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:
Dec. 07, 2021

Filed:

Oct. 24, 2016
Applicant:

Siemens Energy Global Gmbh & Co. KG, Munich, DE;

Inventor:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/141 (2013.01); F05D 2230/21 (2013.01); F05D 2240/301 (2013.01); F05D 2240/303 (2013.01); F05D 2240/304 (2013.01); F05D 2240/305 (2013.01); F05D 2240/306 (2013.01); F05D 2260/201 (2013.01); F05D 2260/22141 (2013.01);
Abstract

A turbine airfoil () includes a trailing edge coolant cavity () located in an airfoil interior () between a pressure sidewall () and a suction sidewall (). The trailing edge coolant cavity () is positioned adjacent to a trailing edge () of the turbine airfoil () and is in fluid communication with a plurality of coolant exit slots () positioned along the trailing edge (). At least one framing passage () is formed at a span-wise end of the trailing edge coolant cavity (). The airfoil () further includes framing features (A-B,A-B) located in the framing passage (). The framing features are configured as ribs (A-B,A-B) protruding from the pressure sidewall () and/or the suction sidewall (). The ribs (A-B,A-B) extend partially between the pressure sidewall () and the suction sidewall ().


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