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
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