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:
Sep. 26, 2017

Filed:

Jul. 22, 2014
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventors:

Rudolf Stanka, Rattenkirchen, DE;

Thomas Hess, Munich, DE;

Karl Maar, Pfaffenhofen an der Ilm, DE;

Karl-Heinz Dusel, Unterschleissheim, DE;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/04 (2006.01); B28B 1/00 (2006.01); F02C 7/24 (2006.01); F01D 25/14 (2006.01); F01D 11/18 (2006.01); F01D 11/12 (2006.01);
U.S. Cl.
CPC ...
F01D 25/04 (2013.01); B28B 1/001 (2013.01); F01D 25/145 (2013.01); F02C 7/24 (2013.01); F01D 11/127 (2013.01); F01D 11/18 (2013.01); F05D 2230/20 (2013.01); F05D 2230/22 (2013.01); F05D 2240/11 (2013.01); F05D 2250/11 (2013.01); F05D 2250/12 (2013.01); F05D 2250/13 (2013.01); F05D 2250/18 (2013.01); F05D 2260/941 (2013.01); F05D 2300/501 (2013.01); F05D 2300/514 (2013.01); Y02T 50/672 (2013.01); Y02T 50/675 (2013.01);
Abstract

A damping device for being situated between a housing wall of a housing of a thermal gas turbine and a casing ring is provided. The casing ring includes an area radially internal with regard to a rotation axis of a rotor of the thermal gas turbine and facing rotating moving blades of the gas turbine. The damping device includes at least sectionally a porous damping structure. A method for manufacturing this type of damping device as well as to a thermal gas turbine, in particular an aircraft engine, in which this type of damping device is situated in a housing of the gas turbine between a housing wall and a casing ring are also provided.


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