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Backswept Impeller and Vane Island Diffuser and Shroud for NASA Advanced-Concepts Compressor Test Rig

机译:为Nasa advanced-Concepts压缩机测试装备提供后掠叶轮和叶片岛扩散器和护罩

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A centrifugal impeller based on an existing backswept design was defined. In addition, a vaned diffuser was designed to match this impeller and also to be compatible with an existing 6:1 compressor test rig. The mechanical integrity of this design was verified by analysis. Hardware was procured and inspected to insure conformity with design tolerances. An overspeed test was successfully conducted on one of the impellers fabricated under this program. (Author)

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