1. 北京航空航天大学机械工程及自动化学院,北京,100191
2. 中国航发南方工业有限公司,株洲,412002
纸质出版:2018
移动端阅览
陈志同1,易鹏2,朱正清1,张云1,项德义2,苏帅1,李珊珊1. 具有误差修正功能的叶片变预压量抛光技术[J]. 航空制造技术, 2018, 61(17): 80-84.
CHEN Zhitong1, YI Peng2, ZHU Zhengqing1, ZHANG Yun1, XIANG Deyi2, SU Shuai1, LI Shanshan1. New Aero-Engine Blade Polishing Technology Available to Correct Machining Errors Through Presetting Wheel Contact Deformation. Aeronautical Manufacturing Technology, 2018, 61(17): 80-84.
陈志同1,易鹏2,朱正清1,张云1,项德义2,苏帅1,李珊珊1. 具有误差修正功能的叶片变预压量抛光技术[J]. 航空制造技术, 2018, 61(17): 80-84. DOI: 10.16080/j.issn1671–833x.2018.017.080.
CHEN Zhitong1, YI Peng2, ZHU Zhengqing1, ZHANG Yun1, XIANG Deyi2, SU Shuai1, LI Shanshan1. New Aero-Engine Blade Polishing Technology Available to Correct Machining Errors Through Presetting Wheel Contact Deformation. Aeronautical Manufacturing Technology, 2018, 61(17): 80-84. DOI: 10.16080/j.issn1671–833x.2018.017.080.
针对目前部分叶片铣削后具有较大轮廓度误差以及微小进排气边,采用力控抛光方法难以达到预定要求的状况,提出了一种利用柔性金刚石抛光轮的变预压量误差修正抛光方法。首先,利用在机快速测量装置测量获取叶片待加工余量情况,然后通过分析测量数据确定叶片抛光轨迹和抛光预压量,从而达到对抛光去除量大小的控制,实现叶片型面自适应抛光的结果。最后,利用常规3 轴机床对某型号叶片进行了包含叶根过渡圆弧的全型面抛光试验,试验结果表明,用该方法抛光后,叶片型面轮廓度由抛光前的0.02~0.12mm改变为–0.04~–0.005mm,余量稳定控制到了公差带内。与传统的方法相比,采用高精度超硬磨料复杂母线弹性抛光轮可以实现叶片非均匀去量,有效地改善了叶片型面轮廓度。该技术可以广泛用于中小叶片的低成本高精度抛光加工。
To decrease or eliminate milled blades’ profile errors and to solve the problem in leading/trail edge polishing under presetting pressure control
a new polishing technology available to correct machining errors through presetting contact deformation for wheels was proposed in this paper. Firstly
to obtain the real distribution of machining margin on the surface of blades. Secondly
to determine the different material depth of each local position on the blade surface to be removed with polishing and to adjust the polishing paths and presetting the wheel deformation contacting with workpiece according the obtained depths distribution. Finally
to polish the engine blades with a conventional threeaxis machine tool to verify the capability of the proposed method. The polishing results show that the blades profile error distribution was changed from 0.02–0.12mm to –0.04– –0.005mm after polishing
which was successfully controlled within the designed tolerance. Comparing with the conventional polishing technology
the proposed method is of the ability to remove different quantity of material in depth with flexible diamond polishing wheel and to increase blade profile accuracy
which can be widely used to realize the low cost and high precision polishing of small and medium size aero-engine blades.
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