logo

For the Inventor, By the Inventor

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.:

US 10328682 B1

PDFFull Text
Date of Patent:
Jun. 25, 2019

Filed:

May. 26, 2017

Sensor integration in the joining of structural elements

Applicant:

Airbus Defence and Space Gmbh, Taufkirchen, DE;

Inventors:

Thomas Koerwien, Taufkirchen, DE;

Alois Friedberger, Taufkirchen, DE;

Andreas Helwig, Taufkirchen, DE;

Uwe Beier, Taufkirchen, DE;

Frank Weiland, Taufkirchen, DE;

Assignee:

Airbus Defence and Space GmbH, Taufkirchen, DE;

Attorney:

Jenkins, Wilson, Taylor & Hunt, P.A.

Primary Examiner:

Michael N Orlando

Assistant Examiner:

Joshel Rivera

Int. Cl.
CPC ...
B32B 41/00 (2006.01); B32B 5/26 (2006.01); B32B 27/08 (2006.01); B32B 37/10 (2006.01); B32B 37/18 (2006.01); B29C 70/44 (2006.01); B29C 70/54 (2006.01); B29C 70/00 (2006.01); B32B 27/28 (2006.01); B29C 65/48 (2006.01); B29C 65/50 (2006.01); B29C 65/00 (2006.01); B29C 65/02 (2006.01); B64D 45/00 (2006.01); B64C 1/00 (2006.01); B64C 27/473 (2006.01);
U.S. Cl.
CPC ...
B32B 41/00 (2013.01); B29C 70/00 (2013.01); B29C 70/443 (2013.01); B29C 70/54 (2013.01); B32B 5/26 (2013.01); B32B 27/08 (2013.01); B32B 37/10 (2013.01); B32B 37/182 (2013.01); B29C 65/02 (2013.01); B29C 65/4815 (2013.01); B29C 65/5057 (2013.01); B29C 66/721 (2013.01); B29C 66/7212 (2013.01); B29C 66/73751 (2013.01); B29C 66/73752 (2013.01); B29C 66/73754 (2013.01); B29C 66/73755 (2013.01); B32B 27/285 (2013.01); B32B 2260/046 (2013.01); B32B 2262/106 (2013.01); B64C 2001/0072 (2013.01); B64C 2027/4736 (2013.01); B64D 2045/0085 (2013.01); Y02T 50/43 (2013.01);
Abstract

A method for joining structural elements to a component made of at least one fiber-reinforced plastics material, includes providing at least two structural elements made of at least one fiber-reinforced plastics material having a particular matrix; providing at least one film element made of a thermoplastic heavy-duty material; arranging the at least one film element on a surface of one of the structural elements or between surfaces to be joined of the at least two structural elements to be joined; and producing the component to be joined in a curing process.

Find Patent Forward Citations

Loading…