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. 03, 2019

Filed:

Aug. 28, 2015
Applicant:

Siemens Aktiengesellschaft, München, DE;

Inventors:

Evan C. Landrum, Charlotte, NC (US);

Jan H. Marsh, Orlando, FL (US);

Paul A. Sanders, Cullowhee, NC (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F02C 7/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/188 (2013.01); F01D 5/189 (2013.01); F02C 7/18 (2013.01); F05D 2250/185 (2013.01); F05D 2260/201 (2013.01);
Abstract

A turbine airfoil () includes a flow displacement element () occupying a space between a pair of adjacent partition walls () in an interior portion () of a generally hollow airfoil body (). The flow displacement element () includes an elongated main body () extending lengthwise in a radial direction and a pair of connector ribs () respectively connecting the main body () to pressure and suction sides () of the airfoil (). A pair of adjacent radial flow passes (--) of symmetrically opposed flow cross-sections are defined on chordally opposite sides of the flow displacement element (). The radial flow passes (--) conduct cooling fluid in opposite radial directions and are connected in series via a chordal passage () defined in the interior portion () between the flow displacement element () and a radial end face () of the airfoil body (), to form a serpentine cooling path ().


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