AEROFOIL PART SHAPE FOR TURBINE BUCKET

PROBLEM TO BE SOLVED: To provide an aerofoil part shape for a turbine bucket. SOLUTION: This turbine bucket includes an aerofoil part 38. The aerofoil part 38 includes a profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1 (not indicated) as contain...

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Bibliographische Detailangaben
Hauptverfasser:	MALINOWSKI CHARLES A, SMITH BRUCE L, BRITTINGHAM ROBERT A
Format:	Patent
Sprache:	eng
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:	PROBLEM TO BE SOLVED: To provide an aerofoil part shape for a turbine bucket. SOLUTION: This turbine bucket includes an aerofoil part 38. The aerofoil part 38 includes a profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1 (not indicated) as contained in the specification, wherein the Z values in Table 1 (not indicated) are non-dimensional values from approximately 0-1 convertible to Z values in inches by multiplying the Z values by a height of the aerofoil part 38 in inches, and wherein X and Y are distances in inches which, when connected by substantially smooth continuing arcs, define profile sections of the aerofoil part 38 at each distance Z, the profile sections at the Z distances being joined substantially smoothly with one another to form a complete airfoil part 38 shape. COPYRIGHT: (C)2010,JPO&INPIT