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:
Aug. 24, 2021

Filed:

Nov. 12, 2019
Applicant:

Leonardo S.p.a., Rome, IT;

Inventors:

Gianni Iagulli, San Severo, IT;

Marco Raffone, Naples, IT;

Alberto Russolillo, Foggia, IT;

Tommaso Nanula, Barletta, IT;

Giuseppe Totaro, Lucera, IT;

Assignee:

LEONARDO S.p.A., Rome, IT;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B32B 3/00 (2006.01); B32B 7/00 (2019.01); B32B 37/00 (2006.01); B64C 3/00 (2006.01); B64F 5/10 (2017.01); B32B 3/08 (2006.01); B32B 7/12 (2006.01); B32B 37/10 (2006.01); B32B 37/12 (2006.01); B64C 3/18 (2006.01); B64C 3/26 (2006.01); B64C 3/34 (2006.01);
U.S. Cl.
CPC ...
B32B 37/0076 (2013.01); B32B 3/085 (2013.01); B32B 7/12 (2013.01); B32B 37/10 (2013.01); B32B 37/12 (2013.01); B64C 3/182 (2013.01); B64C 3/187 (2013.01); B64C 3/26 (2013.01); B64F 5/10 (2017.01); B32B 2260/021 (2013.01); B32B 2260/046 (2013.01); B32B 2262/101 (2013.01); B32B 2262/106 (2013.01); B32B 2605/18 (2013.01); B64C 3/185 (2013.01); B64C 3/34 (2013.01);
Abstract

A method for manufacturing a wing-box for aircraft comprises: arranging, on a curing surface, a first panel of composite material comprising a skin a plurality of longitudinal stringers, and arranging, on each stringer, a caul plate; arranging, on the first panel, pluralities of support inserts so that each support insert rests on a respective caul plate, and on the skin of the first panel, and arranging, on the first panel, a plurality of ribs of non-polymerized composite material, each rib comprising a plate, a first pair of flanges and a second pair of flanges arranged at opposed ends of the plate, and having openings on an edge of the plate, by placing the respective first pair of flanges on the first panel and the respective plurality of openings on the plurality of support inserts, and having the first panel and the plurality of ribs undergo a curing process in autoclave with vacuum bag.


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