ATE228459T1 - Antrieb für auftrieberhöhende klappen an einem flugzeug - Google Patents
Antrieb für auftrieberhöhende klappen an einem flugzeugInfo
- Publication number
- ATE228459T1 ATE228459T1 AT00301400T AT00301400T ATE228459T1 AT E228459 T1 ATE228459 T1 AT E228459T1 AT 00301400 T AT00301400 T AT 00301400T AT 00301400 T AT00301400 T AT 00301400T AT E228459 T1 ATE228459 T1 AT E228459T1
- Authority
- AT
- Austria
- Prior art keywords
- flaps
- aircraft
- lift
- drive
- increase
- Prior art date
Links
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
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
-
- 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)
- Control Of Multiple Motors (AREA)
- Transmission Devices (AREA)
- Current-Collector Devices For Electrically Propelled Vehicles (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/258,470 US6224022B1 (en) | 1999-02-26 | 1999-02-26 | Airplane high lift surface drive system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE228459T1 true ATE228459T1 (de) | 2002-12-15 |
Family
ID=22980686
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT00301400T ATE228459T1 (de) | 1999-02-26 | 2000-02-22 | Antrieb für auftrieberhöhende klappen an einem flugzeug |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6224022B1 (de) |
| EP (1) | EP1038765B1 (de) |
| AT (1) | ATE228459T1 (de) |
| DE (1) | DE60000839T2 (de) |
| ES (1) | ES2188476T3 (de) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB9903500D0 (en) * | 1999-02-17 | 1999-04-07 | Lucas Ind Plc | Detection apparatus |
| DE10313728B4 (de) | 2003-03-27 | 2011-07-21 | Airbus Operations GmbH, 21129 | Klappensystem am Tragflügel eines Starrflügel-Flugzeuges |
| US20040200928A1 (en) * | 2003-04-14 | 2004-10-14 | Arthur Degenholtz | Actuator and flap arrangement with actuator interconnection |
| DE10361891A1 (de) | 2003-12-23 | 2005-08-04 | Airbus Deutschland Gmbh | Vorrichtung zur Ansteuerung und Verstellung von Klappen an Flugzeugtragflächen |
| DE102005008331A1 (de) * | 2005-02-23 | 2006-08-31 | Airbus Deutschland Gmbh | Einrichtung zur Bestimmung eines Rotationswinkels einer Welle in einem Luftfahrzeug |
| DE102005018686B4 (de) * | 2005-04-21 | 2007-03-22 | Barthelt, Hans-Peter, Dipl.-Ing. | Pflegebett mit Doppelmotorantrieb |
| US20070007385A1 (en) * | 2005-06-27 | 2007-01-11 | Honeywell International, Inc. | Electric flight control surface actuation system electronic architecture |
| DE102005059369B4 (de) * | 2005-12-13 | 2012-06-14 | Airbus Operations Gmbh | Verfahren und Einrichtung zur automatischen Entlastung eines Hochauftriebsflächensystems, insbesondere eines Landeklappensystems, eines Flugzeugs |
| FR2972175B1 (fr) * | 2011-03-01 | 2013-10-25 | Sagem Defense Securite | Procede de commande simultanee d'actionneurs de deplacement de volets d'aeronef, dispositif de motorisation de volets d'aeronef et aeronef pourvu d'un tel dispositif |
| EP4393815A1 (de) * | 2022-12-30 | 2024-07-03 | Airbus Operations GmbH | Flugzeugklappensystem |
Family Cites Families (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1373873A (en) * | 1920-05-29 | 1921-04-05 | Gen Electric | Ship propulsion |
| US1407425A (en) * | 1920-06-28 | 1922-02-21 | Junkers Hugo | Stabilization of flying machines |
| US1802184A (en) * | 1922-11-01 | 1931-04-21 | Gen Electric | Propulsion of multiple-screw ships |
| US1856093A (en) * | 1931-03-17 | 1932-05-03 | Merrill Aircraft Company | Airplane |
| FR857515A (fr) * | 1938-09-14 | 1940-09-17 | Dornier Werke Gmbh | Gouvernail commandé par moteur |
| US3935754A (en) | 1974-06-14 | 1976-02-03 | The Boeing Company | Failure detector and indicator for aircraft flap actuation system |
| US3958779A (en) * | 1975-05-27 | 1976-05-25 | Fairchild Industries Inc. | Aircraft control system with a jam isolating coupling |
| US4159642A (en) * | 1978-03-02 | 1979-07-03 | Avco Corporation | Aircraft transmission test set |
| US4398683A (en) * | 1978-12-26 | 1983-08-16 | Schmetzer William M | Aircraft with thrust and lift augmenting airfoil |
| US4688744A (en) * | 1982-09-03 | 1987-08-25 | Sundstrand Corporation | Jam tolerant rotary actuation system |
| EP0146281B1 (de) | 1983-12-20 | 1987-07-22 | LUCAS INDUSTRIES public limited company | Bremsvorrichtung für ein Drehantriebssystem |
| US4695014A (en) * | 1984-05-25 | 1987-09-22 | Western Gear Corporation | Aircraft wing section movement apparatus |
| US4779822A (en) * | 1986-05-23 | 1988-10-25 | Sundstrand Corporation | Actuator system |
| JPH0667738B2 (ja) * | 1986-12-09 | 1994-08-31 | 東海テイ−ア−ルダブリユ−株式会社 | 電動機制動機能を備えた電動パワ−ステアリング装置 |
| IL90789A0 (en) * | 1988-08-05 | 1990-01-18 | Rieter Ag Maschf | Textile machine with drawframes |
| DE4033277A1 (de) | 1990-10-19 | 1992-04-23 | Airbus Gmbh | Antriebsvorrichtung fuer an flugzeugtragfluegeln angeordneten klappen |
| US5884872A (en) * | 1993-05-26 | 1999-03-23 | The United States Of America As Represented By The Secretary Of The Navy | Oscillating flap lift enhancement device |
| US5686907A (en) * | 1995-05-15 | 1997-11-11 | The Boeing Company | Skew and loss detection system for individual high lift devices |
| DE19525593C2 (de) * | 1995-07-13 | 1997-04-30 | Roland Man Druckmasch | Mehrmotorenantrieb für eine Druckmaschine |
| JP3536658B2 (ja) * | 1998-03-31 | 2004-06-14 | 日産自動車株式会社 | ハイブリッド車両の駆動制御装置 |
-
1999
- 1999-02-26 US US09/258,470 patent/US6224022B1/en not_active Expired - Lifetime
-
2000
- 2000-02-22 DE DE60000839T patent/DE60000839T2/de not_active Expired - Fee Related
- 2000-02-22 ES ES00301400T patent/ES2188476T3/es not_active Expired - Lifetime
- 2000-02-22 AT AT00301400T patent/ATE228459T1/de not_active IP Right Cessation
- 2000-02-22 EP EP00301400A patent/EP1038765B1/de not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP1038765B1 (de) | 2002-11-27 |
| DE60000839D1 (de) | 2003-01-09 |
| DE60000839T2 (de) | 2003-09-25 |
| EP1038765A1 (de) | 2000-09-27 |
| ES2188476T3 (es) | 2003-07-01 |
| US6224022B1 (en) | 2001-05-01 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |