Method and apparatus to improve heat transfer in turbine sections of gas turbines

A gas turbine engine system having a combustion section and a turbine section is provided. The turbine section includes at least one turbine stage having a plurality of turbine blades coupled to a rotor and an inner casing circumferentially disposed about the plurality of turbine blades. The turbine...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Danescu Radu Ioan, Ballard, Jr. Henry Grady, Black Kenneth Damon, Bozkurt Ozgur
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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