A rocket or ballistic launch rotary wing air vehicle may include a rocket or ballistic launch propulsion system for launching the vehicle, a rotary wing flight system for providing powered flight comprising dual counter rotating coaxial rotors, and a control system programmed to adjust the pitch of a rotor to anyh determined degree of pitch independently of a flap angle of the flap hinge during a transition of the dual counter rotating coaxial rotors from a stowed position to a deployed position.


    Access

    Download


    Export, share and cite



    Title :

    ROCKET OR BALLISTIC LAUNCHED ROTARY WING UNMANNED AIR VEHICLE


    Additional title:

    UNBEMANNTES DREHFLÜGELUFTFAHRZEUG FÜR RAKETEN- ODER GESCHOSSABSCHUSS
    AÉRONEF SANS PILOTE À VOILURE TOURNANTE À LANCÉMENT BALLISTIQUE OU PAR FUSÉE


    Contributors:

    Publication date :

    2018-02-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rocket or ballistic launch rotary wing vehicle

    GREEN JOHN / GEOGHEGAN PHILIP / SNOOK MICHAEL ALEXANDER | European Patent Office | 2019

    Free access

    Fixed-wing unmanned aerial vehicle launched by booster rocket

    JIAN YONGQING / YI BIN / CHEN QIQUAN et al. | European Patent Office | 2023

    Free access

    ROTARY-WING UNMANNED AERIAL VEHICLE

    LEUSCHNER ANDRIES HERMANN | European Patent Office | 2023

    Free access

    ROTARY-WING UNMANNED AERIAL VEHICLE

    LEUSCHNER ANDRIES | European Patent Office | 2019

    Free access

    ROTARY-WING UNMANNED AERIAL VEHICLE

    LEUSCHNER ANDRIES HERMANN | European Patent Office | 2021

    Free access