FR2769285B1 - Dispositif de commande d'un systeme anticouple mixte d'un helicoptere - Google Patents

Dispositif de commande d'un systeme anticouple mixte d'un helicoptere

Info

Publication number
FR2769285B1
FR2769285B1 FR9712454A FR9712454A FR2769285B1 FR 2769285 B1 FR2769285 B1 FR 2769285B1 FR 9712454 A FR9712454 A FR 9712454A FR 9712454 A FR9712454 A FR 9712454A FR 2769285 B1 FR2769285 B1 FR 2769285B1
Authority
FR
France
Prior art keywords
helicopter
controlling
couple system
mixed anti
mixed
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
Application number
FR9712454A
Other languages
English (en)
Other versions
FR2769285A1 (fr
Inventor
Andre Michel Louis Dequin
Valery Lionel Delisle
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 Helicopters SAS
Original Assignee
Eurocopter France SA
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 Eurocopter France SA filed Critical Eurocopter France SA
Priority to FR9712454A priority Critical patent/FR2769285B1/fr
Priority to US09/167,613 priority patent/US6290171B1/en
Publication of FR2769285A1 publication Critical patent/FR2769285A1/fr
Application granted granted Critical
Publication of FR2769285B1 publication Critical patent/FR2769285B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • 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)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
FR9712454A 1997-10-07 1997-10-07 Dispositif de commande d'un systeme anticouple mixte d'un helicoptere Expired - Fee Related FR2769285B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9712454A FR2769285B1 (fr) 1997-10-07 1997-10-07 Dispositif de commande d'un systeme anticouple mixte d'un helicoptere
US09/167,613 US6290171B1 (en) 1997-10-07 1998-10-06 Device for controlling a helicopter hybrid countertorque system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9712454A FR2769285B1 (fr) 1997-10-07 1997-10-07 Dispositif de commande d'un systeme anticouple mixte d'un helicoptere

Publications (2)

Publication Number Publication Date
FR2769285A1 FR2769285A1 (fr) 1999-04-09
FR2769285B1 true FR2769285B1 (fr) 1999-12-03

Family

ID=9511890

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9712454A Expired - Fee Related FR2769285B1 (fr) 1997-10-07 1997-10-07 Dispositif de commande d'un systeme anticouple mixte d'un helicoptere

Country Status (2)

Country Link
US (1) US6290171B1 (fr)
FR (1) FR2769285B1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR2916418B1 (fr) 2007-05-22 2009-08-28 Eurocopter France Helicoptere hybride rapide a grande distance franchissable.
FR2926786B1 (fr) * 2008-01-30 2010-02-19 Eurocopter France Procede d'optimisation d'un rotor anti-couple carene a gene acoustique minimale pour un giravion, notamment un helicoptere, et rotor anti-couple carene ainsi obtenu
US8271151B2 (en) 2008-03-31 2012-09-18 Sikorsky Aircraft Corporation Flight control system for rotary wing aircraft
FR2943620B1 (fr) 2009-03-27 2012-08-17 Eurocopter France Procede et dispositif pour optimiser le point de fonctionnement d'helices propulsives disposees de part et d'autre du fuselage d'un giravion
US8882024B1 (en) * 2013-06-24 2014-11-11 Bell Helicopter Textron Inc. Rotorcraft anti-torque rotor and rudder system
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
JP5979798B2 (ja) * 2015-01-07 2016-08-31 エアバス ヘリコプターズ 補助回転翼から出る騒音と回転翼航空機の性能の双方の最適化に貢献する方法及び回転翼航空機

Family Cites Families (10)

* Cited by examiner, † Cited by third party
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
US3464651A (en) * 1967-05-02 1969-09-02 United Aircraft Corp Rotor load proportioner for a compound helicopter
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
JP3051357B2 (ja) * 1997-03-26 2000-06-12 株式会社コミュータヘリコプタ先進技術研究所 主ロータトルク補正装置

Also Published As

Publication number Publication date
FR2769285A1 (fr) 1999-04-09
US6290171B1 (en) 2001-09-18

Similar Documents

Publication Publication Date Title
FR2764560B1 (fr) Dispositif de commande d'un systeme de transmission de couple
FR2756229B1 (fr) Dispositif de commande d'un systeme de transmission de couple
FR2812737B1 (fr) Systeme de commande d'un dispositif de bureautique
FR2778164B1 (fr) Systeme de commande mixte pour surface aerodynamique d'aeronef
FR2748720B1 (fr) Systeme pour la commande d'un volet compensateur de gouverne d'aeronef
FR2742387B1 (fr) Dispositif d'actionnement d'un systeme de transmission d'un couple de rotation
FR2591896B1 (fr) Systeme de commande d'un dispositif medical, notamment pour circulation auxiliaire
FR2830631B1 (fr) Dispositif et systeme de pilotage automatique d'un helicoptere
FR2789500B1 (fr) Systeme pour la commande en lacet d'un aeronef
FR2761659B1 (fr) Dispositif de commande de vol d'un aeronef, en particulier d'un helicoptere
FR2769285B1 (fr) Dispositif de commande d'un systeme anticouple mixte d'un helicoptere
FR2764026B1 (fr) Dispositif de commande d'un systeme de changement de vitesses automatique pour les voitures
FR2774200B1 (fr) Dispositif de commande a distance d'un aspirateur
FR2733286B1 (fr) Dispositif de commande d'escamotage d'une structure mobile
FR2744187B1 (fr) Dispositif de commande pour un accouplement
FR2722311B3 (fr) Dispositif de commande d'un curseur
FR2631901B1 (fr) Dispositif de commande electronique pour installation d'entrainement
FR2759656B1 (fr) Dispositif de commande d'un moteur d'essuie-glace
FR2768243B1 (fr) Dispositif de commande manuelle d'un mecanisme
FR2729513B1 (fr) Dispositif de controle-commande d'un systeme electrique
FR2764250B1 (fr) Dispositif de commande d'un etat d'embrayage d'un embrayage
FR2733626B3 (fr) Dispositif de commande d'un interrupteur
FR2765644B1 (fr) Procede et dispositif de commande d'un embrayage
FR2772972B1 (fr) Dispositif de commande d'un electroaimant
FR2793765B1 (fr) Dispositif de commande de vol d'un aeronef

Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20140630