CA2660094A1 - High-lift system for an aircraft - Google Patents

High-lift system for an aircraft Download PDF

Info

Publication number
CA2660094A1
CA2660094A1 CA002660094A CA2660094A CA2660094A1 CA 2660094 A1 CA2660094 A1 CA 2660094A1 CA 002660094 A CA002660094 A CA 002660094A CA 2660094 A CA2660094 A CA 2660094A CA 2660094 A1 CA2660094 A1 CA 2660094A1
Authority
CA
Canada
Prior art keywords
flap
wing
rotation point
lever
lift system
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.)
Abandoned
Application number
CA002660094A
Other languages
English (en)
French (fr)
Inventor
Bernhard Schlipf
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations GmbH
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of CA2660094A1 publication Critical patent/CA2660094A1/en
Abandoned legal-status Critical Current

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)
  • Connection Of Plates (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Geophysics And Detection Of Objects (AREA)
  • Coupling Device And Connection With Printed Circuit (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Retarders (AREA)
  • Radio Relay Systems (AREA)
  • Feedback Control In General (AREA)
CA002660094A 2006-08-04 2007-08-06 High-lift system for an aircraft Abandoned CA2660094A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102006036464A DE102006036464B4 (de) 2006-08-04 2006-08-04 Hochauftriebssystem für ein Flugzeug
DE102006036464.3 2006-08-04
PCT/EP2007/006945 WO2008015024A1 (en) 2006-08-04 2007-08-06 High-lift system for an aircraft

Publications (1)

Publication Number Publication Date
CA2660094A1 true CA2660094A1 (en) 2008-02-07

Family

ID=38566163

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002660094A Abandoned CA2660094A1 (en) 2006-08-04 2007-08-06 High-lift system for an aircraft

Country Status (10)

Country Link
US (1) US8302913B2 (enExample)
EP (2) EP2199200B1 (enExample)
JP (1) JP2009545478A (enExample)
CN (1) CN101506050B (enExample)
AT (2) ATE469025T1 (enExample)
BR (1) BRPI0714773A2 (enExample)
CA (1) CA2660094A1 (enExample)
DE (2) DE102006036464B4 (enExample)
RU (1) RU2438927C2 (enExample)
WO (1) WO2008015024A1 (enExample)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006036464B4 (de) * 2006-08-04 2009-08-20 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
DE102006052724B4 (de) * 2006-11-08 2010-03-18 Liebherr-Aerospace Lindenberg Gmbh Vorrichtung zum Verstellen der Wölbung eines Tragflügels eines Flugzeuges
DE102007036996A1 (de) * 2007-08-06 2009-02-19 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
DE102009015397A1 (de) * 2009-03-27 2010-09-30 Airbus Deutschland Gmbh Tragflügel mit einer Hochauftriebsklappe
DE102009015330A1 (de) * 2009-03-27 2010-09-30 Airbus Deutschland Gmbh Tragflügel mit einer Hochauftriebsklappe
DE102009002435A1 (de) * 2009-04-16 2010-10-21 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug und Verfahren zum Detektieren von Fehlern in einem Hochauftriebssystem für ein Flugzeug
DE102009037707B4 (de) * 2009-08-17 2013-12-24 Airbus Operations Gmbh Verstellmechanismus einer Verstellvorrichtung zur Ankopplung einer Verstellklappe an einen Hauptflügel und eine solche Verstellvorrichtung
US8763953B2 (en) * 2010-07-14 2014-07-01 The Boeing Company Aircraft flap actuator assembly
DE102012111690A1 (de) * 2012-11-30 2014-06-05 Airbus Operations Gmbh Formvariabler aerodynamischer Verkleidungskörper für einen Klappen-Verstellmechanismus eines Luftfahrzeugs
EP2746151B1 (en) * 2012-12-19 2017-04-12 Airbus Operations GmbH Flap system for an aircraft, method for adjusting the lift of an aircraft and aircraft comprising a main wing and at least one flap system
CN103287574B (zh) * 2013-01-05 2015-07-01 中国航空工业集团公司西安飞机设计研究所 一种飞机增升装置控制方法
US9227720B2 (en) 2013-03-01 2016-01-05 Roller Bearing Company Of America, Inc. Composite annular seal assembly for bearings in aircraft
CN103332288B (zh) * 2013-06-13 2015-05-27 西北工业大学 一种飞机主翼后缘处的边条及其设计方法
FR3018767B1 (fr) * 2014-03-21 2018-01-12 Airbus Operations Ensemble de support pour un systeme de volet d'aile d'un avion.
CN104494843B (zh) * 2014-11-19 2017-09-22 中国航空工业集团公司沈阳飞机设计研究所 一种飞机开缝襟翼设计方法
US10082179B2 (en) 2014-12-16 2018-09-25 Roller Bearing Company Of America, Inc. Seal for self aligning roller bearing
CN109415116B (zh) 2016-06-30 2022-04-08 庞巴迪公司 用于展开飞机的后缘襟翼的组件和方法
BE1024276B1 (fr) * 2016-11-04 2018-01-11 Sonaca Sa Aile d’aeronef comprenant un volet mobile de bord de fuite entraine par un moteur electrique lineaire
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
US11091248B2 (en) * 2019-09-17 2021-08-17 The Boeing Company Flap actuator mechanism
US11548616B1 (en) 2020-03-02 2023-01-10 Lucas Kai-Luen Hung Split-flap wing assembly for a high endurance aircraft
CN113844640B (zh) * 2021-10-20 2023-09-29 中航贵州飞机有限责任公司 一种机翼后缘襟翼驱动结构
EP4446218A1 (en) * 2023-04-11 2024-10-16 Airbus Operations GmbH Aircraft system

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2407401A (en) 1941-09-08 1946-09-10 Douglas Aircraft Co Inc Lateral control arrangement
US3874617A (en) * 1974-07-17 1975-04-01 Mc Donnell Douglas Corp Stol flaps
GB1508389A (en) * 1976-05-03 1978-04-26 Boeing Co Aerodynamic lift enhancing apparatus
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
US4381093A (en) * 1980-10-07 1983-04-26 The Boeing Company Flap assembly for aircraft wing
US4381082A (en) * 1980-12-19 1983-04-26 Fmc Corporation Particulate material handling means
US4381092A (en) 1981-05-01 1983-04-26 Martin Marietta Corporation Magnetic docking probe for soft docking of space vehicles
DE3522448A1 (de) * 1985-06-22 1987-01-02 Messerschmitt Boelkow Blohm Antriebs- und fuehrungsvorrichtung fuer eine an einem flugzeugtragfluegel angeordnete klappe
DE3643808A1 (de) * 1986-12-20 1988-06-30 Dornier Gmbh Einrichtung fuer aerodynamisch arbeitende klappen an flugzeugtragfluegeln, insbesondere spaltklappen
DE59001450D1 (de) 1989-02-23 1993-06-17 Zahnradfabrik Friedrichshafen Antriebseinrichtung mit variablem drehmoment-begrenzungssystem.
CN2060763U (zh) * 1989-05-21 1990-08-22 郭朝光 直升飞机增升力环翼
DE4107556C1 (enExample) * 1991-03-08 1992-05-14 Deutsche Airbus Gmbh, 2000 Hamburg, De
US5788190A (en) * 1996-10-22 1998-08-04 The Boeing Company Slotted cruise trailing edge flap
DE19732953C1 (de) 1997-07-31 1999-03-11 Daimler Benz Ag Tragflügel mit Landeklappe
DE10133920B4 (de) * 2001-07-12 2004-05-13 Eads Deutschland Gmbh Auftriebsklappen-Mechanismus
RU2214347C2 (ru) * 2001-07-23 2003-10-20 Открытое акционерное общество Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева Устройство для выдвижения закрылка
DE10328540B4 (de) 2003-06-24 2008-02-14 Eads Deutschland Gmbh Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe
DE10339030B4 (de) 2003-08-25 2005-11-03 Man Technologie Ag Tragstruktur für eine ein- und ausfahrbare Klappe und deren Verwendung
DE102004006940B4 (de) * 2004-02-12 2009-02-26 Airbus Deutschland Gmbh Landeklappenführung für Luftfahrzeuge
DE102004049504A1 (de) * 2004-10-11 2006-04-13 Airbus Deutschland Gmbh Flugzeugflügel, Verfahren zum Betreiben eines Flugzeugflügels und Verwendung einer schwenkbaren Hinterkante an einem Hauptflügel eines Flugzeugflügels zum Justieren der Form und Breite eines Luftspalts
DE102006036464B4 (de) 2006-08-04 2009-08-20 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug

Also Published As

Publication number Publication date
EP2199200A1 (en) 2010-06-23
ATE528208T1 (de) 2011-10-15
WO2008015024A1 (en) 2008-02-07
BRPI0714773A2 (pt) 2013-10-29
DE602007006808D1 (de) 2010-07-08
DE102006036464B4 (de) 2009-08-20
RU2009107490A (ru) 2010-09-10
CN101506050A (zh) 2009-08-12
US8302913B2 (en) 2012-11-06
EP2046650B1 (en) 2010-05-26
US20090308982A1 (en) 2009-12-17
DE102006036464A1 (de) 2008-02-14
CN101506050B (zh) 2013-01-16
RU2438927C2 (ru) 2012-01-10
EP2046650A1 (en) 2009-04-15
JP2009545478A (ja) 2009-12-24
EP2199200B1 (en) 2011-10-12
ATE469025T1 (de) 2010-06-15

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Legal Events

Date Code Title Description
FZDE Discontinued

Effective date: 20130806

FZDE Discontinued

Effective date: 20130806