Air injection system for cooling rotor in gas turbine engine and method of cooling such rotor

An air injection system for use in a gas turbine engine includes at least one outlet port (42) through which air is extracted from the engine only during less than full load operation, at least one rotor cooling pipe (46A-D), which is used to inject the air extracted from the outlet port(s) (42) int...

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Bibliographische Detailangaben
Hauptverfasser: TERPOS BRIAN H, THAM KOK-MUN, LI JINGBANG, SIMKO DUSTAN M
Format: Patent
Sprache:eng
Schlagworte:
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