- Patent Title: Axially divided inner ring for a turbomachine and guide vane ring
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Application No.: US15017729Application Date: 2016-02-08
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Publication No.: US10174628B2Publication Date: 2019-01-08
- Inventor: Werner Humhauser , Josef Wagner , Hermann Klingels
- Applicant: MTU Aero Engines AG
- Applicant Address: DE Munich
- Assignee: MTU Aero Engines AG
- Current Assignee: MTU Aero Engines AG
- Current Assignee Address: DE Munich
- Agency: Barlow, Josephs & Holmes, Ltd.
- Priority: EP15155241 20150216
- Main IPC: F01D9/04
- IPC: F01D9/04 ; F01D17/16 ; F04D29/56 ; F01D11/00 ; F01D25/24 ; F04D29/52 ; F04D29/54 ; F04D29/64

Abstract:
An axially divided inner ring for a turbomachine, for fastening to guide vanes of the turbomachine. The inner ring comprises at least one first, solid ring segment disposed upstream, and a second, solid ring segment disposed downstream, wherein the first ring segment is joined to the second ring segment in a detachable manner by means of at least one fastening element. The first ring segment and/or the second ring segment is joined to at least one sealing segment. The inner ring comprises a securing element for securing the fastening element, wherein the securing element is joined to the first ring segment and/or to the second ring segment. In addition, the present invention relates to a guide vane ring of a turbomachine having guide vanes, which have an axially divided inner ring according to the invention.
Public/Granted literature
- US20160237855A1 AXIALLY DIVIDED INNER RING FOR A TURBOMACHINE AND GUIDE VANE RING Public/Granted day:2016-08-18
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