Vane carrier thermal management arrangement and method for clearance control

A thermal management arrangement (110) in a gas turbine engine (60), including: a conduit arrangement (62) providing fluid communication between a compressor section (156) and: a relatively thermally responsive portion (52) of a turbine vane carrier (10); and a relatively thermally unresponsive port...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	TERPOS BRIAN H, LEE CHING-PANG, THAM KOK-MUN, SIMKO DUSTAN M
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL 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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