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:
May. 29, 2018

Filed:

Jul. 11, 2014
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventors:

Walter Gieg, Eichenau, DE;

Petra Kufner, Poing, DE;

Rudolf Stanka, Rattenkirchen, DE;

Assignee:

MTU AERO ENGINES AG, Munich, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/18 (2006.01); F01D 11/12 (2006.01); F01D 9/02 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F01D 25/183 (2013.01); F01D 9/02 (2013.01); F01D 11/12 (2013.01); F01D 25/246 (2013.01); F05D 2230/64 (2013.01); F05D 2240/11 (2013.01);
Abstract

A turbomachine includes a sealing segment ring that is provided between a front guide vane row and a back guide vane row for sealing a radial gap between a casing section and a rotor blade row rotating between the guide vane rows, wherein the sealing segment ring has a plurality of identical sealing segments and at least one of the guide vane rows has a plurality of identical guide vane segments, wherein the sealing segments each have a plurality of engagement sites lying adjacent to one another in the peripheral direction for interaction with securing elements of this guide vane row, wherein the engagement sites and securing elements are distributed uniformly over the periphery and the engagement sites are a multiple of the securing elements, a sealing element, and a guide vane segment.


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