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:
Apr. 05, 2022

Filed:

Sep. 18, 2019
Applicant:

Airbus Operations Sas, Toulouse, FR;

Inventor:

Maxime Zebian, Saint-Sauveur, FR;

Assignee:

Airbus Operations SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/14 (2006.01); F02C 7/24 (2006.01); F02K 1/82 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/14 (2013.01); F02C 7/24 (2013.01); F02K 1/827 (2013.01); F02K 3/06 (2013.01); F05D 2260/208 (2013.01); F05D 2260/213 (2013.01); F05D 2260/96 (2013.01);
Abstract

A turbomachine for an aircraft comprising a thermo-acoustic system associated with a fluid circuit allowing the turbomachine engine to be supplied with fluid, the thermo-acoustic system comprising an exchanger connected to the fluid circuit and through which the fluid that is to be cooled passes, an acoustic noise-attenuation structure forming, in full or in part, a wall of the duct of a fan duct, the structure being situated some distance from the exchanger, and a pulsating heat pipe comprising a tube extending between the exchanger and the acoustic noise-attenuation structure, the tube having a serpentine form with a plurality of elbows bent over at 180° housed alternately in the exchanger and the structure.


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