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. 26, 2014

Filed:

Oct. 06, 2011
Applicants:

Daniel Clark, Derby, GB;

Claudia Berkenhoff, Wehrheim, DE;

Claus T Haubold, Wehrheim, DE;

Inventors:

Daniel Clark, Derby, GB;

Claudia Berkenhoff, Wehrheim, DE;

Claus T Haubold, Wehrheim, DE;

Assignees:

Rolls-Royce PLC, London, GB;

Rolls-Royce Deutschland Ltd & Co KG, Blankenfelde-Mahlow, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23P 6/00 (2006.01); B23K 15/00 (2006.01); B23K 26/322 (2014.01); B23K 26/32 (2014.01); B23K 26/34 (2014.01); B23K 26/03 (2006.01); B23K 26/067 (2006.01);
U.S. Cl.
CPC ...
B23K 15/0006 (2013.01); B23K 15/0086 (2013.01); B23K 26/3213 (2013.01); B23P 6/00 (2013.01); B23K 15/00 (2013.01); B23K 26/345 (2013.01); B23K 26/322 (2013.01); B23K 15/0046 (2013.01); B23K 15/0093 (2013.01); B23K 26/034 (2013.01); B23K 26/0673 (2013.01); B23K 2201/001 (2013.01);
Abstract

In a method for beam welding on components with a laser beam or electron beam generated by a beam source, the heat treatment of the welded component required to remove stresses is integrated into the welding process. In a work cycle combined with the welding process, a regulated heat supply to a selected region takes place, according to its residual heat resulting from the welding process and the predicted stresses in that region, using the residual heat remaining from the welding process following the welding process from the same or other beam source(s). The welding region is cooled in a controlled manner, so that welded components which are likely to be subject to high stress in use, provided for example for a aircraft engine, can be made available without inherent stresses and with the desired microstructure in a single—combined—work step.


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