发明名称 Use of non-uniform nozzle vane spacing to reduce acoustic signature
摘要 A stator for a turbomachine. The stator includes a plurality of nozzle vanes, with the distance between each of the plurality of nozzle vanes varying circumferentially around the stator in a repeating pattern configured to distribute a vibration energy over a plurality of side band vibration frequencies around a nominal passing frequency in a rotor.
申请公布号 US8277166(B2) 申请公布日期 2012.10.02
申请号 US20090486501 申请日期 2009.06.17
申请人 TECZA JOSEPH ANDREW;RASHID STEPHEN SAMUEL;DRESSER-RAND COMPANY 发明人 TECZA JOSEPH ANDREW;RASHID STEPHEN SAMUEL
分类号 F01D9/04 主分类号 F01D9/04
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