DE602005018230D1 - Systeme und verfahren zur bereitstellung von differenzieller bewegung für flügelhochauftriebsvorrichtungen - Google Patents

Systeme und verfahren zur bereitstellung von differenzieller bewegung für flügelhochauftriebsvorrichtungen

Info

Publication number
DE602005018230D1
DE602005018230D1 DE602005018230T DE602005018230T DE602005018230D1 DE 602005018230 D1 DE602005018230 D1 DE 602005018230D1 DE 602005018230 T DE602005018230 T DE 602005018230T DE 602005018230 T DE602005018230 T DE 602005018230T DE 602005018230 D1 DE602005018230 D1 DE 602005018230D1
Authority
DE
Germany
Prior art keywords
deployable lift
wing
lift device
drive link
deployable
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.)
Active
Application number
DE602005018230T
Other languages
English (en)
Inventor
Seth E Gitnes
Paul M Vijgen
Mark S Good
Glynn M Thomas
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.)
Boeing Co
Original Assignee
Boeing Co
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=35432683&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE602005018230(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Publication of DE602005018230D1 publication Critical patent/DE602005018230D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/44Varying camber
    • B64C3/50Varying camber by leading or trailing edge flaps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/26Transmitting means without power amplification or where power amplification is irrelevant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/30Wing lift efficiency
DE602005018230T 2004-09-08 2005-09-07 Systeme und verfahren zur bereitstellung von differenzieller bewegung für flügelhochauftriebsvorrichtungen Active DE602005018230D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/935,846 US7494094B2 (en) 2004-09-08 2004-09-08 Aircraft wing systems for providing differential motion to deployable lift devices
PCT/US2005/031659 WO2006029132A1 (en) 2004-09-08 2005-09-07 Systems and methods for providing differential motion to wing high lift devices

Publications (1)

Publication Number Publication Date
DE602005018230D1 true DE602005018230D1 (de) 2010-01-21

Family

ID=35432683

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005018230T Active DE602005018230D1 (de) 2004-09-08 2005-09-07 Systeme und verfahren zur bereitstellung von differenzieller bewegung für flügelhochauftriebsvorrichtungen

Country Status (6)

Country Link
US (2) US7494094B2 (de)
EP (1) EP1786667B2 (de)
AT (1) ATE451300T1 (de)
CA (1) CA2578800C (de)
DE (1) DE602005018230D1 (de)
WO (1) WO2006029132A1 (de)

Families Citing this family (56)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US7424350B2 (en) * 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
DE102004040313B4 (de) * 2004-08-19 2008-02-21 Airbus Deutschland Gmbh System zum Einstellen der spannweitigen Lastverteilung eines Tragflügels
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
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
WO2007120199A2 (en) 2005-11-09 2007-10-25 Morgan Aircraft, Llc Aircraft attitude control configuration
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
FR2901537B1 (fr) * 2006-05-29 2008-07-04 Airbus France Sas Procede et dispositif de pilotage d'un aeronef optimisant la commande des ailerons en configuration hypersustentee
DE102006053259A1 (de) * 2006-11-11 2008-05-21 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs und Verfahren zu seiner Betätigung
US7641152B2 (en) * 2007-04-13 2010-01-05 The Boeing Company Dynamic adjustment of wing surfaces for variable camber
DE102007045547A1 (de) * 2007-09-24 2009-04-16 Airbus Deutschland Gmbh Automatische Steuerung eines Hochauftriebssystems eines Flugzeugs
GB0722415D0 (en) * 2007-11-15 2007-12-27 Airbus Uk Ltd Aircraft wing and flap deployment system
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
DE102008022092A1 (de) * 2008-05-05 2009-11-19 Airbus Deutschland Gmbh Fehlertolerantes Stellsystem zur Verstellung von Klappen eines Flugzeugs mit einer Verstell-Kinematik mit feststehender Drehachse
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
GB0906270D0 (en) 2009-04-14 2009-05-20 Ge Aviat Systems Ltd High lift devices for aircraft
DE102009017653A1 (de) * 2009-04-16 2010-10-21 Airbus Deutschland Gmbh Hochauftriebssystem eines Flugzeugs, Flugzeugsystem und Propeller-Flugzeug mit einem Hochauftriebssystem
FR2947242B1 (fr) * 2009-06-24 2013-02-22 Airbus Procede et dispositif d'equilibrage lateral en vol d'un avion
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
US9327824B2 (en) * 2010-12-15 2016-05-03 The Boeing Company Adjustment of wings for variable camber for optimum take-off and landing
FR2979615B1 (fr) * 2011-09-04 2013-09-20 Eric Chantriaux Aeronef equipe d'un groupe electromoteur distribue a roues libres.
DE102012022287A1 (de) 2012-11-14 2014-05-15 Liebherr-Aerospace Lindenberg Gmbh Vorrichtung zur Verstellung von Klappen von Tragflächen von Luftfahrzeugen
US9327827B2 (en) 2013-09-24 2016-05-03 The Boeing Company Leading and trailing edge device deflections during descent of an aircraft
US9771141B2 (en) 2013-09-24 2017-09-26 The Boeing Company Leading edge system and method for approach noise reduction
US10017243B2 (en) * 2013-09-24 2018-07-10 The Boeing Company Adaptive trailing edge actuator system and method
US9193440B2 (en) * 2013-09-24 2015-11-24 The Boeing Company Variable camber flap system and method
US9656741B2 (en) * 2013-09-24 2017-05-23 The Boeing Company Control interface for leading and trailing edge devices
US9296475B2 (en) 2013-09-24 2016-03-29 The Boeing Company System and method for reducing the stopping distance of an aircraft
US9359065B2 (en) 2013-09-24 2016-06-07 The Boeing Company System and method for optimizing performance of an aircraft
US9180962B2 (en) 2013-09-24 2015-11-10 The Boeing Company Leading edge variable camber system and method
US9254909B2 (en) * 2013-09-24 2016-02-09 The Boeing Company Optimized flap positioning for go-around operations
CN105939929B (zh) 2014-01-31 2019-05-03 庞巴迪公司 用于致动飞行控制表面的设备和方法
US9821903B2 (en) 2014-07-14 2017-11-21 The Boeing Company Closed loop control of aircraft control surfaces
US9623957B2 (en) * 2014-08-26 2017-04-18 The Boeing Company Torque tube door
US10196131B2 (en) * 2016-02-16 2019-02-05 The Boeing Company Hydraulic system and method for an aircraft flight control system
FR3052251B1 (fr) * 2016-06-03 2018-05-18 Airbus Operations (S.A.S.) Procede d'optimisation des parametres de decollage d'un aeronef
US10669014B2 (en) * 2016-12-02 2020-06-02 The Boeing Company Differential for control surface actuators
CN107187579A (zh) * 2017-05-22 2017-09-22 北京航空航天大学 一种适用于多翼面飞机布局的气动力和力矩控制方法
US10766602B2 (en) * 2017-11-01 2020-09-08 The Boeing Company Mechanical droop for spoiler operation
EP3495258A1 (de) * 2017-12-06 2019-06-12 Airbus Operations GmbH Flügel für ein flugzeug
CA3037923A1 (en) * 2018-03-29 2019-09-29 Bombardier Inc. System and method for improving the operation of an aircraft
US11001371B2 (en) * 2018-08-07 2021-05-11 The Boeing Company Hydraulic droop control for aircraft wing
CN110877714A (zh) * 2018-09-04 2020-03-13 庞巴迪公司 具有离合器架构的高升力致动系统
EP3653493B1 (de) * 2018-11-16 2023-01-18 Bombardier Inc. Hochauftriebsbetätigungssystem mit zentralisierter innenaktuatorensteuerung und unabhängiger aussenaktuatorensteuerung
EP3653494A1 (de) * 2018-11-16 2020-05-20 Bombardier Inc. Hochauftriebsbetätigungssystem mit unabhängiger betätigungssteuerung
WO2021062229A1 (en) 2019-09-26 2021-04-01 Joby Aero, Inc. Three-dimensional extension linkage
US11608161B2 (en) * 2020-04-08 2023-03-21 The Boeing Company Flap actuation systems and related methods
US11370527B2 (en) * 2020-06-08 2022-06-28 The Boeing Company Variable camber trim units, aircraft comprising the same, and associated methods of operation
US11370528B2 (en) * 2020-06-08 2022-06-28 The Boeing Company Variable camber trim units, aircraft comprising the same, and associated methods of operation
US20230348043A1 (en) * 2022-05-02 2023-11-02 The Boeing Company Systems and methods for controlling a flight control surface of an aircraft

Family Cites Families (336)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2899152A (en) 1959-08-11 Aircraft control surface operating mechanism
US2563453A (en) 1951-08-07 Device fob controlling the trailing
DE387833C (de) 1921-05-27 1924-01-04 Handley Page Ltd Tragfluegel fuer Flugzeuge
US1770575A (en) 1927-12-03 1930-07-15 Ksoll Joseph Aeroplane with supporting surface subdivided by gaps
US1724456A (en) 1928-04-24 1929-08-13 Louis H Crook Aerodynamic control of airplane wings
FR705155A (fr) 1930-11-05 1931-06-02 Perfectionnements apportés aux engins de navigation aérienne
US2086085A (en) 1935-05-14 1937-07-06 Handley Page Ltd Aircraft control gear
US2169416A (en) 1936-06-12 1939-08-15 United Aircraft Corp Slotted deflector flap
US2282516A (en) 1938-07-11 1942-05-12 Messerschmitt Boelkow Blohm Airplane wing structure
US2347230A (en) * 1938-12-16 1944-04-25 Daniel R Zuck Airplane with nonstalling and glide angle control characteristics
US2378528A (en) 1939-05-17 1945-06-19 Arsandaux Louis Supporting element for aircraft
US2358985A (en) 1940-02-23 1944-09-26 James P Mcandrew Aircraft
US2289704A (en) 1940-02-26 1942-07-14 Charles H Grant Aircraft wing
US2389274A (en) 1941-02-04 1945-11-20 Lockheed Aircraft Corp Aircraft control system
US2422296A (en) 1941-08-22 1947-06-17 Curtiss Wright Corp Slat and flap control system
US2319383A (en) 1942-01-19 1943-05-18 Edward F Zap Linkage mounting for aerodynamic members
US2383102A (en) 1942-02-13 1945-08-21 Edward F Zap Aerodynamic member
US2385351A (en) 1942-06-23 1945-09-25 Jess S W Davidsen Control system for hydraulically actuated devices
US2458900A (en) * 1942-08-10 1949-01-11 Curtiss Wright Corp Flap operating means
FR978969A (fr) 1942-12-29 1951-04-20 Perfectionnement aux avions à ailes à fente hypersustentatrice
US2387492A (en) 1943-03-22 1945-10-23 Curtiss Wright Corp Hydraulically operated split flap
US2518854A (en) * 1943-06-14 1950-08-15 Douglas Aircraft Co Inc Wing high lift flap device
US2444293A (en) 1943-06-18 1948-06-29 Curtiss Wright Corp Gap seal for flaps
FR984443A (fr) 1943-09-24 1951-07-05 Aile hypersustentatrice
US2406475A (en) 1944-02-19 1946-08-27 Samuel H Pearis Slotted airplane wing
US2504684A (en) * 1946-01-30 1950-04-18 Goodrich Co B F Extensible structure for varying the configuration of an aircraft surface
FR61015E (de) 1946-12-03 1955-03-23
US2555862A (en) 1947-05-23 1951-06-05 Onera (Off Nat Aerospatiale) High-lift appliance for largely sweptback wings
US2665084A (en) * 1949-11-14 1954-01-05 Northrop Aircraft Inc Flap actuator and control system
US2665085A (en) * 1950-06-13 1954-01-05 Blackburn & Gen Aircraft Ltd Selective dual aileron control for aircraft
US2652812A (en) 1952-05-13 1953-09-22 Gen Electric Combined manual and automatic hydraulic servomotor apparatus
US2886008A (en) 1953-08-03 1959-05-12 Gen Motors Corp Locking actuator and valve mechanism therefor
US2877968A (en) * 1954-10-28 1959-03-17 Gen Electric Combined manual and automatic servomotor apparatus
US2851229A (en) 1956-05-03 1958-09-09 Chance Vought Aircraft Inc Variable-contour airfoil
US2864239A (en) 1956-10-04 1958-12-16 Sperry Rand Corp Electro-hydraulic servo system for steering dirigible craft
US2990144A (en) 1956-11-05 1961-06-27 Gen Electric Integrated hydraulic power actuator
US2990145A (en) 1956-11-05 1961-06-27 Gen Electric Integrated hydraulic power actuator
US2920844A (en) * 1957-04-12 1960-01-12 North American Aviation Inc Aircraft boundary-layer control system
US2891740A (en) 1957-06-27 1959-06-23 John P Campbell External-flow jet flap
US2938680A (en) 1957-07-02 1960-05-31 North American Aviation Inc Multiple position airfoil slat
US2892312A (en) 1958-01-27 1959-06-30 Deere & Co Demand compensated hydraulic system
US2912190A (en) 1958-05-05 1959-11-10 Chance Vought Aircraft Inc Variable-contour airfoil
US3013748A (en) 1959-03-11 1961-12-19 Douglas Aircraft Co Inc Aircraft flap supporting and operating mechanism
GB886136A (en) 1960-01-20 1962-01-03 Smith & Sons Ltd S Improvements in or relating to visual indicating devices for use in aircraft
US3112089A (en) 1960-10-12 1963-11-26 Dornier Werke Gmbh Airplane wing flaps
DE1129379B (de) 1960-11-11 1962-05-10 Dornier Werke Gmbh Flugzeugtragfluegel mit festem Vorfluegel
US3102607A (en) 1960-12-19 1963-09-03 Charles E Roberts Carrier system for transport and delivery along a trackway
US3089666A (en) 1961-04-13 1963-05-14 Boeing Co Airplane having changeable thrust direction
US3203647A (en) 1961-12-06 1965-08-31 Alvarez-Calderon Alberto High lift fdaps for aircraft wings
US3375998A (en) * 1962-04-16 1968-04-02 Alberto Alvarez Calderon Leading edge flap and apparatus thereof
US3166271A (en) * 1962-08-20 1965-01-19 Daniel R Zuck Airplane having non-stalling wings and wing-mounted propellers
US3203275A (en) 1962-11-26 1965-08-31 Vaino A Hoover Mechanical actuator
US3136504A (en) 1963-07-02 1964-06-09 William F Carr Electrical primary flight control system
US3263946A (en) * 1964-08-19 1966-08-02 Boeing Co Drive mechanism
US3282535A (en) 1964-11-12 1966-11-01 Boeing Co Leading edge spoiler and flap wing stall control means
GB1083267A (en) 1964-12-11 1967-09-13 Power Jets Res & Dev Ltd Flap systems for aircraft
US3423858A (en) * 1967-01-10 1969-01-28 Speno International Automatic control system for railway work apparatus
GB1181991A (en) 1967-04-14 1970-02-18 Edward M Lanier Aircraft Lift-Increasing Device
GB1227316A (de) 1967-05-16 1971-04-07
US3504870A (en) * 1967-12-08 1970-04-07 Boeing Co Aircraft wing variable camber leading edge flap
US3463418A (en) 1968-03-20 1969-08-26 Edmond S Miksch Vortex generator for airplane wing
US3539133A (en) * 1968-05-20 1970-11-10 Robertson Aircraft Corp Inherently stable tapered wing flaperon airplane
US3659810A (en) * 1968-05-20 1972-05-02 James L Robertson Inherently stable tapered wing flaperon airplane
US3556439A (en) * 1968-11-22 1971-01-19 Boeing Co Methods and high lift systems for making an aircraft wing more efficient for takeoffs and landings
FR1601027A (de) * 1968-12-30 1970-08-03
US3589648A (en) 1969-01-02 1971-06-29 Lockheed Aircraft Corp Means for controlling the vertical path of an aircraft
US3587311A (en) 1969-06-19 1971-06-28 Teledyne Inc Aircraft instrument system
GB1308445A (en) 1969-07-21 1973-02-21 Baker Perkins Ltd Manufacture of foundry mixtures in the production of foundry moulds and cores
DE1943680C2 (de) 1969-08-28 1982-06-24 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Steuerklappenanordnung
US3730459A (en) 1969-09-18 1973-05-01 D Zuck Airplane with floating wing and reverse propeller thrust
FR2064681A5 (de) * 1969-10-13 1971-07-23 Onera (Off Nat Aerospatiale)
DE1962956C3 (de) 1969-12-16 1975-09-04 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Einrichtung zum Ab- und Umlenken des Strahls von Schub- und Hubgebläsen
US3653611A (en) * 1970-03-24 1972-04-04 Mason Trupp Slotted delta wing aircraft
US3704843A (en) 1970-06-11 1972-12-05 Mc Donnell Douglas Corp Aircraft control system
US3711039A (en) * 1970-10-26 1973-01-16 Boeing Co Pneumatic leading edge flap for an aircraft wing
US3743219A (en) 1971-06-30 1973-07-03 Boeing Co High lift leading edge device
GB1404762A (en) * 1971-10-07 1975-09-03 Lucas Industries Ltd Electro-hydraulic actuating systems for aircraft control surfaces
US3813062A (en) 1971-10-12 1974-05-28 A Prather Fan-like tail section for man-powered glider aircraft
US3767140A (en) 1971-11-03 1973-10-23 Mc Donnell Douglas Corp Airplane flaps
DE2309116C3 (de) * 1972-02-24 1975-06-12 Daikin Kogyo Co. Ltd., Osaka (Japan) Verteilereinrichtung für die Druckmittelzufuhr bei hydrostatischen Getrieben
US3804267A (en) * 1972-04-03 1974-04-16 Sperry Rand Corp Bale wagon
US3993584A (en) 1972-12-20 1976-11-23 The Harshaw Chemical Company Agglomerate containing fibrous polytetrafluoroethylene
US3831886A (en) 1973-01-26 1974-08-27 Lockheed Aircraft Corp Airfoil with extendible and retractable leading edge
US3837601A (en) 1973-03-09 1974-09-24 Boeing Co Aerodynamic slot closing mechanism
US3827658A (en) 1973-04-05 1974-08-06 Lockheed Aircraft Corp Actuating means for a vane
US3913450A (en) 1973-05-11 1975-10-21 Dreis & Krump Manufacturing Co Hydraulic Control system for press brakes or the like
US3917192A (en) 1973-07-09 1975-11-04 Alvarez Calderon Alberto Flap mechanisms and apparatus
US3897029A (en) 1973-07-09 1975-07-29 Alberto Alvarez Calderon Variable camber multi-slotted flaps
US3836099A (en) 1973-09-28 1974-09-17 Us Navy Airfoil camber change system
US3862730A (en) * 1973-10-23 1975-01-28 United Aircraft Corp Fas actuation system
FR2249804B1 (de) * 1973-11-06 1976-10-01 Aerospatiale
US3910530A (en) 1973-11-07 1975-10-07 Boeing Co Leading edge flap
US3904152A (en) 1974-03-13 1975-09-09 Lockheed Aircraft Corp Variable area, variable camber wing for aircraft
US3994451A (en) 1974-03-28 1976-11-30 The Boeing Company Variable camber airfoil
US3874617A (en) * 1974-07-17 1975-04-01 Mc Donnell Douglas Corp Stol flaps
US3941341A (en) * 1974-12-13 1976-03-02 Brogdon Jr Glenn F Quick-release roller attachment for supporting a rope or hose and the like on an aerial ladder
US3987983A (en) 1974-12-20 1976-10-26 The Boeing Company Trailing edge flaps having spanwise aerodynamic slot opening and closing mechanism
US3992979A (en) 1974-12-20 1976-11-23 Joseph Lucas (Industries) Limited Hydraulic actuating arrangements
US3991574A (en) 1975-02-03 1976-11-16 Frazier Larry Vane W Fluid pressure power plant with double-acting piston
US3985319A (en) * 1975-02-03 1976-10-12 The Boeing Company Variable pivot trailing edge flap
US3941334A (en) * 1975-03-28 1976-03-02 The Boeing Company Variable camber airfoil
US3968946A (en) 1975-03-31 1976-07-13 The Boeing Company Extendable aerodynamic fairing
US4074878A (en) 1975-06-23 1978-02-21 Sherman Irving R Programmed flap system for an aircraft having wings
US4015787A (en) * 1975-11-17 1977-04-05 Fairchild Industries Inc. Aircraft wing
US4011888A (en) 1976-03-12 1977-03-15 Elevator Equipment Co. Unitary elevator up level control valve
US4120470A (en) 1976-09-28 1978-10-17 The Boeing Company Efficient trailing edge system for an aircraft wing
US4106730A (en) * 1976-10-01 1978-08-15 The Boeing Company Engine out control system for STOL aircraft
US4180222A (en) * 1976-12-27 1979-12-25 Lockheed Aircraft Corporation Aileron segment control for a flaperon system
GB1596642A (en) * 1977-04-06 1981-08-26 British Aerospace Aircraft wings
DE2725632C2 (de) * 1977-06-07 1982-11-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Querruder und Landeklappenantrieb für ein FLugzeug
US4131253A (en) 1977-07-21 1978-12-26 The Boeing Company Variable camber trailing edge for airfoil
US4171787A (en) 1977-07-21 1979-10-23 Zapel Edwin J Variable camber leading edge for airfoil
US4146200A (en) * 1977-09-14 1979-03-27 Northrop Corporation Auxiliary flaperon control for aircraft
DE2751361C2 (de) 1977-11-17 1984-09-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zur Flugzeugsteuerung durch Steuerung abgelöster Flügelvorderkanten-Wirbelströme
US4189120A (en) * 1977-12-14 1980-02-19 Boeing Commercial Airplane Company Variable camber leading edge flap
US4189121A (en) * 1978-01-23 1980-02-19 Boeing Commercial Airplane Company Variable twist leading edge flap
FR2427499A1 (fr) 1978-06-01 1979-12-28 Sarrazin Applic Hydr Dispositif de commande integre pour circuit de fluide, et ses applications
US4479620A (en) * 1978-07-13 1984-10-30 The Boeing Company Wing load alleviation system using tabbed allerons
US4189122A (en) * 1978-07-21 1980-02-19 The United States Of America As Represented By The Secretary Of The Navy Wide angle gimbal system
US4325123A (en) * 1978-07-28 1982-04-13 The Boeing Company Economy performance data avionic system
US4202519A (en) * 1978-09-08 1980-05-13 The Boeing Company Airfoil leading edge slat apparatus
US4275942A (en) 1978-12-26 1981-06-30 The Boeing Company Stowage bin 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
US4293110A (en) 1979-03-08 1981-10-06 The Boeing Company Leading edge vortex flap for wings
US4262868A (en) * 1979-05-29 1981-04-21 The Boeing Company Three-position variable camber flap
US4285482A (en) 1979-08-10 1981-08-25 The Boeing Company Wing leading edge high lift device
US4312486A (en) * 1979-09-20 1982-01-26 The Boeing Company Variable camber trailing edge for airfoil
US4360176A (en) 1979-11-05 1982-11-23 The Boeing Company Wing leading edge slat
US4461449A (en) 1980-05-01 1984-07-24 The Boeing Company Integral hydraulic blocking and relief valve
US4351502A (en) 1980-05-21 1982-09-28 The Boeing Company Continuous skin, variable camber airfoil edge actuating mechanism
US4358077A (en) 1980-06-16 1982-11-09 Coronel Paul K Transverse wing actuation system
US4363098A (en) * 1980-06-24 1982-12-07 The Boeing Company Electric command spoiler system
US4365774A (en) 1980-08-08 1982-12-28 Coronel Paul K Convertible delta wing aircraft
US4353517A (en) 1980-10-07 1982-10-12 The Boeing Company Flap assembly for aircraft wing
FR2492337A1 (fr) 1980-10-16 1982-04-23 Aerospatiale Aile d'aeronef pourvue d'un systeme hypersustentateur dans son bord d'attaque et aeronef comportant une telle aile
US4368937A (en) * 1981-02-17 1983-01-18 The Boeing Company Overhead stowage bin mechanism
US4459084A (en) 1981-05-26 1984-07-10 Clark Garry E Internal combustion driven pumping system and variable torque transmission
US4498646A (en) * 1981-07-01 1985-02-12 Dornier Gmbh Wing for short take-off and landing aircraft
US4485992A (en) 1981-09-10 1984-12-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Leading edge flap system for aircraft control augmentation
US4472780A (en) * 1981-09-28 1984-09-18 The Boeing Company Fly-by-wire lateral control system
US4471927A (en) 1981-09-29 1984-09-18 The Boeing Company Trailing edge flap assembly
US4427168A (en) * 1981-09-29 1984-01-24 The Boeing Company Variable camber leading edge mechanism with Krueger flap
DE3140350A1 (de) 1981-10-10 1983-04-28 Dornier Gmbh, 7990 Friedrichshafen Profile, insbesondere tragfluegelprofile fuer luftfahrzeuge
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
DE3149629C1 (de) 1981-12-15 1983-04-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum Abdichten eines Luftspaltes an einer Flugzeugklappe
US4700911A (en) 1982-02-09 1987-10-20 Dornier Gmbh Transverse driving bodies, particularly airplane wings
US4441675A (en) * 1982-06-25 1984-04-10 Mcdonnell Douglas Corporation High lift surface actuation system
DE3275176D1 (en) 1982-08-09 1987-02-26 Boeing Co Wing leading edge slat
US4747375A (en) 1982-08-31 1988-05-31 Williams John K Device for controlling the phased displacement of rotating shafts
EP0103038A1 (de) 1982-09-13 1984-03-21 The Boeing Company Antriebmechanismus für veränderbares Flügelprofil mit durchgehender Haut
US4575030A (en) * 1982-09-13 1986-03-11 The Boeing Company Laminar flow control airfoil
US4496121A (en) * 1982-09-21 1985-01-29 The Boeing Company Control surface lock for flutter constraint
SE434762B (sv) 1982-11-29 1984-08-13 Ingemanssons Ingenjorsbyra Ab Tetningsanordning vid troskellos dorr
US4712752A (en) 1982-12-06 1987-12-15 The Boeing Company Wing trailing edge air dam
US4475702A (en) 1982-12-28 1984-10-09 The Boeing Company Variable camber leading edge assembly for an airfoil
US4706913A (en) 1982-12-28 1987-11-17 The Boeing Company Variable camber leading edge assembly for an airfoil
US4553722A (en) 1982-12-30 1985-11-19 The Boeing Company Variable-camber airfoil
US4533096A (en) 1982-12-30 1985-08-06 The Boeing Company High lift system control assembly
US4729528A (en) * 1983-02-28 1988-03-08 Northrop Corporation Aeroelastic control flap
US4542869A (en) 1983-06-23 1985-09-24 Mcdonnell Douglas Corporation Flap mechanism
GB8321281D0 (en) 1983-08-06 1983-09-28 British Aerospace Underwing engine installation
US4544117A (en) 1983-11-14 1985-10-01 Lockheed Corporation Leading edge flap and boundary layer control system
FR2555960B1 (fr) * 1983-12-06 1986-09-19 Aerospatiale Aile d'aeronef en fleche pourvue d'un systeme hypersustentateur et d'un mat de suspension de moteur, ainsi que mat de suspension de moteur pour une telle aile
US4575099A (en) * 1984-01-27 1986-03-11 General Electric Company High excursion seal with flexible membrane to prevent gas leakage through hinge
US4899284A (en) * 1984-09-27 1990-02-06 The Boeing Company Wing lift/drag optimizing system
US4576347A (en) * 1984-10-30 1986-03-18 The Boeing Company Flap torque tube slot seal
US4702441A (en) 1984-12-31 1987-10-27 The Boeing Company Aircraft wing stall control device and method
US5082207A (en) * 1985-02-04 1992-01-21 Rockwell International Corporation Active flexible wing aircraft control system
DE3530865A1 (de) * 1985-08-29 1987-03-12 Messerschmitt Boelkow Blohm Antriebs- und fuehrungsvorrichtung fuer ein an einem flugzeugtragfluegel angeordnetes klappensystem
EP0218021B1 (de) * 1985-08-29 1988-06-08 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Klappenanordnung für einen Flugzeugtragflügel
US4796192A (en) * 1985-11-04 1989-01-03 The Boeing Company Maneuver load alleviation system
US4650140A (en) * 1985-12-30 1987-03-17 The Boeing Company Wind edge movable airfoil having variable camber
US4717097A (en) * 1986-03-03 1988-01-05 The Boeing Company Aircraft wings with aileron-supported ground speed spoilers and trailing edge flaps
US4779822A (en) * 1986-05-23 1988-10-25 Sundstrand Corporation Actuator system
US4691879A (en) 1986-06-16 1987-09-08 Greene Vibert F Jet airplane
DE3620886A1 (de) 1986-06-21 1988-01-14 Messerschmitt Boelkow Blohm Antriebseinrichtung mit variablem drehmoment-begrenzungssystem
FR2606363B1 (fr) * 1986-11-07 1989-03-03 Aerospatiale Systeme pour la commande des volets hypersustentateurs d'un aeronef
US4784355A (en) 1986-11-10 1988-11-15 The United States Of America As Represented By The Secretary Of The Air Force Flap system for short takeoff and landing aircraft
DE3641247A1 (de) 1986-12-03 1988-06-16 Messerschmitt Boelkow Blohm Landeklappenfuehrungsschienen-verkleidung fuer luftfahrzeuge
GB8711252D0 (en) 1987-05-13 1987-07-15 British Aerospace High lift device
US5100082A (en) * 1987-09-17 1992-03-31 The Boeing Company Hydraulic power supplies
US4834319A (en) * 1987-10-05 1989-05-30 Allied-Signal Inc. Differentially coupled dual channel actuator
US5074495A (en) 1987-12-29 1991-12-24 The Boeing Company Load-adaptive hybrid actuator system and method for actuating control surfaces
US4823836A (en) * 1988-05-31 1989-04-25 Lothar Bachmann Dampers with leaf spring seals
US4867394A (en) 1988-06-23 1989-09-19 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Compression pylon
US5046688A (en) 1988-10-28 1991-09-10 The Boeing Company Wing major assembly jig
US5039032A (en) 1988-11-07 1991-08-13 The Boeing Company High taper wing tip extension
US4991800A (en) * 1988-11-14 1991-02-12 Sundstrand Corporation Backdrive control system for aircraft flight control surfaces
US5050081A (en) 1988-11-14 1991-09-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method and system for monitoring and displaying engine performance parameters
GB8827345D0 (en) 1988-11-23 1988-12-29 Smiths Industries Plc Aircraft instrument systems
DE59001679D1 (de) 1989-02-06 1993-07-15 Airbus Gmbh Decken-gepaeckablagen-kombination fuer die passagierkabine eines flugzeuges.
US4962902A (en) 1989-03-20 1990-10-16 The Boeing Company Aircraft control surface linkage
GB8915487D0 (en) 1989-07-06 1989-08-23 Short Brothers Plc A flap assembly
DE3930862A1 (de) 1989-09-15 1991-03-28 Vdo Schindling Verfahren und einrichtung zur darstellung von flugfuehrungsinformation
US5056741A (en) * 1989-09-29 1991-10-15 The Boeing Company Apparatus and method for aircraft wing stall control
US5082208A (en) * 1989-09-29 1992-01-21 The Boeing Company System and method for controlling an aircraft flight control member
US5094412A (en) * 1989-10-13 1992-03-10 Bell Helicopter Textron Inc. Flaperon system for tilt rotor wings
US5088665A (en) * 1989-10-31 1992-02-18 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Serrated trailing edges for improving lift and drag characteristics of lifting surfaces
US5114100A (en) 1989-12-29 1992-05-19 The Boeing Company Anti-icing system for aircraft
US5167383A (en) 1990-08-18 1992-12-01 Yoshio Nozaki STOL aircraft
US5094411A (en) * 1990-10-19 1992-03-10 Vigyan, Inc. Control configured vortex flaps
DE4033277A1 (de) * 1990-10-19 1992-04-23 Airbus Gmbh Antriebsvorrichtung fuer an flugzeugtragfluegeln angeordneten klappen
US5203619A (en) * 1990-11-07 1993-04-20 Intermetro Industries Corporation Storage system including a vertically retractable storage unit
GB9026451D0 (en) 1990-12-05 1991-01-23 Smiths Industries Plc Aircraft display systems
DE4105459A1 (de) 1991-02-21 1992-08-27 Heilmeier & Weinlein Hydraulische steuervorrichtung
JPH07112836B2 (ja) 1991-06-14 1995-12-06 富士重工業株式会社 航空機の油圧操舵装置
DE4130644A1 (de) 1991-09-14 1993-03-18 Airbus Gmbh Ueberkopf-gepaeckablage mit einer absenkbaren schale, insbesondere fuer ein passagierflugzeug
US5158252A (en) 1991-10-24 1992-10-27 The Boeing Company Three-position variable camber Krueger leading edge flap
US5280863A (en) * 1991-11-20 1994-01-25 Hugh Schmittle Lockable free wing aircraft
GB9201762D0 (en) 1992-01-28 1992-03-11 Wes Technology Inc Seals for gas isolators
DE4209037C2 (de) 1992-03-20 1994-06-23 Deutsche Aerospace Airbus Vorrichtung zur Aufnahme von Gepäck in Flugzeugen
US5681014A (en) 1992-05-15 1997-10-28 Palmer; Harry W. Torsional twist airfoil control means
US5493497A (en) * 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
FR2695905B1 (fr) 1992-09-24 1994-12-16 Aerospatiale Bec kruger rigide, pour bord d'attaque de voilure d'aéronef.
US5310387A (en) * 1992-09-30 1994-05-10 Hughes Aircraft Company Differential motor drive
US5282591A (en) * 1992-12-21 1994-02-01 The United States Of America As Represented By The Secretary Of The Navy Active vortex control for a high performance wing
FR2709110B1 (fr) * 1993-08-20 1995-11-10 Lucas Air Equipement Dispositif de servocommande d'un organe de commande de vol d'aéronef.
US5544847A (en) 1993-11-10 1996-08-13 The Boeing Company Leading edge slat/wing combination
US5388788A (en) * 1993-12-16 1995-02-14 The Boeing Company Hinge fairings for control surfaces
DE4422152C2 (de) * 1994-06-27 2000-02-03 Daimler Chrysler Aerospace Verfahren und Anordnung zum Optimieren der aerodynamischen Wirkung eines Tragflügels
US5535852A (en) 1994-08-17 1996-07-16 Bishop; David J. Lift apparatus
FR2728535A1 (fr) * 1994-12-26 1996-06-28 Aerospatiale Aerofrein a fente variable pour voilure d'aeronef
US5680124A (en) 1995-05-15 1997-10-21 The Boeing Company Skew and loss detection system for adjacent high lift devices
US5609020A (en) * 1995-05-15 1997-03-11 The Boeing Company Thrust reverser synchronization shaft lock
US5686907A (en) 1995-05-15 1997-11-11 The Boeing Company Skew and loss detection system for individual high lift devices
US5711496A (en) * 1995-06-30 1998-01-27 Nusbaum; Steve R. STOL aircraft and wing slat actuating mechanism for same
US5681013A (en) 1995-12-26 1997-10-28 The Boeing Company Vortex leading edge flap assembly for supersonic airplanes
US5915653A (en) 1996-01-02 1999-06-29 The Boeing Company Spherical mating fairings for hingeline applications
US5875998A (en) * 1996-02-05 1999-03-02 Daimler-Benz Aerospace Airbus Gmbh Method and apparatus for optimizing the aerodynamic effect of an airfoil
US5743490A (en) * 1996-02-16 1998-04-28 Sundstrand Corporation Flap/slat actuation system for an aircraft
JPH11509804A (ja) * 1996-04-13 1999-08-31 マイケル クレイグ ブロードベント 可変キャンバーウイング機構
US5927656A (en) 1996-06-26 1999-07-27 The Boeing Company Wing leading edge flap and method therefor
SE507968C2 (sv) 1996-07-25 1998-08-03 Electrolux Ab Bäranordning, t.ex. för väggmonterad hushållsugn
GB9619488D0 (en) 1996-09-18 1996-10-30 Dowty Boulton Paul Ltd Flight control surface actuation system
US5746490A (en) 1996-10-02 1998-05-05 Grass America, Inc. Drawer guide support bracket
DE19643222C2 (de) 1996-10-19 1998-12-10 Daimler Benz Ag Auftriebskörper mit veränderbarer Wölbung
WO1998017529A1 (en) 1996-10-22 1998-04-30 The Boeing Company Airplane with unswept slotted cruise wing airfoil
US5788190A (en) 1996-10-22 1998-08-04 The Boeing Company Slotted cruise trailing edge flap
JP3638745B2 (ja) * 1997-02-07 2005-04-13 富士重工業株式会社 ロータリスポイラ付ロータブレード
DE19712034A1 (de) 1997-03-21 1998-09-24 Deutsch Zentr Luft & Raumfahrt Profilkante eines aerodynamischen Profils
GB2323576B (en) 1997-03-26 2001-08-22 British Aerospace Fairing arrangements for aircraft
US6082679A (en) * 1997-06-26 2000-07-04 The Boeing Company Active system for early destruction of trailing vortices
US5934615A (en) 1997-08-25 1999-08-10 Hexcel Corporation Luggage bins with articulating mechanism
US7455264B2 (en) 1997-08-26 2008-11-25 Mcdonnell Douglas Corporation Reconfiguration control system for an aircraft wing
US6209824B1 (en) * 1997-09-17 2001-04-03 The Boeing Company Control surface for an aircraft
US5978715A (en) 1997-10-15 1999-11-02 Dassault Aviation Apparatus and method for aircraft display and control
US5839698A (en) 1997-10-23 1998-11-24 Northrop Grumman Corporation Control surface continuous seal
US6085129A (en) 1997-11-14 2000-07-04 Rockwell Collins, Inc. Integrated vertical profile display
US5984230A (en) 1997-12-15 1999-11-16 Orazi; Paul Wing assemblies for aircraft
US6079672A (en) * 1997-12-18 2000-06-27 Lam; Lawrence Y. Aileron for fixed wing aircraft
US6145791A (en) 1998-01-09 2000-11-14 Northrop Grumman Corporation Elastomeric transition for aircraft control surface
ES2156660B1 (es) 1998-01-14 2002-02-16 Saiz Manuel Munoz Mandos de vuelo con compensacion automatica.
US7051982B1 (en) 1998-03-27 2006-05-30 Bae Systems Plc Fairing arrangements for aircraft
US6068219A (en) 1998-04-13 2000-05-30 Northrop Grumman Corporation Single surface multi axis aircraft control
DE19819341C2 (de) 1998-04-30 2000-06-15 Daimler Chrysler Aerospace Verfahren zur Reduktion von an einem Flugzeug auftretenden Böenlasten unterhalb der Reiseflughöhe
DE69916360T3 (de) * 1998-05-21 2008-06-05 Mcdonnell Douglas Corp. Flügelprofil
US6045204A (en) * 1998-10-13 2000-04-04 Hexcel Corporation Overhead stowage bins in aircraft
GB9823599D0 (en) * 1998-10-28 1998-12-23 Lucas Ind Plc Brake assembly
US6189837B1 (en) * 1998-10-29 2001-02-20 The Boeing Company Auxiliary spoiler retract system
DE19858872C2 (de) 1998-12-19 2001-02-08 Daimler Chrysler Ag Adaptiver Flugzeugtragflügel
FR2787759B1 (fr) 1998-12-28 2001-03-16 Aerospatiale Procede et systeme de commande d'une gouverne d'un aeronef a actionnement par verins hydrauliques multiples et a puissance modulable
US6382566B1 (en) * 1998-12-29 2002-05-07 The Boeing Company Method and apparatus for detecting skew and asymmetry of an airplane flap
US6466234B1 (en) 1999-02-03 2002-10-15 Microsoft Corporation Method and system for controlling environmental conditions
DE19910551C2 (de) * 1999-03-10 2001-04-05 Eads Airbus Gmbh Flugzeugtragfläche mit mindestens einem kurzgekoppelten Triebwerk
US6164598A (en) 1999-03-10 2000-12-26 Northrop Grumman Corporation Adaptive control surface apparatus
US6328265B1 (en) 1999-05-25 2001-12-11 Faruk Dizdarevic Slot forming segments and slot changing spoilers
US6173924B1 (en) * 1999-06-15 2001-01-16 Northrop Grumman Corporation Low density flexible edge transition
US6244542B1 (en) 1999-07-20 2001-06-12 Northrop Grumman Corporation Rotor driven edge
GB9920318D0 (en) 1999-08-27 1999-11-03 British Aerospace A fairing arrangement for an aircraft
US6466141B1 (en) 1999-09-28 2002-10-15 Lucas Industries Limited Skew detection system
DE10001038B4 (de) 2000-01-13 2004-01-29 Airbus Deutschland Gmbh Gepäckablage mit einem absenkbaren Gepäckfach, insbesondere für eine Flugzeugpassagierkabine
US6598834B2 (en) 2000-02-14 2003-07-29 Aerotech Services Inc. Method for reducing fuel consumption in aircraft
FR2806488B1 (fr) 2000-03-16 2002-05-17 Snecma Moteurs Dispositif et procede de regulation de pression et debit de carburant d'alimentation d'une unite de servovannes
DE10019187C1 (de) * 2000-04-17 2002-01-03 Airbus Gmbh Drucksteuerung für einen Verdrängungskörper
JP2001343032A (ja) 2000-06-01 2001-12-14 Komatsu Ltd クラッチ又はブレーキの流体圧力制御弁装置及び流体圧力制御方法
FR2811037B1 (fr) 2000-06-28 2002-10-18 Aerospatiale Matra Airbus Systeme d'actionnement hydraulique a commande electrique
US6431498B1 (en) 2000-06-30 2002-08-13 Philip Watts Scalloped wing leading edge
US6561463B1 (en) 2000-07-14 2003-05-13 Honeywell International Inc. Flight control module with integrated spoiler actuator control electronics
US6464175B2 (en) * 2000-07-14 2002-10-15 Honda Giken Kogyo Kabushiki Kaisha Rotor blade operating device in airplane and flaperon operating device in airplane
US6439512B1 (en) 2000-08-24 2002-08-27 Hr Textron, Inc. All-hydraulic powered horizontal stabilizer trim control surface position control system
US6980198B1 (en) 2000-09-19 2005-12-27 Honeywell International Inc. Multifunction keyboard for advanced cursor driven avionic flight decks
US6443394B1 (en) 2000-09-21 2002-09-03 The B.F. Goodrich Company Inflatable airfoil device
DE10055961B4 (de) 2000-11-11 2004-09-09 Eads Deutschland Gmbh Variabler Flügelbereich mit einstellbarer, sich in Spannweiten-Richtung erstreckender Profilform
US6375126B1 (en) * 2000-11-16 2002-04-23 The Boeing Company Variable camber leading edge for an airfoil
US6481667B1 (en) 2001-03-05 2002-11-19 Northrop Grumman Corporation System and method for deflecting an aerodynamic control surface
NL1017811C2 (nl) 2001-04-10 2002-10-11 Stork Prod Eng Handbagagebaksamenstel met onderdrukmiddelen.
US6547183B2 (en) * 2001-08-02 2003-04-15 The Boeing Company Moveable closet
US6478541B1 (en) 2001-08-16 2002-11-12 The Boeing Company Tapered/segmented flaps for rotor blade-vortex interaction (BVI) noise and vibration reduction
US6870490B2 (en) * 2001-08-23 2005-03-22 Honeywell International Inc. Display of altitude and path capture trajectories
US6591169B2 (en) 2001-09-27 2003-07-08 The Boeing Company Method and computer program product for controlling the actuators of an aerodynamic vehicle
US6622972B2 (en) 2001-10-31 2003-09-23 The Boeing Company Method and system for in-flight fault monitoring of flight control actuators
GB0127254D0 (en) * 2001-11-13 2002-01-02 Lucas Industries Ltd Aircraft flight surface control system
EP1338506A1 (de) 2002-02-15 2003-08-27 Fairchild Dornier GmbH Flugzeugflügel mit Spalt- und Krüger-Klappen
US6601801B1 (en) 2002-04-24 2003-08-05 The Boeing Company Gapped trailing-edge control surface for an airfoil
US6745113B2 (en) 2002-06-07 2004-06-01 The Boeing Company Method and system for autoflight information display
FR2840877B1 (fr) 2002-06-13 2004-08-06 Airbus France Dispositif d'articulation d'un volet sur une surface aerodynamique d'aeronef
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
US6698523B2 (en) * 2002-07-02 2004-03-02 Husco International, Inc. Electrohydraulic control system for implement lift cylinders
US6802475B2 (en) 2002-07-04 2004-10-12 Smiths Wolverhampton Limited Flight surface actuator
US6622974B1 (en) 2002-08-14 2003-09-23 The Boeing Company Geometric morphing wing with expandable spars
US6796534B2 (en) 2002-09-10 2004-09-28 The Boeing Company Method and apparatus for controlling airflow with a leading edge device having a flexible flow surface
US20040059474A1 (en) * 2002-09-20 2004-03-25 Boorman Daniel J. Apparatuses and methods for displaying autoflight information
US7048228B2 (en) 2002-10-09 2006-05-23 The Boeing Company Slotted aircraft wing
US7048235B2 (en) 2002-10-09 2006-05-23 The Boeing Company Slotted aircraft wing
US6755375B2 (en) * 2002-10-22 2004-06-29 The Boeing Company Method and apparatus for controlling aircraft devices with multiple actuators
ITBO20020724A1 (it) 2002-11-15 2004-05-16 L E A T S R L Metodo e sistema per l'acquisizione e la registrazione di dati relativi allo spostamento di un veicolo
US6796526B2 (en) 2002-11-25 2004-09-28 The Boeing Company Augmenting flight control surface actuation system and method
DE10313728B4 (de) * 2003-03-27 2011-07-21 Airbus Operations GmbH, 21129 Klappensystem am Tragflügel eines Starrflügel-Flugzeuges
US6827311B2 (en) * 2003-04-07 2004-12-07 Honeywell International, Inc. Flight control actuation system
CA2427416C (en) 2003-05-01 2010-11-16 101039130 Saskatchewan Ltd. Steering device for towed implements
ATE441590T1 (de) 2003-05-23 2009-09-15 Int Paper Co Einstückiger versandbehälter mit verschiedenartigen innen- und aussenwänden und einem schnellverschlussboden
US7243881B2 (en) * 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US7059563B2 (en) 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
DE10326799B3 (de) * 2003-06-13 2004-12-16 Airbus Deutschland Gmbh Vorrichtung zur Betätigung von Klappenelementen an den Tragflächen eines Flugzeuges
US6843452B1 (en) * 2003-06-17 2005-01-18 The Boeing Company Variable trailing edge geometry and spanload control
US6824099B1 (en) * 2003-07-10 2004-11-30 The Boeing Company Brake systems for aircraft wing flaps and other control surfaces
US7028948B2 (en) * 2003-08-28 2006-04-18 The Boeing Company Apparatus for increase of aircraft lift and maneuverability
FR2859976B1 (fr) * 2003-09-22 2006-12-08 Airbus France Aile d'aeronef comportant au moins un volet deporteur et volet deporteur pour ladite aile
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
DE10361891A1 (de) * 2003-12-23 2005-08-04 Airbus Deutschland Gmbh Vorrichtung zur Ansteuerung und Verstellung von Klappen an Flugzeugtragflächen
US7424350B2 (en) 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US7363119B2 (en) * 2004-03-10 2008-04-22 The Boeing Company Methods and systems for automatically displaying information, including air traffic control instructions
US20050242234A1 (en) * 2004-04-29 2005-11-03 The Boeing Company Lifters, methods of flight control and maneuver load alleviation
US7270305B2 (en) * 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
US6978971B1 (en) 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
US7007889B2 (en) * 2004-06-15 2006-03-07 Richard Charron Flexible airfoils and method
DE102004040313B4 (de) * 2004-08-19 2008-02-21 Airbus Deutschland Gmbh System zum Einstellen der spannweitigen Lastverteilung eines Tragflügels
DE102004047008A1 (de) * 2004-09-28 2006-03-30 Liebherr-Aerospace Lindenberg Gmbh Vorrichtung zur Einstellung von Flugzeughöhenflossen
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
TWM271245U (en) 2005-01-28 2005-07-21 Silitech Technology Corp Photosensitive key
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
US7309043B2 (en) 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7611099B2 (en) 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
DE102007021748B4 (de) * 2007-05-09 2019-12-12 Liebherr-Aerospace Lindenberg Gmbh Antriebssystem für einen wölbvariablen Flugzeugflügel

Also Published As

Publication number Publication date
US20060049308A1 (en) 2006-03-09
US7726610B2 (en) 2010-06-01
EP1786667B1 (de) 2009-12-09
ATE451300T1 (de) 2009-12-15
WO2006029132A1 (en) 2006-03-16
EP1786667A1 (de) 2007-05-23
US20090206209A1 (en) 2009-08-20
CA2578800C (en) 2010-07-13
EP1786667B2 (de) 2017-06-07
CA2578800A1 (en) 2006-03-16
US7494094B2 (en) 2009-02-24

Similar Documents

Publication Publication Date Title
DE602005018230D1 (de) Systeme und verfahren zur bereitstellung von differenzieller bewegung für flügelhochauftriebsvorrichtungen
DE602007011896D1 (de) Ausfallsichere steuerflächentropfenverbindung
ES2387001T5 (es) Aparato y método para controlar el flujo de plasma en el borde de salida de un perfil aerodinámico
ATE438566T1 (de) Systeme und verfahren zur steuerung einer luftbetankungsvorrichtung
DE602006014253D1 (de) Systeme und verfahren zur steuerung von flugzeugklappen und -spoilern
WO2008031620A3 (de) Aerodynamischer körper sowie tragflügel mit aerodynamischem körper, stellantriebs -ansteuermodul, computer, computerprogramm und verfahren zur beeinflussung von nachlauf wirbeln
BRPI0719353A2 (pt) Sistemas, dispositivos e métodos para dispositivos de energização e/ou controle, por exemplo, dispositivos de distribuição transdérmicos
EP1798700A3 (de) Systeme und Verfahren zur Darstellung eines Luftfahrzeuges in einer kontrollierten Umgebung
DE602007002862D1 (de) Übertragung von Anweisungsdaten für Flugzeuge
WO2006025860A3 (en) Methods and systems for automatically displaying information, including air traffic control instructions
DE602007001023D1 (de) Gleitanflugverfahren für maximale Vorhersagbarkeit
WO2009082785A8 (en) A method and system of controlling air traffic
DE502004007012D1 (de) Verfahren zur lastbegrenzung in antriebssystemen für flugzeughochauftriebssysteme
EP2077437A3 (de) Priorisierung alternativer Landemöglichkeiten bei der Flugplanung
DE602004014400D1 (de) Architektonischer torbogen für ein flugzeug
EA201290198A1 (ru) Способ и система независимого управления транспортным средством
ATE415341T1 (de) Vorrichtung zur betätigung von klappenelementen an den tragflächen eines flugzeuges
WO2012110569A3 (en) Door system having an actuator
ATE495096T1 (de) Verfahren und einrichtung zur höhenflossentrimmung bei einem flugzeug
WO2013024016A3 (de) Bremsanlage mit magnetschienenbremseinrichtung
ATE518177T1 (de) Verfahren und vorrichtung zur routenplanung
WO2006012391A3 (en) Devices and methods for communicating with a microcontroller
BRPI0814907A2 (pt) Método e sistema para controle de pelo menos um atuador ou para atuação das carenagens de um reversor de empuxo em um motor turbojato
ATE428963T1 (de) Triebwerkgeschwindigkeits-steuereinrichtung, verfahren zum steuern der triebwerkgeschwindigkeit und damit ausgestattetes flugzeug
ATE480810T1 (de) Trimmverfahren für mehrere achsen

Legal Events

Date Code Title Description
8363 Opposition against the patent