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:
Oct. 12, 2021

Filed:

Mar. 11, 2016
Applicant:

Lufthansa Technik Ag, Hamburg, DE;

Inventors:

Jan Oke Peters, Hamburg, DE;

Thomas Gartner, Hamburg, DE;

Joachim Schoen, Halstenbek, DE;

Stefan Kuntzagk, Hamburg, DE;

Assignee:

LUFTHANSA TECHNIK AG, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23C 3/18 (2006.01); B24B 19/14 (2006.01); B24B 21/16 (2006.01); B23P 6/00 (2006.01); F01D 5/00 (2006.01); B23Q 9/00 (2006.01);
U.S. Cl.
CPC ...
B23C 3/18 (2013.01); B23P 6/002 (2013.01); B23Q 9/00 (2013.01); B23Q 9/0014 (2013.01); B24B 19/14 (2013.01); B24B 21/165 (2013.01); F01D 5/005 (2013.01); B23C 2215/44 (2013.01); B23C 2220/40 (2013.01); Y02T 50/60 (2013.01);
Abstract

A device for recontouring a gas turbine blade includes: a holding device having at least one cutting tool; and a guide configured to guide the cutting tool along a leading edge of the gas turbine blade. The cutting tool is configured to remove material from the gas turbine blade using a rotational movement about an axis of rotation. The axis of rotation forms an angle together with a chord of the gas turbine blade in a profile section plane, which extends perpendicularly to a radial extent of the gas turbine blade, and the angle is less than 45°.


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