BE475200A - - Google Patents

Info

Publication number
BE475200A
BE475200A BE475200DA BE475200A BE 475200 A BE475200 A BE 475200A BE 475200D A BE475200D A BE 475200DA BE 475200 A BE475200 A BE 475200A
Authority
BE
Belgium
Prior art keywords
control
pilot
inertia
control device
rotor
Prior art date
Application number
Other languages
English (en)
French (fr)
Publication of BE475200A publication Critical patent/BE475200A/fr

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; 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
    • B64C2027/8236Rotorcraft; 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 including pusher propellers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
BE475200D BE475200A (OSRAM)

Publications (1)

Publication Number Publication Date
BE475200A true BE475200A (OSRAM)

Family

ID=123963

Family Applications (1)

Application Number Title Priority Date Filing Date
BE475200D BE475200A (OSRAM)

Country Status (1)

Country Link
BE (1) BE475200A (OSRAM)

Similar Documents

Publication Publication Date Title
EP0808768B1 (fr) Aérodyne à décollage et atterrissage verticaux
US4367063A (en) Pitch control mechanism for coaxial helicopter steering
WO2001053150A1 (fr) Aeronef a ailes tournantes
EP1165369B1 (fr) Helicoptere a pilotage pendulaire a haute stabilite et a grande manoeuvrabilite
EP0706937B1 (fr) Dispositif de commande du pas des pales d'un rotor de giravion
FR3006294A3 (fr) Aeronef a voilure tournante et a soufflante canalisee appartenant aux categories des mini et micro drones
EP3501980B1 (fr) Rotor a pas collectif variable et aeronef
WO2013026963A1 (fr) Système de rotor d'hélicoptère et hélicoptère comprenant un tel système de rotor
BE475200A (OSRAM)
FR2523546A1 (fr) Equipement pour vehicules ayant au moins un dispositif a pales tournantes et un corps helicoptere et aeronef
EP3381800A1 (fr) Rotor de giravion incluant un ensemble de plateaux cycliques et deux compas tournants
CA1064885A (fr) Helicopteres a rotors coaxiaux, et notamment de type convertible_
US2994386A (en) Control mechanism
FR2486020A1 (fr) Aeronef
WO2004085249A1 (fr) Dispositif de commande de vol pour giravions
BE462718A (OSRAM)
BE475207A (OSRAM)
EP3290335B1 (fr) Aéronef muni d'un ensemble de plateaux cycliques et d'au moins une servocommande inclinée
BE469744A (OSRAM)
BE384909A (OSRAM)
BE410580A (OSRAM)
CH326059A (fr) Aéronef à voilure tournante
BE367557A (OSRAM)
BE388193A (OSRAM)
CH214763A (fr) Machine volante à ailes articulées.