Flow control system and method for controlling two positive displacement pumps

A fuel flow system for a gas turbine engine includes a first pump, a second pump, a bypass loop, an integrating bypass valve and a pilot valve. The first pump connects to an actuator and a metering valve. The second pump connects to the metering valve and is arranged in parallel with the first pump....

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Bibliographische Detailangaben
Hauptverfasser: WICHOWSKI JOHN J, REUTER CHARLES E, HAUGSJAAHABINK TODD, SATO YUKINORI, PRICE AARON V
Format: Patent
Sprache:eng
Schlagworte:
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