TURBINE COMPRESSOR VANE

A compressor vane (62) can comprise at least one of four leakage control structures comprising a leading edge axial stack (160) near the root (128) of the vane (62), a portion (150) ofthe inner platform (132) of an inner band (86) extending forward and having a radiused geometry, a negative dihedral...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	FALK, Eric Andrew, WOOD, Peter John, TARNOWSKI, Andrzej Tomasz, BRZOZOWSKI, Jacek Michal, MOECKEL, Curtis William
Format:	Patent
Sprache:	eng ; fre ; ger
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 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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