FR2769284B1 - Dispositif de commande d'une surface aerodynamique de direction d'un helicoptere - Google Patents
Dispositif de commande d'une surface aerodynamique de direction d'un helicoptereInfo
- Publication number
- FR2769284B1 FR2769284B1 FR9712453A FR9712453A FR2769284B1 FR 2769284 B1 FR2769284 B1 FR 2769284B1 FR 9712453 A FR9712453 A FR 9712453A FR 9712453 A FR9712453 A FR 9712453A FR 2769284 B1 FR2769284 B1 FR 2769284B1
- Authority
- FR
- France
- Prior art keywords
- helicopter
- steering
- controlling
- aerodynamic surface
- aerodynamic
- 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 - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8263—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like
- B64C2027/8272—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like comprising fins, or movable rudders
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Toys (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9712453A FR2769284B1 (fr) | 1997-10-07 | 1997-10-07 | Dispositif de commande d'une surface aerodynamique de direction d'un helicoptere |
US09/167,614 US6142413A (en) | 1997-10-07 | 1998-10-06 | Device for control of an aerodynamic steering surface of a helicopter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9712453A FR2769284B1 (fr) | 1997-10-07 | 1997-10-07 | Dispositif de commande d'une surface aerodynamique de direction d'un helicoptere |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2769284A1 FR2769284A1 (fr) | 1999-04-09 |
FR2769284B1 true FR2769284B1 (fr) | 1999-12-03 |
Family
ID=9511889
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9712453A Expired - Fee Related FR2769284B1 (fr) | 1997-10-07 | 1997-10-07 | Dispositif de commande d'une surface aerodynamique de direction d'un helicoptere |
Country Status (2)
Country | Link |
---|---|
US (1) | US6142413A (fr) |
FR (1) | FR2769284B1 (fr) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2793765B1 (fr) * | 1999-05-18 | 2001-07-13 | Eurocopter France | Dispositif de commande de vol d'un aeronef |
US6416015B1 (en) | 2001-05-01 | 2002-07-09 | Franklin D. Carson | Anti-torque and yaw-control system for a rotary-wing aircraft |
US7424988B2 (en) * | 2001-05-24 | 2008-09-16 | Mcdonnell Helicopter Company Llc | Use of aerodynamic forces to assist in the control and positioning of aircraft control surfaces and variable geometry systems |
US7182297B2 (en) * | 2003-01-17 | 2007-02-27 | The Insitu Group, Inc. | Method and apparatus for supporting aircraft components, including actuators |
US6755374B1 (en) | 2003-01-27 | 2004-06-29 | Franklin D. Carson | Anti-Torque and yaw-control system for a rotary-wing aircraft |
FR2871434B1 (fr) * | 2004-06-15 | 2006-08-18 | Eurocopter France | Procede optimise de commande de lacet d'un aeronef a voilure tournante et systeme pour sa mise en oeuvre |
US7644893B2 (en) * | 2006-02-15 | 2010-01-12 | Sikorsky Aircraft Corporation | Full authority fly-by-wire pedal system |
US7883059B2 (en) * | 2007-05-17 | 2011-02-08 | Insitu, Inc. | Actuator systems and associated methods for unmanned air vehicles and other applications |
US20090283628A1 (en) * | 2008-05-19 | 2009-11-19 | Frederickson Kirk C | Directional control arrangement to provide stabilizing feedback to a structural bending mode |
US8235327B2 (en) | 2009-03-18 | 2012-08-07 | Insitu, Inc. | Adjustable servomechanism assemblies and associated systems and methods |
US9815553B2 (en) * | 2013-07-01 | 2017-11-14 | Bell Helicopter Tectron Inc. | Independent hydraulic control system for rotorcraft secondary rotor |
FR3014411A1 (fr) * | 2013-12-10 | 2015-06-12 | Eurocopter France | Procede pour tendre a optimiser le bruit emis par un rotor auxiliaire et les performances d'un giravion, et un giravion |
CN207141375U (zh) * | 2017-08-21 | 2018-03-27 | 成都天府新区光启未来技术研究院 | 舵装置及具有其的飞行器 |
FR3108094B1 (fr) | 2020-03-12 | 2022-05-13 | Airbus Helicopters | procédé de commande d’au moins un organe aérodynamique de dérive d’un hélicoptère hybride et un hélicoptère hybride. |
CN114261525B (zh) * | 2021-12-30 | 2023-11-03 | 中国航天空气动力技术研究院 | 一种舵面偏转控制与测量系统及方法 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2818224A (en) | 1955-04-20 | 1957-12-31 | United Aircraft Corp | Airfoil contour pylon |
US3332643A (en) * | 1965-10-05 | 1967-07-25 | Piasecki Aircraft Corp | Control system for aircraft |
US3404737A (en) * | 1966-07-08 | 1968-10-08 | United Aircraft Corp | Control mechanism for swivel tail of an aircraft |
FR2167249B1 (fr) * | 1972-01-11 | 1974-06-21 | Aerospatiale | |
US3833188A (en) * | 1972-10-24 | 1974-09-03 | Hughes Tool Co | Pedal force trimming device |
FR2338845A1 (fr) * | 1976-01-26 | 1977-08-19 | Laville Andre | Dispositif de controle en lacet pour aerodynes sustentes par une voilure tournante entrainee mecaniquement |
FR2689854B1 (fr) * | 1992-04-14 | 1994-07-01 | Eurocopter France | Helicoptere monorotor a systeme anticouple mixte et procede pour contrecarrer le couple induit par ce monorotor. |
US5607122A (en) * | 1994-12-22 | 1997-03-04 | Bell Helicopter Textron Inc. | Tail rotor authority control for a helicopter |
-
1997
- 1997-10-07 FR FR9712453A patent/FR2769284B1/fr not_active Expired - Fee Related
-
1998
- 1998-10-06 US US09/167,614 patent/US6142413A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US6142413A (en) | 2000-11-07 |
FR2769284A1 (fr) | 1999-04-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20140630 |