Embodiments herein describe UAVs that utilize tail boom assemblies from pre-existing aircraft designs as lift generating elements. In one embodiment, a UAV includes a fuselage having a first end and a second end opposite the first end, a first tail boom coupler disposed at the first end, and a second tail boom coupler disposed at the second end. Each of the first tail boom coupler and the second tail boom coupler are configured to mechanically couple with a plurality of tail boom assemblies procured from a pre-existing aircraft design.


    Access

    Download


    Export, share and cite



    Title :

    EXPEDITED DESIGN AND QUALIFICATION OF UNMANNED AERIAL VEHICLES


    Contributors:

    Publication date :

    2020-08-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    Expedited design and qualification of unmanned aerial vehicles

    NEWMAN DANIEL I | European Patent Office | 2023

    Free access

    Unmanned aerial vehicles

    RUSSELL IAIN MATTHEW | European Patent Office | 2021

    Free access

    UNMANNED AERIAL VEHICLES

    RUSSELL IAIN MATTHEW | European Patent Office | 2021

    Free access

    UNMANNED AERIAL VEHICLES

    RUSSELL IAIN | European Patent Office | 2019

    Free access

    Unmanned aerial vehicles

    RUSSELL IAIN MATTHEW | European Patent Office | 2021

    Free access