FR2420480A1 - Gouverne d'avion - Google Patents
Gouverne d'avionInfo
- Publication number
- FR2420480A1 FR2420480A1 FR7907428A FR7907428A FR2420480A1 FR 2420480 A1 FR2420480 A1 FR 2420480A1 FR 7907428 A FR7907428 A FR 7907428A FR 7907428 A FR7907428 A FR 7907428A FR 2420480 A1 FR2420480 A1 FR 2420480A1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- rudder
- governor
- rotation
- axis
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/06—Adjustable control surfaces or members, e.g. rudders with two or more independent movements
Abstract
Gouverne d'avion pour l'obtention d'un moment aérodynamique, notamment sur l'empennage horizontal, sur les voilures de sustentation et/ou à la partie arrière du fuselage, pour le vol dans le domaine des angles d'attaque élevés ou très élevés. La gouverne possède, outre son axe de rotation A habituel, un deuxième axe de rotation B prévu dans sa partie h comprise entre le milieu et l'arrière de la gouverne.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19782813188 DE2813188B2 (de) | 1978-03-25 | 1978-03-25 | Ruder zur aerodynamischen Momentenerzeugung an Flugzeugen |
DE2828346 | 1978-06-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2420480A1 true FR2420480A1 (fr) | 1979-10-19 |
Family
ID=25774155
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7907428A Withdrawn FR2420480A1 (fr) | 1978-03-25 | 1979-03-23 | Gouverne d'avion |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPS54131300A (fr) |
FR (1) | FR2420480A1 (fr) |
GB (1) | GB2017020B (fr) |
IT (1) | IT1192641B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0017756A1 (fr) * | 1979-04-12 | 1980-10-29 | Dornier Gmbh | Gouvernes pour un aile d'avion |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2400585B (en) * | 2003-04-14 | 2006-08-09 | Nissan Technical Ct Europ Ltd | A spoiler |
FR2948628B1 (fr) * | 2009-08-03 | 2012-02-03 | Airbus Operations Sas | Avion a controle en lacet par trainee differentielle |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB524865A (en) * | 1939-01-27 | 1940-08-16 | Hendrik Martinus Arends | Improvements in the control surfaces of aircraft |
FR1231084A (fr) * | 1959-03-23 | 1960-09-26 | Perfectionnements aux surfaces aérodynamiques | |
DE2555070A1 (de) * | 1975-12-06 | 1977-06-16 | Ver Flugtechnische Werke | Klappenanordnung fuer flugzeuge |
US4049219A (en) * | 1975-02-03 | 1977-09-20 | The Boeing Company | Variable pivot trailing edge flap |
-
1979
- 1979-03-16 IT IT21057/79A patent/IT1192641B/it active
- 1979-03-23 GB GB7910350A patent/GB2017020B/en not_active Expired
- 1979-03-23 FR FR7907428A patent/FR2420480A1/fr not_active Withdrawn
- 1979-03-26 JP JP3448579A patent/JPS54131300A/ja active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB524865A (en) * | 1939-01-27 | 1940-08-16 | Hendrik Martinus Arends | Improvements in the control surfaces of aircraft |
FR1231084A (fr) * | 1959-03-23 | 1960-09-26 | Perfectionnements aux surfaces aérodynamiques | |
US4049219A (en) * | 1975-02-03 | 1977-09-20 | The Boeing Company | Variable pivot trailing edge flap |
DE2555070A1 (de) * | 1975-12-06 | 1977-06-16 | Ver Flugtechnische Werke | Klappenanordnung fuer flugzeuge |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0017756A1 (fr) * | 1979-04-12 | 1980-10-29 | Dornier Gmbh | Gouvernes pour un aile d'avion |
Also Published As
Publication number | Publication date |
---|---|
GB2017020A (en) | 1979-10-03 |
IT1192641B (it) | 1988-04-27 |
GB2017020B (en) | 1982-04-07 |
JPS54131300A (en) | 1979-10-12 |
IT7921057A0 (it) | 1979-03-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2001058756A3 (fr) | Aeronef | |
DE69402312D1 (de) | Aerodynamische hilfsstrukturen eines unbemannten luftfahrzeuges mit eingelassenen, koaxialen, gegendrehenden rotoren | |
FR2365482A1 (fr) | Ventilateur-propulseur pour fonctionnement a grande vitesse | |
FR2420480A1 (fr) | Gouverne d'avion | |
JPS6428096A (en) | Vertical stabilizer for aircraft | |
GB582206A (en) | Improvements in tailless airplanes | |
FR2430884A1 (fr) | Gouvernes pour avion | |
GB1183921A (en) | Improvements relating to Wing Pivots for Aircraft having Variable Sweep-back Wings | |
SE8704481D0 (sv) | Counterrotating aircraft propulsor blades | |
ES8304863A1 (es) | "perfeccionamientos en los perfiles de las alas para aviones de despegue y aterrizaje cortos". | |
ES2193064T3 (es) | Alas de aviongs | |
Reneaux | Numerical optimization method for airfoil design | |
SE7901512L (sv) | Ringformig vinge | |
HIRSCH et al. | Critical study of the effects of gusts on an aircraft | |
MIDDLETON | Study of supersonic wings employing the attainable leading-edge thrust concept[Final Report, Dec. 1980- Apr. 1982] | |
PORTER et al. | Investigation of the applicability of the free-wing principle to light, general aviation aircraft(Application of unconventional wing pivoting about spanwise axis forward of aerodynamic center for gust alleviation in general aviation aircraft) | |
FR2278569A1 (fr) | Aerodyne a aile circulaire | |
WORTMANN | Design of airfoils with high lift at low and medium subsonic machnumbers(Design characteristics and performance of airfoils with high lift at low and medium subsonic speeds and various angles of attack) | |
SU1839917A1 (ru) | Гидросамолет | |
ZIMMER | Aspects and results of profile development for circulation controlled rotor systems | |
GB1300986A (en) | A unitary cast aerofoil | |
FR2441902A2 (fr) | Dispositif de suspension multidirectionnelle pour giravion | |
SENYUTA et al. | Innovations for improving performance, aerodynamic properties of aircraft | |
JPS6416498A (en) | Rotor-blade for rotary-wing aircraft | |
Ahmed et al. | An experimental study of the aerodynamic characteristics of three model helicopter fuselages |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |