Helicopter counter spin wing

Details Helicopter counter spin wing Helicopter counter spin wing

B - Operations, Transporting

64

C

B64C 27/04 (2006.01) B64C 27/26 (2006.01) B64C 27/82 (2006.01)

Patent

CA 2698431

Rotating blades of a helicopter cause a reaction torque that is usually countered by a propeller rotating at the end of the helicopter tail. In this invention a relatively small wing on the back of the helicopter utilizes airflow created by the main blades to counter the reaction torque.

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