发明名称 Surface treatment for titanium alloy member for aerospace equipment
摘要 Surface processing of titanium alloy members for aerospace equipment imparts high wear resistance, lubricity and high fatigue strength. The method includes an oxygen diffusion step for causing oxygen to diffuse and penetrate in solid solution form into a surface of a titanium alloy member under an oxygen-containing gas atmosphere and a particle bombardment step for bombarding the surface of the titanium alloy member with an airflow containing particles. The aerospace equipment can include a flap rail member and slat rail member for aircraft.
申请公布号 US8252130(B2) 申请公布日期 2012.08.28
申请号 US20050795405 申请日期 2005.02.16
申请人 OGURI KAZUYUKI;KIMURA TAKASHI;SEKIGAWA TAKAHIRO;TAKAHASHI TAKAYUKI;MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 OGURI KAZUYUKI;KIMURA TAKASHI;SEKIGAWA TAKAHIRO;TAKAHASHI TAKAYUKI
分类号 C22F1/16;C22F1/00 主分类号 C22F1/16
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