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FIBROUS TEXTURE FOR TURBINE ENGINE BLADE MADE OF COMPOSITE MATERIAL

机译:涡轮发动机叶片的纤维纹理由复合材料制成

摘要

The invention relates to a fibrous texture (100) intended to form the fibrous reinforcement of a turbine engine (1) blade (10) made of composite material, the texture being in a single piece and having a three-dimensional weave between a plurality of first fibre warp yarns or strands extending in a radial direction (L) and a plurality of first fibre weft yarns or strands extending in a chord direction (T), the texture comprising a blade root portion (110) and a blade airfoil portion (120) extending between the blade root portion and a free end (121) of the fibrous texture. The blade airfoil portion (120) has a reinforced area (140) in the vicinity of the free end (121) of the texture comprising weft yarns or strands made of second fibres different from the first fibres, the second fibres having an elongation at break greater than that of the first fibres, and characterised in that a first ratio of second fibres in the reinforced area (140) is greater than a second ratio of second fibres in the rest of the blade airfoil portion (120).
机译:本发明涉及一种纤维纹理(100),旨在形成由复合材料制成的涡轮发动机(1)叶片(10)的纤维增强,纹理在单件中并在多个之间具有三维编织在径向(L)中延伸的第一纤维翘曲纱线或股线在弦方向(T)中延伸的多个第一纤维纬纱或股线,该纹理包括叶片根部(110)和刀片翼型部分(120 )在叶片根部和纤维纹理的自由端(121)之间延伸。叶片翼型部分(120)具有在纹理的自由端(121)附近的增强区域(140),该纹理包括由与第一纤维不同的第二纤维制成的纬纱或股线,第二纤维在断裂处具有伸长率大于第一纤维的第一纤维,并且其特征在于,增强区域(140)中的第二纤维的第一比率大于叶片翼型部分(120)的其余部分中的第二纤维的第二比率。

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