CPC B64C 39/024 (2013.01) [B64C 1/061 (2013.01); B64C 1/068 (2013.01); B64D 17/00 (2013.01); B64D 47/00 (2013.01); B64U 10/25 (2023.01); B64U 30/10 (2023.01); B64U 50/19 (2023.01)] | 23 Claims |
1. A method of replacing components of an unmanned aerial vehicle, the method comprising:
detaching a first power module from an anchor structure, the anchor structure housed within a fuselage of the unmanned aerial vehicle, wherein the anchor structure extends from a first side wall of the fuselage to a second sidewall of the fuselage opposite of the first sidewall;
detaching a first wing structure from the unmanned aerial vehicle by unseating a first mounting bracket of the first wing structure from a portion of the anchor structure, the anchor structure being configured for releasable coupling with the first mounting bracket;
attaching a second wing structure to the unmanned aerial vehicle by seating a second mounting bracket of the second wing structure on the portion of anchor structure, the anchor structure being further configured for releasable coupling with the second mounting bracket; and
attaching a second power module to the anchor structure.
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