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.:
Date of Patent:
Mar. 19, 2019
Filed:
Mar. 14, 2016
Applicant:
Safran Aircraft Engines, Paris, FR;
Inventors:
Cédric Zaccardi, Saint Maur des Fosses, FR;
Gwenael Sébastien François Marion, Paris, FR;
Assignee:
SNECMA, Paris, FR;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/02 (2006.01); F02C 7/24 (2006.01); F02C 7/045 (2006.01);
U.S. Cl.
CPC ...
F02C 7/045 (2013.01); B64D 33/02 (2013.01); F02C 7/24 (2013.01); B64D 2033/0206 (2013.01); B64D 2033/0266 (2013.01); F05D 2240/14 (2013.01); F05D 2250/283 (2013.01); F05D 2260/96 (2013.01); F05D 2300/603 (2013.01); Y02T 50/672 (2013.01);
Abstract
The present invention relates to an assembly () for an aircraft turbine engine comprising a fan casing () having an inner surface (), at least one acoustic panel () fastened using fastening elements () to the inner surface of the fan casing, and at least one circumferential stiffener () of the fan casing (). According to the invention, the fastening elements () connect the fan casing () to the stiffener () incorporated with the acoustic panel ().