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:

Apr. 29, 2025
Applicant:

GE Avio S.r.l., Rivalta di Torino, IT;

Inventor:

Michele Gravina, Milan, IT;

Assignee:

GE AVIO S.R.L., Rivalta di Torino, IT;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/06 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02C 7/06 (2013.01); F02C 7/36 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/98 (2013.01);
Abstract

A turbine engine includes a fan section including a fan, a fan shaft coupled to the fan, a turbine section including an input shaft, and a planetary gear assembly coupled to the input shaft and the fan shaft. The turbine engine further includes a lubricant transfer unit having a reservoir that has a body, a plurality of sectors angularly positioned about a circumference of the body, a plurality of dams positioned between and defining each of the plurality of sectors, at least one orifice that fluidly couples the plurality of sectors to the planetary gear assembly, and at least one opening to evacuate excess lubricant from each of the plurality of sectors. The reservoir is mounted on the fan shaft of the turbine engine, and the excess lubricant drained from the at least one opening of each of the plurality of sectors lubricates the fan shaft.


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