Fuel flow system

作者: Irwin Wallman

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摘要: A fuel flow measuring system for the rate of in an aircraft and including a turbine transmitter which is inserted line produces output frequency representing functional relationship to volume passing through transmitter, being referred as K factor. control circuit receives converts it into DC valve fuel. The then displayed on indicator such meter. resistor located electrically coupled circuit. set at value compensate variation whereas temperature sensor, also circuit, serves compensator.

参考文章(6)
Kenneth W Foster, Meter compensating system ,(1961)
Carl W Zimmerman, Larry C Clement, Jack R Hulme, Flowmeter measuring system ,(1966)