Helicopter antitorque tail rotor

Details Helicopter antitorque tail rotor Helicopter antitorque tail rotor

B - Operations, Transporting

64

C

B64C 27/46 (2006.01) B64C 27/473 (2006.01)

Patent

CA 2666266

A blade for an antitorque tail rotor of a helicopter, having a leading edge and a trailing edge opposite each other and elongated along a longitudinal axis of the blade; the trailing edge, in use, interacts with the air current after the leading edge; the blade also has two opposite surfaces extending between the leading edge and the trailing edge, and a root portion extending from a radially inner first end, with respect to a rotation axis of the blade, towards a second end opposite the first end; and the root portion, when sectioned in a plane perpendicular to the leading edge and trailing edge, has a profile asymmetrical with respect to a chord joining the leading edge and trailing edge.

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