METHOD AND APPARATUS TO IMPROVE HEAT TRANSFER IN TURBINE SECTION OF GAS TURBINE

PROBLEM TO BE SOLVED: To provide a gas turbine engine system having a combustion section and a turbine section.SOLUTION: A turbine section includes a turbine stage having a plurality of turbine blades coupled to a rotor, and an inner casing circumferentially disposed about the plurality of turbine b...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	OZGUR BOZKURT, BALLARD JR HENRY GRADY, BLACK KENNETH DAMON, RADU IOAN DANESCU
Format:	Patent
Sprache:	eng
Schlagworte:	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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!