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:
Aug. 20, 2019

Filed:

Mar. 15, 2017
Applicant:

Premium Aerotec Gmbh, Augsburg, DE;

Inventors:

Tim Neitzel, Bremen, DE;

Jens Bahnsen, Bremen, DE;

Angelos Miaris, Bremen, DE;

Klaus Edelmann, Ganderkesee, DE;

Assignee:

Premium Aerotec Gmbh, Augsburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/12 (2006.01); B29C 70/54 (2006.01); B29C 65/00 (2006.01); B32B 3/26 (2006.01); C23F 11/00 (2006.01); B29C 70/42 (2006.01); B29C 70/46 (2006.01); B29L 31/30 (2006.01); B29C 65/02 (2006.01); B29C 70/16 (2006.01);
U.S. Cl.
CPC ...
B29C 65/002 (2013.01); B29C 70/42 (2013.01); B29C 70/465 (2013.01); B29C 70/545 (2013.01); B32B 3/263 (2013.01); B64C 1/12 (2013.01); C23F 11/00 (2013.01); B29C 65/02 (2013.01); B29C 66/0246 (2013.01); B29C 66/02241 (2013.01); B29C 66/02245 (2013.01); B29C 66/1286 (2013.01); B29C 66/12841 (2013.01); B29C 66/43421 (2013.01); B29C 66/7212 (2013.01); B29C 66/72326 (2013.01); B29C 66/73921 (2013.01); B29C 70/16 (2013.01); B29L 2031/3076 (2013.01); Y02T 50/43 (2013.01);
Abstract

A method for producing a thermoplastic fiber composite component, in particular for an aircraft or spacecraft, has the following method steps: material-removing processing of a first face of a first plate, wherein the first plate comprises a thermoplastic fiber composite material and a local reduction in thickness of the first plate is made by the material-removing processing of the first face; positioning a second plate relative to the first plate such that the first face of the first plate is brought into alignment with a third face of the second plate; and joining the first plate to the second plate to form a single component, wherein the surface of the first face of the first plate is integrally bonded to the surface of the third face of the second plate.


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