Invention Grant
- Patent Title: Component support and turbomachine
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Application No.: US14508675Application Date: 2014-10-07
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Publication No.: US09752455B2Publication Date: 2017-09-05
- Inventor: Rudolf Stanka , Christoph Lauer , Hans Stricker
- 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: Davidson, Davidson & Kappel, LLC
- Priority: EPEP13187698 20131008
- Main IPC: F01D25/16
- IPC: F01D25/16 ; F01D25/24

Abstract:
A component support of the turbomachine, in particular an aircraft engine, is described, which includes at least two essentially annular components on the stator side, which are in axial contact with each other and are preferably oriented coaxially to the machine axis, the first component having a plurality of radial, groove-like recesses, which are laterally overlapped by the second component with its projection-like bearing sections, and an uncontoured support ring surface section being provided between the adjacent bearing sections, a turbomachine also being described.
Public/Granted literature
- US20150098799A1 COMPONENT SUPPORT AND TURBOMACHINE Public/Granted day:2015-04-09
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