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. 21, 2014

Filed:

Oct. 13, 2008
Applicants:

Sabine Metzech, Delmenhorst, DE;

Georg Wachinger, Rosenheim, DE;

Thomas Meer, Egmating, DE;

Christian Lammel, Ismaning, DE;

Inventors:

Sabine Metzech, Delmenhorst, DE;

Georg Wachinger, Rosenheim, DE;

Thomas Meer, Egmating, DE;

Christian Lammel, Ismaning, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/06 (2006.01); B29C 65/00 (2006.01); B29C 65/50 (2006.01); C09J 5/06 (2006.01); B29C 65/36 (2006.01); C08J 5/12 (2006.01); B29C 65/78 (2006.01); B29C 65/34 (2006.01); B29K 307/00 (2006.01); B29C 65/48 (2006.01); B29L 31/30 (2006.01); B29K 309/08 (2006.01); B29K 305/00 (2006.01);
U.S. Cl.
CPC ...
B29C 66/47 (2013.01); B29C 65/344 (2013.01); B29C 66/91221 (2013.01); B29C 66/7212 (2013.01); B29C 66/91411 (2013.01); B29K 2307/00 (2013.01); B29C 65/3444 (2013.01); B29C 65/5057 (2013.01); B29C 66/91651 (2013.01); B29C 66/91216 (2013.01); B29C 66/90 (2013.01); C09J 2400/226 (2013.01); B29C 65/4815 (2013.01); C09J 5/06 (2013.01); B29C 66/721 (2013.01); B29C 65/3676 (2013.01); B29C 65/3492 (2013.01); B29L 2031/3082 (2013.01); C08J 5/121 (2013.01); B29C 66/80 (2013.01); B29C 65/364 (2013.01); B29C 65/3612 (2013.01); B29C 65/3644 (2013.01); B29C 65/7841 (2013.01); B29C 65/3476 (2013.01); B29C 65/3684 (2013.01); B29C 65/5028 (2013.01); C09J 2400/163 (2013.01); B29K 2309/08 (2013.01); B29C 66/8181 (2013.01); B29K 2305/00 (2013.01);
Abstract

The invention concerns a method of connecting a first material to a second material by means of a heat-activatable adhesive material () in aircraft construction, wherein the adhesive material () is arranged between the first material and the second material and an induction heat which is adequate to activate the adhesive material () is generated. The first material and/or the second material and/or the adhesive material () have an induction heat-generating means. The induction heat-generating means is a non-woven metallic mesh and/or the induction heat-generating means () has an amount of carbon fibers for induction heat generation. The invention further concerns an apparatus comprising a first material and a second material, wherein the first material and the second material have a connection which can be produced by a heat-activatable adhesive material arranged between the first material and the second material, in accordance with the method in accordance with the invention.


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