发明申请
US20140010663A1 GAS TURBINE ENGINE FAN BLADE TIP TREATMENT 审中-公开
燃气涡轮发动机风扇叶片处理

GAS TURBINE ENGINE FAN BLADE TIP TREATMENT
摘要:
A method of manufacturing a fan blade includes providing a metallic fan blade body, and applying at least a 200 volt potential to the fan blade body in a solution to produce a crystalline oxidation layer. A fan blade for a gas turbine engine includes a metallic fan blade body having a tip with a crystalline oxidation layer. A fan blade for a gas turbine engine includes a metallic fan blade body having a tip with a titanium dioxide layer.
信息查询
0/0