Tail rotor

B - Operations – Transporting – 64 – C

Patent

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244/17

B64C 27/82 (2006.01) B64C 27/33 (2006.01)

Patent

CA 1320187

11 ABSTRACT OF THE DISCLOSURE A helicopter tail rotor includes a drive mast having an axis of rotation. A first blade pair is mounted for rotation about the drive mast. The first blade pair includes a pitch change axis perpendicularly disposed to the drive mast axis of rotation. A second blade pair is mounted for rotation about the drive mast and is spaced apart from and parallel disposed to the first blade pair. The second blade pair includes a pitch change axis parallel to the pitch change axis of the first blade pair.

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