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.
Cette invention concerne une pale d'hélice, comprenant un bord d'attaque et un bord de fuite. Le bord de fuite est agencé à l'opposé du bord d'attaque, de façon à former un plan porteur entre ceux-ci. Au moins un élément parmi le bord d'attaque et le bord de fuite comprend au moins une facette.
PROPELLER ROTOR FOR A VERTICAL TAKE OFF AND LANDING AIRCRAFT
ROTOR D'HÉLICE POUR UN AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX
2015-10-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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