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:
Mar. 31, 2020

Filed:

Apr. 11, 2013
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Todd A. Davis, Tolland, CT (US);

Brian P. Cigal, Windsor, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/06 (2006.01); F01D 25/28 (2006.01); F01D 25/16 (2006.01); F01D 15/12 (2006.01); F02K 3/06 (2006.01); F02C 7/20 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02C 7/06 (2013.01); F01D 15/12 (2013.01); F01D 25/162 (2013.01); F01D 25/285 (2013.01); F02C 7/20 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F05D 2230/60 (2013.01); F05D 2230/70 (2013.01); F05D 2230/72 (2013.01); F05D 2230/80 (2013.01); Y02T 50/671 (2013.01); Y10T 29/49245 (2015.01);
Abstract

Disclosed is a gas turbine engine configured to include a propulsor section having a fan drive geared architecture. The gas turbine engine includes a gas generator section that includes a compressor section having a first rotor rotationally mounted to a first spool. The engine further includes a bearing package adapted for rotationally supporting the first spool. The bearing package is configured for supporting the first rotor during at least one of (1) a period prior to installation of the fan drive geared architecture into the engine and (2) a period after removal of the fan drive geared architecture from the engine.


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