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. 23, 2018

Filed:

Dec. 27, 2013
Applicant:

Rolls-royce North American Technologies, Inc., Indianapolis, IN (US);

Inventors:

Peter C. Vandervaart, Indianapolis, IN (US);

Jeffrey F. Rhodes, Zionsville, IN (US);

Okey Kwon, Indianapolis, IN (US);

Tab M. Heffernan, Plainfield, IN (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 25/12 (2006.01);
U.S. Cl.
CPC ...
F01D 25/12 (2013.01); F01D 5/186 (2013.01); F01D 5/187 (2013.01); F05D 2230/21 (2013.01); F05D 2260/202 (2013.01); Y02T 50/676 (2013.01);
Abstract

A gas turbine component having a cooling passage is disclosed. In one form, the passage is oriented as a turned passage capable of reversing direction of flow, such as a turned cooling hole. The gas turbine engine component can include a layered structure having cooling flow throughout a region of the component. The cooling hole can be in communication with a space in the layered structure. The gas turbine engine component can be a cast article where a mold can be constructed to produce the cooling hole having a turn.


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