The present embodiments relate to a boom for an aircraft, and, more particularly, to a tail boom 3 for a helicopter 1, whereby the tail boom 3 may comprise a watertight compartment 7 and watertight bulkheads 5, 6. The watertight bulkheads 5, 6 may close at least one end of watertight compartment 7. Watertight bulkhead 5, 6 may include attachment device 8, frame 12, and watertight fabric 11.


    Access

    Download


    Export, share and cite



    Title :

    A BULKHEAD FOR A BOOM OF AN AIRCRAFT


    Additional title:

    SCHOTT FÜR EINEN AUSLEGER EINES FLUGZEUGS
    CLOISON POUR UNE PERCHE D'UN AÉRONEF


    Contributors:
    FINK AXEL (author)

    Publication date :

    2021-08-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    BULKHEAD FOR A BOOM OF AN AIRCRAFT

    FINK AXEL | European Patent Office | 2022

    Free access

    A BULKHEAD FOR A BOOM OF AN AIRCRAFT

    FINK AXEL | European Patent Office | 2022

    Free access

    Watertight bulkhead for a boom of an aircraft

    FINK AXEL | European Patent Office | 2023

    Free access

    A BULKHEAD FOR A BOOM OF AN AIRCRAFT

    DR FINK AXEL | European Patent Office | 2022

    Free access

    PRESSURE BULKHEAD FOR AN AIRCRAFT

    BUCHER RAIMUND / EDELMANN KLAUS / MIARIS ANGELOS et al. | European Patent Office | 2019

    Free access