US2563453A
(en)
|
|
1951-08-07 |
|
Device fob controlling the trailing |
US1785620A
(en)
|
1927-10-26 |
1930-12-16 |
Bristol Aeroplane Co Ltd |
Control surface for aircraft, submersibles, and the like
|
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
|
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
|
US2138952A
(en)
|
1935-08-31 |
1938-12-06 |
Arado Flugzeugwerke Gmbh |
Auxiliary wing for aircraft
|
US2169416A
(en)
|
1936-06-12 |
1939-08-15 |
United Aircraft Corp |
Slotted deflector flap
|
US2207453A
(en)
|
1937-10-02 |
1940-07-09 |
Arado Flugzeugwerke Gmbh |
Aircraft supporting wing
|
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
|
US2289704A
(en)
|
1940-02-26 |
1942-07-14 |
Charles H Grant |
Aircraft wing
|
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
|
US2421694A
(en)
*
|
1942-07-02 |
1947-06-03 |
Lockheed Aircraft Corp |
Airplane control surface
|
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
|
US2406475A
(en)
|
1944-02-19 |
1946-08-27 |
Samuel H Pearis |
Slotted airplane wing
|
US2502315A
(en)
|
1946-02-26 |
1950-03-28 |
Beech Aircraft Corp |
Operating mechanism for high lift devices for airplanes
|
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
|
US2549760A
(en)
|
1949-04-14 |
1951-04-24 |
Adams George Kenneth |
Aerodynamic flap balance and auxiliary airfoil
|
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
|
US2743887A
(en)
|
1952-11-12 |
1956-05-01 |
Willy A Fiedler |
Split aircraft wing
|
US2864239A
(en)
|
1956-10-04 |
1958-12-16 |
Sperry Rand Corp |
Electro-hydraulic servo system for steering dirigible craft
|
US2990145A
(en)
|
1956-11-05 |
1961-06-27 |
Gen Electric |
Integrated hydraulic power actuator
|
US2990144A
(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
|
US3112089A
(en)
|
1960-10-12 |
1963-11-26 |
Dornier Werke Gmbh |
Airplane wing flaps
|
US3102607A
(en)
|
1960-12-19 |
1963-09-03 |
Charles E Roberts |
Carrier system for transport and delivery along a trackway
|
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
|
US3136504A
(en)
|
1963-07-02 |
1964-06-09 |
William F Carr |
Electrical primary flight control system
|
GB1083267A
(en)
*
|
1964-12-11 |
1967-09-13 |
Power Jets Res & Dev Ltd |
Flap systems for aircraft
|
US3362659A
(en)
*
|
1965-07-06 |
1968-01-09 |
Razak Charles Kenneth |
Method and apparatus for landing jet aircraft
|
GB1181991A
(en)
|
1967-04-14 |
1970-02-18 |
Edward M Lanier |
Aircraft Lift-Increasing Device
|
GB1227316A
(de)
|
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
|
US3493196A
(en)
|
1968-01-24 |
1970-02-03 |
Mc Donnell Douglas Corp |
Airplane flap assembly
|
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
(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
|
US3583660A
(en)
|
1969-08-18 |
1971-06-08 |
Lockheed Aircraft Corp |
Lift and control augmenter for airfoils
|
DE1943680C2
(de)
|
1969-08-28 |
1982-06-24 |
Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen |
Steuerklappenanordnung
|
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
|
US3776491A
(en)
|
1971-06-25 |
1973-12-04 |
R Oulton |
Aircraft with compound 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
|
US3767140A
(en)
|
1971-11-03 |
1973-10-23 |
Mc Donnell Douglas Corp |
Airplane flaps
|
GB1443333A
(en)
*
|
1972-08-12 |
1976-07-21 |
Mtu Muenchen Gmbh |
Aircraft having apparatus for augmenting the lift of the aircraft
|
US3790106A
(en)
*
|
1973-01-24 |
1974-02-05 |
J Morris |
Flap system
|
US3831886A
(en)
|
1973-01-26 |
1974-08-27 |
Lockheed Aircraft Corp |
Airfoil with extendible and retractable leading edge
|
US3853289A
(en)
|
1973-02-15 |
1974-12-10 |
Boeing Co |
Trailing edge flap and actuating mechanism therefor
|
US3837601A
(en)
|
1973-03-09 |
1974-09-24 |
Boeing Co |
Aerodynamic slot closing mechanism
|
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
|
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
|
US3992979A
(en)
|
1974-12-20 |
1976-11-23 |
Joseph Lucas (Industries) Limited |
Hydraulic actuating arrangements
|
US3987983A
(en)
|
1974-12-20 |
1976-10-26 |
The Boeing Company |
Trailing edge flaps having spanwise aerodynamic slot opening and closing mechanism
|
US3985319A
(en)
|
1975-02-03 |
1976-10-12 |
The Boeing Company |
Variable pivot trailing edge flap
|
US4049219A
(en)
|
1975-02-03 |
1977-09-20 |
The Boeing Company |
Variable pivot trailing edge flap
|
US4248395A
(en)
|
1975-03-24 |
1981-02-03 |
The Boeing Company |
Airplane wing trailing-edge flap-mounting mechanism
|
US4172575A
(en)
|
1975-03-24 |
1979-10-30 |
Boeing Commercial Airplane Company |
Airfoil flap conical extension mechanism
|
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
|
GB1596642A
(en)
|
1977-04-06 |
1981-08-26 |
British Aerospace |
Aircraft wings
|
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
(fr)
|
1978-06-01 |
1979-12-28 |
Sarrazin Applic Hydr |
Dispositif de commande integre pour circuit de fluide, et ses applications
|
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
|
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
|
US4395008A
(en)
|
1980-01-22 |
1983-07-26 |
British Aerospace Public Limited Company |
Aircraft wing and flap arrangement
|
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
|
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
|
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
|
US4427168A
(en)
*
|
1981-09-29 |
1984-01-24 |
The Boeing Company |
Variable camber leading edge mechanism with Krueger flap
|
US4471927A
(en)
|
1981-09-29 |
1984-09-18 |
The Boeing Company |
Trailing edge flap assembly
|
DE3140350C2
(de)
*
|
1981-10-10 |
1987-02-05 |
Dornier Gmbh, 7990 Friedrichshafen |
Profile, insbesondere Tragflügelprofile für 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
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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
|
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
|
US4706913A
(en)
|
1982-12-28 |
1987-11-17 |
The Boeing Company |
Variable camber leading edge assembly for an airfoil
|
US4475702A
(en)
|
1982-12-28 |
1984-10-09 |
The Boeing Company |
Variable camber leading edge assembly for an 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
|
GB8321281D0
(en)
|
1983-08-06 |
1983-09-28 |
British Aerospace |
Underwing engine installation
|
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
|
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
|
US4669687A
(en)
*
|
1985-03-06 |
1987-06-02 |
The Boeing Company |
Airfoil flap member with flap track member
|
DE3522448A1
(de)
|
1985-06-22 |
1987-01-02 |
Messerschmitt Boelkow Blohm |
Antriebs- und fuehrungsvorrichtung fuer eine an einem flugzeugtragfluegel angeordnete klappe
|
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
|
DE3620886A1
(de)
|
1986-06-21 |
1988-01-14 |
Messerschmitt Boelkow Blohm |
Antriebseinrichtung mit variablem drehmoment-begrenzungssystem
|
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
|
DE3702294C1
(de)
|
1987-01-27 |
1988-04-14 |
Messerschmitt Boelkow Blohm |
Stelleinrichtung fuer Tragflaechenklappen von Flugzeugen
|
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
|
US5046688A
(en)
|
1988-10-28 |
1991-09-10 |
The Boeing Company |
Wing major assembly jig
|
WO1990008674A1
(de)
|
1989-02-06 |
1990-08-09 |
Deutsche Airbus Gmbh |
Decken-gepäckablagen-kombination für 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
|
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
|
US5203619A
(en)
|
1990-11-07 |
1993-04-20 |
Intermetro Industries Corporation |
Storage system including a vertically retractable storage unit
|
DE4105459A1
(de)
|
1991-02-21 |
1992-08-27 |
Heilmeier & Weinlein |
Hydraulische steuervorrichtung
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JPH07112836B2
(ja)
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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
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DE4130644A1
(de)
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1991-09-14 |
1993-03-18 |
Airbus Gmbh |
Ueberkopf-gepaeckablage mit einer absenkbaren schale, insbesondere fuer ein passagierflugzeug
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US5158252A
(en)
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1991-10-24 |
1992-10-27 |
The Boeing Company |
Three-position variable camber Krueger leading edge flap
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DE4209037C2
(de)
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1992-03-20 |
1994-06-23 |
Deutsche Aerospace Airbus |
Vorrichtung zur Aufnahme von Gepäck in Flugzeugen
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FR2695905B1
(fr)
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1992-09-24 |
1994-12-16 |
Aerospatiale |
Bec kruger rigide, pour bord d'attaque de voilure d'aéronef.
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FR2709110B1
(fr)
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1993-08-20 |
1995-11-10 |
Lucas Air Equipement |
Dispositif de servocommande d'un organe de commande de vol d'aéronef.
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US5544847A
(en)
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1993-11-10 |
1996-08-13 |
The Boeing Company |
Leading edge slat/wing combination
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DE4422152C2
(de)
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1994-06-27 |
2000-02-03 |
Daimler Chrysler Aerospace |
Verfahren und Anordnung zum Optimieren der aerodynamischen Wirkung eines Tragflügels
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US5535852A
(en)
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1994-08-17 |
1996-07-16 |
Bishop; David J. |
Lift apparatus
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FR2728535A1
(fr)
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1994-12-26 |
1996-06-28 |
Aerospatiale |
Aerofrein a fente variable pour voilure d'aeronef
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US5680124A
(en)
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1995-05-15 |
1997-10-21 |
The Boeing Company |
Skew and loss detection system for adjacent high lift devices
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US5686907A
(en)
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1995-05-15 |
1997-11-11 |
The Boeing Company |
Skew and loss detection system for individual high lift devices
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US5609020A
(en)
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1995-05-15 |
1997-03-11 |
The Boeing Company |
Thrust reverser synchronization shaft lock
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US5875998A
(en)
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1996-02-05 |
1999-03-02 |
Daimler-Benz Aerospace Airbus Gmbh |
Method and apparatus for optimizing the aerodynamic effect of an airfoil
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US5743490A
(en)
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1996-02-16 |
1998-04-28 |
Sundstrand Corporation |
Flap/slat actuation system for an aircraft
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US6015117A
(en)
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1996-04-13 |
2000-01-18 |
Broadbent; Michael C |
Variable camber wing mechanism
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US5927656A
(en)
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1996-06-26 |
1999-07-27 |
The Boeing Company |
Wing leading edge flap and method therefor
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SE507968C2
(sv)
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1996-07-25 |
1998-08-03 |
Electrolux Ab |
Bäranordning, t.ex. för väggmonterad hushållsugn
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GB9619488D0
(en)
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1996-09-18 |
1996-10-30 |
Dowty Boulton Paul Ltd |
Flight control surface actuation system
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US5788190A
(en)
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1996-10-22 |
1998-08-04 |
The Boeing Company |
Slotted cruise trailing edge flap
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USRE44313E1
(en)
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1996-10-22 |
2013-06-25 |
The Boeing Company |
Airplane with unswept slotted cruise wing airfoil
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DE19712034A1
(de)
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1997-03-21 |
1998-09-24 |
Deutsch Zentr Luft & Raumfahrt |
Profilkante eines aerodynamischen Profils
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GB2323576B
(en)
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1997-03-26 |
2001-08-22 |
British Aerospace |
Fairing arrangements for aircraft
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US5934615A
(en)
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1997-08-25 |
1999-08-10 |
Hexcel Corporation |
Luggage bins with articulating mechanism
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US5921506A
(en)
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1997-09-25 |
1999-07-13 |
Northrop Grumman Corporation |
Extendible leading edge flap
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US5984230A
(en)
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1997-12-15 |
1999-11-16 |
Orazi; Paul |
Wing assemblies for aircraft
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US6079672A
(en)
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1997-12-18 |
2000-06-27 |
Lam; Lawrence Y. |
Aileron for fixed wing aircraft
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1998-01-14 |
2002-02-16 |
Saiz Manuel Munoz |
Mandos de vuelo con compensacion automatica.
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(de)
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1998-04-30 |
2000-06-15 |
Daimler Chrysler Aerospace |
Verfahren zur Reduktion von an einem Flugzeug auftretenden Böenlasten unterhalb der Reiseflughöhe
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(de)
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1998-05-21 |
2008-06-05 |
Mcdonnell Douglas Corp. |
Flügelprofil
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US6045204A
(en)
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1998-10-13 |
2000-04-04 |
Hexcel Corporation |
Overhead stowage bins in aircraft
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GB9823599D0
(en)
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1998-10-28 |
1998-12-23 |
Lucas Ind Plc |
Brake assembly
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FR2787759B1
(fr)
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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
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DE19910551C2
(de)
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1999-03-10 |
2001-04-05 |
Eads Airbus Gmbh |
Flugzeugtragfläche mit mindestens einem kurzgekoppelten Triebwerk
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US6328265B1
(en)
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1999-05-25 |
2001-12-11 |
Faruk Dizdarevic |
Slot forming segments and slot changing spoilers
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DE10001038B4
(de)
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2000-01-13 |
2004-01-29 |
Airbus Deutschland Gmbh |
Gepäckablage mit einem absenkbaren Gepäckfach, insbesondere für eine Flugzeugpassagierkabine
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US6598834B2
(en)
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2000-02-14 |
2003-07-29 |
Aerotech Services Inc. |
Method for reducing fuel consumption in aircraft
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(de)
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2000-04-17 |
2002-01-03 |
Airbus Gmbh |
Drucksteuerung für einen Verdrängungskörper
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JP2001343032A
(ja)
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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
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FR2811037B1
(fr)
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2000-06-28 |
2002-10-18 |
Aerospatiale Matra Airbus |
Systeme d'actionnement hydraulique a commande electrique
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US6443394B1
(en)
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2000-09-21 |
2002-09-03 |
The B.F. Goodrich Company |
Inflatable airfoil device
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(de)
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2000-11-11 |
2004-09-09 |
Eads Deutschland Gmbh |
Variabler Flügelbereich mit einstellbarer, sich in Spannweiten-Richtung erstreckender Profilform
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US6375126B1
(en)
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2000-11-16 |
2002-04-23 |
The Boeing Company |
Variable camber leading edge for an airfoil
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US20020046087A1
(en)
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2000-12-18 |
2002-04-18 |
John Hey |
Method of drawing attention to advertisements
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2001-04-10 |
2002-10-11 |
Stork Prod Eng |
Handbagagebaksamenstel met onderdrukmiddelen.
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US6547183B2
(en)
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2001-08-02 |
2003-04-15 |
The Boeing Company |
Moveable closet
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(en)
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2001-09-21 |
2003-07-17 |
Honeywell International, Inc. |
Interface for visual cueing and control for tactical flightpath management
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US6591169B2
(en)
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2001-09-27 |
2003-07-08 |
The Boeing Company |
Method and computer program product for controlling the actuators of an aerodynamic vehicle
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US6622972B2
(en)
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2001-10-31 |
2003-09-23 |
The Boeing Company |
Method and system for in-flight fault monitoring of flight control actuators
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US6601801B1
(en)
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2002-04-24 |
2003-08-05 |
The Boeing Company |
Gapped trailing-edge control surface for an airfoil
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US7258308B2
(en)
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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
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US6796534B2
(en)
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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
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US20040059474A1
(en)
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2002-09-20 |
2004-03-25 |
Boorman Daniel J. |
Apparatuses and methods for displaying autoflight information
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US7048235B2
(en)
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2002-10-09 |
2006-05-23 |
The Boeing Company |
Slotted aircraft wing
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US7243881B2
(en)
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2003-06-03 |
2007-07-17 |
The Boeing Company |
Multi-function trailing edge devices and associated methods
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US6799739B1
(en)
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2003-11-24 |
2004-10-05 |
The Boeing Company |
Aircraft control surface drive system and associated methods
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