ES2072078T3 - Mecanismo de apertura para puertas de avion. - Google Patents
Mecanismo de apertura para puertas de avion.Info
- Publication number
- ES2072078T3 ES2072078T3 ES92121057T ES92121057T ES2072078T3 ES 2072078 T3 ES2072078 T3 ES 2072078T3 ES 92121057 T ES92121057 T ES 92121057T ES 92121057 T ES92121057 T ES 92121057T ES 2072078 T3 ES2072078 T3 ES 2072078T3
- Authority
- ES
- Spain
- Prior art keywords
- door
- support rods
- torque shaft
- support
- rod
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Hinges (AREA)
- Wing Frames And Configurations (AREA)
Abstract
LA INVENCION CONCIERNE A UN MECANISMO DE APERTURA PARA PUERTAS DE AERONAVES, QUE PRESENTA UNA BISAGRA GIRATORIA (14), QUE AL ABATIR LA PUERTA (10) POSICIONA EL EJE DE LA BISAGRA (13) EN EL LADO EXTERIOR DE A BORDO, MIENTRAS QUE CON LA PUERTA CERRADA (10) ESTE EJE DE BISAGRA (13) SE ENCUENTRA EN EL INTERIOR DEL FUSELAJE, Y CON ELLO PERMITE UN ANGULO DE APERTURA DE MAS DE 90 (GRADOS) , SIN PELIGRO DE COLISION CON EL FUSELAJE. SE DESCRIBE UN EJEMPLO DEL PROCESO, Y EN LAS FIGURAS DEL DIBUJO SE REPRESENTA DE TAL MODO QUE LA CONSTRUCCION Y EL FUNCIONAMIENTO SON COMPRENSIBLES EN GENERAL.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4200930A DE4200930C1 (es) | 1992-01-16 | 1992-01-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2072078T3 true ES2072078T3 (es) | 1995-07-01 |
Family
ID=6449591
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES92121057T Expired - Lifetime ES2072078T3 (es) | 1992-01-16 | 1992-12-10 | Mecanismo de apertura para puertas de avion. |
Country Status (5)
Country | Link |
---|---|
US (1) | US5316241A (es) |
EP (1) | EP0551615B1 (es) |
AT (1) | ATE119838T1 (es) |
DE (1) | DE4200930C1 (es) |
ES (1) | ES2072078T3 (es) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4413307C2 (de) * | 1994-04-16 | 1997-03-06 | Eurocopter Deutschland | Türsystem, insbesondere für ein Passagierflugzeug |
IT1302160B1 (it) * | 1997-09-03 | 2000-07-31 | Eurocopter Deutschland | Sportello in particolare per un velivolo per passeggeri |
IT1302159B1 (it) * | 1997-09-03 | 2000-07-31 | Eurocopter Deutschland | Sistema a sportello per un velivolo per passeggeri |
US6446393B1 (en) | 2000-05-12 | 2002-09-10 | Bath Iron Works Corporation | Watertight door apparatus |
DE10132361C1 (de) * | 2001-07-04 | 2002-11-07 | Eurocopter Deutschland | Vorrichtung zur Sicherung des Mechanismus zum Heben und Senken der Passagiertür eines Flugzeuges |
CA2865515C (en) | 2012-02-29 | 2019-06-18 | Bombardier Inc. | Connection assembly for aircraft door |
CN103523202B (zh) * | 2012-07-06 | 2016-08-10 | 哈尔滨飞机工业集团有限责任公司 | 直升机滑门支臂机构 |
EP3356628B1 (en) * | 2015-09-30 | 2022-01-19 | Howmet Aerospace Inc. | Pressure relief door |
CN112229556A (zh) * | 2020-10-12 | 2021-01-15 | 西北工业大学 | 一种测量飞机舱门u型手柄开启力的装置及方法 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA637243A (en) * | 1962-02-27 | O. Wilmer Maurice | Doors for the fuselages of pressurised aircraft | |
US3085297A (en) * | 1956-08-28 | 1963-04-16 | Douglas Aircraft Co Inc | Door for pressurized cabin |
US3051028A (en) * | 1959-05-14 | 1962-08-28 | Detroit Stamping Company | Toggle clamp opening mechanism |
US3791073A (en) * | 1972-04-28 | 1974-02-12 | Boeing Co | Aircraft door with moving hinge line |
GB1551821A (en) * | 1976-08-31 | 1979-09-05 | Hawker Siddeley Aviation Ltd | Aircraft doors |
US4262447A (en) * | 1979-08-20 | 1981-04-21 | Sybron Corporation | Double acting hinged pressure vessel closure |
DE3245249A1 (de) * | 1981-12-10 | 1983-06-16 | British Aerospace Plc, London | Tueraufbau, insbesondere fuer flugzeuge |
US4497462A (en) * | 1983-03-28 | 1985-02-05 | The Boeing Company | Outward opening electrically powered plug-type cargo door |
DE3807067A1 (de) * | 1988-03-04 | 1989-09-14 | Messerschmitt Boelkow Blohm | Verriegelung fuer eine flugzeugtuer |
-
1992
- 1992-01-16 DE DE4200930A patent/DE4200930C1/de not_active Expired - Fee Related
- 1992-12-10 ES ES92121057T patent/ES2072078T3/es not_active Expired - Lifetime
- 1992-12-10 AT AT92121057T patent/ATE119838T1/de not_active IP Right Cessation
- 1992-12-10 EP EP92121057A patent/EP0551615B1/de not_active Expired - Lifetime
-
1993
- 1993-01-19 US US08/006,232 patent/US5316241A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0551615B1 (de) | 1995-03-15 |
EP0551615A1 (de) | 1993-07-21 |
DE4200930C1 (es) | 1993-01-28 |
US5316241A (en) | 1994-05-31 |
ATE119838T1 (de) | 1995-04-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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