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:
Nov. 14, 2023

Filed:

Apr. 28, 2020
Applicant:

Raytheontechnologies Corporation, Farmington, CT (US);

Inventors:

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

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

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

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/10 (2006.01); F01N 3/20 (2006.01); F01D 25/18 (2006.01); F02K 3/06 (2006.01); F02C 7/36 (2006.01); F01D 25/16 (2006.01); F02C 7/06 (2006.01); F02C 7/10 (2006.01); F01N 11/00 (2006.01); F16N 7/34 (2006.01);
U.S. Cl.
CPC ...
F01N 3/208 (2013.01); F01D 25/16 (2013.01); F01D 25/18 (2013.01); F01N 3/2066 (2013.01); F01N 11/00 (2013.01); F02C 3/10 (2013.01); F02C 7/06 (2013.01); F02C 7/10 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F01N 2610/01 (2013.01); F01N 2610/02 (2013.01); F01N 2610/142 (2013.01); F01N 2610/1406 (2013.01); F01N 2610/148 (2013.01); F01N 2900/1814 (2013.01); F05D 2260/40311 (2013.01); F16N 7/34 (2013.01); Y02T 10/12 (2013.01); Y02T 50/60 (2013.01); Y10T 29/4932 (2015.01); Y10T 137/0324 (2015.04); Y10T 137/7297 (2015.04);
Abstract

A gas turbine engine includes a fan shaft diving a fan having fan blades. A gear system includes a sun gear surrounded by a plurality of intermediate gears. A carrier at least partially supports the plurality of intermediate gears. A ring gear surrounds the plurality of intermediate gears. The sun gear is driven by a turbine. At least one fan shaft support bearing is located forward of the gear system. A coupling fixes the ring gear from rotation relative to an engine static structure. A lubrication system lubricates components across a rotation gap. The lubrication system includes a lubricant input. A stationary first bearing receives lubricant from the lubricant input and has a first race in which lubricant flows. A second bearing rotates within the first bearing. The second bearing has a first opening in registration with the first race such that lubricant may flow from the first race through the first opening into a first conduit.


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