An aircraft tailcone comprising a tailcone fuselage, a turbomachine, for example an APU, housed inside the tailcone, a ram air intake on the tailcone fuselage for the ingestion of ram air towards the interior of the turbomachine compartment, an inlet flap operable reciprocately from an open position in which ingestion of ram air is allowed, and a closed position in which ram air ingestion is prevented. The ram air intake extends annularly along a perimeter of the tailcone fuselage, and the inlet flap is configured such in its closed position that a surface of the inlet flap is substantially flush with the tailcone fuselage.


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    Title :

    AIRCRAFT TAILCONE INCORPORATING AN APU ANNULAR AIR INTAKE



    Publication date :

    2019-05-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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    AIRCRAFT TAILCONE INCORPORATING AN APU ANNULAR AIR INTAKE

    CHIABRANDO MARCOS JAVIER / FERNANDEZ-LOPEZ PIO / BARREIRO RODRIGUEZ VÍCTOR | European Patent Office | 2021

    Free access


    The Development of a New Tailcone for a Regional Aircraft: A Multidisciplinary Approach

    Senna, J. C. S. M. / Jesus, A. B. / Nerosky, L. A. R. et al. | British Library Conference Proceedings | 2003


    The Development of a New Tailcone for a Regional Aircraft: A Multidisciplinary Approach

    Senna, J. C. S. M. / Jesus, A. B. / Nerosky, L. A. R. et al. | British Library Conference Proceedings | 2003