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