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. 12, 2023

Filed:

Oct. 26, 2021
Applicant:

Safran Nacelles, Gonfreville l'Orcher, FR;

Inventors:

Gina Ferrier, Moissy Cramayel, FR;

Patrick Boileau, Moissy Cramayel, FR;

Pierre Caruel, Moissy Cramayel, FR;

Assignee:

Safran Nacelles, Gonfreville l'Orcher, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/02 (2006.01); B64D 29/06 (2006.01); F02C 7/04 (2006.01);
U.S. Cl.
CPC ...
B64D 33/02 (2013.01); B64D 29/06 (2013.01); F02C 7/04 (2013.01); B64D 2033/0206 (2013.01); B64D 2033/0273 (2013.01); B64D 2033/0286 (2013.01); F05D 2230/60 (2013.01);
Abstract

An air intake includes a substantially cylindrical inner wall, a substantially cylindrical outer wall, a front lip connecting the inner wall and the outer wall, a front mounting flange, and a support structure. The front mounting flange is configured to cooperate with a rear flange of a wall of an aircraft engine. The support structure is configured to be secured to the wall of the aircraft engine at a location longitudinally downstream of the mounting flange. The outer wall includes a downstream end configured to be positioned in a junction area flush with a front end of a fan external cowl. A portion of the outer wall being configured to bear at least against the support structure. The support structure is configured to be secured to the wall of the aircraft engine so that a load path passes directly from the outer wall towards the fan casing.


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