航空学报2025,Vol.46Issue(16):137-151,15.DOI:10.7527/S1000-6893.2025.31607
基于RD-S校正的叶端整剖面间隙微波测量方法
Microwave measurement method for blade tip profile clearance through RD-S correction
摘要
Abstract
The non-contact,high-precision measurement of complex blade tip profile clearance is critical for ensuring the safe and efficient operation of aero-engines.In a 120 GHz microwave sensor-based static and dynamic measure-ment system,the static echo signal is affected by amplitude modulation interference,while the tip information reflected by the dynamic echo signal from complex-shaped blades is susceptible to abrupt boundary phase changes.These challenges significantly hinder accurate static and dynamic measurements of blade tip profile clearance.To address these issues,this paper first introduces the Ratio Differentiation-Spectrum(RD-S)correction method to estimate im-balance parameters under amplitude modulation.This method leverages the attenuation consistency of I/Q signals to eliminate amplitude modulation interference in static echo signals via ratio differentiation,and subsequently estimates imbalance parameters using the main and mirror frequency components.Secondly,by employing the Deimoffer theo-rem and integrating amplitude-phase information,the method mitigates boundary phase mutation effects and enables the measurement of tip profile clearance across any half-wavelength.The experimental results demonstrate that the proposed RD-S correction method in static measurements reduces the demodulation displacement error by an average of 79.2%in comparison with the conventional correction method,achieving an average displacement error of 1.31 μm and a nonlinearity of less than 0.06%.In dynamic measurements,the method achieves an average blade tip clear-ance error of less than 2.5 μm within a relative tip variation range of 300 μm.Additionally,the average measurement error for the concave depth of H-shaped blades is 2.09 μm.关键词
叶端间隙/微波测量/RD-S校正/整剖面间隙/相位差/频谱校正Key words
blade tip clearance/microwave measurements/RD-S correction/blade tip profile clearance/phase difference/spectral correction分类
航空航天引用本文复制引用
樊薇,陈赛赛,熊玉勇,鲁金忠,彭志科..基于RD-S校正的叶端整剖面间隙微波测量方法[J].航空学报,2025,46(16):137-151,15.基金项目
国家自然科学基金(52375100) (52375100)
江苏省自然科学基金(BK20240156) National Natural Science Foundation of China(52375100) (BK20240156)
Natural Science Foundation of Jiangsu Province(BK20240156) (BK20240156)