An aircraft having an empennage rotatable about a longitudinal axis via an electric motor drive is disclosed herein. A pair of horizontal stabilizers extend from opposing sides of the rotatable empennage and are independently rotatable via electric motor drives. The rotatable empennage is operable for controlling yaw, pitch and rolling moments without a traditional vertical stabilizer and rudder system which can reduce weight as well as the radar cross section of the aircraft. This technology can also be applied to a weapon control system such missile such as a missile.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotatable empennage for an aircraft


    Beteiligte:
    JOO JAMES (Autor:in)

    Erscheinungsdatum :

    31.05.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT EMPENNAGE

    GARCIA NIETO CARLOS / PEREIRA MOSQUEIRA FERNANDO / VELEZ DE MENDIZABAL ALONSO IKER et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT EMPENNAGE

    LINARES VILLEGAS MARIO / GARCIA TORAN SILVIA | Europäisches Patentamt | 2025

    Freier Zugriff

    Aircraft empennage

    LINARES VILLEGAS MARTA / GARCIA TORRAN SONIA | Europäisches Patentamt | 2022

    Freier Zugriff

    Aircraft empennage

    GARCIA NIETO CARLOS / PEREIRA MOSQUEIRA FERNANDO / VELEZ DE MENDIZABAL ALONSO IKER et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Aircraft empennage

    LINARES VILLEGAS MARIO / GARCIA TORAN SILVIA | Europäisches Patentamt | 2024

    Freier Zugriff