(1. 南京航空航天大學(xué) 航天學(xué)院，南京 210016；
2. 固體潤滑國家重點(diǎn)實(shí)驗(yàn)室 中國科學(xué)院蘭州化學(xué)物理研究所，蘭州 730000；
3. 中國航空工業(yè)集團(tuán)公司 成都飛機(jī)設(shè)計(jì)研究所，成都 610041)
摘 要: 采用正交實(shí)驗(yàn)設(shè)計(jì)法，選擇影響鈦合金微動(dòng)磨損的位移、載荷、頻率3個(gè)主要因素，設(shè)計(jì)L16(45)正交表，研究鈦合金TC4-DT在不同試驗(yàn)條件下的抗微動(dòng)性能。以磨損量、摩擦因數(shù)為指標(biāo)研究其微動(dòng)摩擦磨損特性。結(jié)果表明：影響鈦合金TC4-DT微動(dòng)磨損性能的3個(gè)因素中，位移、載荷為高度顯著影響，頻率為顯著影響。鈦合金TC4-DT的微動(dòng)磨損為磨粒磨損、粘著磨損和剝層磨損交互作用的結(jié)果。
關(guān)鍵字: TC4-DT鈦合金；正交實(shí)驗(yàn)；微動(dòng)磨損性能
（1. College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
2. State Key Laboratory of Solid Lubrication, Lanzhou Institute of Chemical Physics, Lanzhou 730000, China;
3. China Aviation Industry Corporation, Chengdu Aircraft Design and Research Institute, Chengdu 610091, China）
Abstract:The fretting wear characteristics of TC4-DT alloy were studied using orthogonal design experiment. According to the three major factors that affect the fretting wear of titanium alloy, the anti-fretting properties of TC4-DT alloy by L16 (45) orthogonal table were studied. The fretting friction and wear characteristics were evaluated by the abrasion and friction coefficient. The results show that displacement and load are highly significant factors whereas frequency is significant factor for the fretting wear performance of TC4-DT alloy. The fretting properties of TC4-DT alloy are the results of the interaction of abrasive wear, adhesive wear and peel wear.
Key words: TC4-DT alloy; orthogonal design experiment; fretting wear property
