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US08172511B2 Radial compressor with blades decoupled and tuned at anti-nodes 有权
带叶片的径向压缩机在反节点上解耦并调谐

Radial compressor with blades decoupled and tuned at anti-nodes
Abstract:
A gas turbine engine includes a radial compressor with first and second blades. The first and second blades have tuned leading edges that prevent natural frequencies from exciting at speeds within an expected operating speed range.
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