Laser triangulation measurement of blade oscillation in a transonic compressor cascade

Author:

Šidlof Petr,Šidlof Pavel,Štěpán Martin,Šimurda David,Lepicovsky Jan

Abstract

Abstract The paper describes a method for optical measurement of oscillation of blades in a linear cascade designed for flutter research. The method uses laser triangulation, which measures the distance between the sensor and the oscillation object. The distance can be recalculated to angular displacement of the blade. However, the relation is nonlinear due to the curvature of the blade. The nonlinear dependence between the distance and angular displacement is derived and quantified analytically. The paper further analyzes the influence of light refraction in the optical window, surface quality and sensor inclination. A procedure for the nonlinear calibration is proposed and used during wind tunnel measurements in a blade cascade with forced oscillation of the middle blade.

Publisher

IOP Publishing

Subject

Computer Science Applications,History,Education

Reference13 articles.

1. A comparative study of coupled and decoupled fan flutter prediction methods under variation of mass ratio and blade stiffness;Chahine;Journal of Fluids and Structures,2019

2. Contribution to Numerical and Experimental Studies of Flutter in Space Turbines;Ferria,2011

3. Effects of a Single Blade Incidence Angle Offset on Adjacent Blades in a Linear Cascade;Fürst;Processes,2021

4. Self-Excited Blade Vibration Experimentally Investigated in Transonic Compressors: Acoustic Resonance;Holzinger;Journal of Turbomachinery,2015

5. Investigation of flow separation in a transonic-fan linear cascade using visualization methods;Lepicovsky;Experiments in Fluids,2008

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