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. 07, 2024

Filed:

Sep. 16, 2020
Applicant:

Safran Transmission Systems, Colombes, FR;

Inventors:

Alexis Claude Michel Dombek, Moissy-Cramayel, FR;

Patrice Jocelyn Francis Gedin, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16N 29/02 (2006.01); F01D 25/18 (2006.01); F02C 7/06 (2006.01); F02C 7/36 (2006.01); F16H 57/04 (2010.01); F16N 27/00 (2006.01); F16H 57/08 (2006.01);
U.S. Cl.
CPC ...
F16N 27/005 (2013.01); F01D 25/18 (2013.01); F02C 7/06 (2013.01); F02C 7/36 (2013.01); F16H 57/042 (2013.01); F16H 57/0479 (2013.01); F16N 29/02 (2013.01); F05D 2220/32 (2013.01); F05D 2260/98 (2013.01); F16H 57/0469 (2013.01); F16H 57/082 (2013.01); F16H 2057/085 (2013.01);
Abstract

An oil restrictor for emergency lubrication of a component for an aircraft turbine engine includes a metal cylindrical body having a longitudinal axis and configured to be housed in and shrink-fitted into a cylindrical bore of a part of the turbine engine. The restrictor further includes an integrated oil circuit enabling oil to pass through the restrictor along the axial extent thereof. The body is a one-piece body, and the circuit has at least two oil channels recessed on an outer cylindrical surface of the body and extending around and/or along the axis.


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