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:
Dec. 17, 2019

Filed:

Mar. 27, 2017
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventors:

Christian Liebl, Bockhorn, DE;

Alexander Ladewig, Bad Wiessee, DE;

Laura Buerger, Dachau, DE;

Georg Schlick, Munich, DE;

Steffen Schlothauer, Erdweg, DE;

Karl-Heinz Dusel, Unterschleissheim, DE;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B29C 64/264 (2017.01); B22F 3/105 (2006.01); B33Y 10/00 (2015.01); B33Y 30/00 (2015.01); B33Y 40/00 (2015.01); B33Y 50/02 (2015.01); B33Y 80/00 (2015.01); B23K 26/342 (2014.01); B23K 26/70 (2014.01); B23K 26/08 (2014.01); B23K 31/12 (2006.01); B23K 101/00 (2006.01); B22F 5/00 (2006.01);
U.S. Cl.
CPC ...
B22F 3/1055 (2013.01); B23K 26/083 (2013.01); B23K 26/342 (2015.10); B23K 26/702 (2015.10); B23K 31/125 (2013.01); B33Y 10/00 (2014.12); B33Y 30/00 (2014.12); B33Y 40/00 (2014.12); B33Y 50/02 (2014.12); B33Y 80/00 (2014.12); B22F 5/009 (2013.01); B22F 2003/1056 (2013.01); B22F 2003/1057 (2013.01); B22F 2998/10 (2013.01); B22F 2999/00 (2013.01); B23K 2101/001 (2018.08); Y02P 10/295 (2015.11);
Abstract

The invention relates to a method for the additive manufacture of at least one region of a component. Here, at least the following steps are carried out: a) layer-wise application of at least one powder-form component material onto a component platform in the region of a build-up and joining zone; b) layer-wise and local solidifying of the component material by selective exposure of the component material by at least one high-energy beam in the region of the build-up and joining zone, with the formation of a component layer; c) layer- wise lowering of the component platform by a pre-defined layer thickness; and d) repeating steps a) to c) until the component region or the component has been completely fabricated.


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