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
An escape device for aircraft crew and passengers comprises seats (1) for crew and passengers, which are mounted for ejection from an aircraft in the event of an emergency, wherein seats with crew and passengers are ejected from the aircraft via bottom hatches (3), and the bottom hatches are opened by means of emergency pedals (5) provided with detents with a ring. Ejection from the aircraft takes place along guides (2) mounted in the cabin at an angle to the bottom hatch (3) and parallel to the backs of the seats (1), the tip-back bottom hatches (3) being fixed in a tipped back state so that the bottom hatches (3) and their guides (4) form, in conjunction with the guides (2) for the seats (1), a single plane along which ejection from the aircraft takes place. The device is further equipped with a thrust accelerator (9) mounted on one side of the seat in a vertical plane and on the line of the centre of mass of the seat and its occupant, wherein said thrust accelerator is activated 5-10 seconds after opening of the bottom hatch, and a second bottom hatch opens 5-10 seconds after activation of the thrust accelerator of the first seat.
Description
УСТРОЙСТВО ДЛЯ СПАСЕНИЯ ЭКИПАЖА И ПАССАЖИРОВ DEVICE FOR RESCUE CREWS AND PASSENGERS
ЛЕТАТЕЛЬНЫХ АППАРАТОВ AERIAL VEHICLES
Устройство предназначено для авиационной отрасли, а именно для спасения экипажа и пассажиров летательных аппаратов. The device is intended for the aviation industry, namely to save the crew and passengers of aircraft.
Известно, в частности из Патента РФ на изобретение Ν» 2101217, В 64 D 25/10, 19. 01. 1990., катапультное кресло. Данное кресло предназначено для аварийного спасения пилота катапультированием вверх. Это кресло невоз- можно использовать для вертолётов, у которых не отстреливается винт. It is known, in particular, from the RF Patent for the invention Ν "2101217, B 64 D 25/10, 19. 01. 1990., ejection seat. This seat is designed for emergency rescue of the pilot by ejection up. This seat cannot be used for helicopters for which the propeller does not shoot.
Заявленное устройство решает задачу аварийного спасения экипажа и пассажиров таких вертолётов. Данное устройство может использоваться и для самолётов, там, где кроме спасения экипажа необходимо спасение и пас- сажиров. The claimed device solves the problem of emergency rescue of the crew and passengers of such helicopters. This device can also be used for aircraft, where, in addition to saving the crew, it is necessary to save passengers.
Устройство для спасения экипажа и пассажиров летательных аппаратов содержит кресла для экипажа и пассажиров, установленные с возможностью покидания летательных аппаратов в аварийных ситуациях, при этом кресла с экипажем и пассажирами покидают летательные аппараты через нижние люки, при этом открывание нижних люков происходит при помощи аварий- ных педалей, снабжённых фиксаторами с кольцом, само же покидание лета- тельных аппаратов происходит по направляющим, установленным в кабине под углом к нижнему люку и параллельно спинкам кресел, кроме того, от- кидные нижние люки фиксируется в откинутом состоянии так, чтобы они и их направляющие составляли с направляющими для кресел одну плоскость, по которой и происходит покидание летательного аппарата. The device for saving the crew and passengers of aircraft contains seats for the crew and passengers, installed with the possibility of leaving the aircraft in emergency situations, while the seats with crew and passengers leave the aircraft through the lower hatches, while the opening of the lower hatches occurs using emergency pedals equipped with clamps with a ring, the very leaving the aircraft takes place along the guides installed in the cockpit at an angle to the lower hatch and parallel to the backs of the seats, in addition, the hinged lower hatches are fixed in the tilted state so that they and their guides form one plane with the guides for the seats along which the aircraft leaves.
Вторая задача, на решение которой направлено изобретение - повыше- ние безопасности покидания аварийного летательного аппарата. Данная за- дача решается тем, что спасательное кресло снабжено маршевым ускорите-
лем, установленным сбоку кресла в общей вертикальной плоскости и на го- ризонтальной линии с центром масс кресла с пилотом или пассажиром. The second task, the invention is aimed at, is to increase the safety of leaving an emergency aircraft. This task is solved by the fact that the rescue chair is equipped with a march accelerate. A unit installed on the side of the chair in a common vertical plane and on a horizontal line with the center of mass of the chair with the pilot or passenger.
На Фиг. 1 - изображено устройство до аварийной ситуации, где 1 - кресло пилота, 2 - направляющие, 3 - нижний люк, 4 - место расположения направляющих нижнего люка. На Фиг. 2, Фиг. 3, Фиг.4 - в увеличенном раз- мере показано действие аварийной педали— 5, со штифтом - 6, с фиксатором - 7, убирающимся в гнездо - 8. На Фиг. 5 и Фиг. 6 - спасение пилота (увели- чено показана конструкция направляющих кабины и нижнего люка, см. раз- рез А- А). In FIG. 1 - the device is shown before the emergency, where 1 is the pilot's seat, 2 are the guides, 3 is the lower hatch, 4 is the location of the guides of the lower hatch. In FIG. 2, FIG. 3, Fig. 4 - enlarged view shows the action of the emergency pedal - 5, with a pin - 6, with a latch - 7, retractable into the socket - 8. In Fig. 5 and FIG. 6 - pilot rescue (the design of the guides of the cockpit and the lower hatch is enlarged, see section A-A).
На Фиг. 7, Фиг. 8, Фиг. 9 - вид в разрезе Б - Б спереди показаны стадии покидания аварийного вертолёта. При этом маршевые ускорители— 9, уста- новлены так, чтобы кресло с человеком смещалось в сторону от аварийного летательного аппарата. Левое кресло снабжено ускорителем справа, а правое кресло— слева. Кроме того, после открывания нижнего люка и выпадения кресла с человеком, маршевый ускоритель включается через 5 - 10 секунд. Открывание люка под правым креслом происходит через 5 - 10 секунд, а ещё через 5 - 10 секунд включается маршевый ускоритель правого кресла. In FIG. 7, FIG. 8, FIG. 9 is a sectional view B - B in front showing the stages of leaving the emergency helicopter. At the same time, the mid-flight accelerators — 9, are installed so that the seat with the person moves away from the emergency aircraft. The left seat is equipped with an accelerator on the right, and the right seat is on the left. In addition, after opening the lower hatch and falling out of a chair with a person, the mid-flight accelerator turns on after 5 - 10 seconds. Opening the hatch under the right seat occurs after 5 - 10 seconds, and after another 5 - 10 seconds the marching accelerator of the right seat is turned on.
На Фиг. 10, Фиг. 1 1 , Фиг. 12 вид в разрезе спереди аварийного самолё- та с двумя рядами кресел по левому и правому бортам. При этом вначале от- кидываются сегменты— 10, нижней части обшивки самолёта, а затем через 5 - Ю секунд открывается нижний люк, а уж после этого включается марше- вый ускоритель. В креслах слева маршевые ускорители установлены справа, а в креслах справа маршевые ускорители установлены слева. Использование в креслах маршевых ускорителей позволяет избежать столкновения с корпу- сом летательного аппарата, винтом вертолёта, крыльями и двигателями са- мол та. In FIG. 10, FIG. 1 1, FIG. 12 is a cross-sectional front view of an emergency aircraft with two rows of seats on the port side and port side. In this case, at first, segments — 10, of the lower part of the skin of the aircraft — are tilted, and then after 5 to 10 seconds the lower hatch opens, and only then the marching accelerator turns on. In the seats on the left, the mid-flight accelerators are installed on the right, and in the seats on the right, the mid-flight accelerators are installed on the left. The use of mid-flight accelerators in chairs allows avoiding a collision with the aircraft body, helicopter propeller, wings and aircraft engines.
В задачу данного изобретения не входит описание системы управления маршевыми ускорителями.
The purpose of this invention is not included in the description of the control system of mid-flight accelerators.
Claims
1.Устройство для спасения экипажа и пассажиров летательных аппара- тов содержащее кресла для экипажа и пассажиров, установленные с возмож- ностью покидания летательных аппаратов в аварийных ситуациях, отли- чающееся тем, что кресла с экипажем и пассажирами покидают летательные апараты через нижние люки, при этом открывание нижних люков происхо- дит при помощи аварийных педалей, снабжёнными фиксатороми с кольцом, само же покидание летательных аппаратов происходит по направляющим, установленным в кабине под углом к нижнему люку и параллельно спинкам кресел, кроме того, откидные нижние люки фиксируется в откинутом со- стоянии так, чтобы они и их направляющие составляли с направляющими для кресел одну плоскость, по которой и происходит покидание летательного аппарата. 1. A device for saving the crew and passengers of aircraft containing seats for the crew and passengers, installed with the possibility of leaving the aircraft in emergency situations, characterized in that the seats with the crew and passengers leave the aircraft through the lower hatches, In this case, the opening of the lower hatches occurs with the help of emergency pedals equipped with a latch with a ring, while the aircraft themselves leave along the guides installed in the cockpit at an angle to the lower hatch and parallel but the back seat, in addition, folding bottom hatches locked in the tilted co-standing, so that they and their guides were the guide for a seat plane on which takes place leaving the aircraft.
2.Устройство по п. 1 отличающееся тем, что оно снабжено маршевым ускорителем, установленным сбоку кресла в одной вертикальной плоскости и на линии центра масс кресла с человеком, кроме того включение маршевого ускорителя происходит через 5 - 10 секунд после открытия нижнего люка, открытие второго нижнего люка происходит через 5 - 10 секунд после вклю- чения маршевого ускорителя первого кресла, кроме того, при использовании кресла в самолётах, вначале откидывается сегмент нижней части обшивки, а затем через 5—10 секунд происходит открывание нижнего люка, кроме того, в первую очередь открывается нижний люк под крайним к борту самолёта креслом, а затем, после включения его маршевого ускорителя, через 5 - 10 секунд открывается второй нижний люк.
2. The device according to claim 1, characterized in that it is equipped with a marching accelerator installed on the side of the chair in the same vertical plane and on the line of the center of mass of the chair with a person, in addition, the marching accelerator is turned on 5-10 seconds after opening the lower hatch, opening the second the lower hatch occurs 5 to 10 seconds after turning on the marching accelerator of the first seat; in addition, when using the seat on airplanes, the segment of the lower part of the skin is first tilted, and then after 5-10 seconds the lower part opens of the hatch, in addition, first opens the lower hatch under extreme to board an airplane seat, and then, after turning it sustainer accelerator, 5 - 10 seconds the second lower hatch.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2017111966 | 2017-04-10 | ||
RU2017111966A RU2017111966A (en) | 2017-04-10 | 2017-04-10 | Fokin device for rescue of crew and passengers of aircraft |
RU2017122125 | 2017-06-23 | ||
RU2017122125A RU2017122125A (en) | 2017-06-23 | 2017-06-23 | Fokine Rescue Chair |
Publications (1)
Publication Number | Publication Date |
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WO2018190744A1 true WO2018190744A1 (en) | 2018-10-18 |
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PCT/RU2017/000506 WO2018190744A1 (en) | 2017-04-10 | 2017-07-07 | Escape device for aircraft crew and passengers |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20220185488A1 (en) * | 2020-12-10 | 2022-06-16 | Hyundai Motor Company | Air mobility |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1991012989A1 (en) * | 1990-02-26 | 1991-09-05 | Mcdonnell Douglas Corporation | Anti tip-off ejection rails |
UA67783C2 (en) * | 2000-12-26 | 2004-07-15 | Олександр Опанасович Камінський | Aircraft ensuring rescue of passengers and crew at approaching the inevitable catastrophe |
US20090212160A1 (en) * | 2006-07-13 | 2009-08-27 | Michael Lawrence Beauchamp | Method for producing lateral ejection apparattii for helicopter or plane |
RU105260U1 (en) * | 2011-01-12 | 2011-06-10 | Николай Николаевич Топалов | AIRCRAFT PASSENGER RESCUE SYSTEM |
-
2017
- 2017-07-07 WO PCT/RU2017/000506 patent/WO2018190744A1/en active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1991012989A1 (en) * | 1990-02-26 | 1991-09-05 | Mcdonnell Douglas Corporation | Anti tip-off ejection rails |
UA67783C2 (en) * | 2000-12-26 | 2004-07-15 | Олександр Опанасович Камінський | Aircraft ensuring rescue of passengers and crew at approaching the inevitable catastrophe |
US20090212160A1 (en) * | 2006-07-13 | 2009-08-27 | Michael Lawrence Beauchamp | Method for producing lateral ejection apparattii for helicopter or plane |
RU105260U1 (en) * | 2011-01-12 | 2011-06-10 | Николай Николаевич Топалов | AIRCRAFT PASSENGER RESCUE SYSTEM |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20220185488A1 (en) * | 2020-12-10 | 2022-06-16 | Hyundai Motor Company | Air mobility |
US11518529B2 (en) * | 2020-12-10 | 2022-12-06 | Hyundai Motor Company | Air mobility |
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