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:
Feb. 20, 2018

Filed:

Dec. 18, 2013
Applicant:

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

Inventors:

Roy David Fulayter, Avon, IN (US);

Jonathan Michael Rivers, Indianapolis, IN (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); F01D 5/00 (2006.01); F01D 5/34 (2006.01); B23P 15/02 (2006.01); B23K 20/12 (2006.01);
U.S. Cl.
CPC ...
F01D 5/3061 (2013.01); B23K 20/12 (2013.01); B23P 15/02 (2013.01); F01D 5/005 (2013.01); F01D 5/34 (2013.01); F05D 2230/239 (2013.01); Y10T 29/49318 (2015.01); Y10T 29/49336 (2015.01);
Abstract

In some examples, an apparatus may include a gas turbine engine component comprising a blade, a platform forming an airflow surface from which the blade extends on one side, and a motion weld receiving surface disposed on a non-airflow side of the platform, and a disk having a motion weld disk portion to receive the motion weld receiving surface of the gas turbine engine component and form a motion weld coupling when the disk and gas turbine engine component are coupled, wherein, prior to coupling, the gas turbine engine component further includes a blade stalk disposed on the non-airflow side of the platform and in which is formed the motion weld receiving surface.


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