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:
Apr. 13, 2021

Filed:

Jul. 25, 2019
Applicant:

Safran Transmission Systems, Colombes, FR;

Inventors:

Adrien Louis Simon, Moissy-Cramayel, FR;

Jean-Charles Michel Pierre Di Giovanni, Moissy-Cramayel, FR;

Boris Pierre Marcel Morelli, Moissy-Cramayel, FR;

Florian Rappaport, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16H 57/04 (2010.01); F02C 7/36 (2006.01); F16H 1/28 (2006.01); F16H 57/02 (2012.01);
U.S. Cl.
CPC ...
F16H 57/0401 (2013.01); F02C 7/36 (2013.01); F16H 1/2863 (2013.01); F16H 2057/02073 (2013.01);
Abstract

Device of the reduction gear or differential type for a turbine engine of an aircraft. A central sun gear and a row of planet gears, each of the planet gears are rotationally guided by at least one bearing extending around a tubular support. The tubular support includes an inner cavity for the reception of oil and through-orifices for the passage of oil of the tubular support to the at least one bearing. A member for circulating the oil is mounted in the cavity and includes at least one oil duct intended to be connected to an oil supply. The oil is intended to flow from the at least one duct into the inner cavity to form an oil film in contact with said tubular support, and to flow through the orifices.


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