GAS TURBINE ENGINE

A gas turbine engine is provided having a turbomachine comprising a compressor section, a combustion section, and a turbine section arranged in serial flow order, the compressor section having a high pressure compressor defining a high pressure compressor exit area (AHPCExit) in square inches and th...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	de Luis, Jorge, Turner, Douglas Downey, Wilkinson, Keith W, Niergarth, Daniel Alan, Sibbach, Arthur William, Martina, Vincenzo, Macrorie, Michael
Format:	Patent
Sprache:	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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