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Wind Energy Science The interactive open-access journal of the European Academy of Wind Energy
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WES | Articles | Volume 3, issue 1
Wind Energ. Sci., 3, 97-105, 2018
© Author(s) 2018. This work is distributed under
the Creative Commons Attribution 3.0 License.
Wind Energ. Sci., 3, 97-105, 2018
© Author(s) 2018. This work is distributed under
the Creative Commons Attribution 3.0 License.

Research articles 14 Mar 2018

Research articles | 14 Mar 2018

Friction torque of wind-turbine pitch bearings – comparison of experimental results with available models

Friction torque of wind-turbine pitch bearings
Matthias Stammler1, Fabian Schwack2, Norbert Bader2, Andreas Reuter1, and Gerhard Poll2 Matthias Stammler et al.
  • 1Fraunhofer IWES, Appelstraße 9A, 30167 Hanover, Germany
  • 2IMKT, Leibniz Universität Hannover, Welfengarten 1a, 30167 Hanover, Germany
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Pitch bearings of wind turbines are large, grease-lubricated rolling bearings that connect the rotor blades with the rotor hub. They are used to turn the rotor blades to control the power output and/or structural loads of the turbine. Common actuators turning the blades are hydraulic cylinders or electrical motor–gearbox combinations. In order to design pitch actuator systems that are able to turn the blades reliably without imposing an excessive power demand, it is necessary to predict the friction torque of pitch bearings for different operating conditions. In this paper, the results of torque measurements under load are presented and compared to results obtained using different calculation models. The results of this comparison indicate the various sources of friction that should be taken into account for a reliable calculation model.

1 Introduction
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Pitch bearings (also called blade bearings) are subject to unfavorable operating conditions as they have to accommodate high bending moments while stationary or rotating at very low speeds. The connected parts, especially the rotor blades, provide limited stiffness. Usually, four-point contact ball bearings are used for this application, but for newer models of turbines, three-row bearing types have been chosen as well (Stammler and Reuter, 2015; Burton, 2011).

Pitch bearings are driven by combinations of electric motors and gearboxes with a total ratio exceeding 1:1000 or by hydraulic systems. In order to guarantee emergency-stop capability, accumulators have to store and provide sufficient energy for at least one pitch rotation into the feather position should serious faults occur in the pitch system (Burton, 2011).

Figure 1Pitch-bearing test rig at Fraunhofer IWES and corresponding FE model.


In order to design pitch actuator systems that are able to turn the bearings reliably but do not require excessive power, it is necessary to predict the friction torque for pitch bearings under all operating conditions.

Several equations and numerical models are available to calculate the friction torque of rolling bearings. However, there are no publications which compare them with experimental results of pitch bearings. In this paper, experimental results obtained at the Fraunhofer IWES pitch bearing test rig in Bremerhaven are compared to the results of different calculation models. Torque values throughout this paper are normalized instead of absolute values. The models considered range from two bearing manufacturers' catalog equations (SKF, 2014; Rothe Erde, 2016), which are based on Palmgren's classical approach for friction prediction (Palmgren, 1957), to the numerical model developed by Wang (Wang, 2015). These four models represent the available types of approaches used for friction torque calculations, as such other bearing manufacturer models with comparable approaches were not taken into account.

2 Methods
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2.1 Test rig, torque measurement and finite element model

The pitch-bearing test rig at Fraunhofer IWES (see Fig. 1) is designed for bearings of 3 MW class wind turbines. In order to reproduce the operating conditions of pitch bearings, all interfaces (hub, blade, pitch drive) are the same as in the actual wind turbine.

All loads are applied by hydraulic cylinders that are connected to ropes (see red rectangle in Fig. 1). The loads are measured by means of load cells. The rope is attached to a load frame, whose center point is 30 m from the blade root.

Figure 2Optical position measurement.


The bending moment applied to the bearing is calculated with the force measured and the load vector, which is calculated with the aid of an optical measurement system. This optical measurement system consists of four cameras and several reflecting marks. Some of these marks are reference marks with known positions. These references are used to calculate the position of the camera and the coordinates of the marks of interest. At the rotor blade, three marks indicate the current deflection (see Fig. 2). Another mark is fixed to the lower end of the load rope.

The pitch drive is equipped with a strain-gauge torque measurement system at the pinion shaft on the low-speed side. A full bridge of strain gauges is mounted on the shaft (see Fig. 3), together with a rotary unit. Data transfer and power supply is performed telemetrically via a ring stator. The measurement system has been calibrated by applying known torques to the shaft.

Figure 3Torque measurement strain gauges on shaft.


Figure 4Oscillating rotations and torque measurements (example).


The bearing is a grease-lubricated two-row four-point bearing of a 3 MW class turbine with an outer diameter of roughly 2.3 m. In addition to the tests with a mounted rotor blade, tests without the blade were executed to obtain data for zero load. The torque measurements were carried out under different pitch speeds and different external forces. The oscillating rotations of the bearings had a peak-to-peak amplitude of 10. The torque values were measured for the middle 5 (see “Cleaned torque” curve in Fig. 4).

To determine the load on the rolling elements of the bearing, a finite element (FE) model of the test rig was set up in ANSYS 15. For the bearing, this model uses the simplifications described in Daidie et al. (2008). These element loads are necessary for some of the friction calculation models. An example result of such FE calculations can be found in Schwack et al. (2016).

2.2 Bearing friction issues

Simple bearing friction models use external influences (speed and load) to calculate the overall friction of a bearing. To obtain sound results with such an approach, it is necessary to actually measure the bearing friction under different external conditions. A change to the bearing system, e.g., a different lubricant or sealing, will require a new measurement to determine the bearing friction in order to obtain exact results.

To actually predict the friction behavior of a bearing without the need for measurements, several friction mechanisms must be taken into account (Harris and Kotzalas, 2007). These mechanisms may be categorized according to influencing factors. For a given bearing, load, speed or both influence the friction torque exerted by the different mechanisms.

  • Factors that are load and speed dependent:

    • Heathcote (conformity) slip due to differential velocities

    • Sliding due to roller body spinning

    • Rolling friction due to lubricant movements in the rolling contact

    • Sliding of rolling bodies against cage/spacer

    • Cage sliding against bearing rings

  • Factors that are load dependent:

    • Sub-surface hysteresis due to load changes

    • Sliding of the sealing(s) against the bearing rings

  • Factors that are speed dependent:

    • Lubricant flow (churning) losses

In the following sections, two simple models (see Sect. 2.3 and 2.6) and two more detailed models (Sect. 2.4 and 2.5) are presented. In the literature, another model explicitly identified for blade-bearing friction evaluation was evaluated (González et al., 2008), but as this model is contained within the more detailed model described in Sect. 2.5, it was not used for the subsequent calculations.

2.3 Palmgren's friction torque calculation model

In Palmgren's model (Palmgren, 1957), the friction torque of a bearing is divided into a load-independent and a load-dependent part. The load-independent part T0 takes into account an empirical value f0 and the bearing diameter DM; see Eq. (1). A speed dependence is not part of the model for low rotational speeds as observed in pitch-bearing applications. At higher rotational speeds, the lubricant viscosity v and the bearing speed n must also be taken into account.


The load-dependent part T1 depends on another empirical value f1, the bearing diameter DM and the equivalent load P1:


The equivalent load P1 is defined as the sum of the absolute values of all individual ball loads derived from the FE calculations described in Sect. 2.1. Note that according to the Palmgren model for the low-speed regime, the friction torque is independent of the rotational speed of the bearing.

As the empirical values are not available for the pitch bearing used for this test, a minimum square deviation over all measured points is used to best fit the results obtained. Since the parameters have to be fitted to experimental data, the model is of little use to predict the friction of untested types of bearing.

2.4 Bearing manufacturer's friction model 1

The Palmgren model was further refined to take account of the various components of the bearing that contribute to the total friction. One of these models was developed by a bearing manufacturer (SKF, 2014). The following Eq. (3) shows the different elements of the total friction Mtot,S used in this model:


where Mrr is the friction caused by rolling, Msl the friction caused by sliding movements, Mseal the friction caused by the sealing and Mdrag the drag caused by the lubricant flow. Mrr is calculated as follows:


where ϕish and ϕrs are factors to take account of the lubricant film thickness and the lubrication displacement, and Grr is a base value for the rolling friction. This value depends on external loads.

To calculate Msl, a coefficient for the sliding friction, μsl, and a base value for the sliding friction, Gsl, are multiplied together:


The sealing friction Mseal is calculated according to Eq. (6):


where all values are empirically determined and depend on the bearing type, sealing type and the bearing diameter. These values are not available for pitch bearings and are chosen so as to deliver a best fit for the measured values of the overall friction torque at zero load.

The last part of Mtot is the friction caused by lubricant flow, Mdrag. Equation (7) contains the individual elements used to calculate this component. VM is a factor determined by the lubricant's resistance against movement, KBall a factor taking into account the behavior and number of the rolling elements, ft a factor taking into account the amount of lubricant in the bearing, and RS a value depending on the bearing type.


2.5 Wang rheological model

Wang (Wang, 2015) considers enhanced rheological fluid models and experimental results in his model for calculating the friction torque. The model follows the assumptions of Steinert (Steinert, 1995) and Zhou (Zhou and Hoeprich, 1991), who divide the friction torque into different parts that can be calculated independently from each other. For ball bearings, these parts are the friction torque, which results from the irreversible deformation work on the bearing steel Mdef, the torque from the hydrodynamic rolling friction Mroll and, if the bearing is axially loaded and the contact angle α is greater than 0, the torque caused by the spinning friction Mspin (FVA, 2010). The friction moment MHC takes account of the differential slippage which occurs due to the different velocities in the contact between ball and raceway, also known as the Heathcote effect (Harris and Kotzalas, 2007).

Equation (8) shows the different parts in a mathematical relationship for a better understanding. The parts Mspin and MHC cannot be analyzed separately because they both occur in the sliding moment Mslide; see Eq. (9).


The friction moment of the deformation work Mdef based on the approach of Johnson (Johnson, 1970) considers the damping of the material κ, the semiaxis of the Hertzian contact ellipse b and the load on each roller Q:


To calculate Mroll, the energy balance between the subsystem and the whole system needs to be considered (Steinert, 1995):


Equation (11) takes into account the diameter of the rolling element DRE, the angular velocity of the rolling elements ωRE and the inner ring ωIR, and the hydrodynamic forces at the inner Froll,IR,i and outer ring Froll,OR,i of each rolling element i.

According to Zhou (Zhou and Hoeprich, 1991), the hydrodynamic force Froll can be calculated from the isothermal hydrodynamic force Froll,isoth (Goksem and Hargreaves, 1978) and from a factor Cth, which takes account of losses due to shear and compression heating to obtain a linear relationship between film thickness and hydrodynamic rolling friction (Baly, 2005).


As mentioned before, the physical effect which leads to a sliding moment Mslide cannot be calculated separately. In the numerical model, Mslide can be calculated due to the relative sliding velocities and the resulting local shear stresses. For a better understanding, the physical effects in the sliding moment will be briefly explained.

Mspin is calculated from the inner diameter r, the contact area A and the shear stress τ in the lubricant, which can be determined with the aid of the Newtonian shear stress approach (FVA, 2005):


It must be borne in mind that it is difficult to apply this approach for Mspin because most lubricants exhibit nonlinear flow behavior. These non-Newtonian lubricants exhibit shear thinning and a limiting shear stress under elastohydrodynamic lubrication (EHL) conditions. τ needs to be limited to τlim due to rheological effects (Wang, 2015).

The friction from the differential slippage and Heathcote effect depends on the energy balance and takes into account the frictional losses at the inner (PHC,IR,i) and the outer ring (PHC,AR,i) of each rolling element i:


All sliding losses in the contact lead to high shear rates within the contact areas and are thus dominated by the lubricant behavior. Empirical results are used to calculate the friction torque, which takes into account the limiting shear stress. These results are obtained using a two-disc machine (see Fig. 5).

Figure 5Two-disc machine.


Figure 6Measured friction torque at different speeds and loads.


The relationship between the medium shear stress τ¯ and the shear rate γ˙ in the EHL contact is important to take account of rheological effects (Poll, 2011; Poll and Wang, 2012). A relationship among maximum shear stress τmax and the mean pressure p, temperature T, and the shear rate γ˙ can be obtained from the experiment. If the calculated Newtonian shear stress τ is greater than the maximum shear stress τmax from the experiment, the shear stress is truncated at the maximum value. The local shear stress is then integrated to yield the total friction force of the contact. The sum of the contact friction losses gives the friction torque due to sliding (Leonhardt et al., 2016).

2.6 Bearing manufacturer's friction model 2

While the two aforementioned approaches try to split the friction torque according to different friction causes, the following model is taken from a manufacturer's current bearing catalog (Rothe Erde, 2016). This method has no speed-dependent component and is adapted to different bearing types by the friction coefficient μ. The friction torque Mr is calculated according to Eq. (15):


This model does not take into account any load-independent part. In practice, however, all bearings experience frictional losses even under unloaded conditions. Consequently, the bearing manufacturer states that the equation must not be used for unloaded conditions.

3 Results and discussion
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3.1 Validation of the FE model

The results of the FE calculations have been compared to the results of the optical measurement system described in Sect. 2.1. A bending moment of 5 MNm is applied both to the real test rig and in the FE model, and the deformations at the three positions are measured and compared with the model results. Table 1 shows the deviations of the total deformations between the FE calculation and test rig measurements.

Table 1Deviations of deformations between FE model and test rig measurements.

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While positions 5 and 3 show satisfactory agreement, position 6 shows a large relative deviation between FE analysis and test rig. The large relative deviation is partly caused by the low absolute deformation (less than 20 mm) near the blade root (small absolute values result in high relative values) and the longer distance to the camera positions, which result in higher uncertainty.

3.2 Friction torque measurements and comparison with models

Figure 6 shows the results of friction torque measurements at different rotating speeds of the pitch bearing. The measurements were executed with the bending moment varied in steps of 1 MNm. Figure 6 contains lines indicating values between 1 MNm steps; these are interpolations. The external load was applied via a load frame (see Fig. 2) and is expressed as the resulting bending moment at the blade root. The measurements for each load–speed combination were repeated at least 20 times with no significant deviation between the mean values of friction torque. However, owing to the oscillating rotations used for the torque measurements, there is a relatively high standard deviation in the single measurements (shown for 2 and 5 MNm in Fig. 6) due to torque vibrations caused by the repeated accelerations of the blade- and pitch-bearing masses.

The values of the friction torque are normalized to the highest value of the measurements obtained at 1.04 rpm and the 6 MNm bending moment. For the conditions shown, the theoretical lubricant film thickness according to Dowson and Hamrock (Dowson and Hamrock, 1977) is close to or above the combined surface roughness of raceway and roller (Stammler and Poll, 2014). As the bearing is grease-lubricated, lubricant starvation might reduce the lubricant film thickness; thus a mixed lubrication regime is the most likely lubrication condition. The speeds examined are within the usual range of pitch-bearing speeds. From the measured values, it is not possible to derive the speed dependence of the friction torque.

In Fig. 7, the values are again normalized to the highest friction torque measured. The error bars refer to the standard deviation of the measured values.

In order to obtain results for the first manufacturer's and the Palmgren calculations, previously unavailable empirical values had to be chosen to match the curves with the measured values: for the Palmgren calculation, the value f0 was adapted to fit the zero load condition and the value f1 was adapted so that the difference between zero load torque and the highest load torque match the measured values. The first manufacturer's model includes all empirical values except the sealing friction of large slewing bearings. The empirical values provided with the model only include values for the sealing friction of bearings with a maximum diameter of 340 mm. Thus, the KS1 value that is part of the sealing friction was set in such a way that the non-load friction matches the measured values for the non-load condition.

Figure 7Measured and calculated friction torque at different loads.


Figure 8Measured and calculated friction torque at different speeds and a 5 MNm load.


The aforementioned choices of empirical values come with some drawbacks: currently, the Palmgren model cannot be used to predict the friction torque of other pitch bearings as there are no available values for the empirical factors f0 and f1. It is unclear whether the values used in this work are correct for loads higher than the measured loads or other bearing diameters. f1 was adapted to match the slope between a 0 and 6 MNm external load; if it had been adapted to the slope between 2 and 4 MNm, the differences between measurements and model calculations would have been higher.

Table 2Overview of agreement between bearing friction models and experimental results.

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Similar to the Palmgren model, the first manufacturer model contains only one empirical factor, which can be adjusted (KS1, which is part of the Mseal calculation). In order to achieve a match, the value had to be raised drastically compared to values for much smaller bearing diameters. Looking at the individual elements of the model, the adjusted Mseal is by far the largest part of the calculated friction at zero load and makes up nearly 99 % of the friction at 2 MNm, which does not seem plausible (considering that the seal is a V-ring-like lip seal). Additionally, the load dependence of the friction torque is underestimated by 67 % in comparison to the measurements. This may be caused by the Mseal part as well, due to the fact that a four-point bearing suffers relatively large deformations of the bearing rings under loads and should exhibit a load-dependent behavior of the sealing friction.

The Wang and the second manufacturer model contain all necessary empirical values. However, the results are not completely satisfactory: the second manufacturer's equation is explicitly not intended for zero load; as such this value is not displayed in the chart. The friction torque calculated with this model deviates by 35 % from the measured values at a load of 2 MNm and by 10 % at a load of 6 MNm. As the slope of the load dependence of the calculated curve is 15 % higher than that of the measured values, it might result in overestimated friction torques at loads higher than 6 MNm.

The model proposed by Wang does not take account of the sealing friction and shows the friction torque to have a rather high speed dependence that does not match the measured values. The model was originally intended for the calculation of friction under fully lubricated conditions and needs some further adjustments for mixed friction conditions.

Figure 8 shows the speed dependence of the different calculation methods and the measurement results at a 5 MNm external load. While the measurement values and most of the model calculations show either no speed dependence or the speed dependence depending on revolutions per minute (which does not lead to a drastic increase in the torque while the velocity of the rollers does rise due to the large diameters), the model of Wang contains a dependence on roller speed.

Only the models from Wang and from the second manufacturer can be used to predict the friction torque of pitch bearings without additional tests, as the other models need the adjustment of empirical values. The second manufacturer's model relies on empirical values as well, but in this case these values for different types of pitch bearings are available in the public domain.

4 Conclusions
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In this paper, torque measurements of a loaded four-point ball-type pitch bearing on which realistic interfaces were mounted have been presented. The measurements were executed at a pitch-bearing test rig with realistic interfaces (hub, pitch actuator, blade). While the measurements show a clear load dependence, no systematic dependence on the rotational speed of the bearing is observed within the range of speeds tested.

The load dependence exhibits nearly linear behavior, with a positive value at zero load condition. This supports the assumption that the friction torque has a load-independent part that is present in all of the calculation methods except for the second manufacturer's model.

With the Palmgren model, empirical values were adapted to match the measurement results, but it is doubtful if these values match other load conditions and/or types of pitch bearing. The sealing friction part of the first manufacturer's model was adjusted to match the measured values at zero load. This led to a dominance of the sealing friction, which does not seem plausible. As such, it may be concluded that the other parts of the friction are underestimated by this model. The second manufacturer's model overestimates the load dependence of the friction. The Wang model overestimates the speed dependence of the total friction.

None of the models reviewed are able to predict all aspects of the friction torque behavior of the pitch bearing. With the Palmgren, Wang and first manufacturer's models, this may be due to the range of bearings taken into account to create the models. Both the bearing types and sizes underlying the models differ significantly from those of typical pitch bearings. Additionally, it can be assumed that most of the experiments leading to the creation of these models were conducted under close-to-ideal lubrication conditions with oil lubrication, fully flooded contacts, and a complete separation between raceway and rollers. In grease-lubricated pitch bearings, mixed lubrication is possible under normal operating conditions. As such, the results have only limited comparability to the models based on tests under better lubrication conditions.

With none of the models being able to reliably predict the friction torque of the pitch bearing in the test described, the only way to currently determine the friction torque is with the aid of measurements. In future work, the test rig will be used for further friction torque measurements with different bearings to support the development of models suitable for large grease-lubricated bearings like pitch bearings. Further development work on the models will take into account the influence of the sealing, the lubrication conditions within pitch bearings, and the characteristics of different types of pitch bearing.

Data availability
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Data availability. 

The underlying data are not available due to confidentiality agreements in this commercial project.

Competing interests
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Competing interests. 

The authors declare that they have no conflict of interest.

Edited by: Lars Pilgaard Mikkelsen
Reviewed by: two anonymous referees

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Publications Copernicus
Short summary
Modern wind turbines all share the ability to turn (pitch) the blades around their main axis. By pitching the blades, the aerodynamic forces created by the blades are controlled. Rolling bearings, consisting of two steel rings and balls that roll on raceways between them, are used to allow pitching. To design pitch drives, it is necessary to know the losses within the bearings. This article describes how such losses have been measured and compares them with calculation models.
Modern wind turbines all share the ability to turn (pitch) the blades around their main axis. By...