Helicopter antitorque tail rotor blade

Details Helicopter antitorque tail rotor blade Helicopter antitorque tail rotor blade

B - Operations, Transporting

64

C

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

Patent

CA 2666267

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 an end portion extending between a reference section and a radially outer end of the blade with respect to a rotation axis of the blade; the rotation axis is outside the blade and crosswise with respect to the longitudinal axis; the length of the chord at the end portion decreases from the reference section to the radially outer end; and the leading and trailing edges are joined at the radially outer end.

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