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. 03, 2017

Filed:

Dec. 15, 2014
Applicants:

Airbus Operations (Sas), Toulouse, FR;

Airbus Operations S.l., Getafe, ES;

Airbus S.a.s, Blagnac, FR;

Inventors:

Victor Garcia Solares, Getafe, ES;

Pilar Munoz Lopez, Getafe, ES;

Mar Zuarzo Ruiz, Getafe, ES;

Betty Fantina Llorente, Getafe, ES;

Cyrille Collart, Toulouse, FR;

Bernard Duprieu, Blagnac, FR;

Assignees:

AIRBUS OPERATIONS SAS, Toulouse, FR;

AIRBUS SAS, Blagnac, FR;

AIRBUS OPERATIONS S.L., Getafe, ES;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 70/40 (2006.01); B32B 37/18 (2006.01); B29C 65/00 (2006.01); B29C 70/46 (2006.01); B29C 33/38 (2006.01); B29C 35/02 (2006.01); B32B 37/02 (2006.01); B32B 37/06 (2006.01); B32B 38/18 (2006.01); B32B 38/00 (2006.01); B29C 65/02 (2006.01); B29L 31/30 (2006.01); B29D 99/00 (2010.01);
U.S. Cl.
CPC ...
B32B 37/18 (2013.01); B29C 33/3828 (2013.01); B29C 35/0266 (2013.01); B29C 65/02 (2013.01); B29C 66/112 (2013.01); B29C 66/131 (2013.01); B29C 66/348 (2013.01); B29C 66/532 (2013.01); B29C 66/721 (2013.01); B29C 66/73751 (2013.01); B29C 70/46 (2013.01); B32B 37/02 (2013.01); B32B 37/06 (2013.01); B32B 38/0012 (2013.01); B32B 38/1808 (2013.01); B29C 66/0242 (2013.01); B29D 99/0014 (2013.01); B29L 2031/3076 (2013.01); Y10T 156/1044 (2015.01);
Abstract

An efficient method for manufacturing a partially cured composite component intended to be joined with other component or components to form a composite structure and a manufacturing method of the composite structure. The partial curing of a composite layup is achieved using a mold comprising heat conductive elements and insulating elements and applying heat and pressure over the mold. The heat conductive elements are used to transmit or dissipate heat to/from the composite layup. The insulating elements are used to prevent the transmission or dissipation of heat to/from the composite layup.


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