Compensation apparatus for main rotor torque
AssigneeAdvanced Technology Institute of Commuter-Helicopter, Ltd.
InventorsEiichi Yamakawa, Natsuki Kondo
Life of this patent
Estimating the term…
Abstract
A main rotor torque compensation apparatus for a helicopter having a main rotor and a tail rotor includes vertical tails that are supported at a variable angle of attack. An actuator adjusts the angle of attack such that the main rotor torque is compensated by the torque of the tails together with the torque of the tail rotor.
Claims3
An apparatus for compensating for the main rotor torque in a helicopter having a main rotor and a tail rotor, comprising:
- means for directly sensing the main rotor torque;
- means for adjusting the pitch angle of the tail rotor;
- means for measuring airspeed;
- means for measuring the rotational speed of the main rotor;
- a vertical tail supported at a variable angle of attack;
- means for adjusting the angle of attack of the vertical tail;
- and
- means for controlling the angle of attack adjusting means and the pitch angle adjusting means based on the measured airspeed, the measured rotational speed of the main rotor, and the directly sensed main rotor torque so as to adjust the main rotor torque compensation.
An apparatus for compensating for the main rotor torque in a helicopter equipped with an engine, a speed-changing mechanism whose speed changing ratio is variable, a collector gear, a main rotor and a tail rotor moving together with the collector gear at a constant speed ratio, in which the main rotor and the tail rotor are rotationally driven by transmitting power of the engine to the collector gear via the speed-changing mechanism, the apparatus comprising:
- means for directly sensing the main rotor torque;
- means for adjusting the pitch angle of the tail rotor;
- means for measuring airspeed;
- means for measuring the rotational speed of the main rotor;
- a vertical tail supported at a variable angle of attack;
- means for adjusting the angle of attack of the vertical tail;
- and
- means for controlling the angle of attack adjusting means and the pitch angle adjusting means based on the measured airspeed, the measured rotational speed of the main rotor, and the directly sensed main rotor torque so as to adjust the main rotor torque compensation.
Dependencies are inferred from the claim text.