ES2123022T3 - Mando electronico para el accionamiento de la cinematica de una puerta de avion. - Google Patents
Mando electronico para el accionamiento de la cinematica de una puerta de avion.Info
- Publication number
- ES2123022T3 ES2123022T3 ES93118060T ES93118060T ES2123022T3 ES 2123022 T3 ES2123022 T3 ES 2123022T3 ES 93118060 T ES93118060 T ES 93118060T ES 93118060 T ES93118060 T ES 93118060T ES 2123022 T3 ES2123022 T3 ES 2123022T3
- Authority
- ES
- Spain
- Prior art keywords
- door
- control
- aircraft
- opening
- kinematics
- 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 - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1407—Doors; surrounding frames
- B64C1/1423—Passenger doors
- B64C1/143—Passenger doors of the plug type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1407—Doors; surrounding frames
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power-Operated Mechanisms For Wings (AREA)
- Lock And Its Accessories (AREA)
Abstract
LA INVENCION SE REFIERE A UN CONTROL ELECTRONICO PARA LA REALIZACION DE LA CINEMATICA PARA UNA PUERTA DE AVION. CON EL SE PUEDE CONTROLAR ELECTRONICAMENTE EL CIERRE Y LA APERTURA DE LA PUERTA DEL AVION, CUYOS COMPONENTES SE ACCIONAN ELECTRICAMENTE. EL ACCIONAMIENTO DE LOS COMPONENTES DE LA PUERTA SE REALIZA EN SERVICIO NORMAL Y BAJO CONDICIONES DE EMERGENCIA DE MODO OPTIMO Y SEGURO. EN LOS TIPOS CONOCIDOS DE PUERTAS DE AVION, QUE ESTAN CONSTRUIDAS SEGUN EL PRINCIPIO DE PALANCA DE CONTACTO O DE PALANCA ARTICULADA, SE REALIZAN A MANO LOS DIFERENTES PASOS DEL ACCIONAMIENTO, COMO LA APERTURA Y CIERRE O EL ENCLAVADO Y DESENCLAVADO, ASI COMO LA ACTIVACION DE UNA RAMPA-BALSA DE EMERGENCIA. UN CONTROL PRECISO DE LA CINEMATICA PARA PUERTAS DE AVION QUE SE DESARROLLA SEGUN UN PROGRAMA ALMACENADO EN LA MEMORIA DE UNA CPU, EL CUAL COORDINA LA SUCESION DE LOS PASOS DE ACCIONAMIENTO, NO ES CONOCIDO EN LOS CONTROLES DE PUERTAS DE AVIONES. EL CONTROL ELECTRONICO DE LA CINEMATICA DE LA PUERTA DE UN AVION (1), SE COMPONE EN ESENCIA DE UNA UNIDAD MICROPROCESADORA (50), QUE ESTA UNIDA MEDIANTE CONDUCTOR CON UN SISTEMA DE ACCIONAMIENTO (59) EXISTENTE DENTRO DE LA PUERTA DEL AVION (1). UN ELECTROIMAN (51), QUE REALIZA LA ACTIVACION DE UN CILINDRO NEUMATICO DE APERTURA PARA LA APERTURA DE EMERGENCIA DE LA PUERTA DEL AVION, UN PRIMERO Y UN SEGUNDO SENSORES DE PRESION (52,53), CON LOS CUALES SE COMPRUEBAN LAS CONDICIONES DE PRESION DE LOS RESPECTIVOS ACUMULADORES PARA EL CILINDRO NEUMATICO DE APERTURA O PARA LA RAMPA-BALSA DE EMERGENCIA, UNA VALVULA DEL SUELO (54), QUE GARANTIZA LA COMUNICACION CON UN SISTEMA DE APERTURA DE LA PUERTA, UN SISTEMA DE CONTROL DEL ORDENADOR (55), QUE GARANTIZA LA COMUNICACION CON LA INDICACION EN EL TABLERO DE INSTRUMENTOS Y UNA COMPROBACION EN PANTALLA (63), ESTAN UNIDOS POR CONDUCTORES TAMBIEN CON LA UNIDAD MICROPROCESADORA (50). UN PRIMERO Y UN SEGUNDO PANELES (56,57) CON LOS CUALES SE REALIZA UN CONTROL ACCIONADO A MANO DE LA PUERTA DEL AVION (1), ASI COMO LA INDICACION VISUAL DEL ESTADO EFECTIVO DE LA PUERTA, ESTA UNIDO MEDIANTE CONDUCTOR, ADEMAS, CON LA UNIDAD MICROPROCESADORA (50). EL MICROPROCESADOR (50) REALIZA EL CONTROL DIRECTO O INDIRECTO DEL SISTEMA DE ACCIONAMIENTO ELECTRICO (59), EL CUAL SE COMPONE DE VARIOS MOTORES Y/O GRUPOS DE MOTORES. UNA FUENTE DE ENERGIA (58) UNIDA CON LA UNIDAD MICROPROCESADORA (50) GARANTIZA LA ALIMENTACION PERMANENTE CON CORRIENTE CONTINUA DEL CONTROL.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/975,785 US5251851A (en) | 1990-07-11 | 1992-11-13 | Door operating mechanism for opening and closing an aircraft door in response to a stored program |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2123022T3 true ES2123022T3 (es) | 1999-01-01 |
Family
ID=25523395
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES93118060T Expired - Lifetime ES2123022T3 (es) | 1992-11-13 | 1993-11-08 | Mando electronico para el accionamiento de la cinematica de una puerta de avion. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5251851A (es) |
EP (1) | EP0597418B1 (es) |
DE (1) | DE59308953D1 (es) |
ES (1) | ES2123022T3 (es) |
Families Citing this family (44)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4401899C2 (de) * | 1994-01-24 | 1995-11-16 | Daimler Benz Aerospace Airbus | Vorrichtung zur Verriegelung |
EP0780290A1 (en) * | 1995-12-19 | 1997-06-25 | The Boeing Company | Main deck cargo door electric lock system |
US5735487A (en) * | 1995-12-19 | 1998-04-07 | The Boeing Company | Main deck cargo door control panel indication |
EP1331351B1 (en) * | 1996-04-24 | 2006-07-26 | Baby Dan A/S | Child safety barrier |
US5881973A (en) * | 1996-09-04 | 1999-03-16 | Mcdonnell Douglas Corporation | Passenger door operation control set |
IT1302159B1 (it) * | 1997-09-03 | 2000-07-31 | Eurocopter Deutschland | Sistema a sportello per un velivolo per passeggeri |
IT1302160B1 (it) * | 1997-09-03 | 2000-07-31 | Eurocopter Deutschland | Sportello in particolare per un velivolo per passeggeri |
US5984234A (en) * | 1997-10-15 | 1999-11-16 | The Boeing Company | Engine parameter activated airplane exit locking system |
DE19948844B4 (de) * | 1999-10-08 | 2004-03-25 | Airbus Deutschland Gmbh | Kinematik für eine Flugzeugtür |
DE10100273B4 (de) * | 2000-05-31 | 2010-05-12 | Airbus Deutschland Gmbh | Vorrichtung zur Steuerung und Überwachung von Flugzeug-Kabinensystemen |
DE10032851C2 (de) * | 2000-06-29 | 2003-04-03 | Jenoptik Jena Gmbh | Einrichtung zum elektrischen Betätigen einer Tür eines Luftfahrzeugs |
DE10037621C2 (de) * | 2000-08-02 | 2002-09-19 | Eurocopter Deutschland | Steuerung für eine Passagiertür eines Flugzeuges |
DE10056994C1 (de) | 2000-11-17 | 2002-02-21 | Eurocopter Deutschland | Verfahren und Anordnung zum Steuern des Schließ- und Öffnungsvorganges bei einer Passagiertür eines Flugzeuges |
US6457675B1 (en) | 2001-06-25 | 2002-10-01 | The Boeing Company | Hydraulic actuation system for cargo doors with cam-type latches |
US6633239B2 (en) | 2001-07-17 | 2003-10-14 | The Boeing Company | Cargo door electrical control and warning indication system and method of use |
US6866227B2 (en) | 2001-10-04 | 2005-03-15 | Hartwell Corporation | Pressure responsive blowout latch with reservoir |
EP1438473B1 (en) * | 2001-10-04 | 2012-12-05 | The Hartwell Corporation | Pressure sensing dead bolt |
US6866226B2 (en) | 2001-10-04 | 2005-03-15 | Hartwell Corporation | Pressure responsive blowout latch |
FR2830564B1 (fr) * | 2001-10-05 | 2003-12-26 | Airbus France | Dispositif et procede de commande de l'ouverture d'urgence d'une porte d'evacuation d'un aeronef |
US20030089826A1 (en) * | 2001-11-13 | 2003-05-15 | Barba Valentin G. | Flight lock actuator with dual energy sources |
DE10161562B4 (de) * | 2001-12-14 | 2005-07-21 | Eurocopter Deutschland Gmbh | Notöffnungszylinder einer Passagiertür |
DE10207033B4 (de) | 2002-02-20 | 2004-01-15 | Eurocopter Deutschland Gmbh | Antriebsmittel zum Schwenken einer an einem Tragarm schwenkbar gelagerten Flugzeugtür |
AT412491B (de) * | 2002-07-25 | 2005-03-25 | Knorr Bremse Gmbh | Antrieb einer schiebetüre oder schwenkschiebetüre |
ES2233182B1 (es) * | 2003-05-22 | 2007-02-16 | Fernando Espejo Delgado | Dispositivo de control de la compuerta de descarga, en aeronaves de extincion de incendios. |
DE102004048217B4 (de) * | 2004-09-30 | 2007-04-19 | Eurocopter Deutschland Gmbh | Luftfahrzeug mit Kabinen-Differenzdruck-Warnsystem |
DE102005002544A1 (de) * | 2005-01-19 | 2006-07-27 | Airbus Deutschland Gmbh | Druckunterschied-Warnsystem |
DE102006001685B4 (de) * | 2006-01-12 | 2009-11-12 | Airbus Deutschland Gmbh | Verfahren und System zur Steuerung des Drucks in einer Flugzeugkabine |
RU2482018C2 (ru) * | 2007-07-31 | 2013-05-20 | Б/Е Аэроспейс, Инк. | Дверь для летательного аппарата |
DE102008014691B4 (de) * | 2008-03-18 | 2011-07-21 | Eurocopter Deutschland GmbH, 86609 | Vorrichtung zum Öffnen einer Passagiertür im Notfall |
DE102012206877A1 (de) * | 2012-04-25 | 2013-10-31 | Airbus Operations Gmbh | Vorrichtung und Verfahren zur Kabinendifferenzdruckwarnung für ein Luft- oder Raumfahrzeug |
FR2998259B1 (fr) * | 2012-11-16 | 2015-03-06 | Latecoere | Procede d'ouverture / fermeture d'une porte electrique d'aeronef pour cellule pressurisee et porte de mise en oeuvre |
EP2842873B1 (en) * | 2013-08-30 | 2017-06-14 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Short term, autonomous, electrical power supply system |
FR3015543B1 (fr) * | 2013-12-24 | 2016-02-05 | Ratier Figeac Soc | Dispositif de commande d'ouverture et de fermeture d'une porte d'aeronef |
DE102014008060B4 (de) * | 2014-05-28 | 2020-04-16 | Airbus Operations Gmbh | Signaleinleitung für Flugzeugtüren |
EP3401208A1 (en) | 2017-05-10 | 2018-11-14 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | An aircraft door with at least one weight compensation device |
CN107654158A (zh) * | 2017-10-17 | 2018-02-02 | 西安飞机工业(集团)有限责任公司 | 一种飞机舱门电气控制系统 |
US10752335B2 (en) * | 2018-02-01 | 2020-08-25 | Bell Helicopter Textron Inc. | Emergency release for pushout window evacuation |
DE102018127106B3 (de) * | 2018-10-30 | 2019-11-07 | Airbus Operations Gmbh | Flugzeugtürverriegelungssystem und Flugzeugtüranordnung |
EP3770062B1 (en) | 2019-07-22 | 2023-06-07 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Aircraft with an electromechanical door system |
CN114458098B (zh) * | 2020-11-09 | 2023-05-05 | 空客直升机德国有限公司 | 用于飞行器的机电门系统 |
FR3117088B1 (fr) * | 2020-12-05 | 2023-01-13 | Latecoere | Architecture de porte d’aéronef comportant une source d’énergie de secours |
US20230131378A1 (en) * | 2021-07-19 | 2023-04-27 | Air Cruisers Company, LLC | Power source for inflation system (solid-state battery) |
EP4129819B1 (en) * | 2021-08-02 | 2024-01-03 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | An opening system for a swiveling aircraft door |
US20240083568A1 (en) * | 2022-09-09 | 2024-03-14 | Airbus Operations (S.A.S.) | Aircraft fuselage door comprising an internal panel and an external panel, and aircraft fuselage part comprising such a door |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4720065A (en) * | 1985-01-24 | 1988-01-19 | The Boeing Company | Translatable outward opening plug-type aircraft door and actuating mechanisms therefor |
US4680891A (en) * | 1986-06-27 | 1987-07-21 | Monarch Aviation, Inc. | Door hydraulic arrangement |
DE3877546T2 (de) * | 1987-12-21 | 1993-05-13 | Boeing Co | Flugzeugtuerschloss. |
DE4022067C2 (de) * | 1990-07-11 | 1994-06-09 | Deutsche Aerospace Airbus | Kinematik für eine Flugzeugtür |
DE4104801C1 (en) * | 1991-02-16 | 1992-09-10 | Mercedes-Benz Aktiengesellschaft, 7000 Stuttgart, De | Locking installation for motor vehicle doors - responds to control signals only when sent at correct time intervals |
-
1992
- 1992-11-13 US US07/975,785 patent/US5251851A/en not_active Expired - Lifetime
-
1993
- 1993-11-08 DE DE59308953T patent/DE59308953D1/de not_active Expired - Lifetime
- 1993-11-08 ES ES93118060T patent/ES2123022T3/es not_active Expired - Lifetime
- 1993-11-08 EP EP93118060A patent/EP0597418B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5251851A (en) | 1993-10-12 |
EP0597418B1 (de) | 1998-09-02 |
EP0597418A1 (de) | 1994-05-18 |
DE59308953D1 (de) | 1998-10-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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