发明名称 COMPACT INLET GUIDE VANE FOR TURBOEXPANDER
摘要 <P>PROBLEM TO BE SOLVED: To provide an apparatus and a method for manufacturing a compact inlet guide vane system and reducing the force required to operate the inlet guide vane system. <P>SOLUTION: Components of the inlet guide vane system, including but not limited to an actuation rod, an actuation ring, crank rods, cranks, and associated connectors and bushings, are assembled in the same plane. In this regard, when a force is applied to the actuator rod and transferred through the inlet guide vane system components, the force acts in a single plane. Further, the plane is centered over the rotational axial center of the actuating ring. <P>COPYRIGHT: (C)2013,JPO&INPIT
申请公布号 JP2013053622(A) 申请公布日期 2013.03.21
申请号 JP20120187144 申请日期 2012.08.28
申请人 NUOVO PIGNONE SPA 发明人 ASTI ANTONIO;DEL TURCO PAOLO;LANDI GIACOMO
分类号 F01D17/16;F02B37/24;F02C9/22 主分类号 F01D17/16
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