A detachable multiaxial aircraft is related. The aircraft includes a fuselage and a number of lift arm assemblies. The lift arm assembly includes a landing chassis, an electric motor mounted on the landing chassis, and a propeller fixed on the electric motor. The lift arm assembly further includes a shell located on the landing chassis and surrounding the propeller. The fuselage includes a first connector, and the shell includes a second connector. The lift arm assembly is detachably connected to the fuselage by the first connector and the second connector.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    DETACHABLE MULTIAXIAL AIRCRAFT


    Beteiligte:
    CHEN HAN-XUN (Autor:in)

    Erscheinungsdatum :

    13.06.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT WITH DETACHABLE WINGS

    BEYELER ANTOINE / KLAPTOCZ ADAM / ROBERTS JAMES F et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    DETACHABLE ANNULAR AIRCRAFT WING

    PURNELL DONALD | Europäisches Patentamt | 2022

    Freier Zugriff

    Multipurpose detachable aircraft floor structure

    CAO ZHEN / JI HAILIANG / ZHU TONG et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    Aircraft interior unit with detachable panel

    VUAGNIAUX JOSEPH / DOUGLAS MARK / PARISH DANIEL | Europäisches Patentamt | 2025

    Freier Zugriff

    Detachable Power Tethering Systems for Aircraft

    BRAND ALBERT G / POSTER SCOTT DAVID | Europäisches Patentamt | 2021

    Freier Zugriff