发明名称 MANEUVER CONTROL DEVICE OF PROPELLER PLANE
摘要 PROBLEM TO BE SOLVED: To provide a maneuver control device capable of correcting swings round three axes resulting from a propeller during unsteady flying. SOLUTION: This control device 30 is fed with signals from navigation instruments 31 and various sensors such as a rotating speed sensor 32 to sense the rotating speed of an engine 11 to drive a propeller 12, a displacement sensor 33 for a control stick 19, a displacement sensor 34 for ladder pedal 20 and a displacement sensor 35 for power lever 21, and senses or predicts disturbance round three axes resulting from the torque action of the propeller 12, and calculates the operating amounts of the ladder 18 and an elevator 16 for setting off the disturbances. Actuators 36 and 37 are also controlled, to drive the ladder 18 and elevator 16 to apply necessary steering force.
申请公布号 JP2000225997(A) 申请公布日期 2000.08.15
申请号 JP19990026388 申请日期 1999.02.03
申请人 TOYOTA MOTOR CORP 发明人 TANAKA SHIGEKI
分类号 B64C13/16;B64C13/18;B64D31/06;(IPC1-7):B64C13/16 主分类号 B64C13/16
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