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:
Oct. 15, 2024

Filed:

Oct. 26, 2021
Applicant:

Safran Nacelles, Gonfreville l'Orcher, FR;

Inventors:

Denis Guillois, Moissy Cramayel, FR;

Fabienne Quenu, Moissy Cramayel, FR;

Anne Mounier, Moissy Cramayel, FR;

Franck Philippe Gérald Zaganelli, Moissy Cramayel, FR;

Assignee:

Safran Nacelles, Gonfreville l'Orcher, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/045 (2006.01);
U.S. Cl.
CPC ...
F02C 7/045 (2013.01); F05D 2220/32 (2013.01); F05D 2230/20 (2013.01); F05D 2230/60 (2013.01);
Abstract

An air intake of a turbojet engine nacelle includes an air intake lip, an annular structure, a rear partition, and at least one acoustic attenuation structure. The annular structure includes at least a part of an outer fairing and an inner fairing joined to each other by the air intake lip. The rear partition is connected to the inner fairing. The acoustic attenuation structure is attached to the inner fairing of the annular structure. At least part of the outer fairing, the air intake lip and the inner fairing are integral with each other.


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