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:
Dec. 03, 2024

Filed:

Nov. 30, 2021
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Sébastien Oriol, Moissy-Cramayel, FR;

Nicolas Vincent Pierre-Yves Cotereau, Moissy-Cramayel, FR;

Mohammed-Lamine Boutaleb, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/224 (2006.01); F02C 7/14 (2006.01); F16K 17/04 (2006.01); F16K 17/08 (2006.01); F28F 27/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/224 (2013.01); F02C 7/14 (2013.01); F16K 17/046 (2013.01); F16K 17/082 (2013.01); F28F 27/02 (2013.01); F28F 2265/06 (2013.01); F28F 2265/16 (2013.01);
Abstract

An aircraft turbine engine assembly, including a lubricating oil circuit and a fuel supply device, the assembly also including a passive bypass valve enabling the oil to bypass an exchanger, the valve including a valve body and a piston arranged to move in a sliding space defining a first actuating chamber supplied with oil from the oil circuit, as well as a second actuating chamber supplied with fuel from the device, the valve being configured so that when the differential pressure between the oil pressure in the first actuating chamber and the fuel pressure in the second actuating chamber drops below a predetermined value of differential pressure, the piston moves from a normal operating position to an exchanger bypass position.


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