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:
Mar. 10, 2020

Filed:

Dec. 06, 2017
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventor:

Karl-Hermann Richter, Markt Indersdorf, DE;

Assignee:

MTU AERO ENGINES AG, Munich, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23K 20/12 (2006.01); B23P 15/04 (2006.01); B23K 20/22 (2006.01); C22C 14/00 (2006.01); C22F 1/18 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); B23K 101/00 (2006.01); B23K 103/14 (2006.01);
U.S. Cl.
CPC ...
B23K 20/129 (2013.01); B23K 20/12 (2013.01); B23K 20/22 (2013.01); B23P 15/04 (2013.01); C22C 14/00 (2013.01); C22F 1/183 (2013.01); F01D 5/147 (2013.01); F01D 5/28 (2013.01); B23K 2101/001 (2018.08); B23K 2103/14 (2018.08); C22C 2202/00 (2013.01); F05B 2230/239 (2013.01); F05B 2230/40 (2013.01); F05B 2280/1074 (2013.01); F05C 2201/90 (2013.01); F05C 2251/04 (2013.01); F05D 2230/239 (2013.01); F05D 2300/174 (2013.01); Y02T 50/672 (2013.01);
Abstract

Disclosed is a method for producing a blade comprising a blade airfoil and a blade root for a turbomachine. The method comprises providing a first workpiece based on a first material and a second workpiece based on a second material which is different from the first material and has a higher temperature resistance than the first material; and connecting the first workpiece and the second workpiece by friction welding to form a composite component having a first region of the first material, and a second region of the second material. Optionally upon material-subtracting further processing, the first region forms the blade root, and the second region forms the blade airfoil.


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