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:
May. 03, 2022

Filed:

Jan. 11, 2021
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

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

Lawrence E. Portlock, Bethany, CT (US);

Frederick M. Schwarz, Glastonbury, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16H 57/04 (2010.01); F01D 15/12 (2006.01); F01D 25/18 (2006.01); F01D 25/16 (2006.01); F01D 1/02 (2006.01); F01D 5/02 (2006.01); F02C 7/32 (2006.01); F16H 57/08 (2006.01); F02C 7/36 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F01D 15/12 (2013.01); F01D 1/02 (2013.01); F01D 5/02 (2013.01); F01D 5/027 (2013.01); F01D 25/16 (2013.01); F01D 25/18 (2013.01); F02C 7/32 (2013.01); F16H 57/04 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F05D 2220/32 (2013.01); F05D 2220/36 (2013.01); F05D 2240/70 (2013.01); F05D 2260/34 (2013.01); F05D 2260/40311 (2013.01); F16H 57/0423 (2013.01); F16H 57/0479 (2013.01); F16H 57/0486 (2013.01); F16H 2057/085 (2013.01);
Abstract

A turbine engine according to an example of the present disclosure includes, among other things, a fan shaft, at least one tapered bearing mounted on the fan shaft, the fan shaft including at least one passage extending in a direction having at least a radial component, and adjacent the at least one tapered bearing, a fan mounted for rotation on the at least one tapered bearing. An epicyclic gear train is coupled to drive the fan, the epicyclic gear train including a carrier supporting intermediate gears that mesh with a sun gear, and a ring gear surrounding and meshing with the intermediate gears, wherein the epicyclic gear train defines a gear reduction ratio of greater than or equal to 2.3. A turbine section is coupled to drive the fan through the epicyclic gear train, the turbine section having a fan drive turbine that includes a pressure ratio that is greater than 5. The fan includes a pressure ratio that is less than 1.45, and the fan has a bypass ratio of greater than ten (10).


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