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On the mechanism of tool crater wear in titanium alloy machining

机译:钛合金加工中刀具月牙洼磨损的机理

摘要

Today the aerospace industry spends hundreds of millions of dollars on the machining of titanium alloy components. And with increasing aircraft orders, there is pressure to machine at higher production rates and develop more machinable alloys (e.g. TIMETAL® 54M, TMETAL® 407) without compromising titanium’s excellent mechanical properties. Increasing the tool life by a factor of minutes can have a dramatic effect on machining cost. Unlike steels, the same tool grade is used for all titanium alloy types from alpha to beta rich, with the latter being more difficult to machine. Diffusion dominated crater wear is the primary tool wear phenomena which has yet to be fully understood. This thesis demonstrates the application of a low cost diffusion couple technique which gives a strong indication of the complex reaction mechanisms occurring at the tool-chip interface during the machining of titanium alloys. These small scale tests have been validated with large scale dynamic machining trials and strong agreement has been observed. The results have allowed for hypotheses to be made over the reaction mechanisms behind tool crater wear underpinned by key observations in the literature. Such a testing regime can be incorporated into alloy design approaches to inform the industry e.g. TIMET and Rolls-Royce about the ‘machinability’ qualities at a much earlier stage before costly machining trials. Such a method will also aid tool manufacturers to tailor tool carbide grades as well as new coatings to specific alloy chemistries.ududThis is the first time that small scale testing such as this has shown why different alloy chemistries exhibit different tool wear characteristics. The technique is now being developed further by the aerospace manufacturing supply chain including tool manufacturers and titanium alloy producers. It will be used to; (a) develop more machinable alloys at an earlier stage in the alloy design development and (b) match different titanium alloys to more appropriate tool materials and new coatings. As such this thesis should be of interest to a broad readership including mechanical engineers and materials scientists as well as the machining and manufacturing community.
机译:如今,航空航天业在钛合金零件的机加工上花费了数亿美元。随着飞机订单的增加,在提高生产率和加工更多可加工合金(例如TIMETAL®54M,TMETAL®407)的压力下,钛合金的优异机械性能不会受到损害。将刀具寿命延长几分钟,可以极大地降低加工成本。与钢不同,从富钛到富β的所有钛合金类型都使用相同的工具等级,后者较难加工。扩散占主导的月牙洼磨损是主要的工具磨损现象,目前尚待充分了解。本文证明了低成本扩散耦合技术的应用,该技术强有力地表明了钛合金加工过程中在工具-芯片界面处发生的复杂反应机理。这些小规模测试已通过大规模动态加工试验进行了验证,并且已观察到很强的一致性。这些结果使得可以对文献中关键观察结果支持的工具弹坑磨损背后的反应机理做出假设。可以将这样的测试方案并入合金设计方法中,以通知行业,例如制造商。 TIMET和罗尔斯·罗伊斯(Rolls-Royce)在更昂贵的机加工试验开始之前就已经提出了“可加工性”质量。这样的方法还将帮助工具制造商针对特定的合金化学性质定制工具的碳化物等级以及新的涂层。 ud ud这是诸如此类的小规模测试首次表明为什么不同的合金化学成分表现出不同的工具磨损特性。包括工具制造商和钛合金生产商在内的航空制造供应链目前正在进一步开发该技术。它会被用来; (a)在合金设计开发的早期阶段开发更多可加工合金,以及(b)将不同的钛合金与更合适的工具材料和新涂层匹配。因此,包括机械工程师和材料科学家以及机械加工和制造界在内的广大读者都应该对本论文感兴趣。

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    Hatt Oliver;

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