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:
Jul. 31, 2018

Filed:

Dec. 09, 2015
Applicant:

Ansaldo Energia Switzerland Ag, Baden, CH;

Inventors:

Martin Balliel, Bassersdorf, CH;

Frank Gersbach, Ehrendingen, CH;

Stefan Andreas Retzko, Zürich, CH;

Marco Lamminger, Ennetbaden, CH;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/32 (2006.01); F01D 5/18 (2006.01); F01D 5/22 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 25/32 (2013.01); F01D 5/147 (2013.01); F01D 5/18 (2013.01); F01D 5/187 (2013.01); F01D 5/225 (2013.01); F05D 2220/32 (2013.01); F05D 2230/211 (2013.01); F05D 2240/305 (2013.01); F05D 2240/307 (2013.01); F05D 2260/20 (2013.01); F05D 2260/607 (2013.01);
Abstract

A rotating gas turbine blade is disclosed which includes an airfoil with a suction side and a pressure side, the airfoil extending in a radial direction from a blade root to a blade tip. The blade tip includes a tip shroud, the airfoil having internal cooling passages for a cooling medium, which extend through the tip shroud. Outlet ports are provided above a selected internal airfoil cooling passage for the cooling medium to be ejected above the tip shroud in a direction of the blade's pressure side. Dust accumulation is avoided at the tip end of the selected internal cooling passage.


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