发明名称 TURBINE BLADE 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 2. Each of the cross sections is described by a set of Cartesian coordinates defined at the corresponding fractional span as set forth in Table 4.
申请公布号 US2012057981(A1) 申请公布日期 2012.03.08
申请号 US20100877701 申请日期 2010.09.08
申请人 NASH TIMOTHY CHARLES;O'HEARN JASON L.;UNITED TECHNOLOGIES CORPORATION 发明人 NASH TIMOTHY CHARLES;O'HEARN JASON L.
分类号 F01D5/14 主分类号 F01D5/14
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