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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.

Patent No.:

US 11572833 B1

PDFFull Text
Date of Patent:
Feb. 07, 2023

Filed:

Apr. 02, 2019

Aircraft engine assembly with a supply path to an inter-flow compartment tank of turbine engine

Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Antoine Elie Hellegouarch, Moissy-Cramayel, FR;

Frédéric Paul Eichstadt, Moissy-Cramayel, FR;

Quentin Matthias Emmanuel Garnaud, Moissy-Cramayel, FR;

Assignee:

SAFRAN AIRCRAFT ENGINES, Paris, FR;

Attorney:

Pearne & Gordon LLP

Primary Examiner:

Todd E Manahan

Assistant Examiner:

Marc J Amar

Int. Cl.
CPC ...
F02C 7/06 (2006.01); B64D 27/12 (2006.01); F01M 11/04 (2006.01); F02C 7/20 (2006.01); F02C 7/32 (2006.01); F01D 25/18 (2006.01); B64D 27/26 (2006.01);
U.S. Cl.
CPC ...
F02C 7/06 (2013.01); B64D 27/12 (2013.01); F01D 25/18 (2013.01); F01M 11/0458 (2013.01); F02C 7/20 (2013.01); F02C 7/32 (2013.01); B64D 2027/268 (2013.01); F05D 2260/98 (2013.01);
Abstract

An aircraft engine assembly includes a dual-flow turbine engine, a pylon for mounting the turbine engine, thrust-absorbing rods connecting the turbine engine to the pylon, and an inter-flow compartment housing a lubricant tank. In order to facilitate the filling of the tank, a lubricant supply path is fluidly connected to the tank, this path passing through an inner hollow region of at least one of the two thrust-absorbing rods.

Find Patent Forward Citations

Hellegouarch, Antoine. (2023). Aircraft engine assembly with a supply path to an inter-flow compartment tank of turbine engine (U.S. Patent No. 11572833). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11572833

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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