ATE378250T1 - Fluggerät mit drehbarer vorderkante des rumpfes und der tragflügel - Google Patents

Fluggerät mit drehbarer vorderkante des rumpfes und der tragflügel

Info

Publication number
ATE378250T1
ATE378250T1 AT06075433T AT06075433T ATE378250T1 AT E378250 T1 ATE378250 T1 AT E378250T1 AT 06075433 T AT06075433 T AT 06075433T AT 06075433 T AT06075433 T AT 06075433T AT E378250 T1 ATE378250 T1 AT E378250T1
Authority
AT
Austria
Prior art keywords
leading edge
wings
aircraft
fuse
rotatable leading
Prior art date
Application number
AT06075433T
Other languages
English (en)
Inventor
Allen A Arata
Original Assignee
Northrop Grumman Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Northrop Grumman Corp filed Critical Northrop Grumman Corp
Application granted granted Critical
Publication of ATE378250T1 publication Critical patent/ATE378250T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
AT06075433T 2005-02-25 2006-02-24 Fluggerät mit drehbarer vorderkante des rumpfes und der tragflügel ATE378250T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/066,354 US7246770B2 (en) 2005-02-25 2005-02-25 Aircraft with rotatable leading edge of fuselage and wings

Publications (1)

Publication Number Publication Date
ATE378250T1 true ATE378250T1 (de) 2007-11-15

Family

ID=36179036

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06075433T ATE378250T1 (de) 2005-02-25 2006-02-24 Fluggerät mit drehbarer vorderkante des rumpfes und der tragflügel

Country Status (5)

Country Link
US (1) US7246770B2 (de)
EP (1) EP1695903B1 (de)
AT (1) ATE378250T1 (de)
DE (1) DE602006000224T2 (de)
ES (1) ES2297796T3 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7204454B2 (en) * 2005-02-25 2007-04-17 Northrop Grumman Corporation Aircraft with articulated leading edge of fuselage and wings
US20120141278A1 (en) * 2011-09-06 2012-06-07 General Electric Company Rotor blade assembly and method for modifying load characteristic of rotor blade in wind turbine
EP3231702B1 (de) 2016-04-11 2020-06-17 Asco Industries NV Hochauftriebsvorrichtung
CN115571323A (zh) * 2022-12-08 2023-01-06 中国空气动力研究与发展中心计算空气动力研究所 一种亚声速扁平融合体布局飞行器
CN116985994B (zh) * 2023-09-21 2023-11-28 中国空气动力研究与发展中心计算空气动力研究所 一种隐形飞行器

Family Cites Families (58)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1215295A (en) * 1916-03-14 1917-02-06 Donald Mackay Aeroplane.
US1353666A (en) * 1920-07-06 1920-09-21 Handley Page Ltd Wing and similar member of aircraft
US1414200A (en) 1921-04-27 1922-04-25 Handley Page Ltd Wing and similar member of aircraft
US1427012A (en) 1922-01-04 1922-08-22 Handley Page Ltd Wing and similar member of aircraft
US1606117A (en) * 1926-06-16 1926-11-09 Joseph A Caples Combination aeroplane
US1730249A (en) * 1926-10-04 1929-10-01 Schmidt John Airplane
US1867013A (en) 1929-06-15 1932-07-12 Herbert J Kratzer Pilot vane for the aerofoil wings of airplanes
US1818000A (en) 1930-03-19 1931-08-11 Curtiss Aeroplane & Motor Co Aerofoil operating mechanism
US1891261A (en) 1931-10-05 1932-12-20 Charles H Gunn Safety wing for airplanes
US1945254A (en) 1931-11-02 1934-01-30 Charles C Bittner Aeroplane
US2500512A (en) 1947-03-08 1950-03-14 Bell Aircraft Corp Wing lift modification means
US2793826A (en) 1956-03-23 1957-05-28 Willy A Fiedler Split aircraft wing
US3170657A (en) 1960-05-02 1965-02-23 John M Riebe Landing arrangement for aerial vehicle
US3153523A (en) 1963-05-27 1964-10-20 Iii Jefferson S Lowman Variable lift aircraft wing pivotally mounted for movement about a skewed longitudinal axis
FR94080E (fr) * 1963-12-27 1969-06-27 Breguet Aviat Avion a configuration variable.
US3447761A (en) 1967-06-12 1969-06-03 Boeing Co Supersonic airplane variable-sweep integrated airfoil system
US3486720A (en) 1967-12-07 1969-12-30 Boeing Co Continuous slot forming leading edge slats for cranked wings
US3630471A (en) * 1969-03-07 1971-12-28 Occidental Aircraft Corp Nose slat fuselage lifting body
DE1917532C3 (de) 1969-04-05 1974-05-30 Dornier Gmbh, 7990 Friedrichshafen Spaltklappenanordnung an Tragflügeln für Luftfahrzeuge
US3847369A (en) 1973-03-08 1974-11-12 Us Navy Control surface deployment mechanism
US4008867A (en) 1974-08-16 1977-02-22 Kaniut Herbert M Aircraft with safety tail unit
DE2656692C2 (de) 1976-12-15 1982-07-29 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Entenflugzeug
GB2003807A (en) 1977-08-23 1979-03-21 British Aircraft Corp Ltd Aircraft
DE2751361C2 (de) 1977-11-17 1984-09-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zur Flugzeugsteuerung durch Steuerung abgelöster Flügelvorderkanten-Wirbelströme
DE3013909A1 (de) 1979-04-17 1980-10-30 De Moura Mauricio Jose I Pinto Verfahren und vorrichtung zur aenderung der fluegelumriss-geometrie von flugzeugen waehrend des fluges
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
DE3122137A1 (de) 1981-06-04 1982-12-23 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Vorderkantenklappensystem fuer flugzeugfluegel
US4494713A (en) * 1982-06-24 1985-01-22 Kyusik Kim Shockcone and channeled disk-airframe
US4729528A (en) 1983-02-28 1988-03-08 Northrop Corporation Aeroelastic control flap
US4585192A (en) 1983-03-30 1986-04-29 British Aerospace Public Limited Company Leading edge arrangements for aircraft wings
US4667898A (en) * 1985-08-02 1987-05-26 The United States Of America As Represented By The Secretary Of The Navy Aircraft with single surface membranous airfoils
USD314366S (en) * 1989-04-19 1991-02-05 Northrop Corporation Aircraft
US5056741A (en) 1989-09-29 1991-10-15 The Boeing Company Apparatus and method for aircraft wing stall control
US5062595A (en) 1990-04-26 1991-11-05 University Of Southern California Delta wing with lift enhancing flap
US5156358A (en) * 1991-04-11 1992-10-20 Northrop Corporation Aircraft outboard control
US5897076A (en) 1991-07-08 1999-04-27 Tracy; Richard R. High-efficiency, supersonic aircraft
US5158252A (en) 1991-10-24 1992-10-27 The Boeing Company Three-position variable camber Krueger leading edge flap
US5312070A (en) 1992-04-02 1994-05-17 Grumman Aerospace Corporation Segmented variable sweep wing aircraft
US5538201A (en) * 1993-12-14 1996-07-23 Northrop Grumman Corporation Supersonic natural laminar flow wing
US5681013A (en) 1995-12-26 1997-10-28 The Boeing Company Vortex leading edge flap assembly for supersonic airplanes
US5927656A (en) 1996-06-26 1999-07-27 The Boeing Company Wing leading edge flap and method therefor
US5921506A (en) 1997-09-25 1999-07-13 Northrop Grumman Corporation Extendible leading edge flap
US6073889A (en) 1997-10-16 2000-06-13 The Boeing Company Wing flap seal bump
US6732974B1 (en) * 1997-11-19 2004-05-11 Accurate Automation Corporation Tiperon
US6220551B1 (en) 1998-01-14 2001-04-24 Manuel Munoz Saiz Flight controls with automatic balance
US6068219A (en) * 1998-04-13 2000-05-30 Northrop Grumman Corporation Single surface multi axis aircraft control
DE69916360T3 (de) 1998-05-21 2008-06-05 Mcdonnell Douglas Corp. Flügelprofil
GB9816936D0 (en) 1998-08-05 1998-09-30 British Aerospace An aerofoil having a slat
US6129308A (en) 1998-09-21 2000-10-10 Northrop Grumman Corporation Delta-shaped aircraft with variable camber fuselage and wing
US6328265B1 (en) 1999-05-25 2001-12-11 Faruk Dizdarevic Slot forming segments and slot changing spoilers
US6179248B1 (en) * 1999-11-04 2001-01-30 Aereon Corporation Aircraft
US6475933B1 (en) 2000-01-27 2002-11-05 Northrop Grumman Corporation Highly conductive elastomeric sheet
US6343768B1 (en) * 2000-05-16 2002-02-05 Patrick John Muldoon Vertical/short take-off and landing aircraft
US6659394B1 (en) * 2000-05-31 2003-12-09 The United States Of America As Represented By The Secretary Of The Air Force Compound tilting wing for high lift stability and control of aircraft
US6375126B1 (en) 2000-11-16 2002-04-23 The Boeing Company Variable camber leading edge for an airfoil
GB0114634D0 (en) 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
US6634594B1 (en) * 2002-05-03 2003-10-21 The Boeing Company Hypersonic waverider variable leading edge flaps
CA2444869A1 (en) * 2002-10-21 2004-04-21 The Boeing Company Method and apparatus for actuating movable components, including canards, over multiple ranges

Also Published As

Publication number Publication date
DE602006000224D1 (de) 2007-12-27
ES2297796T3 (es) 2008-05-01
EP1695903A1 (de) 2006-08-30
EP1695903B1 (de) 2007-11-14
DE602006000224T2 (de) 2008-09-18
US20070102586A1 (en) 2007-05-10
US7246770B2 (en) 2007-07-24

Similar Documents

Publication Publication Date Title
DE602007009720D1 (de) Flugzeugflügel
WO2007095931A3 (de) Aerodynamische klappe eines flugzeugs mit einer den klappenwirbel beeinflussenden vorrichtung
US9464532B2 (en) System and method for reducing rotor blade noise
ATE498548T1 (de) Luftfahrzeug mit zugangsöffnung zur beladung
WO2011010155A3 (en) Steering vehicles through control of aerofoils
CN205059998U (zh) 一种用于飞机的增升装置
DE602006015498D1 (de) Dichtungsanordnungen zur verwendung mit regeldifferenzspoilern und anderen steuerungsflächen auf einem flugzeug
BR112018009344A8 (pt) veículo aéreo com componentes desdobráveis
ATE427883T1 (de) Flugelspitzenvorrichtung
NO20070810A (no) System for å kontrollere flygeretning
GB2447176A (en) Wing load alleviation apparatus and method
DE602007009390D1 (de) Flugzeug mit konvertierbarem flugsystem
WO2011069887A3 (de) Hochauftriebssystem für ein flugzeug, verfahren zum bewegen einer auftriebsklappe und flugzeug mit einem hochauftriebssystem
ATE465082T1 (de) Flugzeugvorderkantenvorrichtungs-systeme und entsprechende dimensionierungsverfahren
CN204489176U (zh) 一种无尾飞翼布局飞机的阻力方向舵
DE502006002312D1 (de) Flugzeugflügel mit ausfahrbarer Nasenklappe
ATE378250T1 (de) Fluggerät mit drehbarer vorderkante des rumpfes und der tragflügel
ATE542739T1 (de) Flugzeugflügel
ATE382014T1 (de) Fluggerät mit vorwärts ausfahrbarer vorderkante des rumpfes und der tragflügel
BR0316038B1 (pt) combinaÇço de uma asa e fuselagem de aeronave
ATE380145T1 (de) Fluggerät mit gelenkig verbundener vorderkante des rumpfes und der tragflügel
ES2174690A1 (es) Disposicion sustentadora para aviones.
WO2007018772A3 (en) Rotor blade assembly with high pitching moment airfoil section for a rotary wing aircraft
WO2005044661A3 (en) Supersonic aircraft with aerodynamic control
DE602005007608D1 (de) Bewegliche vorderkantenklappe für einen hauptflügel der tragflächen eines flugzeugs

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties