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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ULTRALIGHT AIRCRAFT


    Beteiligte:
    BURNS SIMON (Autor:in)

    Erscheinungsdatum :

    2016-08-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Ultralight aircraft

    BURNS SIMON | Europäisches Patentamt | 2018

    Freier Zugriff

    Ultralight aircraft

    Markowski, M. A. | TIBKAT | 1982


    Ultralight or Aircraft?

    Online Contents | 1994


    Structural Design Considerations for Ultralight Aircraft

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


    An ultralight freewing aircraft design study

    CHEN, WEIPING / BARLOW, JEWEL | AIAA | 1992