The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 17, 2017

Filed:

Nov. 04, 2014
Applicant:

Mitsubishi Hitachi Power Systems, Ltd., Yokohama, Kanagawa, JP;

Inventors:

Hisato Tagawa, Yokohama, JP;

Yasuhiro Horiuchi, Yokohama, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/08 (2006.01); F01D 5/18 (2006.01); F01D 9/04 (2006.01); F01D 9/06 (2006.01); F01D 11/04 (2006.01); F01D 25/12 (2006.01);
U.S. Cl.
CPC ...
F01D 5/18 (2013.01); F01D 5/082 (2013.01); F01D 9/041 (2013.01); F01D 9/065 (2013.01); F01D 11/04 (2013.01); F01D 25/12 (2013.01); F05D 2240/81 (2013.01); F05D 2260/20 (2013.01); F05D 2260/202 (2013.01);
Abstract

A gas turbine airfoil is provided that is superior in the cooling performance of an end wall and in the thermal efficiency of a gas turbine. A gas turbine airfoil includes an airfoil portion having a cooling passage therein; and an end wall portion located at an inner band end portion of the airfoil portion in the turbine-radial direction. Cooling holes are disposed in the leading edge side hook portion of the end wall portion. The plurality of cooling holes are arranged at different distance of intervals in the circumferential direction of the gas turbine. Cooling air that has flowed in the cooling passage is configured to flow from the cooling holes toward the leading edge of the end wall portion.


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