Helicopter rotor blades

Details Helicopter rotor blades Helicopter rotor blades

B - Operations, Transporting

64

C

244/120

B64C 27/46 (2006.01)

Patent

CA 1326228

ABSTRACT Title: Helicopter Rotor Blades The swept extreme tip edge of a helicopter rotor blade incorporates blade droop to reduce aerodynamic pitching moments caused by spanwise flow encountered in the fore and aft sectors of a rotor rotational disc during forward flight of a helicopter on which the blade is fitted.

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