CA1148522A - Fixed-wing aircraft with tandem supporting surfaces - Google Patents

Fixed-wing aircraft with tandem supporting surfaces

Info

Publication number
CA1148522A
CA1148522A CA000367408A CA367408A CA1148522A CA 1148522 A CA1148522 A CA 1148522A CA 000367408 A CA000367408 A CA 000367408A CA 367408 A CA367408 A CA 367408A CA 1148522 A CA1148522 A CA 1148522A
Authority
CA
Canada
Prior art keywords
canard
aircraft
flight
fuselage
trailing edge
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.)
Expired
Application number
CA000367408A
Other languages
English (en)
French (fr)
Inventor
Roger H. Beteille
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.)
Airbus SAS
Original Assignee
Airbus SAS
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 Airbus SAS filed Critical Airbus SAS
Application granted granted Critical
Publication of CA1148522A publication Critical patent/CA1148522A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/12—Canard-type aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
CA000367408A 1980-01-09 1980-12-23 Fixed-wing aircraft with tandem supporting surfaces Expired CA1148522A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8000443 1980-01-09
FR8000443A FR2473466A1 (fr) 1980-01-09 1980-01-09 Avion a voilure fixe comportant des surfaces portantes placees en tandem

Publications (1)

Publication Number Publication Date
CA1148522A true CA1148522A (en) 1983-06-21

Family

ID=9237390

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000367408A Expired CA1148522A (en) 1980-01-09 1980-12-23 Fixed-wing aircraft with tandem supporting surfaces

Country Status (6)

Country Link
US (1) US4598888A (enExample)
EP (1) EP0033053B1 (enExample)
JP (1) JPS56149294A (enExample)
CA (1) CA1148522A (enExample)
DE (1) DE3068634D1 (enExample)
FR (1) FR2473466A1 (enExample)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1152763B (it) * 1982-01-25 1987-01-14 Ind Aeronautiche E Meccaniche Aeromobile perfezionato
US4797829A (en) * 1986-12-11 1989-01-10 Grumman Aerospace Corporation Flight control optimization system for multi-control surface aircraft
US5098034A (en) * 1989-11-24 1992-03-24 Lendriet William C Vertical/short takeoff or landing aircraft having a rotatable wing and tandem supporting surfaces
US5071088A (en) * 1989-11-29 1991-12-10 The United States Of America As Represented By The Secretary Of The Navy High lift aircraft
US5020740A (en) * 1990-03-28 1991-06-04 Thomas Hugh O Pitch control trimming system for canard design aircraft
US5201478A (en) * 1990-04-06 1993-04-13 Wooley Don H Airplane efficiency, safety and utilization
US5083279A (en) * 1990-05-09 1992-01-21 Honeywell, Inc. Canard based high angle of attack air data sensor
US5094411A (en) * 1990-10-19 1992-03-10 Vigyan, Inc. Control configured vortex flaps
FR2668750B1 (fr) * 1990-11-06 1993-01-22 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
US5320306A (en) * 1992-10-14 1994-06-14 Gennaro Mark A Aircraft construction
FR2719548B1 (fr) * 1994-05-03 1996-07-05 Aerospatiale Avion de transport à empennage avant.
US5503351A (en) * 1994-09-06 1996-04-02 Vass; Gabor I. Circular wing aircraft
US6047923A (en) * 1995-01-13 2000-04-11 Trimbach Turbine, Ltd. Aircraft having multiple fuselages
EP0877706A4 (en) * 1996-02-23 2000-11-22 Trimbach Turbine Ltd PLANE WITH SEVERAL FUSELAGE
US5992796A (en) * 1997-03-13 1999-11-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Secondary wing system for use on an aircraft
US5947422A (en) * 1997-04-29 1999-09-07 Mcdonnell Douglas Tail for an aircraft
DE19835191C1 (de) * 1998-08-04 2000-04-20 Daimler Chrysler Ag Flugsteuerungseinrichtung zur Verbesserung der Längsstabilität eines geregelten Flugzeugs
US6543720B2 (en) * 1998-10-13 2003-04-08 Paul Vincent Ladd Directional control and aerofoil system for aircraft
DE19857644C2 (de) * 1998-12-14 2001-11-29 Eads Airbus Gmbh Passagierflugzeug mit geradem oder gepfeiltem Entenleitwerk
US6666406B2 (en) * 2000-06-29 2003-12-23 The Boeing Company Blended wing and multiple-body airplane configuration
US6915989B2 (en) * 2002-05-01 2005-07-12 The Boeing Company Aircraft multi-axis modal suppression system
US6705567B2 (en) * 2002-05-06 2004-03-16 The Boeing Company Tandem wing aircraft and method for manufacturing and operating such aircraft
US6776376B2 (en) 2002-10-18 2004-08-17 Hamilton Sunstrand Flight control surface actuation system
DE10304336B4 (de) * 2003-02-03 2011-02-24 Eurocopter Deutschland Gmbh Verfahren zur Dämpfung von Heckausleger-Schwingungen von Drehflügelflugzeugen und Drehflügelflugzeug mit einer Heckausleger-Schwingungsdämpfungsvorrichtung
GB0310010D0 (en) * 2003-04-29 2003-11-26 Mass Consultants Ltd Control system for craft and a method of controlling craft
US7111810B2 (en) * 2004-02-09 2006-09-26 Northrop Grumman Corporation Forward pivoted full flying control tail boom
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
ES2356788B1 (es) * 2007-12-18 2012-02-22 Airbus Operations, S.L. Método y sistema para un cálculo rápido de las fuerzas aerodinámicas en una aeronave.
RU2397109C2 (ru) * 2008-08-26 2010-08-20 Андрей Леонидович Шпади Способ планирующего полета и летательный аппарат для осуществления способа
DE102013020601B4 (de) * 2013-12-11 2018-03-22 Airbus Defence and Space GmbH Flugzeugkonfiguration
RU2586741C1 (ru) * 2015-04-21 2016-06-10 Николай Евгеньевич Староверов Электродистанционное управление "утка"
JP6606639B2 (ja) * 2015-04-27 2019-11-20 映二 白石 貨物輸送用の航空機
US10780977B2 (en) * 2016-02-17 2020-09-22 Hamilton Sunstrand Corporation Aerodynamic control surface movement monitoring system
FR3052742B1 (fr) * 2016-06-16 2021-10-29 Airbus Operations Sas Aeronef presentant des gouvernes de profondeur independantes
US10501201B2 (en) * 2017-03-27 2019-12-10 Hamilton Sundstrand Corporation Aerodynamic control surface movement monitoring system for aircraft
US10543902B2 (en) * 2017-03-31 2020-01-28 Hamilton Sundstrand Corporation Laser reflection aerodynamic control surface movement monitoring system
WO2022260894A1 (en) * 2021-06-11 2022-12-15 Patey Michael J Aircraft wing assemblies

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR943005A (fr) * 1942-03-27 1949-02-24 Miles Aircraft Ltd Perfectionnements apportés aux avions
US2402311A (en) * 1943-09-17 1946-06-18 Ernest E Bissett Airplane
US2430793A (en) * 1944-07-07 1947-11-11 Curtiss Wright Corp Aircraft elevator construction
US2541620A (en) * 1945-09-29 1951-02-13 Edward A Stalker Control of aircraft pitching
US2601962A (en) * 1946-01-29 1952-07-01 Douglas Aircraft Co Inc Aircraft balancing means
US2747816A (en) * 1950-05-11 1956-05-29 Ben O Howard Canard type airplane and controls therefor
FR1032665A (fr) * 1950-12-23 1953-07-03 Perfectionnements apportés aux engins de navigation aérienne
US2924400A (en) * 1953-05-22 1960-02-09 Nord Aviation Apparatus for enabling the manoeuvrability and the stability of a supersonic aircraft to be controlled
US3240447A (en) * 1962-01-10 1966-03-15 North American Aviation Inc Vehicle control system
US3253809A (en) * 1963-12-20 1966-05-31 Wren Aircraft Corp Ultra low speed aircraft
US3362659A (en) * 1965-07-06 1968-01-09 Razak Charles Kenneth Method and apparatus for landing jet aircraft
US3680816A (en) * 1969-12-29 1972-08-01 Mc Donnell Douglas Corp Aircraft having auxiliary airfoils
US3848833A (en) * 1972-07-14 1974-11-19 Sperry Rand Corp Aircraft automatic flight control system
FR2272893A1 (en) * 1974-03-18 1975-12-26 Elliott Brothers London Ltd Powered aircraft with small front wing - has freely rotating tabs on front wing forming elevators
US3954231A (en) * 1974-09-09 1976-05-04 Fraser Norman T L Control system for forward wing aircraft
US4159088A (en) * 1977-01-03 1979-06-26 The Boeing Company System for reducing aircraft fuel consumption
US4124180A (en) * 1977-09-08 1978-11-07 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Free wing assembly for an aircraft

Also Published As

Publication number Publication date
US4598888A (en) 1986-07-08
EP0033053A1 (fr) 1981-08-05
JPS56149294A (en) 1981-11-19
FR2473466A1 (fr) 1981-07-17
FR2473466B1 (enExample) 1982-10-29
EP0033053B1 (fr) 1984-07-18
DE3068634D1 (en) 1984-08-23

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Legal Events

Date Code Title Description
MKEX Expiry
MKEX Expiry

Effective date: 20000621