Invention Grant
- Patent Title: Blade-disk assembly, method and turbomachine
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Application No.: US14546675Application Date: 2014-11-18
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Publication No.: US10041363B2Publication Date: 2018-08-07
- Inventor: Werner Humhauser , Herman Klingels , Alexander Kloetzer
- 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: DE102013223583 20131119
- Main IPC: F01D5/30
- IPC: F01D5/30 ; F01D5/14 ; F01D5/32

Abstract:
A blade-disk assembly of a turbomachine is provided, the blade-disk assembly having a plurality of adjacent rotor blades and a closure blade which are tilted into an anchoring groove, and at least one circumferential retention element which interlockingly cooperates with at least one blade, as well as a plurality of tilt-out prevention elements which are disposed between the groove base and the root portions and which, in the rest state, space the blades from the groove base when in the upper position. The blade-disk assembly further has a locking element, a portion of which is located between the groove base and the root portions and which, in the rest state, spaces the closure blade from the groove base when in the upper position. A method for assembling such a blade-disk assembly, as well as a turbomachine, is also provided.
Public/Granted literature
- US20150139811A1 Blade-disk assembly, method and turbomachine Public/Granted day:2015-05-21
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