A tail boom adapted for counteracting a fuselage torque created by an engine carried by a fuselage of a rotary aircraft. The tail boom is positioned within the rotorwash from the rotary and includes a first side surface contoured to create a low-pressure region of an airfoil and a second opposing side surface contoured to create a high-pressure region of an airfoil. The pressure difference between the high-pressure region and the low-pressure region causes the tail boom to move towards the low-pressure region, resulting in a lateral force opposing the torque on the fuselage.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRFOIL SHAPED TAIL BOOM


    Weitere Titelangaben:

    TRAGFLÄCHENFÖRMIGER HECKAUSLEGER
    POUTRE DE QUEUE EN FORME DE PROFIL AÉRODYNAMIQUE


    Beteiligte:
    BRAND ALBERT G (Autor:in) / NARRAMORE JIMMY (Autor:in) / HARSE JAMES H (Autor:in) / LANIGAN BRENDAN P (Autor:in)

    Erscheinungsdatum :

    07.09.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRFOIL SHAPED TAIL BOOM

    BRAND ALBERT G / NARRAMORE JIMMY / HARSE JAMES H et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    AIRFOIL SHAPED TAIL BOOM

    BRAND ALBERT G / NARRAMORE JIMMY / HARSE JAMES H et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    Retractable airfoil-shaped sail with double tail flaps

    LI DONGQIN / ZHENG XIN / XU SHIYOU et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    Boom tail structure, boom tail structure assembling method and cargo boom

    GOU XUYI / ZHAO QINGLI / WANG LUQING et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Swallow tail airfoil

    GRASSO FRANCESCO | Europäisches Patentamt | 2021

    Freier Zugriff