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.:
Date of Patent:
Mar. 09, 2021
Filed:
Dec. 12, 2017
Applicant:
Airbus Operations Gmbh, Hamburg, DE;
Inventor:
Alexei Vichniakov, Hamburg, DE;
Assignee:
AIRBUS OPERATIONS GMBH, Hamburg, DE;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16B 37/06 (2006.01); B29C 65/16 (2006.01); B29C 65/14 (2006.01); B29C 65/56 (2006.01); B29C 65/10 (2006.01); B29C 65/02 (2006.01); B29C 65/08 (2006.01); B64C 1/12 (2006.01); F16B 5/04 (2006.01); B21J 15/08 (2006.01); F16B 25/00 (2006.01); F16B 39/02 (2006.01); B29C 65/00 (2006.01); B29L 31/30 (2006.01); B29K 81/00 (2006.01); B29K 101/10 (2006.01); B29K 101/12 (2006.01);
U.S. Cl.
CPC ...
F16B 37/067 (2013.01); B21J 15/08 (2013.01); B29C 65/562 (2013.01); B29C 66/0242 (2013.01); B29C 66/1122 (2013.01); B29C 66/41 (2013.01); B29C 66/721 (2013.01); B29C 66/72143 (2013.01); B29C 66/7392 (2013.01); B29C 66/73941 (2013.01); B64C 1/12 (2013.01); F16B 25/0015 (2013.01); F16B 39/02 (2013.01); B29C 65/02 (2013.01); B29C 65/08 (2013.01); B29C 65/10 (2013.01); B29C 65/1412 (2013.01); B29C 65/1425 (2013.01); B29C 65/16 (2013.01); B29C 66/71 (2013.01); B29C 66/7212 (2013.01); B29C 66/72141 (2013.01); B29C 66/73115 (2013.01); B29C 66/73117 (2013.01); B29C 2793/0045 (2013.01); B29K 2023/06 (2013.01); B29K 2081/04 (2013.01); B29K 2101/10 (2013.01); B29K 2101/12 (2013.01); B29L 2031/30 (2013.01); B29L 2031/3076 (2013.01); B29L 2031/3097 (2013.01); F16B 5/04 (2013.01);
Abstract
A method for joining together different components or different sections of a single component, wherein at least one of the components is a thermoplastic fiber composite component, by using a threaded fastener. Heat is used for softening the thermoplastic fiber composite component to be joined together with the threaded fastener. A joined-together fiber composite component of a vehicle, aircraft or spacecraft, can be obtained by the disclosed method.