发明名称 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.
申请公布号 WO2014031195(A2) 申请公布日期 2014.02.27
申请号 WO2013US42197 申请日期 2013.05.22
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 PARKOS, JR., JOSEPH;HANSEN, JAMES O.
分类号 F01D5/20;F01D5/12 主分类号 F01D5/20
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