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TURBOMACHINE CASE COMPRISING A CENTRAL PART PROJECTING FROM TWO LATERAL PORTIONS IN A JUNCTION REGION

机译:涡轮机机壳,由一个枢纽区域的两个侧面部分组成的中央部分

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:用于涡轮机环形区段的支撑壳体包括围绕壳体的纵向轴线的环形主体,以及用于附接环形区段的下游边缘。下游边缘从主体径向向壳体内部延伸。下游边缘沿着主体和固定叶片级之间的接合区域周向延伸。接合区域包括中央部分和沿着该中央部分的相对于其纵向轴线的圆周方向位于该中央部分的每一侧上的两个侧向部分。中央部分相对于侧向部分从壳体径向向外突出。

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