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Turbomachine case comprising a central part projecting from two lateral portions in a junction region

机译:涡轮机壳,包括从接合区域中的两个横向部分突出的中心部分

摘要

A support case for a turbomachine ring sector includes an annular body around a longitudinal axis of the case, and a downstream edge for attachment of the ring sector. The downstream edge extends from the body radially towards the inside of the case. The downstream edge extends circumferentially along a junction region between the body and a fixed vanes stage. The junction region includes a central portion and two lateral portions located on each side of the central portion, along a circumferential direction of the case with respect to its longitudinal axis. The central portion projects radially outwards from the case with respect to the lateral portions.
机译:涡轮机环形扇区的支撑壳体包括围绕壳体的纵向轴线的环形主体,以及用于连接环形扇区的下游边缘。下游边缘从主体径向朝向壳体的内部延伸。下游边缘沿着主体和固定叶片级之间的连接区域沿周向延伸。结区域包括沿着壳体部分的沿纵向轴线的圆周方向设置在中心部分的每一侧的中央部分和两个横向部分。中央部分从横向部分径向向外突出。

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