Numerical Investigation on the Influence of Turbine Rotor Parameters on the Eddy Current Sensor for the Dynamic Blade Tip Clearance Measurement

Author:

Zhao Lingqiang1,Liu Fulin1,Lyu Yaguo1ORCID,Liu Zhenxia1,Zhao Ziyu2ORCID

Affiliation:

1. School of Power and Energy, Northwestern Polytechnical University, Youyi West Road 127#, Xi’an 710054, China

2. Xi’an Research Institute of High-Tech, Xi’an 710054, China

Abstract

Eddy current sensors are increasingly being used to measure the dynamic blade tip clearance in turbines due to their robust anti-interference capabilities and non-contact measurement advantages. However, the current research primarily focuses on enhancing the performance of eddy current sensors themselves, with few studies investigating the influence of turbine rotor parameters on the measurements taken by these sensors for dynamic blade tip clearance. Hence, this paper addresses this gap by using COMSOL Multiphysics 6.2 software to establish a finite model with circuit interfaces. Additionally, the model’s validity was verified through experiments. This model is used to simulate the voltage output of the sensor and the measurement of dynamic blade tip clearance under various rotor parameters. The results indicate that the length and number of blades, as well as the hub radius, significantly affect the sensor voltage output in comparison to rotation speed. Furthermore, we show that traditional static calibration methods are inadequate for measuring dynamic blade tip clearance using eddy current sensors. Instead, it is demonstrated that incorporating rotor parameters into the calibration of eddy current sensors can enhance the accuracy of dynamic blade tip clearance measurements.

Funder

National Nature Science

China Postdoctoral Science Foundation

Publisher

MDPI AG

Reference24 articles.

1. Rotor-tip Leakage: Part I—Basic Methodology;Booth;J. Engine Power,1982

2. Optimization of blade pitch angle of an axial turbine used for wave energy conversion;Mohamed;Energy,2013

3. Hao, J. (2013, January 25–27). The investigation about civil aviation engine surge problem: The final solution for PW4000-94′’ engine group 3 surge. Proceedings of the 15th Aeroengine Design, Manufacturing and Application Technology Symposium, Beijing, China.

4. Effects of non-axisymmetric tip clearance on axial compressor performance and stability;Graf;J. Turbomach.,1998

5. High-fidelity rotor gap measurements in a short-duration turbine rig;Lavagnoli;Mech. Syst. Signal Process.,2012

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3