GAS TURBINE POWER GENERATION SYSTEM WITH A HIGH PRESSURE COMPRESSOR AND AN ADDED FORWARD LOW PRESSURE COMPRESSOR

Provided is a gas turbine power generation system, including a core engine and a low pressure compressor. The core engine includes a high pressure compressor, a combustor, and a high pressure turbineconfigured in a serial flow arrangement. The high pressure compressor and the high pressure turbine a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CUNNINGHAM GEORGE GOULD III, ROSE JOSEPH GEORGE, MONIZ THOMAS ORY
Format:	Patent
Sprache:	chi ; eng
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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