Fuel management system

A fuel management system for a gas turbine engine, the fuel management system comprising a fuel supply line configured to supply fuel from a system inlet to a combustor of the gas turbine engine via a combustor pump and combustor valve. A heat exchanger is configured to reject heat from a thermal lo...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Mochrie, Richard G, Sutcliffe, Graeme E F, Whittle, Jade
Format: Patent
Sprache:eng
Schlagworte:
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