发明名称 AIRFOIL PART SHAPE FOR COMPRESSOR
摘要 <P>PROBLEM TO BE SOLVED: To provide a blade as a part of a rotor or a stator related to, for example, a turbo-machine by a device, a system and a method by an illustrative embodiment. <P>SOLUTION: The blade has a specific shape such as the optimization of an operation characteristic. Particularly, a blade thickness as a function of a blade height can be adjusted in conforming to the operation characteristic of the turbo-machine. <P>COPYRIGHT: (C)2012,JPO&INPIT
申请公布号 JP2012047175(A) 申请公布日期 2012.03.08
申请号 JP20110181101 申请日期 2011.08.23
申请人 NUOVO PIGNONE SPA 发明人 LANESE NICOLA;LORUSSO SALVATORE;ARINCI PAOLO;GRIMALDI ANTONIO MARIA
分类号 F04D29/38;F04D19/02 主分类号 F04D29/38
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