GAS TURBINE WITH A VALVE COOLING SYSTEM

The present application provides a gas turbine engine 100. The gas turbine engine 100 may include a compressor air extraction system 110 with a number of valves 365, an exhaust frame cooling system 310 with an exhaust frame blower 330, and a turbine valve cooling system 350 with one or more valve pr...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	AMPILI KISHORE KUMAR, SRINIVAS AVISHETTI, LAXMIKANT MERCHANT, ANIL KUMAR DASOJI
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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