发明申请
US20070077144A1 Dust resistant platform blade 有权
防尘平台刀片

Dust resistant platform blade
摘要:
A gas turbine engine rotor blade includes an airfoil, platform, shank, and dovetail integrally joined together. A dust escape hole extends through the platform adjacent a fillet bridging the platform and shank to bleed dust therefrom during operation.
公开/授权文献
信息查询
0/0