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UNSHROUDED TURBOMACHINE IMPELLER WITH IMPROVED RIGIDITY

机译:刚性提高的无扰动涡轮机叶轮

摘要

An unshrouded turbomachine impeller is disclosed. The impeller comprises a hub and a plurality of sequentially arranged blades. Each blade extends from a blade root at the hub to a blade tip and is comprised of a first blade edge and a second blade edge. A flow vane is formed between each pair of neighboring blades. A connection member extends across each flow vane between neighboring blades and rigidly or monolithically connects a first modal displacement region of a first one of the pair of neighboring blades to a second modal displacement region of a second one of the pair of neighboring blades.
机译:公开了一种无罩涡轮机叶轮。叶轮包括轮毂和多个顺序布置的叶片。每个叶片从轮毂处的叶片根部延伸到叶片尖端,并且包括第一叶片边缘和第二叶片边缘。在每对相邻叶片之间形成导流叶片。连接构件跨过相邻叶片之间的每个导流叶片延伸,并且将所述一对相邻叶片中的第一个的第一模态位移区域刚性或整体地连接到所述一对相邻叶片中的第二个的第二模态位移区域。

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