Turbine engine control system

作者: Raymond P Canale , Wesley J Ross

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摘要: A turbine engine control system, including a fuel is provided with inlet, metering valve assembly responsive to electrical signals generated in response speed and temperature indicia of operator power request, bypass valving means for returning unmetered from the area an low pressure fuel, compressor discharge sensing tending further close as increases, differential pressures which meters opening said order achieve rate metered flow corresponding pressure; variable nozzle within associated variably opened closed by related sections at least part operating parameters.

参考文章(7)
Carl F Schorn, Julius Alberani, Fuel trimming valve ,(1967)
Lael B Taplin, Thomas E Thompson, Joseph P Madurski, Jr Walter F Datwyler, Pneumatic engine fuel control system ,(1963)
Ralph J Sneeden, Harry L Richardson, Low idle fuel control system ,(1965)
Warren H Cowles, Dean F Wheeler, Gas turbine engine control having by-pass valve means ,(1963)