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作 者:Ying Wang Tianfeng Zhou Jia Zhou Min Li Zhiqiang Liang Xibin Wang
机构地区:[1]School of Mechanical Engineering,Beijing Institute of Technology,Beijing,100081,China [2]Beijing Institute of Technology Chongqing Innovation Center,Chongqing,401120,China [3]Department of Manufacturing Technologies,Leibniz Institute for Materials Engineering IWT,28359,Bremen,Germany
出 处:《Nanomanufacturing and Metrology》2022年第4期394-402,共9页纳米制造与计量(英文)
基 金:the financial support from National Natural Science Foundation of China(Nos.51775046&51875043&52005040);Beijing Municipal Natural Science Foundation(No.JQ20014).
摘 要:The machining accuracy of the curved surfaces of integrated turbine blades directly determines the performance and service life of the turbojet engine system.In this paper,a non-contact on-machine measurement system is developed for precision milling of integrated turbines to reduce the impact of workpiece deformation,overcutting,tool chatter,and material work hardening.Milling with the on-machine measurement system obtained high-quality integrated turbine surfaces.The geometric accuracy error(PV)is below 3μm,and the surface roughness(Ra)is less than 2μm.The processed integrated turbine blade can achieve the accuracy requirements in the design and manufacturing and can be practically applied to the entire turbojet engine.
关 键 词:Integrated turbine Precision milling K418 superalloy On-machine measurement Topography compensation
分 类 号:TG5[金属学及工艺—金属切削加工及机床]
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