A turbine blade includes an airfoil and integral platform. The platform is biformally contoured in elevation to include bilaterally disposed elevated ridges and depressed troughs on opposite sides of the airfoil.
申请公布号
WO2011022111(A3)
申请公布日期
2011.08.25
申请号
WO2010US38630
申请日期
2010.06.15
申请人
GENERAL ELECTRIC COMPANY;KUHNE, CRAIG, MILLER;BUBNICK, JOSEPH, STEVEN;KALB, ALISHA, VACHHANI
