TURBINE BLADE WITH COOLING ARRANGEMENT

A turbine blade (100) with a cooling arrangement is disclosed. The turbine blade (100) includes at least one supply chamber (202, 202') and at least one impingement cavity (CI, CI'). The supply chamber (202, 202') includes multiple impingement channels (204) configured to direct a coo...

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Bibliographische Detailangaben
Hauptverfasser:	SZIJARTO, Janos, UTRIAINEN, Esa
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A turbine blade (100) with a cooling arrangement is disclosed. The turbine blade (100) includes at least one supply chamber (202, 202') and at least one impingement cavity (CI, CI'). The supply chamber (202, 202') includes multiple impingement channels (204) configured to direct a cooling fluid from within the supply chamber (202, 202') to the impingement cavity (CI, CI'). The supply chamber (202, 202') also includes one or more collector channels (206) such that the cooling fluid from the impingement cavity (CI, CI') is directed to a collector cavity (CC) within the turbine blade (100).