ES2223208B1 - AIRCRAFT SAFETY DEVICE. - Google Patents

AIRCRAFT SAFETY DEVICE.

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Publication number
ES2223208B1
ES2223208B1 ES200102736A ES200102736A ES2223208B1 ES 2223208 B1 ES2223208 B1 ES 2223208B1 ES 200102736 A ES200102736 A ES 200102736A ES 200102736 A ES200102736 A ES 200102736A ES 2223208 B1 ES2223208 B1 ES 2223208B1
Authority
ES
Spain
Prior art keywords
chamber
gas
opening
doors
cockpit
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
ES200102736A
Other languages
Spanish (es)
Other versions
ES2223208A1 (en
Inventor
Pedro Rodriguez Martinez
Manuel Magaña Cases
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to ES200102736A priority Critical patent/ES2223208B1/en
Publication of ES2223208A1 publication Critical patent/ES2223208A1/en
Application granted granted Critical
Publication of ES2223208B1 publication Critical patent/ES2223208B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
    • B64D45/0036—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by disabling or restraining attackers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
    • B64D45/0021—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems means for restricting access to flight deck
    • B64D45/0028—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems means for restricting access to flight deck doors or door arrangements specially adapted to restrict unauthorized access
    • B64D45/0029—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems means for restricting access to flight deck doors or door arrangements specially adapted to restrict unauthorized access electrically actuated
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
    • B64D45/0036—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by disabling or restraining attackers
    • B64D45/0042—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by disabling or restraining attackers by spraying or injecting chemicals
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
    • B64D45/0051—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by monitoring passengers or crew on aircraft
    • B64D45/0053—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by monitoring passengers or crew on aircraft using visual equipment, e.g. cameras
    • G—PHYSICS
    • G08—SIGNALLING
    • G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
    • G08B15/00—Identifying, scaring or incapacitating burglars, thieves or intruders, e.g. by explosives
    • G08B15/02—Identifying, scaring or incapacitating burglars, thieves or intruders, e.g. by explosives with smoke, gas, or coloured or odorous powder or liquid

Abstract

Dispositivo de seguridad en aeronaves que comprende la hermetización de la cámara de tripulación técnica adyacente a la cabina de mandos, por medio de puertas automáticas de accionamiento rápido, y el vertido automático en la misma, una vez cerrada, de un gas adormizante/paralizante. El accionamiento del dispositivo se produce manualmente al ser detectada una irrupción de personal no autorizado en la cámara por medio de video cámaras. El dispositivo tiene un sensor del nivel de gas en la cámara y mandos independientes de apertura de una válvula de descarga del gas al exterior, una vez reducido el agresor, y de apertura independiente de las puertas de acceso a la cámara desde la cabina de mandos y desde la zona de pasaje.Aircraft safety device comprising the sealing of the technical crew chamber adjacent to the cockpit, by means of automatic doors with rapid actuation, and the automatic pouring into it, once closed, of a sleep / paralyzing gas. The device is activated manually when an irruption of unauthorized personnel in the camera is detected by means of video cameras. The device has a gas level sensor in the chamber and independent controls for opening a gas discharge valve to the outside, once the aggressor is reduced, and for independent opening of the chamber access doors from the control cabin and from the passage area.

Description

Dispositivo de seguridad en aeronaves.Aircraft safety device.

Objeto de la invenciónObject of the invention

La presente invención se refiere a un dispositivo de seguridad en aeronaves, del tipo de aviones de líneas comerciales de pasajeros, con el fin de evitar la toma del control de los mismos por personas no autorizadas, tales como secuestradores o terroristas.The present invention relates to a device aircraft safety, of the type of line aircraft commercial passengers, in order to avoid taking control thereof by unauthorized persons, such as kidnappers or terrorists.

Antecedentes de la invenciónBackground of the invention

A la actualidad, los únicos medios de seguridad existentes en aeronaves tales como aviones comerciales, para evitar la toma del control, esto es, el manejo de los mandos de los mismos, por personas no autorizadas, consiste en la realización de controles en tierra, tanto de los equipajes como de los bultos o efectos personales que pueden portar los pasajeros directamente para evitar la entrada de armas en la aeronave.At present, the only means of security existing in aircraft such as commercial aircraft, to avoid taking control, that is, handling the controls of the themselves, by unauthorized persons, consists in the realization of ground controls of both luggage and packages or personal effects that passengers can carry directly to prevent the entry of weapons into the aircraft.

Estos medios, como desgraciadamente se ha podido comprobar, no aportan la eficiencia suficiente, cosa que si se consigue con el dispositivo de la invención.These means, as unfortunately it has been possible check, they do not provide enough efficiency, which if get with the device of the invention.

Descripción de la invenciónDescription of the invention

El dispositivo de la invención por su constitución y utilización, sirve de una manera óptima para evitar la toma de los mandos de una aeronave, tal como un avión comercial de transporte de pasajeros, por parte de personal no autorizado, tal como secuestradores o terroristas, consiguiendo asimismo reducir a estas personas sin causarles daños ni a ellos ni al resto de la tripulación y/o el pasaje.The device of the invention for its constitution and use, serves in an optimal way to avoid taking the controls of an aircraft, such as a commercial airplane of passenger transport, by unauthorized personnel, such as kidnappers or terrorists, also getting reduce these people without harming them or the rest of the crew and / or the ticket.

De acuerdo con la invención el dispositivo comprende la creación de un departamento hermético y securizado, coincidente con la cámara, adyacente a la cabina de mandos de la aeronave, destinada a la tripulación técnica (azafatas y similares), en el cual se reducirá a los individuos que accedan a la misma con intenciones dudosas.According to the invention the device includes the creation of a tight and secure department, coinciding with the camera, adjacent to the cockpit of the aircraft, intended for the technical crew (hostesses and similar), in which it will be reduced to individuals who access the same with doubtful intentions.

Para esto se dispone en la cámara de tripulación técnica:For this it is available in the crew chamber technique:

- Unas puertas blindadas antibalas y/o deflagraciones, aligeradas, de accionamiento rápido automático, en los accesos desde la cabina de mandos a la cámara de tripulación técnica.- Bulletproof armored doors and / or deflagrations, lightened, automatic quick-acting, in access from the cockpit to the crew chamber technique.

- Unas puertas blindadas antibalas y/o deflagraciones, aligeradas, de accionamiento rápido y automático, que se disponen en cada acceso de la zona de pasaje a la cabina de tripulación técnica.- Bulletproof armored doors and / or deflagrations, lightened, fast and automatic, that are arranged in each access from the passage area to the cabin of technical crew

- Al menos, una videocámara de visualización de la cámara de tripulación técnica con, al menos, un monitor de visualización de las imágenes captadas por la misma, que se dispone en la cabina de mandos preferentemente. La videocámara puede ser fija u orientable remotamente y/o automáticamente.- At least one camcorder display of the technical crew chamber with at least one monitor visualization of the images captured by it, which is available in the cockpit preferably. The camcorder can be fixed or adjustable remotely and / or automatically.

- Unos depósitos de almacenamiento de gas adormizante y/o paralizante, no dañino para la salud humana, con, al menos, una electroválvula de accionamiento automático cuya apertura produce la descarga del gas en la cámara de tripulación técnica una vez que ésta se halla herméticamente cerrada.- Gas storage tanks numbing and / or paralyzing, not harmful to human health, with, at least one auto-operated solenoid valve whose opening produces the discharge of gas into the crew chamber technique once it is tightly closed.

- Al menos, una válvula de descarga del gas adormizante/paralizante desde la cámara de tripulación técnica hacia el exterior de la aeronave, siendo sustituido por aire limpio, una vez que el agresor ha sido reducido por el gas.- At least one gas discharge valve numbing / paralyzing from the technical crew chamber towards the outside of the aircraft, being replaced by air Clean, once the aggressor has been reduced by gas.

- Un sensor del nivel de gas en la cámara de tripulación técnica.- A gas level sensor in the chamber of technical crew

- Unos mandos de accionamiento del dispositivo, que se ubican preferentemente próximos a los monitores de visualización de las imágenes captadas por las videocámaras y que comprenden, al menos, un único mando de accionamiento rápido que produce el cierre rápido de las puertas blindadas así como, inmediatamente a continuación, la apertura de la válvula de descarga del gas desde sus depósitos de almacenamiento hacia la cámara de tripulación técnica. Igualmente, una vez reducido el agresor, los mandos incorporan accionamientos independientes de apertura de la válvula de descarga del gas hacia el exterior así como de las puertas de acceso desde la cabina a la cámara de tripulación técnica con el fin de que la tripulación de la cabina de mando pueda esposar convenientemente al agresor.- Device drive controls, which are preferably located close to the monitors of display of images captured by camcorders and that they comprise at least a single fast-acting command that produces the quick closing of armored doors as well as, immediately then the valve opening gas discharge from its storage tanks to the technical crew chamber. Likewise, once the aggressor, the controls incorporate independent drives of opening of the gas discharge valve outwards as well as from the access doors from the cabin to the chamber of technical crew in order for the cabin crew of command can conveniently handcuff the aggressor.

De este modo, si se produce un intento de acceso no autorizado a la cabina de mandos de la aeronave, cuando el agresor accede a la cámara de tripulación técnica será captado por la cámara y visualizado por la tripulación a través del monitor situado en la cabina de mandos.Thus, if an access attempt occurs unauthorized to the cockpit of the aircraft, when the aggressor accesses the technical crew chamber will be captured by the camera and visualized by the crew through the monitor located in the cockpit.

Actuando sobre el único mando se producirá el cierre simultáneo, automático y hermético de todas las puertas de la cámara tripulación técnica así como la gasificación de la misma, lo que reducirá a la inconsciencia al agresor junto con el resto de las personas que estén en dicha cámara. Una vez reducidas, mediante un mando independiente se abre la válvula de descarga del gas al exterior, mediante otro mando independiente se produce la apertura de las puertas que comunican la cabina de mando con la cámara de tripulación técnica con el fin de que el agresor pueda ser convenientemente esposado. El nivel de gas adecuado para reducir al agresor y para entrar sin peligro a la cámara es monitorizado por el sensor de gas.Acting on the single command will produce the simultaneous, automatic and hermetic closing of all doors the technical crew chamber as well as its gasification, which will reduce the aggressor to unconsciousness along with the rest of the people in that chamber. Once reduced, by an independent control opens the gas discharge valve to the outside, by means of another independent control the opening takes place of the doors that connect the cockpit with the camera technical crew so that the aggressor can be conveniently handcuffed The appropriate level of gas to reduce aggressor and to enter the camera safely is monitored by the gas sensor

Breve descripción de los dibujosBrief description of the drawings

La figura 1 muestra esquemáticamente el dispositivo de la invención.Figure 1 schematically shows the device of the invention.

Descripción de una realización práctica de la invenciónDescription of a practical embodiment of the invention

El dispositivo 1 de la invención está constituido por unas puertas 2 herméticas, blindadas y aligeradas, de accionamiento rápido automático motorizado, que se disponen en los accesos 3 de la zona 4 de pasaje a la cabina 5 de tripulación técnica, y en los accesos 6 de esta cámara a la cabina 7 de mandos de un avión comercial de pasajeros.The device 1 of the invention is constituted  through airtight 2 doors, armored and lightened, of motorized automatic quick drive, which are arranged in the access 3 from passenger zone 4 to crew cabin 5 technique, and in the accesses 6 of this chamber to the cockpit 7 of controls of a commercial passenger plane.

En la cabina 5 y/o en la zona de pasaje 4 se disponen unas microcámaras 8 de vídeo, de visualización de estas zonas, cuyas imágenes captadas son visualizadas en la cabina 7 de mandos, a través de, al menos, un monitor 9.In cabin 5 and / or in passenger zone 4, they have 8 video micro cameras, for viewing these areas, whose captured images are displayed in cabin 7 of controls, through at least one monitor 9.

El dispositivo comprende igualmente unos depósitos 10 de almacenamiento de gas adormizante y/o paralizante sin otros efectos secundarios a la salud humana, con unas válvulas 11 automáticas de apertura para que el gas se vierta en la cámara 5 al cerrarse ésta herméticamente.The device also includes some 10 storage tanks for numbing and / or paralyzing gas without other side effects to human health, with valves 11 automatic opening for gas to be poured into chamber 5 when closed tightly.

En la cámara 5 se dispone igualmente un sensor 12 del nivel de gas, así como una válvula 13 de descarga de gas al exterior.A sensor 12 is also arranged in chamber 5  of the gas level, as well as a gas discharge valve 13 at Exterior.

Cuando se produce un intento de acceso de un terrorista o secuestrador a la cabina de mandos, al pasar por la cámara de tripulación técnica es captado por las microcámaras 8 y visualizado los monitores 9.When an attempt to access a terrorist or kidnapper to the cockpit, when passing through the technical crew chamber is captured by micro cameras 8 and displayed monitors 9.

Entonces, alguno de los ocupantes de la cabina de mandos acciona un único mando 14 que produce el cierre rápido automático y simultáneo de las puertas 2, y una vez cerradas, la apertura de las válvulas 11 y la entrada del gas a la cámara de tripulación técnica, con lo que el individuo, así como cualquier otra persona que esté en la cámara, será reducido.Then, some of the occupants of the cabin  controls actuates a single control 14 that produces quick closing automatic and simultaneous doors 2, and once closed, the opening of the valves 11 and the gas entering the chamber technical crew, with what the individual, as well as any Another person in the chamber will be reduced.

La comprobación de que se ha alcanzado el nivel de gas necesario para reducir al agresor se realiza por medio de las indicaciones de la medición efectuada por el sensor 12, y una vez que se tiene la certeza de que el agresor ha sido reducido, accionando unos mandos 15 independientes, de apertura de la válvula 16 de descarga del gas al exterior, se renueva el aire de la cámara, y una vez efectuado esto se acciona un mando 17 independiente de apertura de las puertas que comunican la cámara 5 con la cabina 7 de mando, con el fin de que la tripulación pueda esposar convenientemente al agresor.Verification that the level has been reached of gas needed to reduce the aggressor is done by means of the indications of the measurement made by the sensor 12, and a once it is certain that the aggressor has been reduced, by operating independent controls 15, valve opening 16 of discharge of the gas to the outside, the air of the camera, and once this is done a command 17 is activated independent opening of the doors that communicate the chamber 5 with the cockpit 7, so that the crew can conveniently handcuff the aggressor.

Igualmente la apertura de las puertas que comunican la cámara 5 con la zona de pasaje se abren mediante otro mando independiente, no representado.Likewise the opening of the doors that they communicate chamber 5 with the passage area they are opened by another independent command, not represented.

Claims (4)

1. Dispositivo de seguridad en aeronaves caracterizado porque comprende la hermetización de la cámara de tripulación técnica adyacente a la cabina de mando, principalmente por medio de unas puertas automáticas de accionamiento rápido que cierran herméticamente los accesos a la cámara de tripulación técnica de la aeronave desde la cabina de mandos así como desde la zona de pasaje, al ser accionado un único mando; simultáneamente se produce en la cámara herméticamente cerrada el vertido de un gas adormizante/paralizante desde, al menos, un depósito de almacenamiento; el nivel de gas en la cámara es controlado por medio de, al menos, un sensor; en la cámara se disponen, al menos, una válvula de descarga del gas adormizante/paralizante al exterior, que es sustituido por aire limpio una vez reducido el agresor; el dispositivo tiene, al menos, unos mandos independientes de apertura de las puertas automáticas de los accesos de la cabina de mando a la cámara de tripulación técnica y de la zona de pasaje a la cámara de tripulación técnica; el dispositivo tiene un mando independiente de apertura de la válvula de descarga del gas al exterior; en la zona donde se dispone el único mando de cierre de puertas y vertido del gas se dispone, al menos, un monitor de visualización de las imágenes captadas por, al menos, una vídeocámara dispuesta en la cámara de tripulación técnica y/o zona de pasaje.1. Aircraft safety device characterized in that it comprises the sealing of the technical crew chamber adjacent to the cockpit, mainly by means of automatic fast-acting doors that hermetically close the accesses to the aircraft's technical crew chamber from the cockpit as well as from the passenger zone, when a single command is activated; Simultaneously, the spill of a sleep / paralyzing gas from at least one storage tank occurs in the hermetically sealed chamber; the level of gas in the chamber is controlled by means of at least one sensor; in the chamber, at least, an unloading / paralyzing gas discharge valve is arranged outside, which is replaced by clean air once the aggressor is reduced; the device has, at least, independent controls for opening the automatic doors of the accesses of the cockpit to the technical crew chamber and the passage area to the technical crew chamber; the device has an independent control for opening the gas discharge valve outside; In the area where the only door closing and gas discharge command is provided, at least one display monitor of the images captured by at least one camcorder arranged in the technical crew chamber and / or area of disposal is available. passage. 2. Dispositivo según reivindicación 1 caracterizado porque el vertido de gas se produce mediante la apertura de, al menos, una electroválvula de cierre del/de los deposito/s de almacenamiento de gas.2. Device according to claim 1 characterized in that the discharge of gas is produced by opening at least one solenoid valve for closing the gas storage tank (s). 3. Dispositivo según reivindicación 1 caracterizado porque el único mando de cierre de las puertas y vertido de gas, así como los monitores de visualización de las imágenes captadas por las videocámaras, se disponen en la cabina de mando.3. Device according to claim 1, characterized in that the only control for closing the doors and pouring gas, as well as the monitors for displaying the images captured by the camcorders, are arranged in the control cabin. 4. Dispositivo según reivindicación 1 caracterizado porque los mandos de apertura independiente de las puertas, así como el de apertura de la válvula de descarga del gas al exterior se disponen en la cabina de mando.4. Device according to claim 1 characterized in that the independent opening controls of the doors, as well as the opening of the gas discharge valve to the outside are arranged in the control cabin.
ES200102736A 2001-12-10 2001-12-10 AIRCRAFT SAFETY DEVICE. Expired - Fee Related ES2223208B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES200102736A ES2223208B1 (en) 2001-12-10 2001-12-10 AIRCRAFT SAFETY DEVICE.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200102736A ES2223208B1 (en) 2001-12-10 2001-12-10 AIRCRAFT SAFETY DEVICE.

Publications (2)

Publication Number Publication Date
ES2223208A1 ES2223208A1 (en) 2005-02-16
ES2223208B1 true ES2223208B1 (en) 2006-04-16

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Family Applications (1)

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ES200102736A Expired - Fee Related ES2223208B1 (en) 2001-12-10 2001-12-10 AIRCRAFT SAFETY DEVICE.

Country Status (1)

Country Link
ES (1) ES2223208B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2973344B1 (en) 2011-04-01 2013-11-29 Latecoere AIRCRAFT WITH A MONITORING SYSTEM

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE759331A (en) * 1970-11-23 1971-05-24 Franki Robert AIRCRAFT ANTI-Hijacking Device
US3658277A (en) * 1970-12-11 1972-04-25 Charles I Anderson Aircraft anti-hijacking structure
FR2641397A1 (en) * 1989-01-05 1990-07-06 Coret Francis Devices for disabling attackers on board aircraft

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