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:
Dec. 03, 2019

Filed:

Aug. 22, 2017
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventor:

Joseph Tomsik, Munich, DE;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/16 (2006.01); F01D 9/04 (2006.01); F01D 11/00 (2006.01); F01D 25/24 (2006.01); F01D 17/16 (2006.01);
U.S. Cl.
CPC ...
F01D 9/042 (2013.01); F01D 11/005 (2013.01); F01D 25/162 (2013.01); F01D 25/246 (2013.01); F01D 17/162 (2013.01); F05D 2260/36 (2013.01);
Abstract

An inner ring () for an annular guide vane assembly () of a turbomachine, which inner ring enables variable guide vanes () to be rotatably supported is provided. The inner ring () includes a first and a second securing ring () which are connected together by at least one securing element () extending axially with respect to a centerline (M) of the inner ring (). The at least one securing element () includes a vane bearing () which projects radially with respect to the centerline (M) and which corresponds to an associated guide vane () and is adapted for rotatably supporting the same. A method for manufacturing an annular guide vane assembly () of a turbomachine using such an inner ring () is also provided.


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