UA52936U - Aircraft with device for rescue of passengers in case of emergency - Google Patents

Abstract

An aircraft with a device for rescue of passengers in case of emergency includes: a fuselage with hatches for entry and exit of passengers and crew from a cockpit equipped with an on-board computer and a device for issuing electric commands in required sequence for implementation of a rescue program that in the event of a decision to evacuate the passengers may be actuated by an on-board computer, pilot or from the ground; wings, a tail, engines, chassis, an emergency hatch in the rear part of fuselage made with possibility of automatic opening, and seats for passengers. The aircraft is equipped with at least one rigid airtight heat-insulated landing container located inside the fuselage, inside which in the longitudinal direction the seats for passengers and crew are located. In the upper and lower parts of fuselage upper and lower guides are installed, respectively which are made with possibility of interaction with them of relevant elements of the container and are means for fastening said container in a fixed position and unfixturing to move the container along the fuselage automatically. The aircraft is equipped with means for automatic closing the emergency hatch after moving-out of the container from the fuselage.

Description

The useful model refers to aircraft construction. Similarly, in KO 2177441 C2, it is used for the removal of the fuze, in particular, for the construction of passenger and passenger capsule cargo-passenger aircraft with increased explosion-proof cutting. which flight In KO 2200688 C2 according to the idea of the inventors for

It is known that, although the number of victims in an air disaster is much less than in the case of a road accident, the problem of ensuring the safety of the tail part, the cockpit and the cockpit as before, is one of the most relevant and la. for its solution, many measures were taken in the world. The same idea was implemented in KO 2021164 C1, where your community. means of separating parts of the aircraft from each other pro-

For example, a plane with a wing is known, which is supposed to be made in the form of pyrobolts, which will connect the inflatable shell with the clock-work detonator attached to it with the attached panels to give the wing the necessary structure. hardness (5 3481569). However, such a wing can be used only for ultralight aircraft. fuselage, characterized by the fact that the ava-

An aircraft with an additional wing is known to have a launch pad with passengers installed on it from the fuselage in the event of an accident (the 05 seats are pushed out in the rear 2193029). It is equipped with a single-layer flexible direction with the help of pyro cartridges and parachutes. sheathing and also cannot be used for However, with such a push-out, it is possible to jam- rescue mainline aircraft. changing the elements of the site.

A well-known device for saving an aircraft. In an airplane according to KO 29032 01, the fuselage is made of a device containing an emergency wing, which is released with the possibility of disconnection both vertically and from the fuselage, which is made telescopic, with horizontal planes. Passengers are placed in the telescopic structure in the front upper part. (5 1839660). In the non-working position, the wing can be drawn inwards in a certain sequence. However, the inflation of the avanosity into several parts with the help of cumulative swarming wings with compressed air through the holes of the ven-charges is characterized and the method according to KO 2200688 tails cannot be carried out instantly. C1. After separating the fuselage nose, wings and tail

In Ky 2335431 C2, this device is improved, the roof and blocks of seats with people, who are placed in the wing of the high-speed parachute device, descend to the ground. detonation in the form of a cumulative explosive charge. The disadvantage of all the above-mentioned detonation solutions with an electric detonator. However, the tele-use of subversive cutting of the plane's body, the Kopic wing at any gas pressure in it, is irreversibility of destruction, with the impossibility of providing the necessary rigidity and further use of the plane. In addition, with disparity. cutting by directed explosions is a danger

The idea of retractable wings develops in Ku damage, depressurization or destruction of cap- 2114030 C1. The essence of the invention lies in the fact that people are separated in a sula or other means in which or on which plane, which contains equipped wings. It becomes more difficult to maintain the upper and lower parts of the aircraft separated from each other due to the need to maintain the integrity of the fuselage, with their longitudinal quick-detachable connectors and pyrobolts and to check this. Finally, the compartments for passengers and the crew are found - a possible detonation of cumulative charges when flashed in the upper part of the fuselage, which is being disembarked. blacksmiths

Engines, energy carriers and the cargo compartment are located in the lower part of the fuselage. The wings of the hnical result, which is achieved, is an airplane from the upper part made retractable. The same device for rescuing passengers in the event of an emergency, the aerodynamic characteristics of the aircraft can confuse situations according to OA 67783 C2. The aircraft has a fuselage that can be extended to the limits that allow you to land the aircraft with hatches for the entry and exit of crew members and without destroying it. The disadvantage is the impossibility of re-docking of the upper and lower parts by means of sajhors, on-board portholes, pilot. cabin and two emergency hatches in the back -

A number of proposals are based on the idea of a slot, wings, tail and propulsion. starting the aircraft in the event of an emergency and passenger seats, equipped with individual rescue parts of its parts with passengers. So, with KO shutters installed on fixed along the fu- 2171209 C1 known aviation passenger capsule iron guides. There are devices for fastening the rescue rope, which is a part of the passenger seats in their regular position, unfixing them in the cabin. It is made in the form of a hermetically sealed compartment placed in the fasteners when an electrical command is applied to the evacuation fuselage, which is also activated for the transportation of seats, with the help of a parachute and a winch. The parachute is connected to the trog of the pulling devices, to the open emergency ones themselves, the other ends of which are connected to the winch through the hatches for landing the seats together with the passenger - a distribution mechanism that reduces the speed of us. Evacuation control is carried out by the capsule's landing device and ensures its soft position for issuing electrical commands in the necessary manner. The release of the capsule from the fuselage is carried out prior to the implementation of the rescue program, which can be started by the pilot or from Earth by cutting the fuselage along the transverse planes. Spaces in which special explosive devices are placed. according to one of the options, all passenger seats can be united by a tubular frame. Pas-

Not only the seats are equipped with slats, but also the fixings themselves for moving the container along the passenger compartment. automatically, at the command of the on-board computer

The advantage of the prototype, in comparison with the character, the pilot or from the Earth, and the rear ends are nitrified above devices, is the preservation of the harvester guides located in the area of the hinges of the integrity of the aircraft. As a drawback, it is worth pointing out the opening of the emergency hatch, and the upper guides in the not: the tail part of the fuselage are elongated by the amount - - insecurity of passengers during evacuation from well, chosen taking into account the length of the container of low temperatures at high flight altitudes; so that the latter could leave the fuselage - for a catastrophic situation, it is too long without contact with the emergency hatch, during its open time, necessary to leave the aircraft in the event of a situation, and with other elements of the fuselage; individual landing of chairs; - the aircraft is equipped with a device for automatic - with short-term use of a large ki- closing of the emergency hatch after extending the number of parachutes, the manifestation of "aerodynamic container from the fuselage, and the container is equipped with: foot shading" is possible, when one of the domes of the parachutes is - a device for moving the container blow holes for others; along the fuselage, in the direction of the emergency hatch; - lack of means of life support (medical - floor and end walls with openings and first aid, water, food, fire extinguishing means, doors in them that close hermetically and communication) for passengers who have landed or are located opposite the cockpit doors and dwelt until rescuers arrived. Necessary adjacent containers; take into account that in hard-to-reach areas, rescue hatches for passenger hatches, for entry and exit, may appear after several days; passengers located opposite the hatches of the same - the possibility of defeating people on the ground when assigned to the fuselage; large number of earth seats; - in its upper part - compartments with fold- - the unrealism of a successful landing (using hatches for placing brake hydrogens in them) of passengers on a parachute due to their pro- parachutes of the container, moreover, the hatches are made of professional unpreparedness. Among the passengers with 0 - the possibility of their automatic opening, and all of them may not necessarily have former parachutes - with the possibility of automatic closure - parachutists or pilots. The special risk of putting them into effect; children, the disabled, and the elderly are susceptible. - in its lower part - compartments with folding

The task of the useful model is to create an airplane with hatches for placing shock-absorbing balusters, a device for rescuing passengers in an emergency, mainly those that fill with gas, from a situation, when using which, not only the possibility of automatic opening of these hatches would ensure its integrity and the possibility of the next automatic inflation of these balloons according to the signal of use, but the altimeter and their installation before landing was significantly increased, the reliability of saving passengers and improved or lowering them below the lower dimensional condition of their life support, starting from the upper container by a given value; evacuation from the plane until the arrival of rescuers. - in its lower part - small-sized ra-

In addition to the passengers, this device also has soft-landing engines; to cover the rescue of crew members, the location - by an on-board computer capable of monitoring which in the pilot's cabin after the occurrence, the orientation of the container in space, the speed of the emergency situation is not necessary for the descent, the distance to the surface of the Earth or water; stopping the flight and saving the plane itself. - compartment of on-board automation and measurement

New equipment is proposed to solve the problem, including a device for determining the location of the container with a device for rescuing passengers; emergency situation, which includes: a fuselage with hatches - individual cushioning means for the entry and exit of passengers and crew members, and with and fixation to ensure the safety of passengers and a cockpit equipped with an on-board computer for crew members at the time of landing or a propeller and a device for submitting electrical commands to the container; in the necessary sequence for the implementation of the program - Individual and collective means of rescue, which, in the case of a decision on autonomous life support after landing - evacuation of passengers, may include lifting or lowering the container. by computer, pilot or from Earth; wings; This version of the aircraft with a rescue device is the tail; engines; chassis; the emergency hatch in it makes it possible to eliminate the noted shortcomings of the proto-tail part of the fuselage, which is made of mozhlyp. The execution of landing, or evacuation, with its automatic opening, and the seat of the container rigid, airtight, passengers. According to the useful model: thermally insulated and equipped with the specified - the aircraft is equipped with at least one, layouts that allow reliable landing or landing inside the fuselage, rigidly sealing the container with passengers and crew members, heat-insulated landing container, determine the coordinates of the location of the containers - inside which in the longitudinal direction of the installer and report them to the rescue services. Under the seats of passengers and crew members; the time of descent and before the arrival of rescuers, the life of the passengers - in the upper and lower parts of the fuselage of the occupants, already of the container, is not exposed to the unmodified, respectively, upper and lower guides, which burn, including, due to low temperatures, made of the possibility of interaction with them corresponds to high heights outside the container. The possibility of these elements of the container, and there are means for fixing the equipment of the container with all the necessary means - the mentioned container in a stationary state and space, from rockets and balloons for soft landing to medical

cargoes, water, food, excludes the dependence of the likely fixation of the container in a stationary state and the fixation of the survival of people on their age, state of health for its movement along the fuselage of the aircraft, professional skills. automatically, according to the received command (not shown).

The essence of the useful model is explained by the schematic drawing in the upper part of the container 11, where: in: fig. 17 shows a side view of compartment 23 with automatically opening hatches of the proposed aircraft; fig. 2 - the same, view (not shown) for placing passengers in them from above; fig. C - section A-A in fig. 2; fig. 4 - section of parachutes 24, 25 (Fig. 6) of the container. In the lower time-

B-B in fig. 3; fig. 5 - removal of the landing continous container, 11 arranged compartments with hatches, the container from the fuselage; fig. 6 - landing containers that open automatically (not shown) for ner. placement of inflatable cushioning balls in them

The proposed aircraft includes a fuselage 1 (fig. 26, the gas filling of which is turned on when 1, 2 is removed) with on-board portholes 2 and the pilot’s wife of the container is carried out by a signal from the cockpit 3, wings 4, tail 5 with a keel 6, a metric altimeter . Cylinders in front of engines 7 and landing gear (not shown). are established by landing or landing

The cockpit is equipped with all the usual at such a height as to be lower than the lower dimensions of the passenger or cargo surface of the container by a given amount. Such a passenger plane is equipped with signaling devices, and in the lower part of the container there are low-loaders, as well as a device for feeding electric general-purpose rocket engines 27 for soft landing. of commands in the necessary sequence according to Each of the 11 containers is equipped with automatic implementation of the rescue program. In the event of a decision to evacuate passengers made by the air conditioning and lighting systems, this device is equipped with an inertial electric generator (it cannot be activated by the on-board computer), which is made of a waterproof, closed type. rum, by pilot or from Earth. In the normal position, when the containers 11 are re-

The fuselage also has hatches 8 for entry and exit are in the middle of the fuselage, the mentioned systems of crew members and passengers, and in the tail part, connected to the corresponding systems of the aircraft is easy to disassemble the fuselage, there is a slot with emergency lu- nium connecting couplings (not shown). . com 9. It is made with the possibility of automatic The passenger part of the container 11 is equipped with opening relative to the hinge 10 (Fig. 5). on the usual headset of passenger cabins

In the middle of the fuselage, in its longitudinal planes. For the placement of hand luggage, there are one or two or more heavable shelves 28, and for oversized luggage, there are airtight, heat-insulated landing containers 29 under the floor 14, which has trench windows 11. They have an ordinary frame bearing cons- with hatches (not shown). In addition, a structure in the form of frames 12 (Fig. 3, 4), a compartment (not shown) for on-board automation and longitudinal beams and stringers with external covering equipment, including a device for lashing (not shown), is provided. in which the portholes are built-in 13. determining the location of the container. Also

The latter are located opposite the on-board illumina- the container is equipped with an on-board computer (not torus 2 of the fuselage. The floor 14 divides the space is shown), capable of controlling the orientation of the container on the upper, passenger, 15 and lower, the container in space, the speed of descent, the distance to the cargo , 16 parts. In the middle of the container is the surface of the Earth or water. seats for 17 passengers are installed. A part of the seats in Each seat 17 is equipped with inflatable rescue- the front part of the front container with life jackets and automatic seat belts is reserved for crew members. In safety to fix the body on landing or the ends of the containers opposite each other if lowered (not shown). More than one container compartment is provided, openings are made (not for medicine, drink and food, but shown) with a door that closes hermetically, as well as a toilet (not shown). (not shown). The front doors of the front container are located opposite the cockpit doors. way. After assessing the situation as an emergency, on-board

In the upper and lower parts of the fuselage, the upper 18 and lower 19 guides are placed by on-board computers, or by the pilot, or from the Earth in flight, respectively. implementation is initiated in the required sequence

Opposite them to the container 11 are fixed wheels 20, rescue programs. These include: opening ava-21 with the possibility of rolling along the fuselage guides. hatch 9, release of container(s) 11, per-

Structurally, these elements can be made by moving the container(s) along the guides 18, 19 to the other. It is important that the container can move the opening of the hatch 9 of the fuselage, push out along the fuselage in the direction of the hatch 9. The brake parachutes 22 after reaching the bottom of the lower guides are located in the zone of the edge of the opening with the container. After the exit of the container 10. The upper guides 18 in the tail part of the ner outside the fuselage from the compartments 23 are extended to the fuselage by the amount selected from the landing parachutes 24, 25, which ensure the melting of the length of the container 11 in such a way that neither landing nor lowering the container. So that the latter could leave the fuselage without contact with the container's speed reduction at the time of its emergency hatch, in its open position, and contact with the Earth's surface to a minimum possible with other elements of the fuselage (Fig. 5). Engines 27 are turned on slowly and the container is dried by inflating and inflating the cylinders 26. of a small-sized rocket engine or an electromechanical drive (not shown). The removal of the mounted operation crew members, not involved in the management of the tank from the fuselage, is carried out by a brake plane, occupying seats in the reserved seats with parachutes 22. Means for 11 are also provided.

After the evacuation of the container from the plane, depending on the The proposed plane can be made from the altitude of the plane and the character and the stones based on the available on the domestic and entrenchment of the seriousness of the accident, the pilot still has bottom markets of components and parts. Tactical and technical some time to correct the situation. In practice, the capabilities of the aircraft do not deteriorate. But, in comparison, there are emergency situations, when the necessary measures are similar to the analogs described above, new regarding the correction of the situation, as well as the landing of the aircraft - the property of the aircraft consists in the elimination of the obligatory - are not allowed if there is a passenger on board, its destruction for implementation of rescue of passengers. In the case of the previous evacuation of fat passengers. As for the prototype, in which the wreckage of the plane in the container, such measures can be carried out, the plane is also not foreseen, and the plane, with an acceptable degree of risk, is provided for the proposed plane can be saved. At the same time, if the level of reliability of the rescue and the possibility of correcting the situation after evacuation are as high as possible in the comfort of the conditions in which the passengers are, the pilot(s) must eject during the rescue operation. save your life

Numerical designations 1 Fuselage 16 Cargo part 2 Porthole 17 Seat

Z Cockpit 18 Upper guide 4 Wing 19 Lower guide

Tail 20 Upper wheel b Keel 21 Lower wheel 7 Engine 22 Brake chute 8 Entry and exit hatch 23 Parachute compartment 9 Emergency hatch 24 Landing parachute

Hinge 25 Landing parachute 11 Landing container 26 Balloon 12 Frame 27 Soft landing rocket engine 13 Porthole 28 Shelf 14 Floor 293 Compartment under the floor

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Ministry of Education and Science of Ukraine

State Department of Intellectual Property, str. Urytskogo, 45, Kyiv, MSP, 03680, Ukraine

SE "Ukrainian Institute of Industrial Property", str. Glazunova, 1, Kyiv - 42, 01601