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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 10343373 B1

PDFFull Text
Date of Patent:
Jul. 09, 2019

Filed:

Dec. 16, 2016

Coated composite component

Applicant:

Airbus Defence and Space Gmbh, Taufkirchen, DE;

Inventors:

Thomas Koerwien, Hoehenkirchen, DE;

Michael Hoffmann, Bremen, DE;

Robert Meissner, Bremen, DE;

Helmut Wehlan, Augsburg, DE;

Andreas Roessmann, Munich, DE;

Jens Holtmannspoetter, Erding, DE;

Sebastian Heckner, Munich, DE;

Thomas Meer, Egmating, DE;

Matthias Geistbeck, Mindelheim, DE;

Assignee:

Airbus Defence and Space GmbH, Taufkirchen, DE;

Attorney:

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

Primary Examiner:

Jeffrey A Vonch

Int. Cl.
CPC ...
B23B 7/06 (2006.01); B29C 65/00 (2006.01); B32B 3/24 (2006.01); B29C 33/68 (2006.01); B32B 7/06 (2019.01); B32B 33/00 (2006.01); B32B 27/12 (2006.01); B32B 3/08 (2006.01); B32B 3/26 (2006.01); B32B 5/14 (2006.01); B32B 27/08 (2006.01); B32B 5/28 (2006.01); B32B 27/32 (2006.01); B32B 5/02 (2006.01); B32B 27/04 (2006.01); B29C 37/00 (2006.01); B29C 70/42 (2006.01); B29C 70/54 (2006.01); D03D 15/00 (2006.01); D06M 17/00 (2006.01); B32B 15/08 (2006.01); B32B 15/14 (2006.01); B32B 27/30 (2006.01); B32B 43/00 (2006.01); B32B 3/14 (2006.01);
U.S. Cl.
CPC ...
B32B 7/06 (2013.01); B29C 66/02 (2013.01); B29C 66/721 (2013.01); B29C 66/7316 (2013.01); B29C 66/7392 (2013.01); B29C 66/73751 (2013.01); B32B 3/08 (2013.01); B32B 3/266 (2013.01); B32B 27/12 (2013.01); B32B 33/00 (2013.01); B29C 33/68 (2013.01); B29C 37/0075 (2013.01); B29C 70/42 (2013.01); B29C 70/542 (2013.01); B32B 3/14 (2013.01); B32B 5/02 (2013.01); B32B 5/142 (2013.01); B32B 5/28 (2013.01); B32B 15/08 (2013.01); B32B 15/14 (2013.01); B32B 27/04 (2013.01); B32B 27/08 (2013.01); B32B 27/304 (2013.01); B32B 27/322 (2013.01); B32B 43/006 (2013.01); B32B 2250/44 (2013.01); B32B 2260/021 (2013.01); B32B 2260/023 (2013.01); B32B 2260/046 (2013.01); B32B 2262/106 (2013.01); B32B 2305/07 (2013.01); B32B 2305/076 (2013.01); B32B 2305/18 (2013.01); B32B 2305/72 (2013.01); B32B 2305/77 (2013.01); B32B 2307/748 (2013.01); B32B 2605/00 (2013.01); D03D 15/00 (2013.01); D06M 17/00 (2013.01); Y10T 428/2476 (2015.01); Y10T 428/24331 (2015.01); Y10T 428/24752 (2015.01); Y10T 428/31 (2015.01);
Abstract

A coated composite component includes, in this order, a composite component, a fluorine-containing film and/or a fluorine-containing woven fabric, knitted fabric or crocheted fabric, and a tear-off fabric. A method for producing a coated composite component including, in this order, a composite component, a fluorine-containing film and/or a fluorine-containing woven fabric, knitted fabric or crocheted fabric, and a tear-off fabric.

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