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:
Sep. 29, 2026

Filed:

Aug. 05, 2021
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

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

Jason Husband, South Glastonbury, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/16 (2006.01); F01D 5/06 (2006.01); F01D 9/02 (2006.01); F01D 15/12 (2006.01); F01D 25/28 (2006.01); F02C 7/32 (2006.01); F02C 7/36 (2006.01); F02K 3/06 (2006.01); F04D 19/02 (2006.01); F04D 25/04 (2006.01); F04D 29/053 (2006.01); F04D 29/056 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
F01D 25/164 (2013.01); F01D 5/06 (2013.01); F01D 9/02 (2013.01); F01D 15/12 (2013.01); F01D 25/16 (2013.01); F01D 25/28 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F04D 19/02 (2013.01); F04D 25/045 (2013.01); F04D 29/053 (2013.01); F04D 29/056 (2013.01); F04D 29/321 (2013.01); F04D 29/325 (2013.01); F05D 2220/32 (2013.01); F05D 2240/60 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/96 (2013.01); Y02T 50/60 (2013.01); Y10T 29/49321 (2015.01);
Abstract

A gas turbine engine includes a fan section that has fan blades that drive air along a bypass flow path in a bypass duct. A fan shaft is drivingly connected to the fan. A turbine section includes a turbine drive shaft. A gear system is connected to the turbine draft shaft through an input and connected to the fan shaft through an output. At least one of the input and the output include a flexible coupling. A gear system flex mount arrangement accommodates misalignment of the fan shaft and the turbine drive shaft during operation. The gear system flex mount arrangement includes a gear mesh that defines a gear mesh lateral stiffness and a ring gear that defines a ring gear lateral stiffness that is less than 12% of the gear mesh lateral stiffness.


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