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:
Feb. 22, 2022

Filed:

Jun. 05, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Serge Rene Morreale, Moissy-Cramayel, FR;

Laurent Gille, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16H 57/08 (2006.01); F16H 57/04 (2010.01); B64D 27/10 (2006.01); F02C 6/20 (2006.01);
U.S. Cl.
CPC ...
F16H 57/082 (2013.01); B64D 27/10 (2013.01); F02C 6/20 (2013.01); F16H 57/043 (2013.01); F16H 57/0479 (2013.01); F05D 2220/323 (2013.01); F05D 2260/40311 (2013.01); F16H 2057/085 (2013.01);
Abstract

A rotary planet carrier for a mechanical reduction gear of a turbomachine having an annular row of tubular members for supporting bearings that are parallel to one another and to an axis of rotation (X) of the planet carrier. The tubular members include grooves for oil to flow through that are connected to oil ducts that extend from the grooves to an external peripheral surface. The grooves are rectilinear and parallel to one another and to an axis of revolution (Y) of an internal cylindrical surface of a corresponding tubular member. Some of the grooves have a width about the axis of revolution that is greater than the diameter of the ducts connected to this groove. Some of the ducts are connected to the corresponding groove that is closest to the axis of rotation (X) of the planet carrier.


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