Airfoil shape for a compressor blade

An article of manufacture is disclosed having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a table. The table selected from the group of tables consisting of TABLES 1S-16S, 1R-17R, and IGV. Wherein X and Y are distances in inches which, wh...

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Hauptverfasser:	HARRELL, JASON THOMAS, SCHIRLE, STEVEN MARK, DEJORIS, TIMOTHY E, CLEVELAND, PETER GAINES, SCHOTT, CARL G, DEIVERNOIS, PAUL, RACE, NATHAN S, STAMPFLI, JOHN DAVID, MISTREANU, ADRIAN MICREA, BEHARRYSINGH, ROGER, MCGOWAN, CHRISTOPHER DAVID, DENMARK, RONALD STUART, DUTKA, MICHAEL JAMES, MILLER, WILLIAM J, BOYD, JEFFERY, CHALUVADI, VENKATA SIVA P, MICHENFELDER, JENNIFER B, TOMBERG, STEVEN ERIC, RYMAN, JOHN F
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING 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:	An article of manufacture is disclosed having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a table. The table selected from the group of tables consisting of TABLES 1S-16S, 1R-17R, and IGV. Wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.