FR2480704A1 - Perfectionnements aux avions de combat munis de dispositifs de stabilisation laterale - Google Patents

Perfectionnements aux avions de combat munis de dispositifs de stabilisation laterale Download PDF

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Publication number
FR2480704A1
FR2480704A1 FR8107831A FR8107831A FR2480704A1 FR 2480704 A1 FR2480704 A1 FR 2480704A1 FR 8107831 A FR8107831 A FR 8107831A FR 8107831 A FR8107831 A FR 8107831A FR 2480704 A1 FR2480704 A1 FR 2480704A1
Authority
FR
France
Prior art keywords
aircraft
nose
longitudinal axis
beard
combat aircraft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
FR8107831A
Other languages
English (en)
French (fr)
Other versions
FR2480704B1 (enExample
Inventor
Donald Pierce
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Publication of FR2480704A1 publication Critical patent/FR2480704A1/fr
Application granted granted Critical
Publication of FR2480704B1 publication Critical patent/FR2480704B1/fr
Granted legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Separation By Low-Temperature Treatments (AREA)
  • Toys (AREA)
  • Emergency Lowering Means (AREA)
FR8107831A 1980-04-18 1981-04-17 Perfectionnements aux avions de combat munis de dispositifs de stabilisation laterale Granted FR2480704A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8012872 1980-04-18

Publications (2)

Publication Number Publication Date
FR2480704A1 true FR2480704A1 (fr) 1981-10-23
FR2480704B1 FR2480704B1 (enExample) 1984-05-25

Family

ID=10512872

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8107831A Granted FR2480704A1 (fr) 1980-04-18 1981-04-17 Perfectionnements aux avions de combat munis de dispositifs de stabilisation laterale

Country Status (3)

Country Link
US (1) US4378922A (enExample)
FR (1) FR2480704A1 (enExample)
GB (1) GB2076109B (enExample)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1235222B (it) * 1982-11-26 1992-06-26 Secratary Of State For Defence Perfezionamento nelle fusoliere di missili e simili
US4569494A (en) * 1982-12-23 1986-02-11 The Boeing Company Pitch control of swept wing aircraft
US4540143A (en) * 1983-08-04 1985-09-10 The Boeing Company Nacelle/wing assembly with wake control device
GB2162610B (en) * 1984-08-02 1987-12-16 Thomas Henderson Regulation of response of bodies to a fluid flow
US4655419A (en) * 1984-12-31 1987-04-07 The Boeing Company Vortex generator
US4691879A (en) * 1986-06-16 1987-09-08 Greene Vibert F Jet airplane
US4884772A (en) * 1986-07-28 1989-12-05 The Boeing Company Cantilevered vortex control device
US4917333A (en) * 1988-05-11 1990-04-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Actuated forebody strakes
US5056741A (en) * 1989-09-29 1991-10-15 The Boeing Company Apparatus and method for aircraft wing stall control
US5150861A (en) * 1990-01-26 1992-09-29 The Boeing Company Variable sweep side force generator and roll control device
US5207397A (en) * 1990-06-08 1993-05-04 Eidetics International, Inc. Rotatable nose and nose boom strakes and methods for aircraft stability and control
US5366180A (en) * 1993-06-30 1994-11-22 Northrop Corporation High-lift device for aircraft
US5901925A (en) * 1996-08-28 1999-05-11 Administrator, National Aeronautics And Space Administration Serrated-planform lifting-surfaces
RU2118271C1 (ru) * 1997-08-27 1998-08-27 Сергей Владимирович Горюнов Головной обтекатель летательного аппарата
US6186445B1 (en) * 1998-03-06 2001-02-13 Paul F. Batcho Method and apparatus for mitigating junction flows
US6318677B1 (en) 1999-08-06 2001-11-20 Charles J. Dixon Method and apparatus for generating a stable leading-edge lifting-vortex controller
US6614626B2 (en) 2000-12-29 2003-09-02 Seagate Technology Llc Saw tooth actuator for a disc drive
US6698684B1 (en) 2002-01-30 2004-03-02 Gulfstream Aerospace Corporation Supersonic aircraft with spike for controlling and reducing sonic boom
JP4220393B2 (ja) 2002-01-30 2009-02-04 ガルフストリーム・エアロスペース・コーポレイション ソニック・ブームの制御及び低減のための超音速航空機の胴体成形及びスパイク状組込体
US6715717B2 (en) 2002-09-06 2004-04-06 Charles J. Dixon Method and apparatus for inducing controlled vortices to reduce afterbody drag
US8333076B2 (en) 2005-12-15 2012-12-18 Gulfstream Aerospace Corporation Isentropic compression inlet for supersonic aircraft
US8393158B2 (en) * 2007-10-24 2013-03-12 Gulfstream Aerospace Corporation Low shock strength inlet
DE102010047643A1 (de) * 2010-10-06 2012-04-12 Airbus Operations Gmbh Vorrichtung und ein Verfahren zum Erhöhen des aerodynamischen Auftriebs an einem Flugzeug
US9428264B2 (en) * 2010-11-02 2016-08-30 Japan Aerospace Exploration Agency Nose for supersonic flying object
US10669026B2 (en) 2016-04-01 2020-06-02 Albert Aguilar Lift cell modules and lift pods

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1522282A (fr) * 1967-02-15 1968-04-26 Sud Aviation Procédé et dispositif améliorant la stabilité de lacet des aérodynes aux grandes incidences de vol
FR2012571A1 (enExample) * 1968-07-09 1970-03-20 Battelle Development Corp

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2694357A (en) * 1950-07-18 1954-11-16 Chance Vought Aircraft Inc Boundary layer energization for flush inlets
GB1119701A (en) * 1964-08-13 1968-07-10 Bristol Siddeley Engines Ltd Guards for air intakes of jet engines
US3744745A (en) * 1971-09-30 1973-07-10 Mc Donnell Douglas Corp Liftvanes
US4176813A (en) * 1977-10-05 1979-12-04 Northrop Corporation Shark nose for aircraft
US4225102A (en) * 1979-03-12 1980-09-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aerodynamic side-force alleviator means

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1522282A (fr) * 1967-02-15 1968-04-26 Sud Aviation Procédé et dispositif améliorant la stabilité de lacet des aérodynes aux grandes incidences de vol
FR2012571A1 (enExample) * 1968-07-09 1970-03-20 Battelle Development Corp

Also Published As

Publication number Publication date
US4378922A (en) 1983-04-05
FR2480704B1 (enExample) 1984-05-25
GB2076109B (en) 1983-10-12
GB2076109A (en) 1981-11-25

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