A propeller blade is provided including a leading edge and a trailing edge. The trailing edge is arranged opposite the leading edge to form an airfoil there between. At least one of the leading edge and the trailing edge include at least one facet.
Propeller rotor for a vertical take off and landing aircraft
2020-07-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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