AIRFOIL COOLING ARRANGEMENT
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 coolin...
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Format | Patent |
Language | English French |
Published |
09.01.2014
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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. |
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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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RelatedCompanies | UNITED TECHNOLOGIES CORPORATION |
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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... |
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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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