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:
Aug. 10, 2021

Filed:

Mar. 20, 2018
Applicant:

Siemens Aktiengesellschaft, Munich, DE;

Inventors:

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

Anthony Waywood, Cincinnati, OH (US);

Steven Koester, Toledo, OH (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F05D 2240/81 (2013.01); F05D 2250/314 (2013.01); F05D 2260/201 (2013.01); F05D 2260/22141 (2013.01);
Abstract

An integrated airfoil and platform cooling system () for a turbine rotor blade () includes an inlet () located at the root () for receiving a supply of a coolant (K), and at least one cooling leg () fluidly connected to the inlet () and configured for conducting the coolant (K) in a radially outboard direction. The cooling leg () is defined at least partially by a span-wise extending internal cavity () within a blade airfoil (). An entrance of the cooling leg () comprises a flow passage () that extends radially outboard and laterally into a blade platform (), so as to direct a radially outboard flowing coolant (K) to impinge on an inner side () of a radially outer surface () of the blade platform (), before leading the coolant (K) into the cooling leg ().


Find Patent Forward Citations

Loading…