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:
Nov. 06, 2018

Filed:

Mar. 25, 2014
Applicant:

Airbus Defence and Space Sas, Les Mureaux, FR;

Inventors:

Audrey Menochet, Le Bouscat, FR;

Christophe Colin, St Medard en Jalles, FR;

Assignee:

ARIANEGROUP SAS, Paris, FR;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B29C 65/34 (2006.01); B29C 65/00 (2006.01); B29C 65/48 (2006.01); B29C 65/50 (2006.01); C08J 5/12 (2006.01); C08J 5/24 (2006.01); B32B 25/08 (2006.01); B32B 25/10 (2006.01); B32B 27/08 (2006.01); B32B 27/12 (2006.01); B32B 27/18 (2006.01); B32B 27/28 (2006.01); B29C 65/20 (2006.01); B29C 65/36 (2006.01); B29L 31/30 (2006.01); B29C 65/02 (2006.01); B29C 35/02 (2006.01); B29K 71/00 (2006.01); B29L 7/00 (2006.01); B29L 9/00 (2006.01);
U.S. Cl.
CPC ...
B29C 66/712 (2013.01); B29C 65/20 (2013.01); B29C 65/344 (2013.01); B29C 65/348 (2013.01); B29C 65/364 (2013.01); B29C 65/486 (2013.01); B29C 65/4815 (2013.01); B29C 65/4835 (2013.01); B29C 65/5021 (2013.01); B29C 65/5057 (2013.01); B29C 66/1122 (2013.01); B29C 66/45 (2013.01); B29C 66/721 (2013.01); B29C 66/7212 (2013.01); B29C 66/7392 (2013.01); B29C 66/73751 (2013.01); B29C 66/73752 (2013.01); B29C 66/73755 (2013.01); B29C 66/742 (2013.01); B29C 66/7465 (2013.01); B29C 66/81455 (2013.01); B32B 25/08 (2013.01); B32B 25/10 (2013.01); B32B 27/08 (2013.01); B32B 27/12 (2013.01); B32B 27/18 (2013.01); B32B 27/281 (2013.01); C08J 5/121 (2013.01); C08J 5/24 (2013.01); B29C 35/02 (2013.01); B29C 65/02 (2013.01); B29C 66/02 (2013.01); B29C 66/02245 (2013.01); B29C 66/71 (2013.01); B29C 66/919 (2013.01); B29C 66/91443 (2013.01); B29C 66/91645 (2013.01); B29C 66/91655 (2013.01); B29C 66/949 (2013.01); B29C 2035/0211 (2013.01); B29K 2071/00 (2013.01); B29K 2995/0005 (2013.01); B29K 2995/0046 (2013.01); B29K 2995/0087 (2013.01); B29L 2007/008 (2013.01); B29L 2009/00 (2013.01); B29L 2031/3097 (2013.01); B32B 2260/021 (2013.01); B32B 2260/046 (2013.01); B32B 2262/101 (2013.01); B32B 2262/103 (2013.01); B32B 2307/304 (2013.01); B32B 2307/306 (2013.01); C08J 2300/22 (2013.01);
Abstract

A method for producing, by welding, a joint between a thermoplastic matrix composite material and an elastomeric material. The elastomeric material is functionalized by forming a thin layer of elastomeric material incorporating particles of thermoplastic material and melting the thin layer onto the surface of the elastomeric material during the pressure-vulcanization of the elastomer. The functionalized surface of the elastomeric material is welded to the thermoplastic material of the composite. The welding operation includes interposing a metal fabric coated with thermoplastic material between the surfaces of the elastomer and the composite that are welded to each other, and passing an electric current through same, resulting in the surface melting of the two materials.


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