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. 12, 2025

Filed:

Jan. 07, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

William G. Sheridan, Southington, CT (US);

Michael E. Mccune, Colchester, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 21/04 (2006.01); F01D 5/02 (2006.01); F01D 15/12 (2006.01); F01D 21/02 (2006.01); F02C 7/06 (2006.01); F02C 7/36 (2006.01); F04D 25/04 (2006.01); F04D 25/16 (2006.01); F04D 29/041 (2006.01); F04D 29/046 (2006.01); F16H 1/28 (2006.01); F16H 57/10 (2006.01);
U.S. Cl.
CPC ...
F01D 21/045 (2013.01); F01D 5/02 (2013.01); F01D 15/12 (2013.01); F01D 21/02 (2013.01); F01D 21/04 (2013.01); F02C 7/06 (2013.01); F02C 7/36 (2013.01); F04D 25/045 (2013.01); F04D 25/163 (2013.01); F04D 29/041 (2013.01); F04D 29/046 (2013.01); F16H 1/28 (2013.01); F16H 57/10 (2013.01); F05D 2220/32 (2013.01); F05D 2240/60 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/50 (2013.01); F05D 2300/50 (2013.01);
Abstract

A gas turbine engine has a fan drive turbine driving a gear reduction, the gear reduction, in turn, driving a fan rotor, the fan rotor delivering air into a bypass duct as bypass air and into a compressor section as core flow. A forward bearing is positioned between the gear reduction and the fan rotor and supports the gear reduction. A second bearing is positioned aft of the gear reduction and supports the gear reduction. The second bearing is a thrust bearing. A fan drive turbine drive shaft drives the gear reduction. The fan drive turbine drive shaft has a weakened link which is aft of the second bearing such that the fan drive turbine drive shaft will tend to fail at the weakened link, and at a location aft of the second bearing.


Find Patent Forward Citations

Loading…