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:
Sep. 12, 2017

Filed:

Dec. 23, 2013
Applicant:

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

Inventors:

Richard C. Uskert, Timonium, MD (US);

Ted J. Freeman, Danville, IN (US);

David J. Thomas, Brownsburg, IN (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/12 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); F23R 3/00 (2006.01); F01D 5/18 (2006.01); F01D 9/02 (2006.01); F01D 25/08 (2006.01);
U.S. Cl.
CPC ...
F01D 25/12 (2013.01); F01D 5/147 (2013.01); F01D 5/185 (2013.01); F01D 5/282 (2013.01); F01D 9/02 (2013.01); F23R 3/002 (2013.01); F23R 3/007 (2013.01); F01D 25/08 (2013.01); F05D 2240/35 (2013.01); F05D 2260/203 (2013.01); F05D 2300/514 (2013.01); F05D 2300/603 (2013.01); F05D 2300/6033 (2013.01); F05D 2300/612 (2013.01); F23R 2900/03041 (2013.01); F23R 2900/03042 (2013.01); F23R 2900/03043 (2013.01); Y02T 50/672 (2013.01); Y02T 50/676 (2013.01); Y10T 29/49316 (2015.01);
Abstract

In one embodiment, a gas turbine engine component includes a foam based core and a composite skin member. Both the foam based core and the composite skin member can be used to structurally support the gas turbine engine component. The composite skin member can be a CMC material and is used to partially encapsulate the foam core. The gas turbine engine component can take the form of an airfoil member such as a blade or a vane, a combustor liner, etc. A first portion of the composite skin member includes a first surface extending past an edge of the component creating a step approximate an edge section. In another embodiment, composite skin members can be used to form a continuous shape for the edge section such that the foam core forms part of a gas path surface.


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