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:
Apr. 09, 2019

Filed:

Feb. 04, 2016
Applicants:

Rolls-royce Corporation, Indianapolis, IN (US);

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

Inventors:

Aaron Sippel, Zionsville, IN (US);

Daniel Kent Vetters, Indianapolis, IN (US);

Ted Freeman, Danville, IN (US);

Joseph Pan Lamusga, Indianapolis, IN (US);

Assignees:

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

Rolls-Royce Corporation, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); B23P 15/02 (2006.01); F01D 5/14 (2006.01); F01D 9/04 (2006.01); B32B 18/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); B23P 15/02 (2013.01); B32B 18/00 (2013.01); F01D 5/147 (2013.01); F01D 5/284 (2013.01); F01D 9/041 (2013.01); C04B 2237/38 (2013.01); C04B 2237/76 (2013.01); C04B 2237/86 (2013.01); F05D 2220/32 (2013.01); F05D 2230/21 (2013.01); F05D 2230/23 (2013.01); F05D 2230/25 (2013.01); F05D 2230/314 (2013.01); F05D 2230/60 (2013.01); F05D 2240/12 (2013.01); F05D 2240/30 (2013.01); F05D 2240/80 (2013.01); F05D 2260/30 (2013.01); F05D 2300/2261 (2013.01); F05D 2300/6033 (2013.01);
Abstract

The disclosure describes a gas turbine engine blade that includes a dovetail portion comprising a first ceramic matrix composite, an airfoil portion comprising the first ceramic matrix composite, a transition portion between the airfoil portion and the dovetail portion, and a platform portion that substantially surrounds the transition portion. The airfoil portion may define a capture feature that is configured to engage with and mechanically restrain the platform portion from moving beyond the capture feature toward a tip of the airfoil portion.


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