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.
Expedited design and qualification of unmanned aerial vehicles
2023-03-28
Patent
Elektronische Ressource
Englisch
EXPEDITED DESIGN AND QUALIFICATION OF UNMANNED AERIAL VEHICLES
Europäisches Patentamt | 2020
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