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:
Sep. 27, 2022

Filed:

Jul. 06, 2016
Applicant:

Broetje-automation Gmbh, Rastede, DE;

Inventors:

Raphael Reinhold, Wittmund, DE;

Leo Muijs, Almere, NL;

Marko Bosman, Amsterdam, NL;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B25J 15/06 (2006.01); B29C 70/02 (2006.01); B29C 70/38 (2006.01); B29C 70/54 (2006.01); B32B 15/14 (2006.01); B32B 5/02 (2006.01); B32B 15/04 (2006.01); B32B 7/12 (2006.01); B32B 38/18 (2006.01); B32B 15/20 (2006.01); B29C 31/08 (2006.01); B32B 1/00 (2006.01); B32B 37/18 (2006.01); B29K 277/00 (2006.01); B29K 309/08 (2006.01); B29K 705/00 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B29C 70/023 (2013.01); B25J 15/0616 (2013.01); B29C 31/08 (2013.01); B29C 31/085 (2013.01); B29C 70/38 (2013.01); B29C 70/541 (2013.01); B32B 1/00 (2013.01); B32B 5/02 (2013.01); B32B 7/12 (2013.01); B32B 15/04 (2013.01); B32B 15/14 (2013.01); B32B 15/20 (2013.01); B32B 37/182 (2013.01); B32B 38/1858 (2013.01); B32B 38/1866 (2013.01); B25J 15/0625 (2013.01); B29K 2277/10 (2013.01); B29K 2309/08 (2013.01); B29K 2705/00 (2013.01); B29L 2031/3076 (2013.01); B32B 2038/1891 (2013.01); B32B 2255/06 (2013.01); B32B 2260/021 (2013.01); B32B 2260/023 (2013.01); B32B 2260/046 (2013.01); B32B 2262/0269 (2013.01); B32B 2262/101 (2013.01); B32B 2262/106 (2013.01); B32B 2305/076 (2013.01); B32B 2305/77 (2013.01); B32B 2307/714 (2013.01); B32B 2307/732 (2013.01); B32B 2311/00 (2013.01); B32B 2315/08 (2013.01); B32B 2377/00 (2013.01); B32B 2605/18 (2013.01); B32B 2607/00 (2013.01);
Abstract

A method for producing a Fiber Metal Laminate component of an airplane, using a manipulator system with an end effector and a control, wherein at least one metal layer and at least one unhardened fiber layer are being stacked onto each other in a mould in a stacking sequence, wherein each stacking cycle comprises picking up a metal layer or a fiber layer from a supply stack according to the stacking sequence, transporting the layer to the mould, placement of the layer at a deposition surface in the mould and depositing the so placed layer onto the deposition surface. After being picked up from the supply stack and before being deposited onto the deposition surface the layer to be stacked can be deformed by the end effector as to adapt the form of the layer to the form of the deposition surface.


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