Helicopter rotor blades

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 27/46 (2006.01)

Patent

CA 2071028

Tn a helicopter rotor blade having a root end for attachment to a rotor head, a central portion of constant chord dimension and a tip portion having a chord dimension greater than that of the central portion, an outboard region of the central portion has a negative basic pitching moment coefficient, an inboard region of the central portion has a basic pitching moment coefficient more positive than that of the outboard region and the tip portion has a positive basic pitching moment coefficient.

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