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:由复合材料制成的空心叶片涡轮机叶片,包括由这种叶片形成的喷嘴或导向叶片组件的涡轮机或压缩机,以及包括该叶片的涡轮机

摘要

A turbine engine vane is made of composite material comprises a hollow airfoil with an internal passage extending along its entire length, an inner platform, and an outer platform. The airfoil is extended on the outside of the outer platform by an upstream attachment portion and a downstream attachment portion for mounting the vane in a casing. The attachment portions are formed by an attachment extending from the outer longitudinal ends of the pressure side wall and the suction side wall of the airfoil with continuity of the fiber reinforcing texture of the composite material between the walls and the attachment tabs.
机译:涡轮发动机叶片由复合材料制成,包括中空翼型,该中空翼型具有沿其整个长度延伸的内部通道,内部平台和外部平台。翼型件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部延伸。附接部分由从翼型件的压力侧壁和吸入侧壁的外纵向端延伸的附接件形成,在壁和附接舌片之间具有复合材料的纤维增强织构的连续性。

著录项

  • 公开/公告号US9708918B2

    专利类型

  • 公开/公告日2017-07-18

    原文格式PDF

  • 申请/专利权人 HERAKLES;SNECMA;

    申请/专利号US201214362186

  • 申请日2012-11-26

  • 分类号F01D5/28;F01D9/04;F01D9/06;B29C70/22;

  • 国家 US

  • 入库时间 2022-08-21 13:45:54

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