Improvement of high-speed charging of a helicopter rotor.

摘要

INCREASES (113.103-105) SPEED REFERENCE ENGINE HELICOPTER (66) IN RESPONSE TO HEAVY LOAD OF ROTOR (108). THE GRADUALLY APPEARS reference speed (113.104) at a rate relatively fast 107% NOMINAL SPEED (114). AFTER A TIMEOUT FIXED (118), CHARGING REDUCED ROTOR (119) will cause the reference speed to decrease slowly (120, 103-105) SPEED TO NOMINAL (121). EXCEEDS TORQUE IF 111% NOMINAL TORQUE (117), the reference speed is decreased similarly (120, 103.105).