AIRCRAFT FUEL SYSTEMS WITH ELECTRIC MOTOR DRIVEN AUGMENTOR PUMPS

A fuel system for a gas turbine engine includes an augmentor pump (102) having an inlet (104) communicating with a fuel supply source and a discharge (106) communicating with an augmentation stage of the engine. An electric motor (108) is operatively connected to drive the augmentor pump for selecti...

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Bibliographische Detailangaben
1. Verfasser:	GOY, Edward W
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 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A fuel system for a gas turbine engine includes an augmentor pump (102) having an inlet (104) communicating with a fuel supply source and a discharge (106) communicating with an augmentation stage of the engine. An electric motor (108) is operatively connected to drive the augmentor pump for selectively activating and deactivating the augmentor pump.