ACCUMULATOR ASSISTED GAS TURBINE ENGINE START SYSTEM AND METHODS THEREFOR

A gas turbine engine assembly is provided having a gas turbine engine (20) and a fuel supply (102) in flow communication with the gas turbine engine (20). An accumulator (104) is positioned in flow communication between the fuel supply (102) and the gas turbine engine (20) to store fuel pressure in...

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Bibliographische Detailangaben
1. Verfasser:	RIPLEY, DAVID LLOYD
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A gas turbine engine assembly is provided having a gas turbine engine (20) and a fuel supply (102) in flow communication with the gas turbine engine (20). An accumulator (104) is positioned in flow communication between the fuel supply (102) and the gas turbine engine (20) to store fuel pressure in fuel flowing from the fuel supply (102) to the gas turbine engine (20).