WO2006135421A3 - Leading edge flap apparatuses and associated methods - Google Patents

Leading edge flap apparatuses and associated methods Download PDF

Info

Publication number
WO2006135421A3
WO2006135421A3 PCT/US2005/033304 US2005033304W WO2006135421A3 WO 2006135421 A3 WO2006135421 A3 WO 2006135421A3 US 2005033304 W US2005033304 W US 2005033304W WO 2006135421 A3 WO2006135421 A3 WO 2006135421A3
Authority
WO
WIPO (PCT)
Prior art keywords
leading edge
edge flap
edge device
flow
associated methods
Prior art date
Application number
PCT/US2005/033304
Other languages
French (fr)
Other versions
WO2006135421A2 (en
Inventor
James M Wheaton
Stephen R Amorosi
Original Assignee
Boeing Co
James M Wheaton
Stephen R Amorosi
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=36385261&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=WO2006135421(A3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co, James M Wheaton, Stephen R Amorosi filed Critical Boeing Co
Priority to EP05858149A priority Critical patent/EP1799542B1/en
Priority to DE602005022332T priority patent/DE602005022332D1/en
Priority to AT05858149T priority patent/ATE473919T1/en
Publication of WO2006135421A2 publication Critical patent/WO2006135421A2/en
Publication of WO2006135421A3 publication Critical patent/WO2006135421A3/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C7/00Structures or fairings not otherwise provided for
    • B64C7/02Nacelles
    • 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
    • B64C9/22Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • 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
    • B64C9/22Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
    • 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
    • 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
    • Y02T50/40Weight reduction

Abstract

The present invention is directed generally toward leading edge flap apparatuses and corresponding methods. One aspect of the invention is directed toward an aircraft system having an airfoil, an actuator driver, and a leading edge device with two flow surfaces (11, 12) and six links. In a further aspect of the invention, the flow surfaces of the leading edge device are at least approximately located in the same position when the actuator device is in two different positions. Another aspect of the invention is directed toward an aircraft system having an airfoil and a leading edge device movable between at least a retracted position and an extended position along a motion path having two segments. The second flow surface (12) can be positioned generally behind and/or generally above the first flow surface (11) when the first and second flow surfaces are located in the first segment of the motion path.
PCT/US2005/033304 2004-09-30 2005-09-16 Leading edge flap apparatuses and associated methods WO2006135421A2 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP05858149A EP1799542B1 (en) 2004-09-30 2005-09-16 Leading edge flap apparatuses and associated methods
DE602005022332T DE602005022332D1 (en) 2004-09-30 2005-09-16 DEVICE FOR PADLOCKING AND ASSOCIATED METHODS THEREOF
AT05858149T ATE473919T1 (en) 2004-09-30 2005-09-16 DEVICES FOR WING FOLDING AND ASSOCIATED METHODS

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/955,686 US7264206B2 (en) 2004-09-30 2004-09-30 Leading edge flap apparatuses and associated methods
US10/955,686 2004-09-30

Publications (2)

Publication Number Publication Date
WO2006135421A2 WO2006135421A2 (en) 2006-12-21
WO2006135421A3 true WO2006135421A3 (en) 2007-02-22

Family

ID=36385261

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2005/033304 WO2006135421A2 (en) 2004-09-30 2005-09-16 Leading edge flap apparatuses and associated methods

Country Status (5)

Country Link
US (3) US7264206B2 (en)
EP (1) EP1799542B1 (en)
AT (1) ATE473919T1 (en)
DE (1) DE602005022332D1 (en)
WO (1) WO2006135421A2 (en)

Families Citing this family (47)

* 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
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing 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
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
DE602006013236D1 (en) * 2005-08-25 2010-05-12 Gkn Aerospace Services Ltd Slat for an aircraft wing
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
GB0604026D0 (en) * 2006-02-28 2006-04-12 Airbus Uk Ltd Aircraft wing
WO2008110521A1 (en) * 2007-03-09 2008-09-18 Asco Industries Wing
GB0721284D0 (en) * 2007-10-31 2007-12-12 Airbus Uk Ltd Actuation system for leading edge high-lift device
GB0722425D0 (en) * 2007-11-15 2007-12-27 Airbus Uk Ltd Slat support funk plate
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
US8256719B2 (en) * 2008-12-01 2012-09-04 The Boeing Company Shape changing airfoil system
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
US8500060B2 (en) * 2009-02-10 2013-08-06 The Boeing Company Aircraft with a pressurized vessel
US8056865B2 (en) 2009-03-05 2011-11-15 The Boeing Company Mechanism for changing the shape of a control surface
EP2272752B1 (en) 2009-07-07 2018-05-30 Goodrich Actuation Systems Limited Actuator arrangement
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
GB201008773D0 (en) * 2010-05-26 2010-07-14 Airbus Uk Ltd Aircraft slat assembly
US9102418B2 (en) * 2010-10-28 2015-08-11 Hamilton Sundstrand Corporation Cantilevered differential motion sensor and associated frame
US8650811B2 (en) 2011-02-04 2014-02-18 The Boeing Company Solar collector frame
DE102011014687A1 (en) 2011-03-22 2012-09-27 Airbus Operations Gmbh A load introduction element for a movable surface of an aircraft, aircraft with at least one movable surface and at least one load introduction element and method for releasing a movable surface connected to a load introduction element
DE102011018906A1 (en) * 2011-04-28 2012-10-31 Airbus Operations Gmbh High lift system for an aircraft and method for influencing the high lift characteristics of an aircraft
US8438743B2 (en) * 2011-06-01 2013-05-14 Hamilton Sundstrand Corporation Resolver type skew sensor with gimbal attachment
DE102011105912A1 (en) * 2011-06-28 2013-01-03 Airbus Operations Gmbh A wing with a main wing and a high-lift body and method for performing adjustment movements of a high-lift body relative to a main wing
GB201111922D0 (en) 2011-07-12 2011-08-24 Airbus Operations Ltd Leading edge rib assembly
US8783604B2 (en) * 2011-10-21 2014-07-22 Raytheon Company Aircraft wing with knuckled rib structure
US8622350B1 (en) * 2011-11-14 2014-01-07 The Boeing Company Compound leading edge device for aircraft
US9016637B2 (en) * 2012-02-10 2015-04-28 The Boeing Company High-positioned 3-position variable camber krueger
US20140076419A1 (en) * 2012-02-27 2014-03-20 Sinhatech Self adjusting deturbulator enhanced flap and wind deflector
FR3020343B1 (en) * 2014-04-23 2017-10-27 Airbus Operations Sas AIRCRAFT ASSEMBLY COMPRISING A PRIMARY STRUCTURE OF HITCHING MATERIAL CONSISTING OF THREE INDEPENDENT ELEMENTS
EP2955102B1 (en) * 2014-06-12 2019-03-27 Airbus Operations GmbH Morphing trailing edge device for an airfoil
US9623957B2 (en) * 2014-08-26 2017-04-18 The Boeing Company Torque tube door
GB2533311A (en) * 2014-12-15 2016-06-22 Airbus Operations Ltd A track container
EP3392895B1 (en) * 2016-01-22 2020-03-11 Asahi Kasei Kabushiki Kaisha Nonaqueous lithium power storage element
KR101984452B1 (en) * 2016-01-22 2019-05-30 아사히 가세이 가부시키가이샤 Non-aqueous lithium secondary battery
US10196131B2 (en) * 2016-02-16 2019-02-05 The Boeing Company Hydraulic system and method for an aircraft flight control system
US10829198B2 (en) 2017-06-21 2020-11-10 The Boeing Company Krueger flap apparatus and methods incorporating a bullnose having a contour variation along a spanwise direction
US10766602B2 (en) * 2017-11-01 2020-09-08 The Boeing Company Mechanical droop for spoiler operation
US11332233B2 (en) * 2018-07-16 2022-05-17 Airbus Operations Gmbh System for driving a flap arrangement between a retracted position and an extended position
US11001371B2 (en) * 2018-08-07 2021-05-11 The Boeing Company Hydraulic droop control for aircraft wing
CN114476020B (en) * 2021-12-20 2024-01-16 中国商用飞机有限责任公司北京民用飞机技术研究中心 High lift device for wing and aircraft

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5158252A (en) * 1991-10-24 1992-10-27 The Boeing Company Three-position variable camber Krueger leading edge flap
US6375126B1 (en) * 2000-11-16 2002-04-23 The Boeing Company Variable camber leading edge for an airfoil
EP1338506A1 (en) * 2002-02-15 2003-08-27 Fairchild Dornier GmbH Airplane wing with slat and Krueger flap

Family Cites Families (344)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2563453A (en) 1951-08-07 Device fob controlling the trailing
US2899152A (en) 1959-08-11 Aircraft control surface operating mechanism
DE387833C (en) 1921-05-27 1924-01-04 Handley Page Ltd Wing for aircraft
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 (en) 1930-11-05 1931-06-02 Improvements to air navigation devices
US1913169A (en) 1931-03-27 1933-06-06 Emil F Martin Wing and like member for aircraft
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 (en) 1942-12-29 1951-04-20 Development of high-lift slit wing planes
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 (en) 1943-09-24 1951-07-05 High lift wing
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 (en) 1946-12-03 1955-03-23
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
US2702676A (en) * 1952-04-26 1955-02-22 Chance Vought Aircraft Inc Slat mechanism for airplanes with sweptback wings
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
GB853034A (en) 1957-09-17 1960-11-02 Smith & Sons Ltd S Improvements in or relating to visual indicators
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 (en) 1960-11-11 1962-05-10 Dornier Werke Gmbh Airplane wing with fixed leading wing
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
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
US3243126A (en) * 1963-09-18 1966-03-29 United Aircraft Corp Variable area exhaust nozzle
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
US4090895A (en) 1966-01-13 1978-05-23 Thiokol Corporation High energy fuel slurry
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 (en) 1967-05-16 1971-04-07
US3486720A (en) 1967-12-07 1969-12-30 Boeing Co Continuous slot forming leading edge slats for cranked wings
US3504870A (en) 1967-12-08 1970-04-07 Boeing Co Aircraft wing variable camber leading edge flap
US3659810A (en) 1968-05-20 1972-05-02 James L Robertson Inherently stable tapered wing flaperon airplane
US3539133A (en) 1968-05-20 1970-11-10 Robertson Aircraft Corp 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 (en) 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
DE1943680C2 (en) 1969-08-28 1982-06-24 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Control flap arrangement
FR2064681A5 (en) 1969-10-13 1971-07-23 Onera (Off Nat Aerospatiale)
DE1962956C3 (en) 1969-12-16 1975-09-04 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Device for deflecting and redirecting the jet of thrust and lifting fans
BE757750A (en) 1969-12-31 1971-04-01 Thomson Csf IMPROVEMENTS TO REAL-TIME ELECTRIC SIGNAL PROCESSING DEVICES
US3653611A (en) 1970-03-24 1972-04-04 Mason Trupp Slotted delta wing aircraft
US4141768A (en) * 1970-05-18 1979-02-27 Rockwell International Corporation Fuel rich solid propellant of boron and a fluoro-nitro-epoxide polymer binder
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
DE2144688C3 (en) 1971-09-07 1978-08-17 Kloeckner-Humboldt-Deutz Ag, 5000 Koeln V-belt tensioning device
GB1404762A (en) 1971-10-07 1975-09-03 Lucas Industries Ltd Electro-hydraulic actuating systems for aircraft control surfaces
US3767140A (en) 1971-11-03 1973-10-23 Mc Donnell Douglas Corp Airplane flaps
FR2173248B1 (en) 1972-02-24 1978-02-03 Daikin Ind Ltd
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
US3847369A (en) 1973-03-08 1974-11-12 Us Navy Control surface deployment mechanism
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 (en) 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
US3985319A (en) 1975-02-03 1976-10-12 The Boeing Company Variable pivot trailing edge flap
US3991574A (en) 1975-02-03 1976-11-16 Frazier Larry Vane W Fluid pressure power plant with double-acting piston
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
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 (en) 1977-06-07 1982-11-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Ailerons and flap drives for an aircraft
US4171787A (en) 1977-07-21 1979-10-23 Zapel Edwin J Variable camber leading edge for airfoil
US4131253A (en) 1977-07-21 1978-12-26 The Boeing Company Variable camber trailing edge for airfoil
US4146200A (en) 1977-09-14 1979-03-27 Northrop Corporation Auxiliary flaperon control for aircraft
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 (en) 1978-06-01 1979-12-28 Sarrazin Applic Hydr INTEGRATED CONTROL DEVICE FOR FLUID CIRCUIT, AND ITS 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
US4247843A (en) * 1978-08-23 1981-01-27 Sperry Corporation Aircraft flight instrument display 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
US4363098A (en) 1980-06-24 1982-12-07 The Boeing Company Electric command spoiler system
US4353517A (en) 1980-10-07 1982-10-12 The Boeing Company Flap assembly for aircraft wing
FR2492337A1 (en) 1980-10-16 1982-04-23 Aerospatiale AIRCRAFT WING WITH A HYPERSUSTENTATOR SYSTEM IN ITS ATTACK EDGE AND AIRCRAFT COMPRISING SUCH AILET
US4399970A (en) 1980-11-13 1983-08-23 The Boeing Company Wing leading edge slat
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 (en) 1981-10-10 1983-04-28 Dornier Gmbh, 7990 Friedrichshafen PROFILES, IN PARTICULAR WING PROFILES 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
DE3149629C1 (en) 1981-12-15 1983-04-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Device for sealing an air gap on an aircraft flap
US4470569A (en) 1981-12-28 1984-09-11 Mcdonnell Douglas Corporation Locking, redundant slat drive mechanism
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
EP0100775B1 (en) 1982-08-09 1987-01-21 The Boeing Company Wing leading edge slat
US4747375A (en) 1982-08-31 1988-05-31 Williams John K Device for controlling the phased displacement of rotating shafts
US4575030A (en) * 1982-09-13 1986-03-11 The Boeing Company Laminar flow control airfoil
EP0103038A1 (en) 1982-09-13 1984-03-21 The Boeing Company Continuous skin, variable camber airfoil edge actuating mechanism
US4496121A (en) * 1982-09-21 1985-01-29 The Boeing Company Control surface lock for flutter constraint
US4448375A (en) * 1982-09-29 1984-05-15 The Boeing Company Folding truss mechanism for trailing edge flaps
SE434762B (en) 1982-11-29 1984-08-13 Ingemanssons Ingenjorsbyra Ab SEALING DEVICE AT 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
EP0130983B1 (en) 1982-12-30 1987-10-21 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 (en) * 1983-12-06 1986-09-19 Aerospatiale BOOM AIRCRAFT WING PROVIDED WITH A HYPERSUSTENTATOR SYSTEM AND AN ENGINE SUSPENSION MAT, AS WELL AS AN ENGINE SUSPENSION MAT FOR SUCH A WING
US4575099A (en) * 1984-01-27 1986-03-11 General Electric Company High excursion seal with flexible membrane to prevent gas leakage through hinge
US4605187A (en) * 1984-03-09 1986-08-12 The Boeing Company Wing flap mechanism
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
US4702442A (en) * 1984-12-06 1987-10-27 The Boeing Company Aircraft trailing edge flap apparatus
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
US4687162A (en) 1985-06-25 1987-08-18 The Boeing Company Apparatus for supporting an aircraft guide track for a movable airfoil
EP0218021B1 (en) * 1985-08-29 1988-06-08 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Flaps arrangement for an aircraft wing
DE3530865A1 (en) * 1985-08-29 1987-03-12 Messerschmitt Boelkow Blohm DRIVE AND GUIDE DEVICE FOR A FLAP SYSTEM ARRANGED ON AN AIRCRAFT WING
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
JP2569003B2 (en) * 1986-03-20 1997-01-08 株式会社日立製作所 Heat conduction device
DE3620886A1 (en) 1986-06-21 1988-01-14 Messerschmitt Boelkow Blohm DRIVE DEVICE WITH VARIABLE TORQUE LIMITING SYSTEM
US4792906A (en) 1986-08-29 1988-12-20 The Boeing Company Navigational apparatus and methods for displaying aircraft position with respect to a selected vertical flight path profile
FR2606363B1 (en) 1986-11-07 1989-03-03 Aerospatiale SYSTEM FOR CONTROLLING THE AIRCRAFT SHUTTERS OF AN AIRCRAFT
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
US4806316A (en) * 1987-03-17 1989-02-21 Becton, Dickinson And Company Disposable device for use in chemical, immunochemical and microorganism analysis
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
US5074495A (en) 1987-12-29 1991-12-24 The Boeing Company Load-adaptive hybrid actuator system and method for actuating control surfaces
US4860007A (en) 1988-01-15 1989-08-22 The Boeing Company Integrated primary flight display
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
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
US5129597A (en) 1989-02-06 1992-07-14 Deutsche Airbus Gmbh Ceiling luggage compartment combination for the passenger cabin of an aircraft
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 (en) 1989-09-15 1991-03-28 Vdo Schindling METHOD AND DEVICE FOR PRESENTING AIRPORT INFORMATION
US5082208A (en) * 1989-09-29 1992-01-21 The Boeing Company System and method for controlling an aircraft flight control member
US5056741A (en) 1989-09-29 1991-10-15 The Boeing Company Apparatus and method for aircraft wing stall control
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 (en) 1990-10-19 1992-04-23 Airbus Gmbh DRIVING DEVICE FOR FLAPS ARRANGED ON AIRCRAFT WINGS
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 (en) 1991-02-21 1992-08-27 Heilmeier & Weinlein HYDRAULIC CONTROL DEVICE
JPH07112836B2 (en) 1991-06-14 1995-12-06 富士重工業株式会社 Aircraft hydraulic steering system
US5313788A (en) * 1991-08-07 1994-05-24 General Electric Company Thrust reversing arrangement for a long duct mixed flow exhaust turbofan engine
DE4130644A1 (en) 1991-09-14 1993-03-18 Airbus Gmbh UPPER LUGGAGE RACK WITH A LOWERABLE TRAY, IN PARTICULAR FOR A PASSENGER PLANE
GB9201762D0 (en) 1992-01-28 1992-03-11 Wes Technology Inc Seals for gas isolators
DE4209037C2 (en) 1992-03-20 1994-06-23 Deutsche Aerospace Airbus Device for carrying luggage in airplanes
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 (en) 1992-09-24 1994-12-16 Aerospatiale Rigid kruger spout, for leading edge of aircraft wings.
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
US6537817B1 (en) * 1993-05-31 2003-03-25 Packard Instrument Company Piezoelectric-drop-on-demand technology
US6521187B1 (en) * 1996-05-31 2003-02-18 Packard Instrument Company Dispensing liquid drops onto porous brittle substrates
US6203759B1 (en) * 1996-05-31 2001-03-20 Packard Instrument Company Microvolume liquid handling system
FR2709110B1 (en) * 1993-08-20 1995-11-10 Lucas Air Equipement Servo-control device of an aircraft flight control member.
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
GB9405001D0 (en) * 1994-03-15 1994-04-27 British Aerospace Rigging of aircraft wing flaps
DE4422152C2 (en) * 1994-06-27 2000-02-03 Daimler Chrysler Aerospace Method and arrangement for optimizing the aerodynamic effect of a wing
US5535852A (en) 1994-08-17 1996-07-16 Bishop; David J. Lift apparatus
FR2728535A1 (en) * 1994-12-26 1996-06-28 Aerospatiale VARIABLE SLOTTED AEROBRAKE FOR AIRCRAFT WING
US5628477A (en) 1995-02-13 1997-05-13 The Boeing Company Auxiliary airfoil lost motion detector and actuator
US5609020A (en) * 1995-05-15 1997-03-11 The Boeing Company Thrust reverser synchronization shaft lock
US5680124A (en) 1995-05-15 1997-10-21 The Boeing Company Skew and loss detection system for adjacent high lift devices
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
US5715163A (en) * 1995-08-22 1998-02-03 The Boeing Company Cursor controlled navigation system for aircraft
US5723320A (en) * 1995-08-29 1998-03-03 Dehlinger; Peter J. Position-addressable polynucleotide arrays
US5681013A (en) 1995-12-26 1997-10-28 The Boeing Company Vortex leading edge flap assembly for supersonic airplanes
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
US6015117A (en) * 1996-04-13 2000-01-18 Broadbent; Michael C Variable camber wing mechanism
US6020141A (en) * 1996-05-09 2000-02-01 3-Dimensional Pharmaceuticals, Inc. Microplate thermal shift assay for ligand development and multi-variable protein chemistry optimization
US5927656A (en) 1996-06-26 1999-07-27 The Boeing Company Wing leading edge flap and method therefor
JP3323067B2 (en) 1996-07-12 2002-09-09 沖電気工業株式会社 CDMA receiver
SE507968C2 (en) 1996-07-25 1998-08-03 Electrolux Ab Carrier, e.g. for wall mounted household stove
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 (en) 1996-10-19 1998-12-10 Daimler Benz Ag Float with variable curvature
US6293497B1 (en) 1996-10-22 2001-09-25 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
DE19712034A1 (en) 1997-03-21 1998-09-24 Deutsch Zentr Luft & Raumfahrt Flexible leading edge profile for aerofoil
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
WO1999003000A1 (en) 1997-07-09 1999-01-21 Massachusetts Institute Of Technology Integrated flight information and control system
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
US5921506A (en) 1997-09-25 1999-07-13 Northrop Grumman Corporation Extendible leading edge flap
US5978715A (en) 1997-10-15 1999-11-02 Dassault Aviation Apparatus and method for aircraft display and control
US6057786A (en) 1997-10-15 2000-05-02 Dassault Aviation Apparatus and method for aircraft display and control including head up display
US6112141A (en) 1997-10-15 2000-08-29 Dassault Aviation Apparatus and method for graphically oriented 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
ES2156660B1 (en) 1998-01-14 2002-02-16 Saiz Manuel Munoz FLIGHT CONTROLS WITH AUTOMATIC COMPENSATION.
US6172780B1 (en) * 1998-03-24 2001-01-09 Samsung Electronics Co., Ltd. Laser scanning apparatus
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 (en) 1998-04-30 2000-06-15 Daimler Chrysler Aerospace Method for reducing gust loads on an aircraft below the cruising altitude
DE69916360T3 (en) * 1998-05-21 2008-06-05 Mcdonnell Douglas Corp. airfoil
US6188937B1 (en) * 1998-09-30 2001-02-13 Honeywell International Inc. Methods and apparatus for annunciation of vehicle operational modes
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
US6689323B2 (en) * 1998-10-30 2004-02-10 Agilent Technologies Method and apparatus for liquid transfer
DE19858872C2 (en) 1998-12-19 2001-02-08 Daimler Chrysler Ag Adaptive aircraft wing
FR2787759B1 (en) 1998-12-28 2001-03-16 Aerospatiale METHOD AND SYSTEM FOR CONTROLLING A GOVERNOR OF AN AIRCRAFT OPERATED BY MULTIPLE HYDRAULIC CYLINDERS AND MODULAR POWER
US6382566B1 (en) 1998-12-29 2002-05-07 The Boeing Company Method and apparatus for detecting skew and asymmetry of an airplane flap
US6326083B1 (en) * 1999-03-08 2001-12-04 Calipher Technologies Corp. Surface coating for microfluidic devices that incorporate a biopolymer resistant moiety
DE19910551C2 (en) * 1999-03-10 2001-04-05 Eads Airbus Gmbh Aircraft wing with at least one short-coupled engine
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
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 (en) 2000-01-13 2004-01-29 Airbus Deutschland Gmbh Luggage rack with a lowerable luggage compartment, especially for an aircraft passenger cabin
US6598834B2 (en) 2000-02-14 2003-07-29 Aerotech Services Inc. Method for reducing fuel consumption in aircraft
EP2202001A3 (en) * 2000-02-23 2011-05-18 Zyomyx, Inc. Microfluidic devices and methods
DE10019187C1 (en) * 2000-04-17 2002-01-03 Airbus Gmbh Pressure control for a sinker
JP2001343032A (en) 2000-06-01 2001-12-14 Komatsu Ltd Fluid pressure control valve of clutch or brake and fluid pressure control method
US6506806B2 (en) * 2000-06-08 2003-01-14 E. I. Du Pont De Nemours And Company Reduction of surface tension
FR2811037B1 (en) 2000-06-28 2002-10-18 Aerospatiale Matra Airbus ELECTRICALLY CONTROLLED HYDRAULIC ACTUATION SYSTEM
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
US6561463B1 (en) 2000-07-14 2003-05-13 Honeywell International Inc. Flight control module with integrated spoiler actuator control electronics
WO2002011888A2 (en) * 2000-08-07 2002-02-14 Nanostream, Inc. Fluidic mixer in microfluidic system
US6439512B1 (en) 2000-08-24 2002-08-27 Hr Textron, Inc. All-hydraulic powered horizontal stabilizer trim control surface position control system
US6443394B1 (en) 2000-09-21 2002-09-03 The B.F. Goodrich Company Inflatable airfoil device
DE10055961B4 (en) 2000-11-11 2004-09-09 Eads Deutschland Gmbh Variable wing area with adjustable profile shape that extends in the span direction
US20020046087A1 (en) * 2000-12-18 2002-04-18 John Hey Method of drawing attention to advertisements
US6481667B1 (en) 2001-03-05 2002-11-19 Northrop Grumman Corporation System and method for deflecting an aerodynamic control surface
NL1017811C2 (en) 2001-04-10 2002-10-11 Stork Prod Eng Cabin baggage assembly with underpressure.
US6844028B2 (en) * 2001-06-26 2005-01-18 Accelr8 Technology Corporation Functional surface coating
US6547183B2 (en) 2001-08-02 2003-04-15 The Boeing Company Moveable closet
US6870490B2 (en) * 2001-08-23 2005-03-22 Honeywell International Inc. Display of altitude and path capture trajectories
US20030132860A1 (en) 2001-09-21 2003-07-17 Honeywell International, Inc. Interface for visual cueing and control for tactical flightpath management
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
US6845787B2 (en) * 2002-02-23 2005-01-25 Nanostream, Inc. Microfluidic multi-splitter
US6601801B1 (en) 2002-04-24 2003-08-05 The Boeing Company Gapped trailing-edge control surface for an airfoil
FR2840877B1 (en) 2002-06-13 2004-08-06 Airbus France DEVICE FOR JOINING A COMPONENT ON AERODYNAMIC AIRCRAFT SURFACE
US6698523B2 (en) * 2002-07-02 2004-03-02 Husco International, Inc. Electrohydraulic control system for implement lift cylinders
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
US6802475B2 (en) 2002-07-04 2004-10-12 Smiths Wolverhampton Limited Flight surface actuator
US6641986B1 (en) * 2002-08-12 2003-11-04 Air Products And Chemicals, Inc. Acetylenic diol surfactant solutions and methods of using same
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
US7048235B2 (en) * 2002-10-09 2006-05-23 The Boeing Company Slotted aircraft wing
US7048228B2 (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
US6796526B2 (en) 2002-11-25 2004-09-28 The Boeing Company Augmenting flight control surface actuation system and method
DE10313728B4 (en) 2003-03-27 2011-07-21 Airbus Operations GmbH, 21129 Flap system on the wing of a fixed-wing aircraft
CA2427416C (en) 2003-05-01 2010-11-16 101039130 Saskatchewan Ltd. Steering device for towed implements
US7070381B2 (en) 2003-05-20 2006-07-04 Khan Farooq A Hydraulic control system for refuse collection vehicle
US7059563B2 (en) 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
US7243881B2 (en) * 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
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 (en) * 2003-09-22 2006-12-08 Airbus France AIRCRAFT WING COMPRISING AT LEAST ONE DEPORTER SHUTTER AND DEPORTER SHUTTER FOR SAID WING
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
DE10361891A1 (en) 2003-12-23 2005-08-04 Airbus Deutschland Gmbh Device for controlling and adjusting flaps on aircraft wings
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
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
DE102004040313B4 (en) * 2004-08-19 2008-02-21 Airbus Deutschland Gmbh System for adjusting the spanwise load distribution of a wing
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
TWM271245U (en) 2005-01-28 2005-07-21 Silitech Technology Corp Photosensitive key
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
DE102005016639B4 (en) * 2005-04-11 2010-12-02 Eads Deutschland Gmbh Wing with extendable aerodynamic wing flaps, in particular lift flaps
US7578484B2 (en) * 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5158252A (en) * 1991-10-24 1992-10-27 The Boeing Company Three-position variable camber Krueger leading edge flap
US6375126B1 (en) * 2000-11-16 2002-04-23 The Boeing Company Variable camber leading edge for an airfoil
EP1338506A1 (en) * 2002-02-15 2003-08-27 Fairchild Dornier GmbH Airplane wing with slat and Krueger flap

Also Published As

Publication number Publication date
US20100025537A1 (en) 2010-02-04
DE602005022332D1 (en) 2010-08-26
US20110024575A1 (en) 2011-02-03
WO2006135421A2 (en) 2006-12-21
EP1799542B1 (en) 2010-07-14
ATE473919T1 (en) 2010-07-15
US7264206B2 (en) 2007-09-04
EP1799542A2 (en) 2007-06-27
US20060102803A1 (en) 2006-05-18
US7992826B2 (en) 2011-08-09
US7828250B2 (en) 2010-11-09

Similar Documents

Publication Publication Date Title
WO2006135421A3 (en) Leading edge flap apparatuses and associated methods
EP1607324B8 (en) Aircraft leading edge apparatuses and corresponding methods
EP1995171A3 (en) Airfoil trailing edge plasma flow control apparatus and method
WO2008051286A3 (en) Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
WO2007095931A3 (en) Aerodynamic flap of an aircraft with a device which influences the flap turbulence
WO2009075963A3 (en) Trailing edge device catchers and associated systems and methods
WO2007093851A3 (en) Airfoil for a third stage nozzle guide vane
WO2007085912A3 (en) Airfoil for a first stage nozzle guide vane
WO2006022833A3 (en) High performance airfoil with co-flow jet flow control
CA2544538A1 (en) Apparatus for reducing drag on unpowered vehicles
WO2008115207A3 (en) Highly efficient supersonic laminar flow wing
WO2009019011A3 (en) High lift system for an aircraft
JP2009516615A5 (en)
WO2008129244A3 (en) Annular airborne vehicle
WO2007125382A3 (en) Third stage turbine airfoil
WO2008035135A3 (en) First stage turbine airfoil
WO2008033778A3 (en) Rendering icons along a multidimensional path having a terminus position
WO2009149932A3 (en) Device for generating aerodynamic vortices, and regulating flap and wing comprising a device for generating aerodynamic vortices
WO2009103865A3 (en) Elongated, torsion-deformable aerodynamic element
ATE498548T1 (en) AIRCRAFT WITH LOADING ACCESS OPENING
CA2560144A1 (en) Retractable windshield for a boat
WO2009024666A3 (en) Actuator for opening an aircraft engine nacelle cowl
WO2009098442A3 (en) Wing control devices
EP1344915A3 (en) A variable position intake for an aircraft mounted gas turbine engine
WO2007071384A3 (en) Flexible control surface for an aircraft

Legal Events

Date Code Title Description
NENP Non-entry into the national phase

Ref country code: DE

WWE Wipo information: entry into national phase

Ref document number: 2005858149

Country of ref document: EP

121 Ep: the epo has been informed by wipo that ep was designated in this application
WWP Wipo information: published in national office

Ref document number: 2005858149

Country of ref document: EP