Non-Destructive Techniques for the Condition and Structural Health Monitoring of Wind Turbines: A Literature Review of the Last 20 Years
<p>Percentage of new WT installations in 2020 (both on- and offshore), in terms of produced MW capacity. Based on data retrieved from [<a href="#B14-sensors-22-01627" class="html-bibr">14</a>].</p> "> Figure 2
<p>Bar chart of the estimated investment (<b>left</b>) and O&M (<b>right</b>) costs per MW of an onshore HAWT, according to the class of mean electric power produced. Based on data retrieved from Ref. [<a href="#B27-sensors-22-01627" class="html-bibr">27</a>].</p> "> Figure 3
<p>Estimated costs of a HAWT, as a percentage of the total and excluding foundations. Based on data retrieved from Ref. [<a href="#B30-sensors-22-01627" class="html-bibr">30</a>].</p> "> Figure 4
<p>Structural components of a fixed offshore HAWT according to IEC 61400-3-1.</p> "> Figure 5
<p>Key components of a typical wind turbine blade. The upper and lower surfaces are also known as the suction (or windward) and pressure (or lee) sides, respectively. The blade root bolt connection shown here is a classic T-bolt type.</p> "> Figure 6
<p>Mechanical and electrical components inside the nacelle of a conventional HAWT.</p> "> Figure 7
<p>Damage and failure statistics. (<b>a</b>) Percentage of unforeseen malfunctions as recorded in Germany for 1500 wind turbines. Based on data retrieved from Ref. [<a href="#B42-sensors-22-01627" class="html-bibr">42</a>], collected over 15 years (34,582 events). (<b>b</b>,<b>c</b>) percentage distribution of the total number of failures and downtime for WTs. Based on data retrieved from Ref. [<a href="#B43-sensors-22-01627" class="html-bibr">43</a>], collected from several sources in Sweden, totalling about 600 WTs from 2000 to 2004 (1202 events, 156,202 h). The nomenclature used in the original sources is reproduced for all charts.</p> "> Figure 8
<p>Maintenance strategies according to EN 13306:2017.</p> "> Figure 9
<p>The range of the electromagnetic spectrum that can be covered by common optical techniques (digital, multi/hyperspectral, and thermographic cameras), as well as Gamma-ray, X-ray, microwave, and terahertz testing technologies.</p> "> Figure 10
<p>The main IRT techniques available as of 2021.</p> "> Figure 11
<p>The basic concept of AE event detection.</p> "> Figure 12
<p>The basic concept of UT. (<b>a</b>) conventional, i.e., through the thickness (reflection mode), (<b>b</b>) guided waves. (through transmission mode).</p> "> Figure 13
<p>Qualitative distribution of costs and deployment levels of different NDTs. Based on data from Refs. [<a href="#B329-sensors-22-01627" class="html-bibr">329</a>,<a href="#B330-sensors-22-01627" class="html-bibr">330</a>,<a href="#B331-sensors-22-01627" class="html-bibr">331</a>].</p> ">
Abstract
:1. Introduction
2. Context: The Worldwide Politics and Economics of Wind Turbines
2.1. Climate Change and the Political Stance on Sustainable Energy Sources
2.2. The Current and Near-Future Economic Impact of Wind Power
2.3. Expected Returns and Benefits from WT Monitoring
3. Wind Turbines: Structural and Mechanical Components
- (i)
- static, load-bearing components;
- (ii)
- moving/rotating parts, needed to harness the wind’s kinetic energy and turn it into electricity.
3.1. Components under Structural Health Monitoring
3.1.1. The Tower
3.1.2. The Substructure
3.1.3. The Foundations
3.1.4. The Rotor
3.1.5. The Blades
3.2. Components under Condition Monitoring
3.2.1. Drive Train (and Other Components Inside the Nacelle)
3.2.2. The Gearbox
3.2.3. The Generator
3.3. Incidence and Main Causes of Structural Collapse
3.4. The Incidence and Main Causes of Mechanical Failure
3.5. Survey and Maintenance Policy for Offshore Wind Farms
4. Main Applications for NDE Techniques in Wind Turbines
4.1. Condition Monitoring of the Mechanical Components
4.2. SHM of the Wind Turbine Blades (Blade Monitoring)
- at the blade root (where the mechanical stress is maximized);
- between % and % of the chord length;
- at 70% of the same;
- at the maximum chord section (subject to potential buckling);
- on the upper flange of the spar, at different chord lengths depending on the pitch angle (thus on the current wind speed).
4.3. SHM of the Supporting Structure and Substructure
- welted, grouted, and bolted joints, due to their relative fragility, in particular to fatigue damage; e.g., on tripod offshore structures, the upper central joint is the most critical location;
- location exposed to an aggressive environment (e.g., underwater or, even worse, in the splash zone). Corrosion monitoring is particularly requested in these most endangered locations.
4.4. SHM of the Foundations
5. Non-Destructive Techniques (NDTs)
5.1. Traditional, Enhanced, and Automatic Visual Inspection (VI)
- if they require human personnel on-site or not;
- if they add any kind of support to the human eyesight.
5.2. Optical Methods
Study | Year | Technique | Notes | Application |
---|---|---|---|---|
Baqersad et al. [119] | 2012 | 3D DIC | The authors used two stereoscopic high-speed cameras to record the vibrations of a WT blade with optical targets attached to its surface (excited with hammer hits). | SHM |
LeBlanc et al. [120] | 2013 | 3D DIC | The full-field displacement and strain fields of one CX-100 9 m-long WT blade were estimated. The damaged areas were located from discontinuities in the curvature shapes. | SHM |
Winstroth et al. [121] | 2014 | 3D DIC and point tracking | A random black-and-white dot pattern was applied at four different radial positions on one blade of a three-bladed rotor. The tests were performed in situ on the operating HAWT. | SHM |
Carr et al. [122] | 2016 | DIC and 3D Dynamic Point Tracking (3DPT) | The authors compared the dynamic stress and strain fields obtained with their video-extracted measurements with the readings from attached strain gauges. | SHM |
5.3. Laser-Based Measurement Techniques (LDV, LiDAR, and Shearography)
5.4. Video Spectroscopy
5.5. Infrared Thermography (IRT) and Other Temperature Measurements
5.5.1. Passive IRT
5.5.2. Active IRT
- eddy current (EC) thermography (or inductive thermography), based on the heath released by resistive losses to the eddy currents induced by electromagnetic pulses [161];
- microwave thermography, based on the well-known principles of microwave heating. The electromagnetic energy is absorbed volumetrically by the target object, favouring uniform and rapid self-heating;
- vibrothermography (or thermo-sonic testing), with mechanical waves.
5.5.3. Physically-Attached Temperature Sensors
5.6. Radiographic Testing (RT)
5.7. Microwave and Terahertz Testing
5.8. Electromagnetic Testing (ET)
5.9. Acoustic Emissions (AEs)
- (1)
- not all the typologies of damage emit strong AE;
- (2)
- even more importantly, many damage-unrelated phenomena emit AEs.
Study | Year | Technique | Notes | Application |
---|---|---|---|---|
Eftekharnejad & Mba [256] | 2009 | AE waveforms. | Applied for the detection of seeded tooth root cracks in one helical gear of the wind turbine gearbox. | CM |
Elforjani & Mba [257] | 2010 | Continuous AE energy monitoring. | The authors applied AEs for the CM of low-speed shafts and bearings (separately) also considering different conditions such as lubricant starvation. The bearing test demonstrated the AE’s efficiency in detecting crack initiation and propagation. | CM |
Eftekharnejad et al. [258] | 2011 | Kurtogram (spectral kurtosis). | Compared the effectiveness of applying the kurtogram to AEs and for a roller bearing on a laboratory test bench. | CM |
Qu et al. [259] | 2012 | Time synchronous averaging (TSA) and kurtosis. | The heterodyne technique used in telecommunication was used to pre-process AE signals, reducing the sampling frequency from MHz to kHz. | CM |
Niknam et al. [260] | 2013 | PAC-energy (Physical Acoustic Corporation PCI-2 AE system). | This study focused on wind turbine drive trains subject to rotor unbalances. These unbalances may be caused by manufacturing defects or non-uniform accumulation of ice, dust, moisture, or even damage on rotor blades. | CM |
Ferrando Chacon et al. [261] | 2016 | Root Mean Square Error, Peak Value, Crest Factor, and Information Entropy of AE waveforms. | The confounding influences induced by different operating conditions (load and torque) on the AE signature of a wind turbine gearbox were investigated. | CM |
Zhang et al. [262] | 2017 | Damage localisation was performed via triangulation (delays in the time of arrival). | The first attempt of mechanical fault localisation for CM inside a wind turbine gearbox. | CM |
Joosse et al. [245] | 2002 | Load-hold test. | An early application of AEs off-site on a detached WT blade. | SHM |
Anastassopoulos et al. [263] | 2002 | Load-hold test. | Machine Learning (specifically, Unsupervised Pattern Recognition) was applied to AE data from ten WT blades. | SHM |
Blanch & Dutton [264] | 2003 | Load-hold, stationary, and operating tests. | AEs applied on-site to attached blades (both stationary and rotating during normal operating conditions). | SHM |
Paquette et al. [265] | 2007 | Three-point bending test. | The article documented a 5-year long project performed at Sandia National Laboratories (USA) to characterize WT blades made of carbon fibres. | SHM |
Zarouchas & Van Hemelrijck [266] | 2011 | Peak frequency analysis of AEs and Digital Image Correlation. | AEs were used to characterize the crack growth at different scales in laboratory specimens, treated with an adhesive used for WT blades composites. Tensile and compression tests were executed. DIC was used to compare the strain measurements with the recorded acoustic activity. | SHM |
Han et al. [267] | 2013 | Static loading test. | AEs and strain measurements of a WT blade inner shear web were compared, to correlate acoustic emissions and stress conditions. | SHM |
Bouzid et al. [268] | 2014 | Ambient excitation(naturally occurring AEs). | Proposed a Wireless Sensor Network (WSN) architecture for damage localisation in the blades of operating wind turbines (via triangulation). | SHM |
Tang et al. [269] | 2016 | Pencil lead break test. | The acoustic emissions were generated by breaking a pencil lead in the blade surface. Proved the feasibility of damage severity assessment and growth tracking. | SHM |
Gómez Muñoz & García Márquez [270] | 2016 | Pencil lead break test. Damage localisation was performed via triangulation (delays in the time of arrival). | Three macro-fibre composite transducers were applied on the surface of a WT blade. | SHM |
Tang et al. [271] | 2017 | 21-day long fatigue test. | Unsupervised Pattern Recognition was applied to a very large dataset of recorded AEs. | SHM |
5.10. Ultrasonic Testing (UT)
5.11. Oil Monitoring
Study | Year | Technique | Notes | Application |
---|---|---|---|---|
Myshkin et al. [302] | 2003 | Optical ferroanalyzer | The document presented the operating principle of the optical ferroanalyzer, a sensing device for the estimation of total lubricant oil contamination, for condition monitoring. | CM |
Dupuis [303] | 2010 | Oil debris monitoring | The technique is based on counting debris particles and measuring their size to assess the severity of the gearbox failure. | CM |
Zhu et al. [301] | 2013 | Several sensing devices | A total of 10 sensors and 6 performance parameters related to oil oxidation, water contamination, and particle contamination were discussed. | CM |
Coronado & Kupferschmidt [307] | 2014 | Water content, particle concentration, particle count, dielectric constant, viscosity, oil colour, and oil density sensors | The paper mainly described a highly accelerated stress screening test chamber to assess the performance of oil properties sensors under extreme ambient temperature and vibration levels. The oil parameters are intended as considered as proxies of wind turbine gearbox conditions. | CM |
Zhu et al. [308] | 2015 | Particle filtering, plus viscosity and dielectric constant sensors | Related to the previous paper by the same authors [301], it applied online oil monitoring for fault detection and remaining useful life prediction. | CM |
Sheng [309] | 2016 | 2.5-MW dynamometer test facility at U.S. National Renewable Energy Laboratory (fully described in Ref. [310]) | The laboratory tests were performed on full-scale wind turbine gearboxes in three configurations: run-in, healthy, and damaged conditions. | CM |
5.12. Static Strain Measurements
5.13. Other NDE Approaches
- Dynamometer testing, performed off-site on the whole drive train system, to assess for potential slipping behaviour in the high-speed shaft tapered roller bearings [321];
- Short-Range Doppler Radar, very recently tested for the son-site SHM of WT blades [324];
- Multi-sensor apparatuses, such as e.g., the one proposed in Ref. [325] (with optical, acoustical, and vibrational sensing devices) to detect bird and bad strikes.
6. Discussion
7. Conclusions
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Acknowledgments
Conflicts of Interest
Abbreviations
AE | Acoustic Emission. |
AI | Artificial Intelligence |
BVID | Barely Visible Impact Damage |
CFRP | Carbon Fibre Reinforced Polymer |
CM | Condition Monitoring |
CT | Coherence Tomography |
DIC | Digital Image Correlation |
EC | Eddy Current |
ET | Electromagnetic testing |
FBG | Fibre Bragg Grating |
GFRP | Glass Fiber Reinforced Polymer |
HAWT | Horizontal Axis Wind Turbine |
IRT | Infrared Thermography |
LCOE | Levelized Cost of Energy |
LDV | Laser Doppler Velocimeter |
NDE | Non-Destructive Evaluation |
NDT | Non-Destructive Technique |
OCT | Optical Coherence Tomography |
O&M | Operation and Maintenance (cost) |
RS | Remote Sensing |
RT | Radiographic Testing |
SCADA | Supervisory Control And Data Acquisition (system) |
SHM | Structural Health Monitoring |
SHT | Surface Heating Thermography |
UAV | Unmanned Aerial Vehicle |
UT | Ultrasonic Testing |
VBI | Vibration-Based Inspection |
VHT | Volume Heating Thermography |
VI | Visual Inspection |
WEC | White Etching Cracks |
WT | Wind Turbine |
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Damage Type | Description |
---|---|
#1 | Damage formation and growth in the adhesive layer joining the skin and main spar flanges (skin/adhesive debonding and/or the main spar/adhesive layer debonding). |
#2 | Damage formation and growth in the adhesive layer joining the up- and downwind skins along leading and/or trailing edges (adhesive joint failure between skins). |
#3 | Damage formation and growth at the interface between the face and core in the sandwich panels in skins and the main spar web (sandwich panel face/core debonding). |
#4 | Internal damage formation and growth in laminates in the skin and/or main spar flanges, under a tensile or compression load (delamination driven by a tensional or a buckling load). |
#5 | Splitting and fracture of separate fibres in the laminates of the skin and main spar (fibre failure in tension; laminate failure in compression). |
#6 | Buckling of the skin due to damage formation and growth in the bond between the skin and main spar under a compressive load. * |
#7 | Formation and growth of cracks in the gel coat; debonding of the gel-coat from the skin (gelcoat cracking and gel-coat/skin debonding). |
Damage Type | Description | Possible causes |
---|---|---|
Flaking | Creation of regions with a rough and coarse texture due to the splitting off of small pieces from the raceway surface. | Rolling fatigue, caused in turn by excessive load, misalignment, poor lubrification, water or debris inclusions, unsuitable bearing clearance, unevenness in housing rigidity, rust, corrosion pits, dents. |
Peeling | Light wear and dull spots on the surface, with micrometric cracks and minor flaking. | Poor or unsuitable lubricant, debris intrusion in the lubricant. |
Scoring | Straight lines on the surface, circumferentially on the raceway surface. | Generated by accumulated small seizures, caused in turn by sliding under improper lubrication or excessive/improper loads and conditions (shaft bending, the inclination of inner and outer rings, etc). |
Smearing | Surface damage, with the formation of rough and partially melted material. | Generated by accumulated small seizures between bearing components, caused in turn by oil film rupture (because of poor/improper lubrication or high speeds with very light loads). |
Fracture | Small pieces broke off due to shock loads or stress accumulation. | Impacts during mounting/dismounting, excessive loads, progression of surface cracks. |
Cracks | Formation of surface cracks on the raceway rings and/or rolling elements. | Excessive loads, progression of flaking damage, creep-induced heating, inappropriate shaft (e.g., poor taper angle). |
Cage damage | Cage deformation, fracture, and/or wear (considering the cage guide surface, pocket surface, and cage pillars). | Excessive speed, sudden acceleration/deceleration, high temperature, poor lubrication, excessive vibrations, bearing misalignment. |
Denting | Small dents on the surface of raceway rings or rolling elements. | Caused by metallic particles or other very small debris caught in the surface during rolling. |
Pitting | Pitted surface on the raceway rings or rolling elements. | Poor lubricant, debris in the lubricant, or exposure to moisture. |
Wear | Surface deterioration on the raceway rings, rolling elements, cage pockets, and/or roller end faces. | Sliding friction between two surfaces, caused in turn by an irregular motion of the rolling elements, poor lubrication, debris intrusions in the lubricant, or as a progression from chemical or electrical corrosion. |
Fretting | Corrosion happening at the contact area between the raceway ring and the rolling elements. It may happen at regular roller pitch intervals. | Repeated sliding on the fitting surface. |
False brinelling | Hollow spots that resemble Brinell dents. | Caused by wear, induced in turn by vibration and swaying at the contact points between the raceway and the rolling elements, especially with poor lubrication. |
Creep | Shiny appearance on the fitting surface, potentially coupled with scoring and wear. | Relative slipping at the fitting surfaces, due to a loose fit or insufficient sleeve tightening. |
Seizure | Softened, deformed, and/or melt material in the raceway rings, rolling elements, or cage. | Excessive load, speed, shaft bending, poor housing or lubrication, small internal clearance. |
Electrical corrosion | Corrugations resulting from locally melted material. | Melting by arcing, induced by the passage of electric currents. In turn, these are induced by the electrical potential between the inner and the outer rings. |
Pit corrosion | Pits on the surface of raceway rings or rolling elements due to chemical corrosion. | Entry of corrosive gas or liquid, improper lubricant, moisture, high humidity, improper handling and storage conditions. |
Mounting flaws | Scratches on the surface of raceway rings or rolling elements caused by mounting/dismounting. | Incorrect mounting/dismounting (impulse loads, the inclination of inner or outer rings, etc). |
Discolouration | Discolouration of the cage, rolling elements, or raceway rings. | Poor lubrication and/or high temperature. |
Mechanical Component | Common Failure Modes |
---|---|
Gearbox and drive train | Gear tooth damages, high- or low-speed shafts faults, gearbox bearing failures. |
Generator | Generator stator failure, generator rotor failure, generator bearing failure. |
Main bearing | Bearing failure, bearing rubs, bearing looseness |
Pitch gears | Pitch Gear tooth damages. |
Yaw gears | Yaw Gear tooth damages. |
Study | Year | Mentioned Factors |
---|---|---|
Henderson et al. [62] | 2003 | Accessibility of the offshore platform and reliability of the monitoring strategy. |
Nielsen et al. [63] | 2011 | Weather conditions, total power generation, repair strategies, transportation strategies. |
Dinwoodie et al. [64] | 2012 | Repair time, wave height, wind speed, number of wind turbines in the wind farm, ship availability, availability of spare parts stocks. |
Scheu et al. [65] | 2012 | Expected typologies of component failures, ship fleet size, ship type, travel time, number of maintenance workers on staff. |
Besnard et al. [66] | 2013 | Location of accommodation facilities for maintenance staff, vessels for the transfer of crew (type and number), availability of helicopters, organization of work shifts, management of spare parts stocks, technical support, availability of cranes (purchase or contract), environmental conditions (depending on weather and season), economic parameters (electricity prices, ship rental costs). |
Halvorsen-Weare et al. [67] | 2013 | Investment costs, ship costs (fixed and variable costs), failure probability, downtime costs, meteorological data. |
Hofmann & Sperstad [68] | 2013 | Weather conditions (including uncertainty), breakdown rates, electricity price, ship price (costs, fleet composition, type, quantity), workers (shift length, quantity), location of the maintenance base of operations. |
Perveen et al. [69] | 2014 | Protection methodologies, occurrence of cable and component failures, repair strategy, wind speed predictions, and condition monitoring systems. |
Endrerud et al. [70] | 2015 | Weather conditions, ships (availability, operating limits, costs), availability of maintenance technicians, repair times, wind farm layout, cost of spare parts, logistics (warehousing and other costs). |
Nguyen & Chou [71] | 2018 | Duration of maintenance (downtime), expected loss of production during maintenance time, the market price of electricity, location of the wind farm. |
Study | Year | Platform | Computer Vision/Video or Image Processing1 Technique | Application |
---|---|---|---|---|
Stokkeland et al. [91] | 2015 | Digital camera-equipped multi-copter UAV. | Computer Vision was also utilized for autonomous navigation (moving along the blades to acquire pictures). | SHM |
Park et al. [92] | 2015 | Fixed Digital camera (laboratory test only) | Image segmentation, canny edge detection, and Hough Transform are applied to evaluate the angle changes in the nuts. The method is proposed for bolt loosening monitoring in the ring flange joints in WT towers. | SHM |
Wang et al. [93] | 2017 | Remotely-controlled, digital camera-equipped UAV. | Cascading classifiers (several variants) were applied to detect and locate pixel regions containing cracks in the images. | SHM |
Reddy et al. [94] | 2019 | Digital camera-equipped multi-copter UAV. | A convolutional neural network (CNN) architecture. | SHM |
Shihavuddin et al. 1 [95]. | 2019 | Digital camera-equipped multi-copter UAV. | Deep learning-based damage detection and classification. Specifically, the authors used the well-established faster region-based CNN (R-CNN) algorithm [96] and compared it to other similar architectures (R-CNN, Fast R-CNN, SSD, and R-FCN). | SHM |
Yang et al. [97] | 2021 | Digital camera-equipped UAV. | The authors used the pre-trained CNNs described in Ref. [98] after integrating them with their image dataset via Transfer Learning 2. | SHM |
Study | Year | Technique | Notes | Application |
---|---|---|---|---|
Rumsey & Musial [193] | 2001 | Passive IRT | Infrared thermography was applied by the National Wind Technology Center at the National Renewable Energy Laboratory for the testing of full-size WT blades. One of the tests performed was a fatigue test in which a cyclic load was applied to the WT blade until failure. | SHM |
Dattoma et al. [194] | 2001 | Active IRT (external heating and readings during the cooling phase) | The IRT procedure was experimentally tested on a WT blade sandwich panel, taken from the box spar. Glue infiltration, water ingress, and skin–core debonding were tested. | SHM |
Hahn et al. [195] | 2002 | Thermoelastic stress analysis | Used to monitor the stress distribution on a GFRP blade during static and fatigue tests. Strain gauges were applied as well to assess the integrity of the root section. | SHM |
Cheng & Tian [196] | 2011 | Inductive IRT (pulsed eddy current thermography) | The proposed method is based on inductive thermography for the inspection and assessment of CFRP components. | SHM |
Pan et al. [197] | 2012 | Pulsed eddy current | The inductor and the IR camera were placed on opposite sides to detect damage in the heat transmission mode on CFRP specimens intended for WT blades. | SHM |
Cheng & Tian [198] | 2013 | Pulsed eddy current | Detected surface cracks, impact cracks, defects, and delaminations from transient thermal images or videos on CFRP specimens. | SHM |
Dattoma & Giancane [199] | 2013 | Passive IRT during fatigue tests | Compared DIC and IRT results on a GFRP specimen employed for WT blades. | SHM |
Galleguillos et al. [200] | 2015 | Passive IRT from a UAV platform | Performed in situ surveys on rotating WT blades (in-service) with passive IRT from an unmanned rotorcraft. | SHM |
Gao et al. [201] | 2016 | Pulsed eddy current | Developed a multidimensional tensor model based not only on the analysis of a single physical field such as heat conduction (conventional approach) but also on the inclusion of other properties such as electrical conductivity and magnetic permeability as well. | SHM |
Paulmbo et al. [202] | 2016 | Lock-in IRT analysis (heat source: halogen lamps) | The technique was tested for the debonding of GFRP joints and compared to ultrasonic testing. | SHM |
Yang et al. [203] | 2016 | Pulsed eddy current | Combined eddy current pulsed thermography and thermal-wave-radar analysis for the assessment of delamination on CFRP blades. | SHM |
Palumbo et al. [204] | 2017 | Thermoelastic phase analysis | The study focused on the fatigue damage analysis on GFRP specimens, analysing the thermal signal in the frequency domain. | SHM |
Study | Year | Technique | Notes | Application |
---|---|---|---|---|
Jørgensen et al. [289] | 2004 | Ultrasonic immersion test | An early example of UT for the detection of damages and manufacturing defects. The skin, glue, laminate, and sandwich layers were all clearly visible from the scans. | SHM |
Jasiüniené et al. [290] | 2008 | Ultrasonic immersion test with moving water container | A particular type of ultrasonic immersion test (contact pulse–echo immersion testing) was used to assess internal defects in a WT blade. The geometry of the defects was recognized from the ultrasound images obtained. | SHM |
Raišutis et al. [291] | 2008 | Air-coupled guided wave ultrasonic test | The authors used an ultrasonic air-coupled technique to transmit guided waves, locating internal defects in a WT blade. | SHM |
Jüngert [292] | 2008 | Guided wave ultrasonic test | It compared acoustic waves (from hammer tests, using local resonance spectroscopy) with ultrasonic guided waves. Acoustic waves were found to be less subject to scattering and damping while travelling through the fibre-reinforced material but less sensitive to small damages (due to their larger wavelength). | SHM |
Jüngert & Grosse [293] | 2009 | Contact pulse-echo tests | Compared local resonance spectroscopy (from hammer tests) with contact pulse–echo UT on sandwich composites and pristine and delaminated GFRP. Ultrasonic waves correctly detected debonding at adhesive areas. | SHM |
Jasiüniené et al. [294] | 2009 | Air-coupled ultrasonic tests, ultrasonic immersion tests with moving water container, and contact pulse–echo tests | UT and radiographic techniques were compared on WT blade specimens. The ultrasonic techniques proved to be more efficient in terms of implementation as they only require access from one side. The best imaging results, however, were obtained by combining RT and UT techniques. | SHM |
Lee et al. [295] | 2011 | Long distance laser ultrasonic test | To overcome the attenuation due to air travelling, a portable laser-based device was proposed for long-distance UT, up to 40 m (indoor laboratory conditions). | SHM |
Park et al. [296] | 2013 | Long distance laser ultrasonic test | It proposed a new laser ultrasonic imaging technique, specifically intended for rotating blades | SHM |
Ye et al. [297] | 2014 | Pulse-echo test | A portable device for 2D (surface) and 3D (volume) UT scanning was proposed and tested on GFRP WT blade specimens. | SHM |
Park et al. [298] | 2014 | Long-distance laser ultrasonic test | Delamination and debonding were successfully visualized in a GFRP composite wind blade structure. | SHM |
Park et al. [299] | 2015 | Laser ultrasonic propagation imaging system | A two-step UT imaging strategy was proposed, with an initial coarse scanning followed by a second refined one limited to the areas deemed of major interest after the first step. Tested on a 10 kW GFRP WT blade. | SHM |
García Marquez & Gómez Muñoz [300] | 2020 | Macro fibre composite transducers and sinusoidal shaped signals | Cross-correlation and wavelet analysis were applied to detect, assess, and localize delaminations in WT blades. | SHM |
Study | Year | Notes | Application |
---|---|---|---|
Papadopoulos et al. [315] | 2000 | An early study on the feasibility of static strain measurements for WT blades. The main potential causes of error were discussed and their impact was experimentally estimated. | SHM |
Kim et al. [316] | 2011 | FBG sensors were embedded into a 1/23 scale of the 750 kW composite blade to evaluate its deflection. | SHM |
Dimopoulos et al. [317] | 2012 | The authors used strain measurements from strain gauges to experimentally investigate the buckling behaviour of the thin steel cylindrical shells which make up the HAWT tower. | SHM |
Choi et al. [318] | 2012 | FBG sensors were applied to estimate the static tip deflection of a 100 kW GFRP blade. This shape sensing is intended to avoid potential collisions with the nearby tower. | SHM |
Kim et al. [319] | 2013 | Similar to Choi et al. [318], the authors suggested installing FBG sensors at the bonding line between the shear web and spar cap | SHM |
Sierra-Pérez et al. [320] | 2016 | Compared strain measurements taken from strain gauges, FBG sensors, and Optical Backscatter Reflectometer (OBR) sensors on a prototype GFRP WT blade. | SHM |
SHM | CM | ||||||
---|---|---|---|---|---|---|---|
Tower | Foundations | Blades | Bearings | Shaft | Generator | Gearbox | |
VI | X | X | X (limited visibility) | X (limited visibility) | X (limited visibility) | ||
Optical measurements | X | X | |||||
Shearography | X | ||||||
IRT | X | X | X | X | X | X | |
Temperature, non IRT | X | X | X | X | |||
X-ray CT | X | X | X | X | |||
ET | X | X (CFRP only) | X | ||||
AEs | X | X | X | X | X | ||
UT | X | X | X | ||||
Oil Monitoring | X | X | X | ||||
Static strain | X | X | X |
Method | Advantages | Disadvantages |
---|---|---|
VI | Non-contact Very simple Low cost Does not require extensive training or specific instruments (man-made VI) Can be automated (Computer Vision and autonomous unmanned platforms) | Limited to surface damages and defects. Safety hazard for the personnel (if man-made). Low accuracy and highly subjective (if man-made). |
Optical Measurements and Shearography | Non-contact Full-field Relatively fast to perform High sensitivity to damage | Shearography requires a specific (and expensive) setup. Difficult to quantify the extension of damage. Some techniques (e.g., DIC) require surface treatment. |
IRT | Non-contact (except vibrothermography) Full-field Relatively fast to perform (except lock-in thermography; depends on the thickness of the material for pulsed and EC pulsed thermography) High sensitivity to damage Many options (surface and volumetric heating, different inputs, etc.) Relatively simple setup (except microwave thermography) Highly standardized (e.g., ISO 10880:2017) Good spatial resolution (depends on the specific option) | Active IRT requires an active source of heating. Only microwaves ensure uniform volumetric heating. Only microwaves and vibrothermography allow selective heating. Only lock-in and pulsed phase thermography are emissivity independent. Surface heating thermography is limited to the outermost layers of the material. Eddy currents cannot be applied to all materials (depending on their conductivity). Pulsed phase thermography requires extensive signal processing to analyze the results. Damage-unrelated factors may cause a rise in temperature. Cannot provide a very accurate damage diagnosis. |
Temperature, non IRT | Highly standardized (e.g., ISO 15312:2018). | Requires an embedded sensor (subject to sensor faults). Damage-unrelated factors may cause temperature rise. |
X-ray CT | Non-contact Very high spatial resolution | Radiation hazard Complex (and expensive) setup |
ET | Non-contact Relatively low-cost. | Sensitive to lift-off Limited by the material conductivity Requires specific instruments. |
AEs | Passive (no input required) Able to detect early-stage cracks and small defects. Can be applied on-site and in-service Can be applied also to low-speed rotating machinery. Can cover relatively large areas/volume. High signal-to-noise ratio. Frequency range far from load perturbation. | Relatively expensive. Requires a very high sampling rate. Acoustic wave attenuation in the material. Only detect damages at their inception or during their growth. Difficult to quantify the extension of damage In general, very noisy and difficult to interpret. |
UT | Can be applied on-site and in-service Many options Can cover relatively large areas/volume, also with complex geometries | Require an active source of ultrasounds Coupling issues (especially for water-incompatible materials) Ultrasound attenuation in the material The analysis of the results requires an expert user |
Oil Monitoring | Easy to install. Enables the direct characterisation of several oil parameters. The results are easy to interpret | Only viable for mechanical systems with a closed-loop oil supply system. Expensive for continuous online monitoring. |
Static strain | Can provide both damage detection and shape sensing capabilities. Conventional strain gauges are easy to install. Can be used to monitor dynamic strain as well (for vibration-based inspection). | Fibre optics are still expensive and difficult to install. |
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Civera, M.; Surace, C. Non-Destructive Techniques for the Condition and Structural Health Monitoring of Wind Turbines: A Literature Review of the Last 20 Years. Sensors 2022, 22, 1627. https://doi.org/10.3390/s22041627
Civera M, Surace C. Non-Destructive Techniques for the Condition and Structural Health Monitoring of Wind Turbines: A Literature Review of the Last 20 Years. Sensors. 2022; 22(4):1627. https://doi.org/10.3390/s22041627
Chicago/Turabian StyleCivera, Marco, and Cecilia Surace. 2022. "Non-Destructive Techniques for the Condition and Structural Health Monitoring of Wind Turbines: A Literature Review of the Last 20 Years" Sensors 22, no. 4: 1627. https://doi.org/10.3390/s22041627
APA StyleCivera, M., & Surace, C. (2022). Non-Destructive Techniques for the Condition and Structural Health Monitoring of Wind Turbines: A Literature Review of the Last 20 Years. Sensors, 22(4), 1627. https://doi.org/10.3390/s22041627