ES2063277T3 - Un conjunto de aleta. - Google Patents
Un conjunto de aleta.Info
- Publication number
- ES2063277T3 ES2063277T3 ES90307288T ES90307288T ES2063277T3 ES 2063277 T3 ES2063277 T3 ES 2063277T3 ES 90307288 T ES90307288 T ES 90307288T ES 90307288 T ES90307288 T ES 90307288T ES 2063277 T3 ES2063277 T3 ES 2063277T3
- Authority
- ES
- Spain
- Prior art keywords
- wing
- bracket
- aleron
- mounting arm
- fin
- 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Orthopedics, Nursing, And Contraception (AREA)
- Toys (AREA)
Abstract
UN CONJUNTO DE ALERON INCLUYE UN MIEMBRO DE ALERON (2) SITUADO EN EL BORDE DE COLA DEL ALA (4) DE UN AVION. UNA MENSULA (12) SE EXTIENDE HACIA ABAJO DESDE EL MIEMBRO DEL ALERON (2), Y UN BRAZO DE MONTAJE (8) SE EXTIENDE HACIA ATRAS FORMAN LA SUPERFICIE INFERIOR DEL ALA. DOS BRAZOS DE ARTICULACION (14 Y 16) ESTAN MONTADOS PIVOTANTEMENTE EN SUS EXTREMOS SUPERIORES (18 Y 20) AL BRAZO DE MONTAJE (8), Y EN SUS EXTEMOS INFERIORES (22 Y 24) A LA MENSULA (12). EL MIEMBRO DE ALERON (2) SE MUEVE ENTRE SUS POSICIONES OCULTA Y EXTENDIDA HACIA ABAJO MEDIANTE UN MECANISMO ACTUADOR (26) QUE ESTA MONTADO SOBRE EL ALA (4) DEL AVION, Y CONECTADO BIEN AL MIEMBRO DE ALERON O A LA MENSULA (12). EL MECANISMO ACTUADOR (26) PUEDE SER DEL TIPO LINEAL O GIRATORIO
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB898915487A GB8915487D0 (en) | 1989-07-06 | 1989-07-06 | A flap assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2063277T3 true ES2063277T3 (es) | 1995-01-01 |
Family
ID=10659626
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES90307288T Expired - Lifetime ES2063277T3 (es) | 1989-07-06 | 1990-07-04 | Un conjunto de aleta. |
Country Status (11)
Country | Link |
---|---|
US (1) | US5207400A (es) |
EP (1) | EP0407159B1 (es) |
JP (1) | JPH04500649A (es) |
AU (1) | AU637387B2 (es) |
BR (1) | BR9006847A (es) |
CA (1) | CA2020555A1 (es) |
DE (1) | DE69013243T2 (es) |
ES (1) | ES2063277T3 (es) |
GB (2) | GB8915487D0 (es) |
IL (1) | IL95000A (es) |
WO (1) | WO1991000824A1 (es) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE44313E1 (en) | 1996-10-22 | 2013-06-25 | The Boeing Company | Airplane with unswept slotted cruise wing airfoil |
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 |
US7059563B2 (en) * | 2003-06-03 | 2006-06-13 | The Boeing Company | Systems, apparatuses, and methods for moving aircraft control surfaces |
JP4516022B2 (ja) * | 2003-11-21 | 2010-08-04 | エアバス | 航空機流体冷却システムおよびそうしたシステムを備えた航空機 |
US6799739B1 (en) | 2003-11-24 | 2004-10-05 | The Boeing Company | Aircraft control surface drive system and associated methods |
US7357358B2 (en) * | 2004-02-27 | 2008-04-15 | The Boeing Company | Aircraft leading edge device systems and corresponding sizing 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 |
DE102005016639B4 (de) * | 2005-04-11 | 2010-12-02 | Eads Deutschland Gmbh | Tragflügel mit ausfahrbaren aerodynamischen Flügelklappen, insbesondere Auftriebsklappen |
US7309043B2 (en) * | 2005-04-27 | 2007-12-18 | The Boeing Company | Actuation device positioning systems and associated methods, including aircraft spoiler droop systems |
US7721999B2 (en) | 2005-05-20 | 2010-05-25 | The Boeing Company | Aerospace vehicle fairing systems and associated methods |
US7300021B2 (en) * | 2005-05-20 | 2007-11-27 | The Boeing Company | Aerospace vehicle fairing systems and associated methods |
US7367530B2 (en) * | 2005-06-21 | 2008-05-06 | The Boeing Company | Aerospace vehicle yaw generating systems and associated methods |
DE102005045759A1 (de) | 2005-09-23 | 2007-04-12 | Airbus Deutschland Gmbh | Fortschrittlicheflügelhinterkante am Flügel eines Flugzeugs |
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 |
FR2902078B1 (fr) * | 2006-06-13 | 2008-07-11 | Airbus France Sas | Procede de pilotage d'un aeronef en phase d'approche |
DE102007036996A1 (de) * | 2007-08-06 | 2009-02-19 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug |
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. |
GB0808349D0 (en) * | 2008-05-09 | 2008-06-18 | Airbus Uk Ltd | Spoiler deployment mechanism |
US8226048B2 (en) * | 2008-12-09 | 2012-07-24 | The Boeing Company | Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods |
US8382045B2 (en) | 2009-07-21 | 2013-02-26 | The Boeing Company | Shape-changing control surface |
US9108715B2 (en) * | 2012-05-29 | 2015-08-18 | The Boeing Company | Rotary actuated high lift gapped aileron |
IL226859A (en) * | 2013-06-10 | 2017-09-28 | Abramov Danny | Slot wing with groove and wings for aircraft |
BR102013024469B1 (pt) * | 2013-09-24 | 2021-09-21 | Embraer S.A | Mecanismo de acionamento de superfícies aerodinâmicas |
US9856014B2 (en) * | 2015-12-03 | 2018-01-02 | The Boeing Company | Aircraft wing fairing drive assembly, system, and method |
US10472046B1 (en) * | 2016-02-03 | 2019-11-12 | Lockheed Martin Corporation | Internal wing control surface linkage system |
US10766600B2 (en) * | 2017-07-28 | 2020-09-08 | The Boeing Company | Articulation assemblies for retracting aircraft flap support fairings and related methods |
US10974816B2 (en) * | 2017-09-28 | 2021-04-13 | The Boeing Company | High-fowler flap actuation apparatus and related methods |
CN108045556B (zh) * | 2017-11-30 | 2021-05-25 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机襟副翼运动机构 |
US11623734B2 (en) * | 2020-12-02 | 2023-04-11 | The Boeing Company | Apparatus, system and method for supporting a wing flap of an aircraft |
US12024287B2 (en) * | 2021-06-09 | 2024-07-02 | The Boeing Company | Truncated flap support fairings with active flow control systems for aircraft and related methods |
ES1302354Y (es) | 2023-01-03 | 2023-10-19 | Jin Pengliang | Dispositivo de ayuda al despegue y/o aterrizaje de aeronaves |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2137879A (en) * | 1935-02-26 | 1938-11-22 | Ksoll Joseph | Supporting surface for flying machines |
FR994382A (fr) * | 1945-01-25 | 1951-11-15 | D Aviat Latecoere Soc Ind | Perfectionnement aux aérodynes comportant un dispositif hypersustentateur à double volet |
DE2103639A1 (de) * | 1971-01-27 | 1972-09-07 | Messerschmitt-Bölkow-Blöhm GmbH, 8000 München | Tragflügel für Luftfahrzeuge mit einer oder mehreren ein- oder mehrteiligen Spaltklappen |
US3985319A (en) * | 1975-02-03 | 1976-10-12 | The Boeing Company | Variable pivot trailing edge flap |
GB1547904A (en) * | 1975-03-24 | 1979-06-27 | Boeing Co | Mounting mechanism for an airplane wing trailing-edge flaps |
US4248395A (en) * | 1975-03-24 | 1981-02-03 | The Boeing Company | Airplane wing trailing-edge flap-mounting mechanism |
US4283029A (en) * | 1979-01-02 | 1981-08-11 | Rudolph Peter K C | Actuating apparatus for a flap system having an upper surface blowing powered lift system |
US4353517A (en) * | 1980-10-07 | 1982-10-12 | The Boeing Company | Flap assembly for aircraft wing |
DE3175717D1 (en) * | 1981-12-16 | 1987-01-29 | Boeing Co | Flap assembly aircraft wing |
US4448375A (en) * | 1982-09-29 | 1984-05-15 | The Boeing Company | Folding truss mechanism for trailing edge flaps |
US4702442A (en) * | 1984-12-06 | 1987-10-27 | The Boeing Company | Aircraft trailing edge flap apparatus |
-
1989
- 1989-07-06 GB GB898915487A patent/GB8915487D0/en active Pending
-
1990
- 1990-07-04 AU AU60397/90A patent/AU637387B2/en not_active Ceased
- 1990-07-04 BR BR909006847A patent/BR9006847A/pt not_active IP Right Cessation
- 1990-07-04 EP EP90307288A patent/EP0407159B1/en not_active Expired - Lifetime
- 1990-07-04 WO PCT/GB1990/001031 patent/WO1991000824A1/en unknown
- 1990-07-04 ES ES90307288T patent/ES2063277T3/es not_active Expired - Lifetime
- 1990-07-04 JP JP2510322A patent/JPH04500649A/ja active Pending
- 1990-07-04 US US07/663,871 patent/US5207400A/en not_active Expired - Fee Related
- 1990-07-04 GB GB9014849A patent/GB2233613B/en not_active Expired - Fee Related
- 1990-07-04 DE DE69013243T patent/DE69013243T2/de not_active Expired - Fee Related
- 1990-07-05 CA CA002020555A patent/CA2020555A1/en not_active Abandoned
- 1990-07-06 IL IL9500090A patent/IL95000A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
GB2233613B (en) | 1993-04-07 |
GB9014849D0 (en) | 1990-08-22 |
CA2020555A1 (en) | 1991-01-07 |
GB8915487D0 (en) | 1989-08-23 |
IL95000A0 (en) | 1991-06-10 |
AU6039790A (en) | 1991-02-06 |
BR9006847A (pt) | 1991-08-06 |
WO1991000824A1 (en) | 1991-01-24 |
DE69013243D1 (de) | 1994-11-17 |
EP0407159A1 (en) | 1991-01-09 |
US5207400A (en) | 1993-05-04 |
EP0407159B1 (en) | 1994-10-12 |
JPH04500649A (ja) | 1992-02-06 |
GB2233613A (en) | 1991-01-16 |
DE69013243T2 (de) | 1995-05-18 |
AU637387B2 (en) | 1993-05-27 |
IL95000A (en) | 1994-04-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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