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:
Jul. 14, 2020

Filed:

Oct. 24, 2017
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventors:

Lothar Albers, Munich, DE;

Thomas Binsteiner, Munich, DE;

Johann Geppert, Turkenfeld, DE;

Stefan Herbst, Gerolsbach, DE;

Manuel Hertter, Munich, DE;

Alexander Scharf, Munich, DE;

Robert Winsy, Weichs, DE;

Stephen Royston Williams, Seefeld, DE;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/00 (2006.01); F16J 15/447 (2006.01); F01D 11/02 (2006.01); F01D 5/02 (2006.01); F01D 9/04 (2006.01); F04D 29/08 (2006.01); F04D 29/32 (2006.01); F04D 29/54 (2006.01);
U.S. Cl.
CPC ...
F01D 11/001 (2013.01); F01D 5/02 (2013.01); F01D 9/041 (2013.01); F01D 11/02 (2013.01); F16J 15/447 (2013.01); F04D 29/083 (2013.01); F04D 29/321 (2013.01); F04D 29/542 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2230/90 (2013.01);
Abstract

A rotor member is described for a gas turbine that is adapted for rotating about a central axis, the rotor member being a blisk having a rotor blade row that extends around the central axis or a rotor disk having a mounting portion for installing rotor blades of a rotor blade row that extends around the central axis, and being axially offset from the rotor blade row and/or the mounting portion and, extending coaxially, having at least one annular and axially asymmetrical sealing fin that has a radially outer tip portion having a front flank facing the rotor blade row and/or the mounting portion, and an opposite flank facing away from the rotor blade row and/or the mounting portion; the front flank being less steep than the opposite flank; a turbine and a compressor having such a rotor member, and a method for manufacturing such a rotor member having at least one sealing fin coating.


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