FR2445798A1 - Mecanisme d'actionnement de volet dans un avion comportant un systeme de sustentation operant par soufflage sur surface d'extrados - Google Patents
Mecanisme d'actionnement de volet dans un avion comportant un systeme de sustentation operant par soufflage sur surface d'extradosInfo
- Publication number
- FR2445798A1 FR2445798A1 FR7931826A FR7931826A FR2445798A1 FR 2445798 A1 FR2445798 A1 FR 2445798A1 FR 7931826 A FR7931826 A FR 7931826A FR 7931826 A FR7931826 A FR 7931826A FR 2445798 A1 FR2445798 A1 FR 2445798A1
- Authority
- FR
- France
- Prior art keywords
- blowing
- system operating
- flap
- extrados
- aircraft
- 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
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/30—Wing lift efficiency
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Transmission Devices (AREA)
- Toys (AREA)
Abstract
L'invention concerne un mécanisme d'actionnement de volet dans un avion comportant un système de sustentation opérant par soufflage sur surface d'extrados. Le mécanisme comprend une bielette avant 68 et une biellette arrière 70 qui sont articulées par leurs extrémités inférieures sur un bras porteur fixe 56 et qui s'étendent vers le haut, et en divergeant l'une par rapport à l'autre, pour être fixées sur le volet 30, le mécanisme permettant de faire tourner le volet avec un rayon variable qui maintient sa surface d'extrados en contact et en alignement tangentiel avec le bord de fuite de la surface d'extrados de l'aide 14 de l'avion. Application aux avions à décollage et atterrissage sur courtes distances.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/000,118 US4283029A (en) | 1979-01-02 | 1979-01-02 | Actuating apparatus for a flap system having an upper surface blowing powered lift system |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2445798A1 true FR2445798A1 (fr) | 1980-08-01 |
FR2445798B1 FR2445798B1 (fr) | 1985-07-19 |
Family
ID=21689999
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7931826A Expired FR2445798B1 (fr) | 1979-01-02 | 1979-12-27 | Mecanisme d'actionnement de volet dans un avion comportant un systeme de sustentation operant par soufflage sur surface d'extrados |
Country Status (6)
Country | Link |
---|---|
US (1) | US4283029A (fr) |
JP (1) | JPS5594895A (fr) |
DE (1) | DE2951265A1 (fr) |
FR (1) | FR2445798B1 (fr) |
GB (1) | GB2038737A (fr) |
IT (1) | IT1126858B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2473982A1 (fr) * | 1980-01-22 | 1981-07-24 | British Aerospace | Agencement d'aile et de volet pour avions |
Families Citing this family (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4398683A (en) * | 1978-12-26 | 1983-08-16 | Schmetzer William M | Aircraft with thrust and lift augmenting airfoil |
US4447027A (en) * | 1979-01-02 | 1984-05-08 | The Boeing Company | Upper surface blown powered lift system for aircraft |
US4426054A (en) | 1979-01-02 | 1984-01-17 | The Boeing Company | Upper surface blown powered lift system |
US4447028A (en) * | 1979-01-02 | 1984-05-08 | The Boeing Company | Upper surface blown powered lift system for aircraft |
US4444368A (en) * | 1981-10-30 | 1984-04-24 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Slotted variable camber flap |
EP0081610B1 (fr) * | 1981-12-16 | 1986-12-17 | The Boeing Company | Assemblage de volets d'ailes d'avions |
US4712752A (en) * | 1982-12-06 | 1987-12-15 | The Boeing Company | Wing trailing edge air dam |
WO1984002320A1 (fr) * | 1982-12-06 | 1984-06-21 | Boeing Co | Barrages contre le passage d'air dans le bord de fuite d'une aile |
JPS62113697A (ja) * | 1985-11-14 | 1987-05-25 | 財団法人 日本航空機開発協会 | 飛行機翼後縁フラツプのリンク式作動機構 |
GB8915487D0 (en) * | 1989-07-06 | 1989-08-23 | Short Brothers Plc | A flap assembly |
JPH05321946A (ja) * | 1992-05-22 | 1993-12-07 | Jidosha Kiki Co Ltd | クラッチ操作装置 |
USRE44313E1 (en) | 1996-10-22 | 2013-06-25 | The Boeing Company | Airplane with unswept slotted cruise wing airfoil |
US6435458B1 (en) * | 2001-02-12 | 2002-08-20 | The Boeing Company | Tailored wing assembly for an aircraft moveable slat system |
US7243881B2 (en) * | 2003-06-03 | 2007-07-17 | The Boeing Company | Multi-function trailing edge devices and associated methods |
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 |
US7270305B2 (en) * | 2004-06-15 | 2007-09-18 | The Boeing Company | Aircraft leading edge apparatuses and corresponding 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 |
US7322547B2 (en) | 2005-01-31 | 2008-01-29 | The Boeing Company | Aerospace vehicle leading edge slat devices and corresponding 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 |
US7578484B2 (en) | 2006-06-14 | 2009-08-25 | The Boeing Company | Link mechanisms for gapped rigid krueger flaps, and associated systems and methods |
DE102006036464B4 (de) * | 2006-08-04 | 2009-08-20 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug |
DE102007036996A1 (de) * | 2007-08-06 | 2009-02-19 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug |
GB0721284D0 (en) | 2007-10-31 | 2007-12-12 | Airbus Uk Ltd | Actuation system for leading edge high-lift device |
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 |
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 |
NL2009762C2 (en) | 2012-11-06 | 2014-05-08 | Fokker Aerostructures Bv | An airplane wing, airplane and flap system. |
DE102012111690A1 (de) * | 2012-11-30 | 2014-06-05 | Airbus Operations Gmbh | Formvariabler aerodynamischer Verkleidungskörper für einen Klappen-Verstellmechanismus eines Luftfahrzeugs |
GB201222308D0 (en) * | 2012-12-11 | 2013-01-23 | Airbus Operations Ltd | Support assembly |
US9550559B1 (en) | 2013-07-08 | 2017-01-24 | The Boeing Company | Aircraft wing assemblies |
BR102013024469B1 (pt) * | 2013-09-24 | 2021-09-21 | Embraer S.A | Mecanismo de acionamento de superfícies aerodinâmicas |
US9567063B2 (en) * | 2015-05-21 | 2017-02-14 | Embraer S.A. | Airfoil flap assembly with split flap track fairing system |
US10538306B2 (en) | 2016-12-21 | 2020-01-21 | The Boeing Company | Wing flap deflection control removal |
DE102017114772A1 (de) * | 2017-07-03 | 2019-01-03 | Hettich-Oni Gmbh & Co. Kg | Klappenbeschlag und Möbel |
US10766600B2 (en) * | 2017-07-28 | 2020-09-08 | The Boeing Company | Articulation assemblies for retracting aircraft flap support fairings and related methods |
GB2568743B (en) * | 2017-11-27 | 2020-06-17 | Airbus Operations Ltd | Variable deployable wing flap |
US11034432B2 (en) * | 2018-10-27 | 2021-06-15 | The Boeing Company | Flap support mechanism—C bar |
US11192628B2 (en) * | 2019-06-30 | 2021-12-07 | The Boeing Company | Articulated flap support forward fairing |
CN111017194B (zh) * | 2019-12-24 | 2023-08-04 | 中国航空工业集团公司西安飞机设计研究所 | 一种动力增升机翼 |
US20240278905A1 (en) * | 2023-02-22 | 2024-08-22 | The Boeing Company | Linear Actuator Driven Flap Mechanism |
EP4446218A1 (fr) * | 2023-04-11 | 2024-10-16 | Airbus Operations GmbH | Système d'aéronef |
CN118514858B (zh) * | 2024-07-23 | 2024-09-20 | 中国空气动力研究与发展中心计算空气动力研究所 | 飞行器复合式操纵舵射流环量控制方法、系统及存储介质 |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR951122A (fr) * | 1947-06-26 | 1949-10-17 | Dispositif de support applicable aux volets d'hypersustentation ou de freinage des aérodynes | |
GB1508389A (en) * | 1976-05-03 | 1978-04-26 | Boeing Co | Aerodynamic lift enhancing apparatus |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2700516A (en) * | 1950-01-31 | 1955-01-25 | Phiroze P Nazir | Aircraft lift control device |
US3987983A (en) * | 1974-12-20 | 1976-10-26 | The Boeing Company | Trailing edge flaps having spanwise aerodynamic slot opening and closing mechanism |
DE2622901A1 (de) * | 1976-05-21 | 1977-12-01 | Boeing Co | Tragfluegel fuer flugzeuge mit einer anordnung zur verbesserung des auftriebs |
US4120470A (en) * | 1976-09-28 | 1978-10-17 | The Boeing Company | Efficient trailing edge system for an aircraft wing |
-
1979
- 1979-01-02 US US06/000,118 patent/US4283029A/en not_active Expired - Lifetime
- 1979-12-12 GB GB7942841A patent/GB2038737A/en not_active Withdrawn
- 1979-12-17 DE DE19792951265 patent/DE2951265A1/de active Granted
- 1979-12-26 JP JP16844379A patent/JPS5594895A/ja active Granted
- 1979-12-27 FR FR7931826A patent/FR2445798B1/fr not_active Expired
-
1980
- 1980-01-02 IT IT47505/80A patent/IT1126858B/it active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR951122A (fr) * | 1947-06-26 | 1949-10-17 | Dispositif de support applicable aux volets d'hypersustentation ou de freinage des aérodynes | |
GB1508389A (en) * | 1976-05-03 | 1978-04-26 | Boeing Co | Aerodynamic lift enhancing apparatus |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2473982A1 (fr) * | 1980-01-22 | 1981-07-24 | British Aerospace | Agencement d'aile et de volet pour avions |
Also Published As
Publication number | Publication date |
---|---|
FR2445798B1 (fr) | 1985-07-19 |
DE2951265A1 (de) | 1980-07-17 |
DE2951265C2 (fr) | 1990-06-28 |
US4283029A (en) | 1981-08-11 |
IT8047505A0 (it) | 1980-01-02 |
IT1126858B (it) | 1986-05-21 |
JPS647920B2 (fr) | 1989-02-10 |
GB2038737A (en) | 1980-07-30 |
JPS5594895A (en) | 1980-07-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |