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:
Aug. 14, 2018

Filed:

Nov. 23, 2015
Applicants:

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

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

Inventors:

Kerry J. Lighty, Avon, IN (US);

Jared I. Taketa, 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 25/16 (2006.01); F16C 19/55 (2006.01); F02C 7/06 (2006.01); F02C 7/36 (2006.01); F02C 3/107 (2006.01); F01D 5/02 (2006.01); F01D 25/18 (2006.01); F01D 25/24 (2006.01); F16C 19/26 (2006.01); F16C 33/66 (2006.01);
U.S. Cl.
CPC ...
F01D 25/16 (2013.01); F01D 5/026 (2013.01); F01D 25/162 (2013.01); F01D 25/18 (2013.01); F01D 25/24 (2013.01); F02C 3/107 (2013.01); F02C 7/06 (2013.01); F02C 7/36 (2013.01); F16C 19/55 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2240/54 (2013.01); F05D 2240/63 (2013.01); F05D 2260/98 (2013.01); F16C 19/26 (2013.01); F16C 33/6659 (2013.01); F16C 33/6677 (2013.01); F16C 2360/23 (2013.01);
Abstract

An exemplary gas turbine engine includes a radially stacked intershaft bearing assembly. The assembly includes an outer stubshaft having outer and inner diameter surface portions disposed concentrically with respect to one another. The outer diameter surface portion is rotatably connected to a body of the engine, and the inner diameter surface portion is rotatably connected to an inner stubshaft of the engine, so as to provide a stacked configuration of the inner stubshaft, the outer stubshaft, and the body along a radial direction orthogonal to a longitudinal axis of the engine.


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