Air foil shape for a compressor blade

An article of manufacture 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...

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Hauptverfasser: MISTREANU ADRIAN MIRCEA, BOYD JEFFREY, STAMPFLI JOHN DAVID, RACE NATHAN S, DENMARK RONALD STUART, DEIVERNOIS PAUL, CLEVELAND PETER GAINES, DUTKA MICHAEL JAMES, CHALUVADI VENKATA SIVA P, SCHOTT CARL G, RYMAN JOHN F, DEJORIS TIMOTHY E, MILLER WILLIAM J, HARRELL JASON THOMAS, SCHIRLE STEVEN MARK, BEHARRYSINGH ROGER, TOMBERG STEVEN ERIC, MCGOWAN CHRISTOPHER DAVID, MICHENFELDER JENNIFER B
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creator MISTREANU ADRIAN MIRCEA
BOYD JEFFREY
STAMPFLI JOHN DAVID
RACE NATHAN S
DENMARK RONALD STUART
DEIVERNOIS PAUL
CLEVELAND PETER GAINES
DUTKA MICHAEL JAMES
CHALUVADI VENKATA SIVA P
SCHOTT CARL G
RYMAN JOHN F
DEJORIS TIMOTHY E
MILLER WILLIAM J
HARRELL JASON THOMAS
SCHIRLE STEVEN MARK
BEHARRYSINGH ROGER
TOMBERG STEVEN ERIC
MCGOWAN CHRISTOPHER DAVID
MICHENFELDER JENNIFER B
description An article of manufacture 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.
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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.</abstract><oa>free_for_read</oa></addata></record>
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recordid cdi_epo_espacenet_US7186090B2
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subjects BLASTING
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
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ARTCOLLECTIONS [XRACs] AND DIGESTS
WEAPONS
title Air foil shape for a compressor blade
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