ES2156660A1 - Mandos de vuelo con compensacion automatica. - Google Patents
Mandos de vuelo con compensacion automatica.Info
- Publication number
- ES2156660A1 ES2156660A1 ES009800050A ES9800050A ES2156660A1 ES 2156660 A1 ES2156660 A1 ES 2156660A1 ES 009800050 A ES009800050 A ES 009800050A ES 9800050 A ES9800050 A ES 9800050A ES 2156660 A1 ES2156660 A1 ES 2156660A1
- Authority
- ES
- Spain
- Prior art keywords
- aileron
- flight controls
- balance
- automatique
- rotates
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/30—Balancing hinged surfaces, e.g. dynamically
Abstract
Mandos de vuelo con compensación automática que consiste en alerones formados de dos partes, los cuales a baja velocidad adoptan una forma de alerón convencional y giran en su totalidad con el mismo ángulo y a altas velocidades una porción de él gira o se extiende a un ángulo determinado movido por el actuador y el resto del alerón, que es flexible y está unido a la porción principal del alerón al que está integrado, gira respecto a la porción principal en función de la presión del aire, oponiendose a este giro por medio de su disposición flexible.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES009800050A ES2156660B1 (es) | 1998-01-14 | 1998-01-14 | Mandos de vuelo con compensacion automatica. |
US09/110,744 US6109567A (en) | 1998-01-14 | 1998-07-02 | Flight controls with automatic balance |
US09/139,524 US6220551B1 (en) | 1998-01-14 | 1998-08-25 | Flight controls with automatic balance |
EP98500280A EP0937641B1 (en) | 1998-01-14 | 1998-12-28 | Flight controls with automatique balance |
DE69824945T DE69824945D1 (de) | 1998-01-14 | 1998-12-28 | Flugzeugsteuerungseinrichtungen mit automatischer Kompensation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES009800050A ES2156660B1 (es) | 1998-01-14 | 1998-01-14 | Mandos de vuelo con compensacion automatica. |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2156660A1 true ES2156660A1 (es) | 2001-07-01 |
ES2156660B1 ES2156660B1 (es) | 2002-02-16 |
Family
ID=8302377
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES009800050A Expired - Fee Related ES2156660B1 (es) | 1998-01-14 | 1998-01-14 | Mandos de vuelo con compensacion automatica. |
Country Status (4)
Country | Link |
---|---|
US (1) | US6109567A (es) |
EP (1) | EP0937641B1 (es) |
DE (1) | DE69824945D1 (es) |
ES (1) | ES2156660B1 (es) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0888202B1 (en) * | 1996-03-22 | 2005-08-10 | The Boeing Company | Determinant wing assembly |
US7509740B2 (en) * | 2001-11-13 | 2009-03-31 | The Boeing Company | Method of manufacturing a wing |
DE69718659T2 (de) | 1996-10-22 | 2003-05-22 | Boeing Co | Flugzeug mit ungepfeiltem schlitzflügel für den reiseflug |
US6484971B2 (en) * | 2000-07-24 | 2002-11-26 | Thombi Layukallo | Control of flow separation and related phenomena on aerodynamic surfaces |
DE10147827A1 (de) * | 2001-09-27 | 2003-04-24 | Airbus Gmbh | Vorrichtung zur Änderung der Quertriebsgröße eines Flugzeughauptelementes mit vorzugsweise flächenförmiger Hinterkante |
US7258308B2 (en) * | 2002-07-02 | 2007-08-21 | The Boeing Company | Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface |
FR2853622B1 (fr) * | 2003-04-14 | 2005-05-27 | Eurocopter France | Volet rotatif et element sustentateur, en particulier pale d'helicoptere, muni d'un tel volet rotatif |
US6799739B1 (en) | 2003-11-24 | 2004-10-05 | The Boeing Company | Aircraft control surface drive system and associated methods |
US6978971B1 (en) * | 2004-06-15 | 2005-12-27 | The Boeing Company | Methods and apparatuses for controlling airflow proximate to engine/airfoil systems |
US7494094B2 (en) | 2004-09-08 | 2009-02-24 | The Boeing Company | Aircraft wing systems for providing differential motion to deployable lift devices |
US7264206B2 (en) | 2004-09-30 | 2007-09-04 | The Boeing Company | Leading edge flap apparatuses and associated methods |
US7338018B2 (en) | 2005-02-04 | 2008-03-04 | The Boeing Company | Systems and methods for controlling aircraft flaps and spoilers |
US7721999B2 (en) | 2005-05-20 | 2010-05-25 | The Boeing Company | Aerospace vehicle fairing systems and associated methods |
US7475854B2 (en) | 2005-11-21 | 2009-01-13 | The Boeing Company | Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods |
US7708231B2 (en) | 2005-11-21 | 2010-05-04 | The Boeing Company | Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods |
US7954769B2 (en) | 2007-12-10 | 2011-06-07 | The Boeing Company | Deployable aerodynamic devices with reduced actuator loads, and related systems and methods |
US7766282B2 (en) | 2007-12-11 | 2010-08-03 | The Boeing Company | Trailing edge device catchers and associated systems and methods |
FR2929590B1 (fr) * | 2008-04-02 | 2011-01-14 | Airbus France | Ensemble de surfaces aerodynamiques pour aeronef. |
FR2930235B1 (fr) * | 2008-04-21 | 2011-09-30 | Airbus France | Mat de suspension pour turbomoteur. |
US8382045B2 (en) | 2009-07-21 | 2013-02-26 | The Boeing Company | Shape-changing control surface |
US8844879B2 (en) * | 2011-12-12 | 2014-09-30 | The Boeing Company | Wing variable camber trailing edge tip |
JP5906158B2 (ja) * | 2012-08-10 | 2016-04-20 | 一般社団法人日本航空宇宙工業会 | フラップ |
CN102901595B (zh) * | 2012-10-12 | 2014-07-16 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种舵面铰链力矩测量方法 |
US10633078B2 (en) * | 2017-12-07 | 2020-04-28 | The Boeing Company | Pre-deformed aircraft spoilers and droop panels designed to seal with flap in deflected state |
CN108016591A (zh) * | 2017-12-30 | 2018-05-11 | 镇江同舟螺旋桨有限公司 | 一种稍部折翼形螺旋桨叶片稍部造型装置 |
US11260958B2 (en) | 2019-09-04 | 2022-03-01 | The Boeing Company | Double over center crankshaft flap mechanism |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1413258A (en) * | 1919-02-06 | 1922-04-18 | Christmas Aeroplane Company In | Flying machine |
GB346251A (en) * | 1930-08-27 | 1931-04-09 | Ugo Antoni | Improvements in and relating to the construction of flexible aeroplane wings having a variable profile |
GB360273A (es) * | 1930-01-21 | 1931-11-05 | Jacques Gerin | |
US4053124A (en) * | 1975-08-22 | 1977-10-11 | The Boeing Company | Variable camber airfoil |
US5335886A (en) * | 1992-01-30 | 1994-08-09 | The United States Of America As Represented By The Seceretary Of The Navy | Lift enhancement device |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3987984A (en) * | 1973-04-09 | 1976-10-26 | Albert George Fischer | Semi-rigid aircraft wing |
US3994452A (en) * | 1974-03-28 | 1976-11-30 | The Boeing Company | Variable camber airfoil |
US5115996A (en) * | 1990-01-31 | 1992-05-26 | Moller International, Inc. | Vtol aircraft |
US5794893A (en) * | 1995-06-07 | 1998-08-18 | Northrop Grumman Corporation | Elastomeric transition for aircraft control surface |
-
1998
- 1998-01-14 ES ES009800050A patent/ES2156660B1/es not_active Expired - Fee Related
- 1998-07-02 US US09/110,744 patent/US6109567A/en not_active Expired - Fee Related
- 1998-12-28 EP EP98500280A patent/EP0937641B1/en not_active Expired - Lifetime
- 1998-12-28 DE DE69824945T patent/DE69824945D1/de not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1413258A (en) * | 1919-02-06 | 1922-04-18 | Christmas Aeroplane Company In | Flying machine |
GB360273A (es) * | 1930-01-21 | 1931-11-05 | Jacques Gerin | |
GB346251A (en) * | 1930-08-27 | 1931-04-09 | Ugo Antoni | Improvements in and relating to the construction of flexible aeroplane wings having a variable profile |
US4053124A (en) * | 1975-08-22 | 1977-10-11 | The Boeing Company | Variable camber airfoil |
US5335886A (en) * | 1992-01-30 | 1994-08-09 | The United States Of America As Represented By The Seceretary Of The Navy | Lift enhancement device |
Also Published As
Publication number | Publication date |
---|---|
EP0937641B1 (en) | 2004-07-07 |
EP0937641A3 (en) | 2000-05-10 |
DE69824945D1 (de) | 2004-08-12 |
ES2156660B1 (es) | 2002-02-16 |
EP0937641A2 (en) | 1999-08-25 |
US6109567A (en) | 2000-08-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EC2A | Search report published |
Date of ref document: 20010701 Kind code of ref document: A1 Effective date: 20010701 |
|
FD1A | Patent lapsed |
Effective date: 20050115 |