发明名称 Turbine vane airfoil
摘要 An airfoil comprises an external surface formed in substantial conformance with a plurality of cross sections. Each of the cross sections has an axial chord and an offset at a corresponding fractional span as set forth in Table 1. Each of the cross sections is described by a set of Cartesian coordinates defined at the corresponding fractional span as set forth in Table 3.
申请公布号 US8602740(B2) 申请公布日期 2013.12.10
申请号 US20100877703 申请日期 2010.09.08
申请人 O'HEARN JASON L.;NASH TIMOTHY CHARLES;UNITED TECHNOLOGIES CORPORATION 发明人 O'HEARN JASON L.;NASH TIMOTHY CHARLES
分类号 F01D9/02;F01D5/14 主分类号 F01D9/02
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