• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2026, Vol. 62 ›› Issue (7): 255-268.doi: 10.3901/JME.260376

• 机械动力学 • 上一篇    

扫码分享

无转速参考的叶尖定时振动速度测量方法

朱昱达1,2, 乔百杰1, 王亚南1, 伏宇3, 梁俊3, 刘美茹1,3, 文璧4, 陈雪峰1   

  1. 1. 西安交通大学航空动力系统与等离子体技术全国重点实验室 西安 710049;
    2. 中国矿业大学机电工程学院 徐州 221116;
    3. 中国航空发动机集团有限公司四川燃气涡轮研究院 绵阳 621000;
    4. 太行实验室 成都 610000
  • 收稿日期:2025-07-18 修回日期:2025-12-26 发布日期:2026-05-25
  • 作者简介:朱昱达,男,1995年出生,博士。主要研究方向为航空发动机叶片振动叶尖定时监测技术。E-mail:zyd917@stu.xjtu.edu.cn
    乔百杰(通信作者),男,1985年出生,博士,教授,博士研究生导师。主要研究方向为航空发动机叶片振动叶尖定时监测技术。E-mail:qiao1224@xjtu.edu.cn.
  • 基金资助:
    国家自然科学基金(52075414,52305127)和高端仪器设备(20251.6XT213-001)资助项目。

OPR-free Blade Tip Timing Vibration Velocity Measurement Method

ZHU Yuda1,2, QIAO Baijie1, WANG Yanan1, FU Yu3, LIANG Jun3, LIU Meiru1,3, WEN Bi4, CHEN Xuefeng1   

  1. 1. National Key Lab of Aerospace Power System and Plasma Technology, Xi'an Jiaotong University, Xi'an 710049;
    2. School of Mechatronic Engineering, China University of Mining and Technology, Xuzhou 221116;
    3. Sichuan Gas Turbine Establishment, Aero Engine Corporation of China, Mianyang 621000;
    4. Taihang Laboratory, Chengdu 610000
  • Received:2025-07-18 Revised:2025-12-26 Published:2026-05-25

摘要: 在传统的叶尖定时测量技术中,通常使用转速传感器作为参考来获得每个叶片的理想到达时间,然后将其与测量的实际到达时间进行比较,以计算叶尖振动位移。然而,在实际应用中,由于发动机内部空间限制,找到一个真实的或虚拟的转速参考来计算叶片振动变得非常困难。同时,叶片理想到达时间的计算会引入计算误差。此外,在变转速工况下,转速波动往往会引起计算的叶尖振动位移出现趋势项或稳态偏移,严重影响后续的叶片振动分析。为了解决这些问题,提出了一种不需要转速参考传感器和计算理想到达时间来获得振动速度的方法。该方法仅需一对叶尖定时传感器和测量的实际到达时间,即可在没有转速参考传感器的情况下获得叶尖振动速度。该方法用振动速度代替了传统的振动位移,减少了叶尖定时测量中的计算误差等不确定性,同时仍能准确获取叶片振动参数。更重要的是,基于振动速度能够更好地表征高频成分,从而为高频振动的辨识奠定基础。最后,基于振动位移与速度的关系,可以在不需要任何激励阶次等先验信息的条件下,直接获得叶片的固有频率。

关键词: 叶尖定时, 无转速参考, 振动速度, 参数辨识

Abstract: In traditional blade tip timing (BTT) measurement technology, a once-per-revolution (OPR) sensor is typically used as a reference to obtain the ideal time of arrival (ToA). The measured actual ToA is then compared with the ideal ToA to calculate the blade tip vibration displacement. However, in practical applications, due to the limited space inside the engine, it is often difficult to obtain a true or virtual rotational reference for vibration calculation. Moreover, the computation of the ideal ToA introduces additional errors. Under variable rotational speed conditions, speed fluctuations can cause the calculated blade tip vibration displacement to exhibit trends or steady-state offsets, which severely affect subsequent vibration analyses. To overcome these challenges, this study proposes an OPR-free method that does not require a rotational reference or the computation of ideal ToA to obtain vibration velocity. The method relies on a pair of BTT sensors and the measured actual ToAs, enabling the estimation of blade tip vibration velocity. By replacing traditional vibration displacement with vibration velocity, the proposed method minimizes computational errors and uncertainties in BTT measurements while maintaining accurate identification of blade vibration parameters. More importantly, vibration velocity provides a better characterization of high-frequency components, laying a foundation for high-frequency vibration identification. Finally, based on the intrinsic relationship between vibration displacement and velocity, the blade’s natural frequency can be directly determined without any prior knowledge of engine orders.

Key words: blade tip timing, OPR-free, vibration velocity, parameter identification

中图分类号: