Invention Grant
- Patent Title: High-pressure turbine blades made of ceramic matrix composites
- Patent Title (中): 高压涡轮叶片由陶瓷基复合材料制成
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Application No.: US14059968Application Date: 2013-10-22
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Publication No.: US09482104B2Publication Date: 2016-11-01
- Inventor: Francois Gallet
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1260045 20121022
- Main IPC: F01D5/30
- IPC: F01D5/30 ; F01D5/28 ; B29D99/00

Abstract:
A turbine blade for a turbojet engine, made of a ceramic matrix composite material and including a vane that extends above a platform and a root that extends below the platform is provided. The pressure face and the suction face of the vane is formed by sheets of a composite material, the sheets meeting at the leading edge and trailing edge of the vane. The pressure face and suction face are formed by the same sheet bent back on itself, in a radial direction, at the leading edge or trailing edge.
Public/Granted literature
- US20140119939A1 HIGH-PRESSURE TURBINE BLADES MADE OF CERAMIC MATRIX COMPOSITES Public/Granted day:2014-05-01
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