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. 12, 2021

Filed:

Aug. 29, 2019
Applicants:

Safran Nacelles, Gonfreville l'Orcher, FR;

Safran Ceramics, Le Haillan, FR;

Inventors:

Bertrand Desjoyeaux, Moissy Cramayel, FR;

Davi Silva De Vasconcellos, Moissy Cramayel, FR;

Aline Planckeel, Moissy Cramayel, FR;

Assignees:

Safran Nacelles, Gonfreville l'Orcher, FR;

SAFRAN CERAMICS, Le Haillan, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C04B 35/64 (2006.01); B32B 18/00 (2006.01); C04B 35/628 (2006.01); B64D 29/00 (2006.01); B64C 1/00 (2006.01); B64F 5/10 (2017.01); B28B 1/00 (2006.01); C04B 35/117 (2006.01); C04B 35/18 (2006.01); C04B 35/565 (2006.01); C04B 35/80 (2006.01);
U.S. Cl.
CPC ...
B32B 18/00 (2013.01); B28B 1/002 (2013.01); B64C 1/00 (2013.01); B64D 29/00 (2013.01); B64F 5/10 (2017.01); C04B 35/117 (2013.01); C04B 35/18 (2013.01); C04B 35/565 (2013.01); C04B 35/62849 (2013.01); C04B 35/62852 (2013.01); C04B 35/62863 (2013.01); C04B 35/64 (2013.01); C04B 35/80 (2013.01); C04B 2235/3217 (2013.01); C04B 2235/3463 (2013.01); C04B 2235/3826 (2013.01); C04B 2235/5224 (2013.01); C04B 2235/5228 (2013.01); C04B 2235/5244 (2013.01); C04B 2235/5252 (2013.01);
Abstract

A part for an aircraft turbojet engine nacelle is made of a composite material and includes at least one outer face (S), a fibrous preform including fiber locks and having a surface(s) delimiting depressions between fiber locks, a covering material which at least partially covers the surface(s) of the fibrous preform and in particular the depressions, and a matrix which binds entirely the covering material and the fibrous preform. The covering material is a fibrous mat and the outer face (S) is smooth. A method for manufacturing such a part includes manufacturing the fibrous preform, providing a fibrous mat, depositing the fibrous preform and fibrous mat in a mold, dispersing the matrix between the fibers of the preform and mat and consolidating the fibrous preform and mat.


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