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Abstract An airfoil includes a leading edge, a trailing edge, a pressure side surface extending from the leading edge to the trailing edge, a suction side surface extending from the leading edge to the trailing edge and generally opposite the pressure side surface and a plurality of cooling holes. The cooling holes are positioned on the airfoil in accordance with X, Y and Z Cartesian coordinate values set forth in an accompanying Table. L'invention concerne une aube qui comprend un bord d'attaque, un bord de fuite, une surface côté pression s'étendant du bord d'attaque au bord de fuite, une surface côté aspiration s'étendant du bord d'attaque au bord de fuite et opposée généralement à la surface côté pression et une pluralité de trous de refroidissement. Les trous de refroidissement sont positionnés sur l'aube en fonction d'un ensemble de valeurs de coordonnées cartésiennes X, Y et Z présentées dans une table annexe.
AbstractList An airfoil includes a leading edge, a trailing edge, a pressure side surface extending from the leading edge to the trailing edge, a suction side surface extending from the leading edge to the trailing edge and generally opposite the pressure side surface and a plurality of cooling holes. The cooling holes are positioned on the airfoil in accordance with X, Y and Z Cartesian coordinate values set forth in an accompanying Table. L'invention concerne une aube qui comprend un bord d'attaque, un bord de fuite, une surface côté pression s'étendant du bord d'attaque au bord de fuite, une surface côté aspiration s'étendant du bord d'attaque au bord de fuite et opposée généralement à la surface côté pression et une pluralité de trous de refroidissement. Les trous de refroidissement sont positionnés sur l'aube en fonction d'un ensemble de valeurs de coordonnées cartésiennes X, Y et Z présentées dans une table annexe.
Author BERGMAN, RUSSELL J
SPANGLER, BRANDON W
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DocumentTitleAlternate AGENCEMENT DE REFROIDISSEMENT D'AUBE
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Snippet An airfoil includes a leading edge, a trailing edge, a pressure side surface extending from the leading edge to the trailing edge, a suction side surface...
SourceID epo
SourceType Open Access Repository
SubjectTerms AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
Title AIRFOIL COOLING ARRANGEMENT
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