ES2177499T3 - Aparato de deteccion. - Google Patents
Aparato de deteccion.Info
- Publication number
- ES2177499T3 ES2177499T3 ES00301133T ES00301133T ES2177499T3 ES 2177499 T3 ES2177499 T3 ES 2177499T3 ES 00301133 T ES00301133 T ES 00301133T ES 00301133 T ES00301133 T ES 00301133T ES 2177499 T3 ES2177499 T3 ES 2177499T3
- Authority
- ES
- Spain
- Prior art keywords
- signal
- detection device
- transmission means
- adjacent surfaces
- hypersustentation
- 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
- 238000001514 detection method Methods 0.000 title abstract 2
- 230000008054 signal transmission Effects 0.000 abstract 3
- 238000006073 displacement reaction Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
- B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
- Length Measuring Devices With Unspecified Measuring Means (AREA)
- Length Measuring Devices By Optical Means (AREA)
Abstract
Un sistema hipersustentador de un ala de avión que tiene una pluralidad de superficies de hipersustentación móviles, cual sistema incluye un dispositivo de detección que comprende unos medios de transmisión de señal (15,16,20) que se extienden a través de cada superficie citada, un generador de señal (18), un receptor de señal (21) y unos medios de interrupción de señal (22) asociados a superficies adyacentes y dispuestos para interrumpir la transmisión de una señal a lo largo de los medios de transmisión de señal (15,16,20) al producirse un cierto desplazamiento relativo de superficies adyacentes de dichas superficies.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB9903500.8A GB9903500D0 (en) | 1999-02-17 | 1999-02-17 | Detection apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2177499T3 true ES2177499T3 (es) | 2002-12-16 |
Family
ID=10847866
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES00301133T Expired - Lifetime ES2177499T3 (es) | 1999-02-17 | 2000-02-15 | Aparato de deteccion. |
Country Status (5)
Country | Link |
---|---|
US (1) | US6386482B1 (es) |
EP (1) | EP1029784B1 (es) |
DE (1) | DE60000244T2 (es) |
ES (1) | ES2177499T3 (es) |
GB (1) | GB9903500D0 (es) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004055740A1 (de) | 2004-06-09 | 2006-01-05 | Liebherr-Aerospace Lindenberg Gmbh | Flugzeughochauftriebssystem mit Überlastsicherung |
DE102004044961B4 (de) * | 2004-09-16 | 2007-02-01 | Liebherr-Aerospace Lindenberg Gmbh | Vorrichtung zur Erfassung von Gleichlauffehlern von Hochauftriebsflächen an Flugzeugen |
US7229046B2 (en) * | 2005-10-25 | 2007-06-12 | Durant Cecil John | Servo mounting system for direct drive of an aircraft control surface |
US20070247555A1 (en) * | 2006-04-21 | 2007-10-25 | Diersing Steven L | Delivery system for dispensing volatile materials with high level of solids using an electromechanical transducer device |
US8115649B2 (en) | 2009-04-30 | 2012-02-14 | The Boeing Company | Slat skew detection system |
DE102010047540A1 (de) * | 2010-10-05 | 2012-04-05 | Airbus Operations Gmbh | Hochauftriebssystem für einen Tragflügel eines Flugzeugs |
GB201120234D0 (en) * | 2011-11-23 | 2012-01-04 | Airbus Operations Ltd | Deployment system |
EP3908519B1 (en) * | 2019-01-09 | 2023-02-22 | Moog Wolverhampton Limited | Aircraft control surface element monitoring system |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4321463A (en) * | 1979-12-17 | 1982-03-23 | Stecher Samuel J | Low frequency laser fiberoptic detector apparatus for musical instruments and intrusion detection |
US4450434A (en) * | 1981-05-19 | 1984-05-22 | The United States Of America As Represented By The Secretary Of The Army | Apparatus for determining break locations in fencing |
JPS61246806A (ja) * | 1985-04-24 | 1986-11-04 | Fanuc Ltd | ロボツト制御装置 |
JPS6221034A (ja) * | 1985-07-19 | 1987-01-29 | Junkosha Co Ltd | 漏液検知センサ |
FR2615944B1 (fr) * | 1987-05-26 | 1989-08-25 | Electronique Sarl Ste Moderne | Dispositif pour detecter a distance le deplacement relatif de deux elements, notamment pour un equipement de protection de porte ou de fenetre |
US4931771A (en) * | 1988-09-27 | 1990-06-05 | Anro Engineering, Inc. | Optical fiber intrusion location sensor for perimeter protection of precincts |
US5144125A (en) * | 1990-12-12 | 1992-09-01 | The Babcock & Wilcox Company | Fiber optic based fire detection and tracking system |
US5152508A (en) * | 1992-03-26 | 1992-10-06 | Fish Robert E | Safety barrier |
US5628477A (en) * | 1995-02-13 | 1997-05-13 | The Boeing Company | Auxiliary airfoil lost motion detector and actuator |
US5965877A (en) * | 1995-04-25 | 1999-10-12 | Lockheed Martin Corporation | Photoluminescence built-in-test for optical systems |
US5680124A (en) * | 1995-05-15 | 1997-10-21 | The Boeing Company | Skew and loss detection system for adjacent high lift devices |
US5639968A (en) * | 1995-10-23 | 1997-06-17 | The United States Of America As Represented By The Secretary Of The Navy | Optical fiber strain-to-failure sensor |
US5719566A (en) * | 1996-06-28 | 1998-02-17 | Sundstrand Corporation | Method and apparatus for detecting dormant actuator failure |
US6204920B1 (en) * | 1996-12-20 | 2001-03-20 | Mcdonnell Douglas Corporation | Optical fiber sensor system |
US5965876A (en) * | 1997-08-20 | 1999-10-12 | Verifiber Technologies, Inc. | Apparatus and method for detecting optical fiber fault location |
US6224022B1 (en) * | 1999-02-26 | 2001-05-01 | Smiths Industries Actuation Systems Inc. | Airplane high lift surface drive system |
-
1999
- 1999-02-17 GB GBGB9903500.8A patent/GB9903500D0/en not_active Ceased
-
2000
- 2000-02-15 DE DE60000244T patent/DE60000244T2/de not_active Expired - Fee Related
- 2000-02-15 EP EP00301133A patent/EP1029784B1/en not_active Expired - Lifetime
- 2000-02-15 ES ES00301133T patent/ES2177499T3/es not_active Expired - Lifetime
- 2000-02-17 US US09/505,535 patent/US6386482B1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US6386482B1 (en) | 2002-05-14 |
GB9903500D0 (en) | 1999-04-07 |
EP1029784B1 (en) | 2002-07-03 |
DE60000244D1 (de) | 2002-08-08 |
EP1029784A1 (en) | 2000-08-23 |
DE60000244T2 (de) | 2003-02-20 |
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