An aircraft which has a supporting structure which has at least one fuselage, a wing structure and at least one drive apparatus. The drive apparatus has at least one propeller and a drive motor. The aircraft has at least one energy store for providing energy for operation of the drive apparatus. The at least one drive apparatus and the at least one energy store are mechanically connected to the supporting structure and/or the wing structure of the aircraft by a securing device.


    Access

    Download


    Export, share and cite



    Title :

    Ultralight aircraft


    Contributors:
    BURNS SIMON (author)

    Publication date :

    2018-10-09


    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



    Ultralight aircraft

    Markowski, M. A. | TIBKAT | 1982


    ULTRALIGHT AIRCRAFT

    BURNS SIMON | European Patent Office | 2016

    Free access

    Structural Design Considerations for Ultralight Aircraft

    Johnson, David B. / Baughn, Terry V. | SAE Technical Papers | 1986


    Capsule drop device for ultralight aircraft

    GANG HYEON SEOP | European Patent Office | 2025

    Free access

    An ultralight freewing aircraft design study

    CHEN, WEIPING / BARLOW, JEWEL | AIAA | 1992