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UNSHROUDED TURBOMACHINE IMPELLER WITH IMPROVED RIGIDITY
UNSHROUDED TURBOMACHINE IMPELLER WITH IMPROVED RIGIDITY
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机译:刚性提高的无扰动涡轮机叶轮
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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.
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