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SINGLE LEVER POWERPLANT CONTROL ON TWIN TURBOPROPELLER AIRCRAFT
SINGLE LEVER POWERPLANT CONTROL ON TWIN TURBOPROPELLER AIRCRAFT
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机译:双涡轮螺旋桨飞机的单杆动力装置控制
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摘要
Herein provided are methods and systems for controlling operation a first propeller of an aircraft, the first propeller associated with a first engine, the aircraft further comprising a second propeller associated with a second engine. A first requested engine power for the first engine is obtained. A second requested engine power for the second engine is obtained. The first propeller is synchronized with the second propeller by setting a first propeller command for the first propeller based on the first and second requested engine power, and the first propeller command is sent for the first propeller.
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