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:
Nov. 26, 2019

Filed:

Dec. 23, 2013
Applicants:

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

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

Inventors:

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

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

Adam L. Chamberlain, Moorseville, IN (US);

Matthew Peter Basiletti, Lafayette, IN (US);

Assignees:

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

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); B23K 1/00 (2006.01); B32B 37/18 (2006.01); B32B 37/24 (2006.01); F01D 5/30 (2006.01);
U.S. Cl.
CPC ...
F01D 5/28 (2013.01); B23K 1/0008 (2013.01); B23K 1/0018 (2013.01); B32B 37/18 (2013.01); B32B 37/24 (2013.01); F01D 5/3084 (2013.01); F01D 5/3092 (2013.01); B32B 2037/243 (2013.01); B32B 2037/246 (2013.01); B32B 2255/205 (2013.01); B32B 2307/30 (2013.01); B32B 2315/02 (2013.01); B32B 2603/00 (2013.01); F05D 2230/23 (2013.01); F05D 2230/237 (2013.01); F05D 2230/31 (2013.01); F05D 2230/313 (2013.01); F05D 2230/314 (2013.01); F05D 2300/6033 (2013.01); Y02T 50/672 (2013.01); Y10T 156/10 (2015.01);
Abstract

A blade for a gas turbine engine comprises a blade portion having a first end and a second end and an engagement portion including a first surface coupled to the second end of the blade portion and a second surface coupled to the second end of the blade portion, the first and second surfaces arranged to extend divergently away from one another. The engagement portion is adapted for coupling to a wheel included in a gas turbine engine wheel.


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