Explanation of principle of power servo, considering helicopter rotor as power control; discussion of power off case, harmonic loads on rotor, engine design, time constant of engine, difficulties with twin engines, simulator studies of load shielding, auto-operation with failed engine, and engine control; how full integration of engine and helicopter requires transfer of master engine control from pilot to rotor. (See also - n 17 Nov 1959 p 93-7)
Helicopter turbine power servo
Control
Control ; 2 , n 18
1959
4 pages
Aufsatz (Zeitschrift)
Englisch
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