发明授权
US07549846B2 Turbine blades 有权
涡轮叶片

Turbine blades
摘要:
A turbine blade is provided for use in a gas turbine engine. The turbine blade has a platform, an airfoil radially extending from the platform, and an attachment portion comprising an asymmetric root neck portion having a higher stress side and a lower stress side. The turbine blade may further have additional material and a compound fillet for dispersing strain in a region where the airfoil overhangs the neck portion.
公开/授权文献
信息查询
0/0