ES2192540T3 - Una disposicion de carenado para un avion. - Google Patents
Una disposicion de carenado para un avion.Info
- Publication number
- ES2192540T3 ES2192540T3 ES00954775T ES00954775T ES2192540T3 ES 2192540 T3 ES2192540 T3 ES 2192540T3 ES 00954775 T ES00954775 T ES 00954775T ES 00954775 T ES00954775 T ES 00954775T ES 2192540 T3 ES2192540 T3 ES 2192540T3
- Authority
- ES
- Spain
- Prior art keywords
- aileron
- fairing
- overlap
- wing
- movement
- 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
- B64C7/00—Structures or fairings not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
- Toys (AREA)
- Insulated Conductors (AREA)
- Laminated Bodies (AREA)
- Radio Relay Systems (AREA)
- Supply And Distribution Of Alternating Current (AREA)
- Fluid-Pressure Circuits (AREA)
Abstract
Una disposición de carenado (28) para un ala de avión (10) que comprende una primera porción de carenado (32) en el ala (10) y una segunda porción de carenado (34) en una superficie de control (12) montada en el ala (10), para desplazamiento angular en relación con el ala (10), sobresaliendo la disposición de carenado (28) hacia fuera de un perfil aerodinámico del ala (S) y de la superficie de control (12), siendo el desplazamiento angular de la superficie de control (12), al menos a lo largo de un rango de movimientos de funcionamiento normal, entre los límites positivo y negativo a cada lado de una posición de vuelo recto y nivelado, caracterizada porque se dispone un solape con conicidad entre la primera y la segunda porciones de carenado (32, 34), básicamente para formar un sello aerodinámico (45) al menos dentro de dicho rango de funcionamiento normal.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB9920318.4A GB9920318D0 (en) | 1999-08-27 | 1999-08-27 | A fairing arrangement for an aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2192540T3 true ES2192540T3 (es) | 2003-10-16 |
Family
ID=10859922
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES00954775T Expired - Lifetime ES2192540T3 (es) | 1999-08-27 | 2000-08-25 | Una disposicion de carenado para un avion. |
Country Status (10)
Country | Link |
---|---|
US (1) | US6450457B1 (es) |
EP (1) | EP1206382B1 (es) |
JP (1) | JP3655586B2 (es) |
AT (1) | ATE236044T1 (es) |
AU (1) | AU6713000A (es) |
CA (1) | CA2382773C (es) |
DE (1) | DE60001964T2 (es) |
ES (1) | ES2192540T3 (es) |
GB (1) | GB9920318D0 (es) |
WO (1) | WO2001015972A1 (es) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
US6799739B1 (en) | 2003-11-24 | 2004-10-05 | The Boeing Company | Aircraft control surface drive system and associated methods |
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 |
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 |
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 |
DE102005062190B3 (de) * | 2005-12-23 | 2007-06-14 | Airbus Deutschland Gmbh | Verfahren zum Herstellen einer lösbaren Dichtung mit einer Dichtmasse sowie Verwendung von Klebestreifen zur Durchführung des Verfahrens |
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 |
US8382045B2 (en) | 2009-07-21 | 2013-02-26 | The Boeing Company | Shape-changing control surface |
WO2012173542A1 (en) * | 2011-06-16 | 2012-12-20 | Saab Ab | A double-curved cover for covering a gap between two structural portions of an aircraft |
US9505485B2 (en) * | 2012-05-08 | 2016-11-29 | Lockheed Martin Corporation | Vortex generation |
GB201522486D0 (en) * | 2015-12-21 | 2016-02-03 | Airbus Operations Ltd | Seal assembly |
EP3318783A1 (en) * | 2016-11-02 | 2018-05-09 | Airbus Operations GmbH | Fairing for an aircraft |
GB2580930A (en) * | 2019-01-30 | 2020-08-05 | Airbus Operations Ltd | Fairing for folding wing tip |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4705236A (en) * | 1981-09-29 | 1987-11-10 | The Boeing Company | Aileron system for aircraft and method of operating the same |
US4962902A (en) | 1989-03-20 | 1990-10-16 | The Boeing Company | Aircraft control surface linkage |
GB8919057D0 (en) * | 1989-08-22 | 1989-10-04 | British Aerospace | Fairing arrangements for aircraft |
GB8921749D0 (en) * | 1989-09-27 | 1989-11-08 | British Aerospace | Fairing arrangements for aircraft |
GB8924982D0 (en) | 1989-11-06 | 1989-12-28 | British Aerospace | Fairing arrangement for aircraft |
US5098043A (en) * | 1990-02-27 | 1992-03-24 | Grumman Aerospace Corporation | Integrated power hinge actuator |
US5388788A (en) | 1993-12-16 | 1995-02-14 | The Boeing Company | Hinge fairings for control surfaces |
US5915653A (en) * | 1996-01-02 | 1999-06-29 | The Boeing Company | Spherical mating fairings for hingeline applications |
GB2323576B (en) | 1997-03-26 | 2001-08-22 | British Aerospace | Fairing arrangements for aircraft |
-
1999
- 1999-08-27 GB GBGB9920318.4A patent/GB9920318D0/en not_active Ceased
-
2000
- 2000-08-25 WO PCT/GB2000/003270 patent/WO2001015972A1/en active IP Right Grant
- 2000-08-25 AU AU67130/00A patent/AU6713000A/en not_active Abandoned
- 2000-08-25 EP EP00954775A patent/EP1206382B1/en not_active Expired - Lifetime
- 2000-08-25 ES ES00954775T patent/ES2192540T3/es not_active Expired - Lifetime
- 2000-08-25 CA CA002382773A patent/CA2382773C/en not_active Expired - Fee Related
- 2000-08-25 DE DE60001964T patent/DE60001964T2/de not_active Expired - Lifetime
- 2000-08-25 JP JP2001519552A patent/JP3655586B2/ja not_active Expired - Fee Related
- 2000-08-25 AT AT00954775T patent/ATE236044T1/de not_active IP Right Cessation
- 2000-08-25 US US09/647,797 patent/US6450457B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1206382A1 (en) | 2002-05-22 |
WO2001015972A1 (en) | 2001-03-08 |
JP2003508287A (ja) | 2003-03-04 |
CA2382773C (en) | 2008-11-18 |
CA2382773A1 (en) | 2001-03-08 |
ATE236044T1 (de) | 2003-04-15 |
GB9920318D0 (en) | 1999-11-03 |
AU6713000A (en) | 2001-03-26 |
US6450457B1 (en) | 2002-09-17 |
DE60001964D1 (de) | 2003-05-08 |
JP3655586B2 (ja) | 2005-06-02 |
DE60001964T2 (de) | 2003-11-06 |
EP1206382B1 (en) | 2003-04-02 |
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