GENERATOR WITH CONTROLLED AIR COOLING AMPLIFIER

A turbine engine (200) includes an electrical system (10) having at least two generator circuits (14, 16), one coupled to a high pressure portion of a gas turbine engine (200) and the other coupled to a low pressure portion of the gas turbine engine (200). The electrical system (10) actively cools a...

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Bibliographische Detailangaben
Hauptverfasser:	WILSON, Eric E, KLEMEN, Donald
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 CONVERSION OR DISTRIBUTION OF ELECTRIC POWER DYNAMO-ELECTRIC MACHINES ELECTRICITY ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS GENERATION HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A turbine engine (200) includes an electrical system (10) having at least two generator circuits (14, 16), one coupled to a high pressure portion of a gas turbine engine (200) and the other coupled to a low pressure portion of the gas turbine engine (200). The electrical system (10) actively cools an electrical generator (20, 36) during operation in order to ensure proper operation as well as extend the lifespan of the generator (20, 36).