发明名称 Profiled blades for turbocharger turbines, compressors, and the like
摘要 A rotor and an apparatus including a rotor are provided. For example, the apparatus can be a turbine or compressor having a housing in which the rotor rotates while gas is circulated therethrough. The rotor has a plurality of radially extending blades, and each blade defines a nonlinear profile along at least one edge so that the strains induced in the blade during operation are reduced. A method for manufacturing such a rotor is also provided.
申请公布号 US2005106013(A1) 申请公布日期 2005.05.19
申请号 US20030716651 申请日期 2003.11.19
申请人 GHIZAWI NIDAL A. 发明人 GHIZAWI NIDAL A.
分类号 F01D5/14;(IPC1-7):F01D1/02 主分类号 F01D5/14
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