GAS TURBINE BLADE AND GAS TURBINE EQUIPPED THEREWITH

PROBLEM TO BE SOLVED: To provide a gas turbine blade capable of improving the heat transfer performance of a serpentine flow path.SOLUTION: The serpentine flow path is formed of second-fourth cooling flow paths 12B, 12C, 12D so that the second cooling flow path 12B is situated at the most downstream...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	YURI MASANORI, HANEDA SATORU
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
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