Invention Grant
- Patent Title: Self-clamping fastener for CMC turbine blade
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Application No.: US14431294Application Date: 2013-09-26
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Publication No.: US10227881B2Publication Date: 2019-03-12
- Inventor: Francois Gallet
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Womble Bond Dickinson (US) LLP
- Priority: FR1259175 20120928
- International Application: PCT/FR2013/052278 WO 20130926
- International Announcement: WO2014/049280 WO 20140403
- Main IPC: F01D5/30
- IPC: F01D5/30 ; F01D5/26

Abstract:
A turbine blade including an airfoil (31) extending above a platform (32) and a root (33) extending below the platform, the root of the blade having the form of a radially extending arm (34), being produced from composite material and including at least one cylindrical face (34). The direction of the generatrices which are oriented in the direction of the platform to allow a clamping piece (5) to slide towards the latter on the cylindrical face under the action of centrifugal force. The arm includes, at its lower end, a protuberance (35) forming a radial bearing point for engagement with an element for retaining the blade on a turbine disc (1). The root (33) is located entirely on the side of the protuberance with respect to the face.
Public/Granted literature
- US20150275680A1 SELF-CLAMPING FASTENER FOR CMC TURBINE BLADE Public/Granted day:2015-10-01
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