Blade resonance parameter identification based on tip-timing method without the once-per revolution sensor

Author:

Guo Haotian,Duan Fajie,Zhang Jilong

Funder

Doctoral Fund of Ministry of Education of China

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Signal Processing,Control and Systems Engineering

Reference16 articles.

1. Vibration based damage detection of rotor blades in a gas turbine engine,;Madhavan;Engineering Failure Analysis,2014

2. Monitoring low cycle fatigue damage in turbine blade using vibration characteristics,;Kumar;Mechanical Systems and Signal Processing,2007

3. Crack propagation analysis of mechanically damaged compressor blades subjected to high cycle fatigue.;Witek;Engineering Failure Analysis,2011

4. An Optical Fiber Bundle Sensor for Tip Clearance and Tip-timing Measurements in a Turbine Rig,;García;Sensors,2013

5. Blade tip-timing and strain gauge correlation on compressor blades;Knappett;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2008

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