Invention Application
WO2015163855A1 PROPELLER ROTOR FOR A VERTICAL TAKE OFF AND LANDING AIRCRAFT 审中-公开
螺旋桨转子用于垂直起落架和飞机

PROPELLER ROTOR FOR A VERTICAL TAKE OFF AND LANDING AIRCRAFT
Abstract:
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.
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