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Turbomachine stator blade, fan casing comprising such a stator blade, thrust reverser system of a turbomachine with such a stator blade and turbomachine

机译:涡轮机定子叶片,包括这种定子叶片的风扇壳体,具有这种定子叶片的涡轮机的推力反向器系统和涡轮机

摘要

A fan casing comprises a variable-orientation stator vane 1 of a turbine engine 100, comprising a wall 2 that extends between a leading edge 5 and a trailing edge 6 forming a chord line C, where the chord line increases from a root end 3 towards a tip end 4 of the vane 1, and where the profile of the vane is incurved along its direction of extension. The vane may pivot between positions where it straightens the air flow or diverts the air flow towards the exterior of the fan casing. The crown of camber may be between 50 and 300mm, and the ratio between tip chord and root chord may be in the range of 1.1 to 5. The casing may comprise a thrust reverser with at least one occludable opening 56, and the occlusion of the vane may be synchronised with the pivoting of the vane. Also claimed is a thrust reverser system of a turbine engine equipped with such a vane, and a turbine engine equipped with said casing or said thrust reverser.
机译:风扇壳体包括涡轮发动机100的方向可变的定子叶片1,其包括壁2,该壁2在前缘5和后缘6之间延伸形成弦线C,其中弦线从根端3向着弦线3增加。叶片1的末端4,并且叶片的轮廓沿其延伸方向弯曲。叶片可在使气流变直或使气流转向风扇壳体外部的位置之间枢转。弧度的冠部可以在50至300mm之间,并且顶弦和根弦之间的比率可以在1.1至5的范围内。壳体可以包括具有至少一个可封闭的开口56的推力反向器,并且该可逆的齿顶被封闭叶片可以与叶片的枢转同步。还要求保护装备有这种叶片的涡轮发动机的推力反向器系统,以及装备有所述壳体或所述推力反向器的涡轮发动机。

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