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...

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Bibliographic Details
Main Authors KUMAR, Ampili Kishore, MERCHANT, Laxmikant, AVISHETTI, Srinivas, DASOJI, Anil Kumar
Format Patent
LanguageEnglish
French
German
Published 02.05.2018
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
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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Summary: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 protection boxes 360 surrounding one or more of the valves 365. The valve protection boxes 360 may be in communication with a flow of air from the exhaust frame blower 330.
Bibliography:Application Number: EP20160193633