An unmanned aerial vehicle may include a fuselage and an anchor structure coupled to the fuselage and including a wing retention structure and a power module retention structure. The unmanned aerial vehicle may also include a wing releasably coupled to the wing retention structure, thereby coupling the wing to the fuselage, and a power module releasably coupled to the power module retention structure, thereby coupling the power module to the fuselage.
UNMANNED AIRCRAFT SYSTEM WITH SWAPPABLE COMPONENTS
UNBEMANNTES FLUGZEUGSYSTEM MIT AUSTAUSCHBAREN KOMPONENTEN
SYSTÈME D'AÉRONEF SANS PILOTE AVEC COMPOSANTS POUVANT ÊTRE INTERCHANGÉS
2020-06-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |