CPC B64C 11/28 (2013.01) [B64C 39/024 (2013.01); B64U 10/25 (2023.01); B64U 30/12 (2023.01); B64U 50/13 (2023.01)] | 11 Claims |
6. At least one foldable propeller blade configured to an aerial vehicle in a pusher configuration comprising:
a first arrangement, wherein the at least one foldable propeller blade is configured against a fuselage of the aerial vehicle;
a second arrangement, wherein the at least one foldable propeller is deployed in the pusher configuration; and
a locking mechanism that enables the at least one foldable propeller blade to:
transition of at least one foldable propeller blade from the first arrangement to the second arrangement, and
counteract forward folding tendency resulting from thrust generated by the at least one foldable propeller blade.
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