In-process, non-destructive, dynamic testing of high-speed polymer composite rotors. (March 2015)

• Record Type: Journal Article
• Authors: Kuschmierz, Robert; Filippatos, Angelos; Günther, Philipp; Langkamp, Albert; Hufenbach, Werner; Czarske, Jürgen; Fischer, Andreas
• Is Part Of: Mechanical systems and signal processing. Volume 54/55(2015)
• Page Start: 325
• Page End: 335
• Publication Date: 2015-03
• Subjects: Non-linear behaviour -- Deformation -- Non-destructive testing -- High-speed composite rotors -- Finite element analysis (FEA); Structural dynamics -- Periodicals; Vibration -- Periodicals; Constructions -- Dynamique -- Périodiques; Vibration -- Périodiques; Structural dynamics; Vibration; Periodicals; 621
• DOI: 10.1016/j.ymssp.2014.07.016
• Languages: English
• ISSNs: 0888-3270

Abstract

Abstract: Polymer composite rotors are lightweight and offer great perspectives in high-speed applications such as turbo machinery. Currently, novel rotor structures and materials are investigated for the purpose of increasing machine efficiency and lifetime, as well as allowing for higher dynamic loads. However, due to the complexity of the composite materials an in-process measurement system is required. This allows for monitoring the evolution of damages under dynamic loads, for testing and predicting the structural integrity of composite rotors in process. In rotor design, it can be used for calibrating and improving models, simulating the dynamic behaviour of polymer composite rotors. The measurement system is to work non-invasive, offer micron uncertainty, as well as a high measurement rate of several tens of kHz. Furthermore, it must be applicable at high surface speeds and under technical vacuum. In order to fulfil these demands a novel laser distance measurement system was developed. It provides the angle resolved measurement of the biaxial deformation of a fibre-reinforced polymer composite rotor with micron uncertainty at surface speeds of more than 300 m/s. Furthermore, a simulation procedure combining a finite element model and a damage mechanics model is applied. A comparison of the measured data and the numerically calculated data is performed to validate the simulation towards rotor expansion. This validating procedure can be used for a model calibration in the future. The simulation procedure could be used to investigate different damage-test cases of the rotor, in order to define its structural behaviour without further experiments. Abstract : Highlights: The in-plane deformation of composite rotors was determined non-invasive in process. The standard deviation for the estimation of the mean rotor expansion is only 300 nm. An angle dependent expansion was observed due to anisotropy of the composite. The experiential results are used to verify numerical simulations.