WO2012054002A1

WO2012054002A1 - Method for the mass emergency evacuation of passengers from air transport and aeroplane with equipment for rescuing passengers in an emergency situation

Info

Publication number: WO2012054002A1
Application number: PCT/UA2011/000005
Authority: WO
Inventors: Тэтяна Иванивна ДЭМЭНЧУК
Original assignee: Demenchuk Tetyana Ivanivna
Priority date: 2010-10-20
Filing date: 2011-01-28
Publication date: 2012-04-26

Abstract

The inventions relate to aviation, specifically to methods for rescuing passengers from air transport. The method for the emergency evacuation of passengers from air transport is based on the use of a salon in the form of separate hermetic capsules with parachutes. Use is made of air transport which has inter-capsule passages and is equipped with hatches intended for each specific capsule, tubular guides which are fixed on flexible supports, and a pneumatic battery. In an emergency situation, the connecting inter-capsule passages are uncoupled, after which the passengers are automatically secured in passenger seats in the capsule. The capsules are ejected upon opening of the hatches. External capsule safety cushions are opened upon automatic opening of the parachute. An aeroplane with equipment for rescuing passengers comprises an emergency hatch in the fuselage and capsules containing passenger seats. Each capsule is equipped with devices for movement along the fuselage in the direction of the emergency hatch, retarding parachutes, shock-absorbing devices and individual life support means for the passengers, control devices for planning in flight and for controlling the parachute shroud lines. The inventions are directed towards expanding the range of emergency situations in which a mass safe rescue of passengers is achieved.

Description

Method for mass emergency evacuation of passengers from air transport and an aircraft with equipment for rescuing passengers in an emergency

The invention relates to aviation, and in particular to methods for rescuing passengers from an aircraft.

In 1994, the media reported that the European Aerospace Agency completed the development of the aircraft (A380) with a special way to save passengers in an airplane that is in a plane crash. The method consists in the fact that in case of an accident or other extreme situations, the wings detach and fall off the plane, then the aircraft body is divided in half and with the help of powerful parachute systems these parts, together with passengers and equipment, are lowered to the ground. This method is quite expensive to use and the probability of saving all passengers, crew members is quite small. In addition, the implementation of this method is possible under ideal conditions of landing only on the ground.

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. When evacuation is closed doorways Rescue capsule shaped charges carried explosive cutting fuselage separating the rescue capsule from the screw, the bow with the cockpit, the tail

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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 closest to the essential features of the claimed method of mass emergency evacuation of passengers from air transport is the method implemented by an airplane with a device for rescuing passengers in an emergency (see Ukrainian patent N ° 52936, IPC B64D 25/00, B64C 1/32, B64C 3 / 54, published September 10, 2010, Bulletin M> 17, 2010. 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;

in the upper and lower parts of the fuselage, respectively, 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, and the container is equipped with:

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SUBSTITUTE SHEET (RULE 26) a device for moving the container along the fuselage, in the direction of the emergency hatch;

the floor and end walls with slots and a door in them, which are hermetically closed and located opposite the doors of the pilot's cabin and adjacent containers;

passenger hatches, for entry and exit of passengers located opposite to hatches of the same purpose in the fuselage;

in its upper part - compartments with hinged hatches for placing brake container 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;

in its lower part - with compartments with hinged hatches for placement of 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;

in its lower part - small-sized soft landing rocket engines;

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;

individual means for depreciation and fixation, ensuring the safety of passengers and crew members at the time of container landing or landing;

individual and collective means of autonomous life support after landing or splashing the container.

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SUBSTITUTE SHEET (RULE 26) For reasons that impede the achievement of the technical result indicated below when using this technical solution, there is only one emergency hatch, namely in the rear of the fuselage, which makes it impossible to ensure the rescue of passengers in all types of emergency situations.

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.

To solve the problem and achieve the corresponding technical result in the known method of mass emergency evacuation of passengers from air transport, in which 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, according to the invention, in the event of an emergency in air transport, 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.

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SUBSTITUTE SHEET (RULE 26) In this case, the ejection of autonomous rescue capsules occurs when the hatches previously located under the capsules are opened simultaneously, or when the hatches previously located above the capsules are opened or when the hatches previously located in the tail section of the aircraft with the previous tail are 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.

Another feature is that 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,

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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:

a device for moving the capsule along the fuselage, in the direction of the emergency hatch;

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;

compartments with hinged hatches for placement of shock-absorbing devices, with the possibility of automatic opening of these hatches;

passenger seats;

control devices for flight planning and control of parachute slings;

individual means of fixation to ensure the safety of passengers and crew in the capsule and the furniture security system; capsule prolapse;

individual means for depreciation, ensuring the safety of passengers and crew at the time of landing or splashdown;

individual means for the life support of passengers.

The inclusion of the capsule sealing mechanism in the event of an emergency, the fixation of passengers in passenger seats using restraint equipment and airbags, the ejection of self-contained rescue capsules through open hatches ensures safe rescue of passengers from air transport, and the deployment of external capsule airbags and the further opening of the capsule parachute enables safely plant the capsule under different planting conditions. 6

SUBSTITUTE SHEET (RULE 26) The features and nature of the present invention will become more apparent from the detailed description set forth below when taken in conjunction with the drawings in which like reference numerals carry respective identification throughout and in which: · _g

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 4 - capsule of the aircraft;

Figure 5 - section of the fuselage with the capsule in a calm (non-emergency) situation, section aa in figure 2;

6 - placement of the capsule on the tubular guides of the lower hatch, 'A is a side view, B is a top view;

Fig.7 - sliding of the capsule along the tubular guides of the lower hatch using pneumatic piston (top view);

Fig - mechanism for opening the lower hatch;

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;

11 - the ejection of rescue capsules through the upper hatches of the fuselage;

Figure 12 - ejection of rescue capsules through the hatch in the rear of the fuselage with the previous firing of the tail unit along tubular guides (of the "chain" type);

Figure 13 - ejection of rescue capsules through the hatch in the rear of the fuselage along tubular guides;

Fig - the location of the capsules in a relaxed atmosphere when they are thrown through the lower hatches along the vertical guides;

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SUBSTITUTE SHEET (RULE 26) Fig - throwing capsules through the lower hatches along the vertical guides;

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

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SUBSTITUTE SHEET (RULE 26) rotation of the capsule 19, the belt of air cushions of the capsules 20, the movable beam 24, the lever for opening the hatch 25, the fastening of the movable beam to the fuselage 26.

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.

On 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.

On 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.

In 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

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SUBSTITUTE SHEET (RULE 26) carousel on the fuselage 28, the guide for the movement of capsules "in a circle" 29.

To explain the essence of the invention, an example of the operation of an aircraft with a capacity of 48 passenger seats. 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). In the lower part of the fuselage 1 are 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. In the case of assessing a specific situation as emergency and deciding on the 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.

Transitions 8 together with stabilizers create a single

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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). Under the seats is 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. Also, 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. Also in the 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).

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

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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.

Parallel to the capsule 7, along the fuselage 1, on both sides of the capsule 7. 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. When the capsule 7 of the upper edge has already passed through the hole of the hatch 6 and nothing is threatening it, then under the action its weight and pneumatic accumulator mechanism 7 capsule slides along the tubular guide 12 which is rigidly attached to a flexible substrate 15. During deposition of the capsule 7, the hatch 6 is opened streamlined fuselage 1, stabilizes the aircraft, its velocity slows and smoothes possible fall. After the capsule 7 falls out, a similar closing mechanism for the hatch 6 is applied, where the beam 24 moves in the opposite direction and the hatch 7 closes accordingly (Fig. 8 and Fig. 9).

The proposed method for emergency evacuation of passengers from air transport is as follows.

After assessing the specific situation as emergency, that is, one that requires the evacuation of passengers, 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

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SUBSTITUTE SHEET (RULE 26) from the earth. Further sealing is carried out of the capsule passing through the gate and disengaged coupling transitions mezhdukapsulnye 8. Several automatic action occurs within the capsule 7 _J Passengers poluchivshiu signal take their seats in the passenger seats 16 and seat belts are fastened, then doing the same flight attendants, controlling passengers. The second signal is accompanied by the operation of an automatic furniture security system. The system works to provide restraining furniture for the body of people, protecting first of all their head, shoulder girdle, elbows and knees. During such transformations, doors are simultaneously sealed, the hatch cover 6 opens, the capsule 7 turns over and falls out, and during such a turn passengers are constantly in a stable vertical state as opposed to the angle of incidence, thanks to furniture transformations. In the event of a sharp blow or concussion of the capsule 7, the passenger is clamped by air cushions so that they are fully absorbed by the air and avoids possible fractures. 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.

To evacuate the capsule through the lower hatch 6, it is placed inside the aircraft body so that it has several support points 15 on the inner edges of the fuselage 1. Hatchways 6 are the lower hinged part of the fuselage, located directly under the capsule 7.

After the evacuation signal, 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. After the capsule 7 falls out, 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

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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.

When the capsules 7 are evacuated through the upper hatches 21, 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. Similarly, as in the previous version, 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).

When evacuating the capsules 7 through the tail of the aircraft 4, 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. In an emergency or crash, 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.

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

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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.

This method and its implementation options can be used in the design of new, safe aircraft.

The implementation of the invention in essence of the proposed aircraft structure is possible, since the additional equipment necessary to solve the technical problem is well known.

Information sources:

1. RF patent e 2207301, IPC B64C27 / 04, B64C1 / 32, B64D17 / 80, publ. 06/27/2003

2. Patent of Ukraine Jfe 52936, IPC B64D 25/00, B64C 1/32, B64C 3/54, publ. 09/10/2010, bull. JY ° 17, 2010

Digital designations:

1. The fuselage.

2. The pilot's cabin.

3. Wings.

4. The tail.

5. Engines.

6. Luke.

7. Capsules.

8. Transition between capsules.

9. Portholes.

10. Life support system.

11. The luggage compartment.

12. Tubular guides.

13. Locks for opening the hatch.

14. The ejection mechanism.

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SUBSTITUTE SHEET (RULE 26) 15. Support capsules.

16. Passenger seats.

17. The parachute system.

18. The axis of rotation of the hatch.

19. The axis of rotation of the capsule.

20. Capsule airbag belts.

21. Hatches at the top of the fuselage.

22. Hatch in the rear of the fuselage.

23. Vertical guides for the descent of capsules.

24. The movable beam.

25. Lever for opening the hatch.

26. Fastening the movable beam to the fuselage.

27. The piston of the ejection mechanism.

28. Rigid support of the carousel mechanism on the fuselage.

29. Guide for the movement of capsules "in a circle."

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SUBSTITUTE SHEET (RULE 26)

Claims

Formula

1. The method of mass emergency evacuation of passengers from air transport, in which the passenger cabin is made in the form of separate sealed autonomous rescue capsules with parachutes, which consists in discarding sealed autonomous rescue capsules with passengers from the aircraft cabin, characterized in that when an emergency occurs during air transport the passage of the capsule with closures, intercapsular junction transitions are unfastened, after which the passengers are automatically locked into the passages chairs with the help of restraining furniture equipment and airbags, and the release of self-contained rescue capsules occurs while opening the hatches designed specifically for each capsule, moreover, the capsule, which is previously placed rigidly on tubular guides that are rigidly fixed on flexible supports, under the influence of its weight and the pneumatic accumulator slides along the tubular guides, after which the external airbags of the capsule are deployed and then automatically parachute capsule opening.

2. The method according to p. 1, characterized in that the ejection of self-contained rescue capsules occurs while opening the hatches previously located under the capsules.

3. The method according to claim 1, characterized in that the ejection of self-contained rescue capsules occurs while opening the hatches previously located above the capsules.

4. The method according to claim 1, characterized in that the ejection of self-contained rescue capsules occurs when the hatch is opened, previously located in the tail of the aircraft with the previous tail shooting.

5. The method according to p. 1-4, characterized in that the opening of the hatch occurs

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SUBSTITUTE SHEET (RULE 26) with rigid fixation of the hatch until the capsule completely falls out, so that some planning of the flight of the air transport is ensured and resistance to the flow of air is carried out in order to slow down the speed of the falling air transport.

6. The method according to claim 1 to 4, characterized in that, if necessary, after ejecting only one capsule, the hatch is closed and the fuselage is sealed.

7. The method according to claim 1, characterized in that 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.

8. 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 sending electronic commands in the necessary sequence for the implementation of the evacuation program; wings; tail; engines chassis; at least one emergency hatch in the fuselage, made with the possibility of automatic opening, characterized in that it contains at least one sealed autonomous rescue capsule, in which passengers are equipped with:

passenger seats;

control devices for flight planning and control

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SUBSTITUTE SHEET (RULE 26) parachute slings;

individual means for the life support of passengers.

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SUBSTITUTE SHEET (RULE 26)