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:
May. 21, 2024

Filed:

Apr. 24, 2020
Applicant:

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

Inventors:

Denis Torres Gonzalez, Orlando, FL (US);

Matthew Golsen, Orlando, FL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 5/14 (2006.01); F01D 5/16 (2006.01); F01D 5/20 (2006.01); F01D 25/12 (2006.01); F01D 25/06 (2006.01);
U.S. Cl.
CPC ...
F01D 5/189 (2013.01); F01D 5/147 (2013.01); F01D 5/16 (2013.01); F01D 5/20 (2013.01); F01D 25/12 (2013.01); F01D 25/06 (2013.01); F05D 2260/201 (2013.01); F05D 2260/96 (2013.01);
Abstract

A turbine airfoil includes an airfoil body and a generally hollow flow displacement element positioned in an interior portion of the airfoil body and extending along a span-wise extent thereof. The flow displacement element defines an inactive cavity therewithin. The flow displacement element is spaced from a pressure side wall and a suction side wall of the airfoil body to respectively define a first near-wall cooling flow channel and a second near-wall cooling flow channel. The flow displacement element includes an outer surface facing the near-wall cooling flow channels and an inner surface facing the inactive cavity. The inner surface facing the inactive cavity includes features configured to influence a mass and/or stiffness of the turbine airfoil, to thereby produce a predetermined modal frequency response of the turbine airfoil.


Find Patent Forward Citations

Loading…