FR2473466B1 - - Google Patents
Info
- Publication number
- FR2473466B1 FR2473466B1 FR8000443A FR8000443A FR2473466B1 FR 2473466 B1 FR2473466 B1 FR 2473466B1 FR 8000443 A FR8000443 A FR 8000443A FR 8000443 A FR8000443 A FR 8000443A FR 2473466 B1 FR2473466 B1 FR 2473466B1
- Authority
- FR
- France
- 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
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)
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8000443A FR2473466A1 (fr) | 1980-01-09 | 1980-01-09 | Avion a voilure fixe comportant des surfaces portantes placees en tandem |
| CA000367408A CA1148522A (en) | 1980-01-09 | 1980-12-23 | Fixed-wing aircraft with tandem supporting surfaces |
| EP80401899A EP0033053B1 (fr) | 1980-01-09 | 1980-12-31 | Avion à voilure fixe comportant des surfaces portantes placées en tandem |
| DE8080401899T DE3068634D1 (en) | 1980-01-09 | 1980-12-31 | Fixed-wing aircraft comprising airfoil surfaces disposed in tandem configuration |
| JP102681A JPS56149294A (en) | 1980-01-09 | 1981-01-07 | Fixed airfoil aircraft |
| US06/621,261 US4598888A (en) | 1980-01-09 | 1984-06-15 | Fixed-wing aircraft with tandem supporting surfaces |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8000443A FR2473466A1 (fr) | 1980-01-09 | 1980-01-09 | Avion a voilure fixe comportant des surfaces portantes placees en tandem |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2473466A1 FR2473466A1 (fr) | 1981-07-17 |
| FR2473466B1 true FR2473466B1 (US07655746-20100202-C00011.png) | 1982-10-29 |
Family
ID=9237390
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR8000443A Granted FR2473466A1 (fr) | 1980-01-09 | 1980-01-09 | Avion a voilure fixe comportant des surfaces portantes placees en tandem |
Country Status (6)
Families Citing this family (36)
| 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 |
| WO1997030893A1 (en) * | 1996-02-23 | 1997-08-28 | Trimbach Turbine, Ltd. | Aircraft having multiple fuselages |
| 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 |
| DE10362037B4 (de) * | 2003-02-03 | 2010-04-29 | Airbus Deutschland Gmbh | Verfahren zur Dämpfung von Rumpfschwingungen eines Tragflügelflugzeugs sowie Tragflügelflugzeug |
| 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. |
| 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)
| 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 |
-
1980
- 1980-01-09 FR FR8000443A patent/FR2473466A1/fr active Granted
- 1980-12-23 CA CA000367408A patent/CA1148522A/en not_active Expired
- 1980-12-31 EP EP80401899A patent/EP0033053B1/fr not_active Expired
- 1980-12-31 DE DE8080401899T patent/DE3068634D1/de not_active Expired
-
1981
- 1981-01-07 JP JP102681A patent/JPS56149294A/ja active Pending
-
1984
- 1984-06-15 US US06/621,261 patent/US4598888A/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| FR2473466A1 (fr) | 1981-07-17 |
| EP0033053A1 (fr) | 1981-08-05 |
| DE3068634D1 (en) | 1984-08-23 |
| US4598888A (en) | 1986-07-08 |
| CA1148522A (en) | 1983-06-21 |
| EP0033053B1 (fr) | 1984-07-18 |
| JPS56149294A (en) | 1981-11-19 |
