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:
Jan. 21, 2020

Filed:

Oct. 24, 2017
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventor:

Hermann Klingels, Dachau, DE;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/28 (2006.01); F02C 7/20 (2006.01); F01D 25/16 (2006.01);
U.S. Cl.
CPC ...
F01D 25/28 (2013.01); F01D 25/162 (2013.01); F02C 7/20 (2013.01);
Abstract

A turbine center frame for a gas turbine, in particular an aircraft gas turbine, having a hot gas-conveying, segmented annular duct (), a radial outer casing () that is disposed at a distance around the annular duct (), a hub element () that is disposed radially inwardly at a distance from the annular duct (), a plurality of struts () that essentially extend in the radial direction (RR) through the annular duct () and that are coupled radially inwardly to the hub element () and radially outwardly to the outer casing (), and having at least one connecting element (), that is formed obliquely to the struts (), that extends through the annular duct (), and is coupled radially inwardly to a seal carrier element (), the seal carrier element () being supported axially forwardly on the hub element (). At least one connecting element () is coupled radially outwardly to one of the struts ().


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