CORNER COOLED TURBINE NOZZLE

A turbine nozzle (18) includes a hollow vane (22) joined to opposite inner a nd outer bands (24,26). The inner band (24) includes a forward lip (38) under the leading edge (32) of the vane (22), an aft lip (40) under the trailing edge (34) of the vane (22), and a mounting flange (42) spaced therebet...

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Bibliographische Detailangaben
Hauptverfasser:	LU, WENFENG, LEE, CHING-PANG, SHI, BAOLAN, BRASSFIELD, STEVEN ROBERT, GUENTERT, JOSEPH MICHAEL
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION ENGINE PLANTS IN GENERAL GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS 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 TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Beschreibung
Zusammenfassung:	A turbine nozzle (18) includes a hollow vane (22) joined to opposite inner a nd outer bands (24,26). The inner band (24) includes a forward lip (38) under the leading edge (32) of the vane (22), an aft lip (40) under the trailing edge (34) of the vane (22), and a mounting flange (42) spaced therebetween. An impingement bore (52) extends obliquely and aft from the base of the mounting flange (42) under a corner o f the inner band (24) toward the aft lip (40) for impingement cooling thereof.