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. 11, 2022

Filed:

Jan. 29, 2019
Applicants:

Safran Nacelles, Gonfreville L'Orcher, FR;

Safran Aircraft Engines, Paris, FR;

Inventors:

Marc Versaevel, Gonfreville L'Orcher, FR;

Denis Ramage, Gonfreville L'Orcher, FR;

Baptiste Cordier, Gonfreville L'Orcher, FR;

Georges Riou, Moissy Cramayel, FR;

Jacky Mardjono, Moissy Cramayel, FR;

Assignees:

Safran Nacelles, Gonfreville L'Orcher, FR;

Safran Aircraft Engines, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/02 (2006.01); F02K 1/82 (2006.01); F02C 7/045 (2006.01); G10K 11/172 (2006.01); F02K 1/34 (2006.01); B64D 29/00 (2006.01); F02C 7/24 (2006.01); G10K 11/16 (2006.01); G10K 11/168 (2006.01);
U.S. Cl.
CPC ...
B64D 33/02 (2013.01); B64D 29/00 (2013.01); B64D 33/06 (2013.01); F02C 7/045 (2013.01); F02C 7/24 (2013.01); F02K 1/827 (2013.01); G10K 11/172 (2013.01); B64D 2033/0206 (2013.01); B64D 2033/0286 (2013.01); F05D 2240/14 (2013.01); F05D 2250/283 (2013.01); F05D 2260/96 (2013.01); F05D 2260/963 (2013.01); F05D 2300/603 (2013.01); G10K 11/161 (2013.01); G10K 11/168 (2013.01); Y02T 50/60 (2013.01);
Abstract

An acoustic attenuation panel for a propulsion unit including a nacelle and a turbojet engine includes a cellular core disposed between an inner skin and an outer skin, called acoustic skin, the acoustic skin including a plurality of acoustic apertures, the acoustic apertures being inclined, at a non-zero inclination angle (β) relative to the direction normal to the acoustic skin, upstream with respect to the flow direction of the air or gas flow to which the panel is intended to be subjected under normal operating conditions, that is to say upstream of the propulsion unit when the panel is mounted in such a unit.


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