R.Raišutis, E.Jasiūnienė, E. Žukauskas
Abstract :
In order fully to exploit energy of wind power the construction elements of the wind turbine should be inspected periodically. Ultrasonic air-coupled technique using guided waves has been selected for inspection of wind turbine blades, because only one side access is enough and no contact is needed. Dispersion curves of phase velocities as well as leakage losses versus frequency were calculated using numerical global matrix model. Taking into account the results of the performed simulations the frequency of the ultrasonic transducers was selected to be 290 kHz due to non-dispersive region of phase velocities. The ultrasonic air-coupled technique using guided waves was used for investigation of the artificial internal defects in the wind turbine blade. These defects (diameter 19 mm and 49 mm) were made on the internal side of the main spar. From the ultrasonically obtained images it is possible to recognize the geometry of defects and to estimate approximate dimensions of the defects.
Introduction :
Wind power is a fast-growing and very promising source of environmentally safeand renewable energy with a high potential. However, in order to fully exploit energy of wind power the construction elements of wind turbines should be inspected periodically. In order to estimate level of a critical damage at the initial stage before collapsing it is necessary to perform continuous condition monitoring of wind turbine blades and the detailed inspection with elimination of the broken-down components [1].
To keep the wind turbine inoperation, implementation of condition monitoring system becomes very important. There are different techniques, methodologies and algorithms developed to monitor the performance of wind turbines. Inspection methods based on ultrasound, radiography, thermography, acoustics and optics enable to perform quality control and on site inspection [2].
One of the essential components in wind turbines are their blades. Wind turbine blades, while in operation, encounter very complex loading sequences, due to the stochastic nature of wind conditions at wind turbines sites. Blade failure is very costly because it can damage other blades, the wind turbine itself and other wind turbines located in neighbourhood. The efficient NDT procedures should extend wind turbine life and reduce failure possibility [1].
Ultrasonic methods were not applied yet very widely
for inspection of wind turbine blades. Ultrasonic C-scan
imaging has been used for area mapping of the composite
delamination or interface disbond due to fatigue in normal
field operation conditions of the turbine blade [3]. Three
different ultrasonic measurement techniques were used for
such investigation: pulse-echo, through transmission and
pitch-catch. However, the influence of overlapped
reflections, scattering and attenuation of the reflected
ultrasonic waves from the multi-layered structure takes
place. The scattering effect also has negative impact on the
propagation of ultrasonic waves and requires application of
lower frequencies. For example, in results presented by
Gieske et althe contact type testing technique with 400 kHz transducers was used. Such set-up was similar to
the guided waves generation in a particular layer of the
structure and reception in a neighbour layer of the
structure. The authors declare,that the delamination region
between mentioned layers gave the shadowing effect.
Therefore, such feature helped to detect the internal
delamination [3].
Ultrasonic NDT using guided waves
Application of the guided waves is promising for the
detection and sizing of internal defects between individual
defects. In the case of guided wave interaction with a
structural discontinuity, scattering of guided waves in all
directions as well as mode conversion occurs. There are
two approaches commonly used for structure health
monitoring using guided waves: pulse–echo and pitch–
catch [4]. From various characteristics of the received
signal, such as the time of flight, amplitude etc.,
information about the damage in the inspected structure
can be obtained. In order to estimate type of the defect, the
signal processing algorithms have to be applied [4 - 9].
Simulations of phase velocity dispersion curves
and leakage losses
For effective exploitation of the guided waves it is
necessary to select frequency, therefore the global matrix
numerical model has been used for calculation of the
dispersion group and phase velocities curves [7-10].
Leakage losses versus the frequency were taken into
account also. During simulation the scattering losses inside
the GFRP (glass fibre-reinforced plastics) layers have been
neglected due to short propagation distance of the guided
waves inside the segment of the blade (approximately
40 mm) and also low operating frequencies of the air-coupled ultrasonic set-up. Anisotropy was neglected also.
The drawings of the structures, for which phase and
group velocity dispersion curves were calculated, are
presented in Fig. 1. The structure, selected for simulations
was similar to the real structure of the inspected wind turbine blade sample. In Fig. 1, a the defect free structure
is presented, in Fig. 1, b – defected region (without the
third layer, in order to simulate delamination type defect
due to bad adhesion of glue/foam) is presented. Parameters
of the layers used for simulations are listed in Table 1. The
lateral dimensions of the structure have been assumed to be
infinite.
The calculated phase velocity dispersive curves as well
as leakage losses versus frequency for defected and defect
free regions are presented in Fig. 2 -5. From the presented
results it can be seen that for ultrasonic NDT of wind
turbine blades the 290 kHz transducers may be used due to
low leakage losses and less dispersive region.
Experimental investigations
The measurements were performed using the air-coupled ultrasonic measurement system, which has been
developed at Ultrasound Institute of Kaunas University of
Technology. The photo of the experimental set-up is
presented in Fig. 6.
The pair of air-coupled transducers has been used for non-contact scanning of the wind turbine blade sample. Positioning of the ultrasonic transducers has been performed by a precise mechanical scanning unit. Only one-side access to the sample surface was used. The structural diagram of the used air- coupled ultrasonic technique for NDT inspection of the wind turbine sample is presented in Fig. 7.
The frequency of the ultrasonic transducers f=290 kHz has been selected taking into account the simulation results obtained using the global matrix calculation technique. The transducers were mounted into pitch-catch configuration for generation and reception of guided ultrasonic waves. The transmitter was driven by the 8 periods and 750 V amplitude radio pulse. The total gain of the measurement system was 77 dB. Averaging of the 4 received signals was performed. The measurements were performed with the scanning step of 2 mm.
The cross-section of the inspected wind turbine blade sample is presented in Fig. 8. The photo of the inspected artificial circular defects with49 mm and 19 mm diameter is presented in Fig. 9. In Fig.10 the A-scans obtained over defected (1) and defect free (2) regions are presented. As can be seen from the waveforms, the signal amplitude over the defected region is considerably smaller. In Fig.11 the B-scan image of the 19 mm defect is presented. Lack of the leaky wave signal corresponds to the defected region. In Fig.12 the C-scan image of the 49 mm and 19 mm defects is presented. Both defects can be easily recognised and detected using a conventional amplitude detection technique. The ultrasonically obtained C-scan image shows a good contrast, which enables to estimate geometry of the defects and their approximate dimensions. Additionally, the darker line at y=30 mm indicates, that besides the known defects in the sample there are unknown defects or variayions of material properties, which have to be inspected in the future.
Conclusions
For ultrasonic NDT of wind turbine blades ultrasonic
technique using the air-coupled generation of guided
waves has been selected due to only one side access and
non-contact experimental set-up.
Simulations of group and phase velocity dispersion curves as well as leakage losses versus frequency for defected and defect free regions were performed using the numerical global matrix model. From the simulation results it can be seen that for ultrasonic NDT investigations of wind turbine blades fundamental A0 mode should be used due to low leakage losses and less dispersive region at the frequencies higher than 290 kHz. The first measurements show that the proposed air-coupled ultrasonic technique, using Lamb waves allows finding defects in wind turbine blades. The ultrasonically obtained images (A-scan, B-scan, C-scan) show defects geometry and approximate dimensions.
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