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Fibrous texture for producing a fan blade made of composite material

机译:用于生产复合材料风扇叶片的纤维质地

摘要

A fibrous texture to form the fibrous reinforcement of a turbomachine blade made of composite material, the texture being made in one piece and having a three-dimensional weaving, and includes blade root, blade airfoil and blade support portions. The blade support portion includes a first area extending transversely from a first edge of the texture to form a leading edge and a second area extending transversely from the first area up to a second edge of the texture to form a trailing edge, the first area including warp yarns or strands made of second fibers different from the first fibers, the second fibers having an elongation at break greater than that of the first fibers, the first area having a first volume ratio in yarns or strands made of second fibers strictly greater than a second volume ratio in yarns or strands made of second fibers in the second area.
机译:形成由复合材料制成的涡轮机叶片的纤维增强物的纤维质感,该质感被制成一件并且具有三维编织,并且包括叶片根部,叶片翼型件和叶片支撑部分。叶片支撑部分包括从纹理的第一边缘横向延伸以形成前缘的第一区域和从纹理的第一区域直至纹理的第二边缘横向地延伸以形成后缘的第二区域,第一区域包括由不同于第一纤维的第二纤维制成的经纱或股线,第二纤维的断裂伸长率大于第一纤维的断裂伸长率,由第二纤维制成的纱线或股线中的第一面积的第一体积比严格大于a。在第二区域中由第二纤维制成的纱线或股线中的第二体积比。

著录项

  • 公开/公告号GB201914600D0

    专利类型

  • 公开/公告日2019-11-20

    原文格式PDF

  • 申请/专利权人 Safran Aircraft Engines;

    申请/专利号GB201914600

  • 发明设计人

    申请日2019-10-09

  • 分类号

  • 国家 GB

  • 入库时间 2022-08-21 10:55:56

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