INTERCOOLED COMBUSTOR NOZZLE GUIDE VANE AND SECONDARY AIR CONFIGURATION

A gas turbine engine (20) is provided that includes compressor (30) and combustor sections (32), inner and outer casings (52, 54), an annular diffuser (56), an inner diffuser casing (72), a heat exchanger (150), and a high-pressure stator vane stage (60). An annular combustor (35) is disposed radial...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CLARK, Thomas E, ACKERMANN, William K, BREAULT, Andrew E
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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