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:
Jan. 07, 2020

Filed:

Jun. 29, 2015
Applicant:

Siemens Aktiengesellschaft, München, DE;

Inventors:

Kok-Mun Tham, Oviedo, FL (US);

Ching-Pang Lee, Cincinnati, OH (US);

Eric Chen, Cincinnati, OH (US);

Steven Koester, Toledo, OH (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/22 (2006.01); F01D 5/18 (2006.01); F01D 11/08 (2006.01);
U.S. Cl.
CPC ...
F01D 5/225 (2013.01); F01D 5/186 (2013.01); F01D 11/08 (2013.01); F05D 2220/32 (2013.01); F05D 2240/307 (2013.01); F05D 2260/202 (2013.01);
Abstract

A turbine component including a shrouded airfoil with a flow conditioner configured to direct leakage flow and coolant to be aligned with main hot gas flow is provided. The flow conditioner is positioned on a shroud base radially adjacent to the tip of the airfoil and includes a ramped radially outer surface positioned further radially inward than a radially outer surface of the shroud base. The ramped radially outer surface extends from a first edge to a second edge in a direction generally from the suction side to the pressure side of the airfoil, such that the first edge is positioned further radially inward than the second edge. Multiple coolant ejection holes are positioned on the ramped radially outer surface. The coolant ejection holes are connected fluidically to an interior of the airfoil.


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