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:
Jan. 14, 2025

Filed:

Jun. 13, 2021
Applicant:

Safran Power Units, Toulouse, FR;

Inventors:

Victor Georges Maurice Lhomme, Moissy-Cramayel, FR;

Franck Jean-Louis Galibert, Moissy-Cramayel, FR;

Gilles Aime Yann Guyader, Moissy-Cramayel, FR;

Claire Madeleine Martin, Moissy-Cramayel, FR;

Assignee:

SAFRAN POWER UNITS, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/20 (2006.01);
U.S. Cl.
CPC ...
F01D 25/20 (2013.01); F05D 2220/323 (2013.01); F05D 2260/98 (2013.01);
Abstract

A lubrication reservoir for a turbine engine for an aircraft or self-propelled flying machine, comprising a suction strainer in a lower part of the chamber, and at least one degassing device and at least one vent in an upper part. The reservoir is wherein, in order to make it possible to supply the strainer and prohibit lubricant from intruding into the at least one vent, it includes at least one first partition that separates the lower part from the upper part and is pierced with calibrated holes, two vents arranged on either side of a vertical median plane of the chamber and two vent ducts which extend into the upper part below the degassing device, each duct comprising a bend and having the bend located on the other side of the median plane with respect to the inlet thereof.


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