Keyword: «tail rotor pitch»

ABOUT ONE OF THE WAYS TO SOLVE THE PROBLEM OF LEFT SELF-ROTATION OF A HELICOP-TER

Authors:

Aleksei Shirov,

Dmitrii Vereshikov,

Ilya Makarov

This article analyzes the dependence of thrust and required tail rotor torque on crosswind. The problem of left self-rotation of a helicopter is emerging. Problems that require solutions are identified. A method for adaptive correction of the tail rotor pitch is proposed.

Keywords: tail rotor, left self-rotation, propeller thrust, torque, side wind, adaptive correction, tail rotor pitch