基于V型电容探头的轴向位移下篦齿叶顶间隙测量方法
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1.天津大学精密测试技术及仪器全国重点实验室天津300072; 2.中国航发四川燃气涡轮研究院绵阳621000

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TH69

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国家自然科学基金项目(U2241265, 92360306)、 国家科技重大专项(J2022-V-0005-0031)、 中国航发四川燃气涡轮研究院外委课题项目(GJCZ-0202-2024-0006)、天津市全国重点实验室重大专项(24ZXZSSS00290)资助


Measurement method for labyrinth tip clearance under axial displacement based on a V-shaped capacitive probe
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1.State Key Lab of Measuring Technology and Instruments, Tianjin University,Tianjin 300072, China; 2.AECC Sichuan Gas Turbine Establishment,Mianyang 621000, China

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    摘要:

    带冠涡轮叶片在热变形、气动载荷等作用下产生的轴向位移会导致电容传感器偏离标定位置,严重降低其篦齿叶顶间隙的测量精度。针对这一问题,提出了一种基于V型电容探头的叶顶间隙与轴向位移同步测量方法。首先,通过理论分析揭示了传统圆形芯极电容传感器因对称结构无法识别轴向位移方向的根本缺陷,并推导了轴向位移对叶顶间隙测量误差的非线性影响模型。在此基础上,设计了一种V型芯极电容探头,通过其传感信号的电压峰峰值(Vpp)与特征波形面积(Scw)参数分离轴向位移与叶顶间隙的耦合效应。其次,建立了Vpp和Scw与轴向位移、叶顶间隙的二元多项式映射模型,结合自适应滤波和三阶正弦拟合算法,实现了轴向位移和叶顶间隙的精确提取。最后,搭建了篦齿动态实验台,在轴向位移±1 mm、叶顶间隙0.5~1.5 mm范围完成了二维标定与验证实验。实验结果表明:叶顶间隙测量精度优于8 μm,较传统电容法提升96.8%;轴向位移测量精度为21.6 μm,且同步实现了位移方向辨识。此外,与传统圆形芯极探头对比实验显示,叶顶间隙测量误差由0.25 mm降至8 μm,验证了所提方法的有效性。该方法为轴向位移工况下的带冠叶片动态间隙监测提供了可靠解决方案,对航空发动机智能运维与主动间隙控制技术发展具有重要工程意义。

    Abstract:

    Thermal deformation and aerodynamic loads cause axial displacement of shrouded turbine blades, resulting in capacitive sensors deviating from their calibrated positions and thus substantially diminishing the accuracy of labyrinth tip clearance measurements. To tackle this challenge, this study introduces a synchronous measurement method for blade tip clearance and axial displacement using a V-shaped capacitive probe. Initially, theoretical analysis highlights the inherent limitation of traditional circular-core capacitive sensors in detecting the direction of axial displacement due to their symmetrical design, and a nonlinear model is developed to quantify the measurement error induced by axial displacement on blade tip clearance. Subsequently, a V-shaped core capacitive probe is proposed to decouple axial displacement effects from tip clearance measurements by leveraging characteristic waveform parameters such as peak-to-peak voltage (Vpp) and waveform area (Scw). A binary polynomial mapping model is established to associate these parameters with blade tip clearance and axial displacement values. By integrating adaptive filtering and a third-order sinusoidal fitting algorithm, accurate extraction of both parameters is achieved. A dynamic experimental platform is built, and two-dimensional calibration and validation are performed within axial displacement ranges of ±1 mm and tip clearance from 0.5 to 1.5 mm. The results demonstrate that the blade tip clearance measurement achieves an accuracy better than 8 μm—an improvement of 96.8% compared to traditional capacitive methods—while axial displacement is measured with an accuracy of 21.6 μm, including directional identification. Comparative tests with conventional circular-core probes reveal a reduction in tip clearance measurement error under axial displacement from 0.25 mm to 8 μm, validating the effectiveness of the proposed approach. This method offers a robust solution for real-time monitoring of shrouded blade tip clearance under axial displacement, providing significant engineering benefits for intelligent engine operation and active clearance control development.

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李发富,段发阶,郭光辉,滕光蓉,刘美茹.基于V型电容探头的轴向位移下篦齿叶顶间隙测量方法[J].仪器仪表学报,2025,46(7):73-83

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  • 在线发布日期: 2025-11-07
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