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US09482104B2 High-pressure turbine blades made of ceramic matrix composites 有权
高压涡轮叶片由陶瓷基复合材料制成

High-pressure turbine blades made of ceramic matrix composites
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.
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