首页> 外国专利> HOLLOW-BLADE TURBINE VANE MADE FROM COMPOSITE MATERIAL, TURBINE OR COMPRESSOR INCLUDING A NOZZLE OR GUIDE VANE ASSEMBLY FORMED BY SUCH BLADES, AND TURBOMACHINE COMPRISING SAME

HOLLOW-BLADE TURBINE VANE MADE FROM COMPOSITE MATERIAL, TURBINE OR COMPRESSOR INCLUDING A NOZZLE OR GUIDE VANE ASSEMBLY FORMED BY SUCH BLADES, AND TURBOMACHINE COMPRISING SAME

机译:由复合材料,涡轮或压缩机制成的中空涡轮叶片,包括由此类叶片组装而成的喷嘴或导流叶片,以及由相同叶片组成的涡轮机

摘要

A turbomachine vane (10) made from composite material comprises a hollow blade (12) including an internal passage (11) extending along the entire length thereof, an internal platform (14) and an external platform (16). The blade is extended on the external side of the external platform by an upstream attachment portion and a downstream attachment portion for mounting the vane in a casing, said attachment portions being formed by attachment lugs (24, 26, 28) extending from external longitudinal ends of lower surface (12a) and upper surface (12b) walls of the blade, with the fibrous reinforcement texture of the composite material extending continuously between said walls and the attachment lugs.
机译:由复合材料制成的涡轮机叶片(10)包括中空叶片(12),该中空叶片包括沿其整个长度延伸的内部通道(11),内部平台(14)和外部平台(16)。叶片通过用于将叶片安装在壳体中的上游附接部分和下游附接部分在外部平台的外侧上延伸,所述附接部分由从外部纵向端延伸的附接凸耳(24、26、28)形成。叶片的下表面(12a)和上表面(12b)的“夹层”,使复合材料的纤维增强结构在所述壁和连接凸耳之间连续延伸。

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