发明名称 Compressor impeller thickness profile with localized thick spot
摘要 An air foil includes a leading edge, a trailing edge, a hub contour, and a tip contour, whereby the hub contour and tip contour extend between the leading and trailing edges to define a blade surface therebetween. A localized thick spot is disposed between the leading edge and the trailing edge and extends from a first point on the hub contour to a second point on the tip contour. The localized thick spot includes a generally sheared profile and is operable to provide the air foil with a desired strength while concurrently providing desired aerodynamic properties.
申请公布号 US7112043(B2) 申请公布日期 2006.09.26
申请号 US20030652735 申请日期 2003.08.29
申请人 GENERAL MOTORS CORPORATION 发明人 JARRAH YOUSEF M.
分类号 F04D29/66;F01D5/04;F04D29/28;F04D29/30 主分类号 F04D29/66
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