Dynamic monitoring technology of aero-engine blades
摘 要
提出了一种铁磁性发动机壳体内叶片动态原位监测方法,该方法利用涡流检测方法监测铁磁性发动机叶片的个数、转速、损伤状态等。将两个磁极固定于铁磁性发动机壳体外表面,将涡流检测探头固定在磁极之间,叶片转动过程中,叶片的尖部划过表面附近涡流场,探头感生涡流信号传输至涡流检测仪。通过每分钟的涡流信号个数计算叶片转速;通过涡流检测信号的幅值,测算叶片与壳体内表面的间隙;通过信号幅值的不同,判断出叶尖表面的缺损;通过间隔时间出现不均匀的涡流信号,判断叶片弯曲或断裂。该方法可以解决铁磁性发动机壳体内叶片的安全监测难题。
Abstract
In this paper, a method of dynamic monitoring of the blades in the inner shell of ferromagnetic engine is presented, and the number, rotating speed and damage state of blades in ferromagnetic engine are monitored by eddy current testing method. Two magnetic poles are set on the surface of ferromagnetic casing, and the eddy current testing probe is fixed between the poles. Blades rotate though the eddy current field near the surface, and eddy current signal is induced in the probe and is transferred to the eddy current instrument. The rotor speed can be calculated by the number of eddy current signals per minute. By measuring the amplitude of eddy current detecting signal, the clearance between the blade and the inner surface of the shell can be calculated. The defect of tip surface can be determined by different signal amplitude. Whether the blades bend or break can be determined when the eddy signal is not evenly spaced. The method can solve the problem of blade safety monitoring in the ferromagnetic engine casing.
中图分类号 TG115.28 DOI 10.11973/wsjc201911007
所属栏目 试验研究
基金项目 国家重点研发计划重点专项资助项目(2017YFF 0209703);福建省自然科学基金项目(2017J01484)
收稿日期 2019/3/24
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备注林俊明(1956-),男,研究员,主要从事电磁无损检测及其集成技术和云检测方面的研究
引用该论文: LIN Junming,LI Hanlin,DAI Yonghong. Dynamic monitoring technology of aero-engine blades[J]. Nondestructive Testing, 2019, 41(11): 26~29
林俊明,李寒林,戴永红. 航空发动机叶片动态监测技术[J]. 无损检测, 2019, 41(11): 26~29
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参考文献
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【5】张丽攀, 宋凯, 王冲, 等. 航空发动机涡轮叶片裂纹涡流检测仿真及试验研究[J]. 南昌航空大学学报(自然科学版), 2018, 32(3): 35-42.
【2】POURSAEIDI E, BABAEI A, MOHAMMADI A M R, et al. Effects of natural frequencies on the failure of R1 compressor blades[J]. Engineering Failure Analysis, 2012, 25: 304-315.
【3】XU C, AMANO R S, LEE E K. Investigation of an axial fan-blade stress and vibration due to aerodynamic pressure field and centrifugal effects[J]. JSME International Journal Series B, 2004, 47(1): 75-90.
【4】龚模辉, 胡博, 于润桥, 等. 压气机叶片根部原位检测传感器的设计与制作[J]. 无损检测, 2018, 40(10): 10-15.
【5】张丽攀, 宋凯, 王冲, 等. 航空发动机涡轮叶片裂纹涡流检测仿真及试验研究[J]. 南昌航空大学学报(自然科学版), 2018, 32(3): 35-42.
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