Design of Drivetrain and Potential Evaluation of a Gorlov Turbine
Transcription
Design of Drivetrain and Potential Evaluation of a Gorlov Turbine
Design of Drivetrain and Potential Evaluation of a Gorlov Turbine Inigo Garcia de Madinabeitia Hannes Hagmar EEK150 Power Engineering Design Project HT15 Department of Energy and Environment Chalmers University of Technology Gothenburg 2015-10-31 Abstract The Gorlov helical turbine is proposed as a feasible alternative to generate electricity in smaller rivers where the ecological impact of a dam would be too significant. The report examines the possibilities of installing and designing a drivetrain for a Gorlov turbine in the small river of Säveån, close to Nääs castle. The results show that the energy potential in Säveån is severely limited during significant periods of the year, and the location is thus found not to be suitable. The design of the drivetrain and control is thus carried for a hypothetical river with a larger amount of water flow. The design of the drivetrain and control is intentionally simple, robust and with first order response, but simulation shows that the control is found to be adapting well to the applied simulations, and the power output is significantly increased with the controller implemented. The control needed in order to perform fish behaviour studies is chosen to be separated from the ordinary control, and instead a mechanical braking system is proposed. 1 Contents Abstract .................................................................................................................. 1 1 Introduction ..................................................................................................... 3 1.1 Background ............................................................................................... 3 1.2 Purpose ..................................................................................................... 4 1.3 Scope ........................................................................................................ 4 2 Theory ............................................................................................................... 5 2.1 Helical Gorlov turbine .............................................................................. 5 2.1.1 Turbine power and efficiency ....................................................... 5 2.1.2 Tip-speed ratio .............................................................................. 6 2.2 Generator .................................................................................................. 7 2.2.1 Electric model of a PSMG ............................................................ 7 2.3 Diode rectifier ........................................................................................... 8 2.4 Boost (Step-up) converter ......................................................................... 9 3 Methodology ................................................................................................... 11 3.1 Literature review ..................................................................................... 11 3.2 Water flow measurements and estimations ............................................ 11 3.3 Parameterization of a PMSG .................................................................. 13 3.4 Design of drivetrain and control ............................................................. 14 3.4.1 Design of control system ............................................................ 14 3.4.2 Simulations ................................................................................. 16 4 Results ............................................................................................................. 18 4.1 Water measurements............................................................................... 18 4.2 Parameterization results and values for simulation ................................ 21 4.2.1 Efficiency and Power-Speed curves ........................................... 22 4.2.2 Values and parameters for simulations ....................................... 24 4.3 Simulink simulations .............................................................................. 25 5 Analysis ........................................................................................................... 30 6 Conclusions..................................................................................................... 31 References............................................................................................................. 33 2 1 Introduction Hydropower is currently one of the most effective ways of generating renewable electricity in a sustainable way [1]. However, conventional hydropower stations require the use and construction of dams, resulting in a significant environmental impact. Largescale dam hydropower affects not only the water flow but also the wildlife habitat and the possibilities for fish migration. This ecological impact may, especially at smaller rivers, exceed the value of the generated electricity. Consequently, there exists a conflict between the goal of increasing the amount of renewable electricity and keeping the local ecosystem unharmed. Therefore, to still be able to harness power from lesser rivers, a new approach has to be examined. One possible solution is to use low-head micro hydro installations, such as the Gorlov helical turbine. The Gorlov turbine is a vertical axis water turbine, using only the current water flow to operate, therefore eliminating the need of constructing a dam. The Gorlov turbine has been used commercially mostly in tidal power plants; however, the potential for small-scale power generation in smaller rivers may still be vast [2]. 1.1 Background Nääs castle is situated close to Säveån, a relatively small river with two small hydropower stations located in the vicinity. To yield further energy from the river flow, and at the same time keeping the environmental impact at a minimum, the helical Gorlov turbine has been proposed as a feasible solution. Nääs castle is also a popular tourist destination with numerous visits throughout the year. However, as of now, it still lacks a proper public transport connection with the train station, and an investment of some sort would be needed. One suggested method of solving this problem is to use the electricity from the Gorlov turbine to drive an electric bus and transport train passengers to the castle. This would then not only result in a fully renewable and clean mean of transportation, but also as a source of goodwill for the castle. Furthermore, due to the fact that the Gorlov helical turbine is placed in water, it will undoubtedly have an effect on the aquatic life and the surrounding environment [3]. The studies of the impact on fish life is somewhat limited and how a system actually affects the fish is still rather unclear. Previous studies have found that factors such as the size and speed of the turbine, the size of the fishes, and the visibility all affects the impact. Higher speed of the turbine will cause higher chance of a collision and a large turbine will evidently affect a larger area of the river. The visibility is also found to have a significant impact, where a low visibility commonly results in a higher impact [3]. To further study the impact on fish life of a Gorlov helical turbine, the designed drivetrain should enable a wide range of speed control. By being able to control the speed of the turbine, the effect that the speed has on aquatic life can be examined. Up to this moment, 3 the previous studies of the effects that Gorlov helical turbines have on Swedish conditions are highly limited or even non-existent, and it is therefore most interesting to develop such studies. 1.2 Purpose The purpose of the report is to establish the potential of installing a Gorlov turbine in Säveån, and from the results design a suitable electrical drivetrain. Moreover, a control system should be chosen and designed to both yield a high energy output and allow a suitable speed control for future fish studies. 1.3 Scope The report will mainly address the electrical aspects of the drivetrain and there will thus be no analysis of how to physically design the Gorlov turbine. Since the turbine is not available for testing, specific properties such as efficiency and torque behaviour will have to be estimated from previous research [4], [5]. Furthermore, due to the limited time frame of the project, the optimization of the drivetrain will be limited. The main goal of the project is instead to design and simulate a drivetrain that could be applied once the turbine is in place. There are also a number of simplifications in the proposed model. Primarily, there is no modulation of the shaft between the turbine and the generator. Therefore, all the inertia of the whole system is simulated as if it is contained within the generator. The control system is purposely made simple due to both due to the lack of data regarding the turbine and due the project time constraints. Therefore, no regard is taken towards effects such as cross-coupling, backEMF and integrator anti-windup. To enhance the control system further, more effort should be put to examine these aspects. Finally, the potential evaluation of the project will not contain an economic estimation. This technology of small-scale generation of electricity is difficult to compare to other methods of generating electricity, and the results of such an evaluation would thus be inconclusive. Acknowledgements are given to Nusrat Afrin Ani and Iftekhar Zaman Arnab for writing and editing parts of the report and performing measurements. 4 2 Theory In the following section the theory required to follow the rest of the report is presented. The main focus is covering the fundamental aspects of the Gorlov helical turbine and how maximal power extraction can be achieved. A brief section is also covering the function of the main parts of the proposed drivetrain. 2.1 Helical Gorlov turbine The Gorlov helical turbine is an improved version of the Darrieus turbine, with a chosen number of blades swept in a helix profile along its span, rather than using the curved aerofoil blades of the Darrieus turbine [6]. Both designs are used as vertical axis turbines, allowing unidirectional rotation in all flow orientations [2]. However, the Gorlov turbine is found to have a number of advantages to prior designs. For example; the helical blade shape allows the turbine to be self-starting, there is a reduction of torque fluctuations during rotation, a higher efficiency, and a high uniform spinning in slow fluid flows [5]. 2.1.1 Turbine power and efficiency The Gorlov helical turbine can be dimensioned with several different characteristics to suit the application. The height and diameter of the turbine are significantly affecting the possible output as the swept area of the turbine is directly proportional to the output of the turbine. The swept area of the turbine can be calculated as π΄ = 2 β ππ‘π’πππππ β π»π‘π’πππππ (2.1) where π΄ is the swept area, and ππ‘π’πππππ and π»π‘π’πππππ are radius and height of the turbine. Furthermore; the number of blades, the material, the chord length, and the blade inclination angle, all affects the properties of the turbine. The extractable power in a flowing water stream can then be stated as [2] πππππ€ = 1 ππ΄π£ 3 2 (2.2) where πΆπ is the coefficient of power, πππππ€ is the power of the flowing water in a cross sectional area, π is the water density, π΄ the cross sectional area of the stream, and π£ the fluid stream velocity. The coefficient of power, i.e. the efficiency of the turbine, is then directly related to the produced mechanical power and thus to the mechanical torque πΆπ = ππ 1 3 2 ππ΄π£ 5 = ππ Ξ© 1 3 2 ππ΄π£ (2.3) where π is the efficiency of the turbine, ππ the mechanical power, ππ the mechanical torque, and Ξ© the angular velocity. By rearranging (2.3), the power output of the turbine is found to be ππ = 1 ππ΄π£ 3 πΆπ = πππππ€ πΆπ 2 (2.4) 2.1.2 Tip-speed ratio The tip-speed ratio (TSR) is the ratio between the speed of the tip of the blade and the velocity of the water flow, and can be stated as π= Ξ© β ππ‘π’πππππ π£ (2.5) where π is the TSR. The optimal value of TSR is depending on the turbine design and each value of the ratio is related with a value of the coefficient of power πΆπ . In order to generate the highest amount of energy, the TSR should thus be kept to a ratio that results in the highest value of πΆπ . The highest efficiency is thus obtained when πΆπ ,πππ‘ = πΆπ (ππππ‘ ). By combining (2.4) and (2.5) the expression for the maximal power can then be stated as 3 ππππ‘ Ξ©πππ‘ β ππ‘π’πππππ 1 = β π β πΆπ,πππ‘ β π΄ β ( ) 2 ππππ‘ (2.6) This concept of controlling the tip speed ratio to the value corresponding to the highest value of πΆπ is known as maximum power point tracking (MPPT). The power speed characteristics of a Gorlov turbine are presented in Figure 13 in section 4.3, and consists of a curve connecting the highest πΆπ -values at different water velocities. The results from previous studies regarding optimal TSR of Gorlov turbines are somewhat inconclusive. Two studies, using a three-bladed turbine, found that the TSR should be chosen to a value 2.0-2.2 to achieve the highest πΆπ -value [5] and [4]. In contrast, another study, with the same amount of blades, found that the highest πΆπ -value was achieved at about 1.1-1.2 TSR [7]. The efficiency of the turbines is also varying significantly, with an efficiency span ranging from 11.6 - 39 % [2]. The efficiency varies significantly depending on aspects such as number of blades, blade type, helical angle and water flow velocity. However, one of the more recent reports states that the efficiency for a 3-bladed helical turbine is closer to 27 % [4]. 6 2.2 Generator The generator transforms the mechanical power from the shaft into electric power that is then fed to either the grid or to a battery cell. The most common generator types for driving wind turbines are the induction generator (IG) and the permanent magnet synchronous generator (PMSG). The PMSG has generally a larger torque density and requires less maintenance, but is generally more expensive than IG. Due to the proximity to open air and water, the aspects of corrosion and sealing are important. The easiest solution to handle this would be to either select a generator with a high IP rating or construct a suitable sealing. The dust protection should be at least enough for dust not to interfere with the performance and the water protection should at least be enough to withstand splashing of water [8]. 2.2.1 Electric model of a PSMG The PMSG is a synchronous generator that uses permanent magnets, rather than windings in the rotor, to create the required magnetic field [9]. The related stator equation can be stated [10] as πΈπΜ = πππ β πΌπ Μ + π π β πΌπ Μ + ππ Μ (2.7) where πΈπΜ is the electromotive force (EMF) of the generator, πππ is the reactance of the generator, π π is the stator resistance, ππ Μ is the stator voltage , and πΌπ Μ is the line current. Note that all currents and voltages are expressed as phasors by using the notation of the dot above the symbol [10]. The generated EMF voltage πΈπ is directly proportional to the rotor speed [9] πΈπΜ = ππΈ β Οr (2.8) where ππΈ is a machine dependent constant and Οr the rotor speed measured in radians/second. Using (2.7) and (2.8) we can state the line current as πΌπ Μ = ππΈ Οr β ππ Μ π π + πππ πΏπ (2.9) From (2.9) it is found that if ππ is varied, the current will change accordingly. This is however only true for lower values of Οr ; at higher frequencies the πππ πΏπ -term will increase as much as the generated ππΈ Οr -term and the control will be lost. The electrical torque ππ produced by the machine can similarly be stated as ππ = 3 β ππΈ β πΌπ Μ The mechanical relationship between the torque and the speed is 7 (2.10) π½ πππ = ππ β ππΏ ππ‘ (2.11) where π½ is the inertia of the machine, and ππΏ is the load torque. If the PMSG is connected to a rectifying unit, then speed of the PMSG is possible to estimate by measuring the DC current and voltage. The relation for the speed is governed by the following equation [11] Οr = 2π (πππ + 2π π πΌππ ) ππ 3β3 Μ 60 ( π Ξ¨ m β 2 πΏπ πΌππ ) (2.12) where πππ and πΌππ is the DC voltage and current, and ππ is the number of pole pairs 2.3 Diode rectifier In order to transform the AC-output of the generator to a DC-voltage, a rectifying unit is required [12]. The design of the rectifying unit is often made with respect to the application it is going to be used in. Normal power diodes have an on-state forward voltage drop of about 0.7-1 V depending on the design [12]. The Schottky diode has a significantly lower on-state voltage drop, around 0.3-0.4 V, and is therefore more preferable in the sense of reduced losses. However, the Schottky diode has higher reverse leakage current and a smaller breakdown voltage. Since the output voltage of the rectifier should be as ripple free as possible, a large capacitor should be connected on the DC side. By neglecting the voltage drop and the losses of the rectifying unit, the DC voltage can easily be referred to the AC side by using the concept of power balance. Thus, from the rule of conservation of energy, the power on the DC side must be equal to the power on the AC side 3ππ πΌπ = ππ·πΆ πΌπ·πΆ (2.13) where ππ·πΆ and πΌπ·πΆ is the DC voltage and current respectively. Note that there is no need for a cosine term at the AC side due to the unity power factor. The mean value of the voltage on the DC side is found by integrating the rectified AC voltage as ππ·πΆ = 3 π/6 3β6 β« ππ β β3 = π π βπ/6 π π By combining (2.13) and (2.14), the DC current can then be stated as 8 (2.14) πΌπ·πΆ = 3ππ πΌπ 3ππ πΌπ π = = πΌπ ππ·πΆ 3β6 β6 π ππ (2.15) 2.4 Boost (Step-up) converter A boost (step-up) converter is mainly used for DC power regulated supplies and for regenerative breaking of DC motors [12]. As the name indicates, the output voltage of the converter is always greater than the voltage input. In order to be able to keep the voltage on the high voltage side, a large capacitor is generally needed. The basic circuit diagram of a boost converter is found in Figure 1. Figure 1. Circuit diagram of boost (step-up) converter The converter equations are 1 π (1 β π·) π·πΆ1 (2.16) πΌπ·πΆ2 = (1 β π·)πΌπ·πΆ1 (2.17) ππ·πΆ2 = π·= π‘ππ π (2.18) where ππ·πΆ2 and πΌπ·πΆ2 are converter output voltage and current, respectively; ππ·πΆ1 and πΌπ·πΆ1 are converter input voltage and current, respectively; π· is the duty cycle; π‘ππ is the converter on time per period; and π is the converter switching period. Using these equations, the DC resistance can be varied by changing the duty cycle of the converter 9 π π·πΆ2 1 ππ·πΆ2 (1 β π·) = = π = (1 β π·)2 β π π·πΆ1 πΌπ·πΆ2 (1 β π·) π·πΆ1 (2.19) where π π·πΆ2 is the DC effective output resistance and π π·πΆ1 is the DC input resistance. To reduce the current ripple to a certain value, the inductance should be designed according to [12] βπ = (ππ·πΆ2 β πππ1 + ππ )π πΏ 10 (2.20) 3 Methodology In the following section, the used methodology is thoroughly described. A short literature review is presented to give the reader an overview of the general progress within this field of research. Furthermore, the procedure for the water flow measurements are discussed and argued for and the method for the parameterization of the proposed PMSG is described. Finally, the choice, design, and selections for the drivetrain and control system are presented. 3.1 Literature review The project will commence with a significant literature study, covering mainly previous research of the Gorlov turbine, as well as how to actually design a working drivetrain for a small generator. The previous studies regarding the efficiency of the Gorlov turbine are somewhat limited [5] , [6] and [7]. The results differ significantly from each study and the results are therefore also somewhat questionable. Thus, for the purpose of this report, the required values will have to be estimated. The literature covering the design of drivetrain is vast, and a huge number of articles and reports are available. However, most reports cover advanced methods of control and few are focusing on the simple and robust control needed in this project. 3.2 Water flow measurements and estimations The water flow measurements were carried out by using an electromagnetic water current meter from a bridge overpassing Säveån, see the marked location in Figure 3. In order to find the most suitable spot for placing the turbine with the highest water velocity, the water flow of several of the bridge openings were tested; for reference see Figure 2. The measurements were also performed at different depths in order to examine if there was variations in water flow. Moreover, the depth of the river was measured in order to find a feasible location to physically place the turbine. Due to the time constraint of the project, it is impossible to measure the water flow during a long period. The proposed method to still be able to estimate the annual water flow is to compare the actual measurements with data from the southern hydro power station in Floda located nearby (see Figure 3). Thus, from the correlation between these data, it will be possible to make an estimation in the differences of total annual water flow. By assuming a linear relationship between the measured water speed value and the data from the power station, a reference value for the water velocity can be found. 11 Figure 2. Bridge over Säveån where the measurements where performed Figure 3. Map over Säveån and surroundings 12 3.3 Parameterization of a PMSG The generator chosen for this project is a 12 V, 600 W permanent magnet synchronous generator. Due to the higher efficiency and the robustness it was found to be the most suitable choice in this application. In order to simulate its behaviour in Simulink, measurements of the machine parameters were required. The mechanical parts of the PMSG were assembled and then connected to an 87 kW driving motor. Due to the low power rating of the motor, it is not possible to directly measure the resistance with a multimeter. Therefore, a current was applied between two phases and the voltage was then measured. By then using Ohmβs law the resistance could be calculated. The inductance was measured by using an autotransformer as a source of a variable AC power supply, and then measuring the impedance between two phases. The inductance is sensitive to physical movement, may vary significantly due to outer vibrations. Therefore, the measurements of the inductance were conducted both during vibrating and nonvibrating conditions. A current of about 2 A was applied and the voltage was then measured. Using the data from the resistance measurements, the inductance is possible to distinguish from the measured impedance, see following equations ππ = ππ πΌπ 2 β π 2 πππ ,π = βππ π πΏπ ,π = ππ ,π 2ππ (3.1) (3.2) (3.3) where ππ is the measured complex impedance, ππ is the measured applied voltage, πΌπ is the measured applied current, π π the measured resistance, ππ ,π the estimated stator reactance of the generator, and πΏπ ,π the estimated inductance. Finally, the flux linkage has to be estimated. This was done by performing a no load-test and measuring the voltage at different speeds of the machine. From the results, a voltagevs-speed curve could be found and the flux factor estimated. Moreover, the number of pole pairs was found by using the following formula ππ = 60 β π Ξ©πΊ where ππ is the number of pole pairs and π the frequency. 13 (3.4) 3.4 Design of drivetrain and control The drivetrain should be designed to be as efficient, reliable, and robust as possible. The turbine is therefore to be connected directly to the PMSG without the interconnection of a gearbox. Due to the high number of poles of the PMSG, the efficiency is still high even at low speeds. The generator is then connected directly to a three-phase rectifier, which in turn is connected to a boost converter and a battery bank. A simple design of the proposed drivetrain is found in Figure 4. Figure 4. Proposed drivetrain for a PMSG The effective load of the battery bank may be, due to the simple connection of the rectifying unit, modelled as an AC voltage source with a unity power factor [13]. The stator current πΌπ , and thus the torque, can then be controlled by regulating the duty cycle value of the boost converter. By then using the data from the water flow measurements, simulations will be performed in order to accomplish the potential evaluation. Initially, a Simulink model will be designed in order to test the properties of the drivetrain and the control system. Since the turbine is not available for testing, specific properties such as efficiency and torque behaviour will have to be estimated from previous research. If the results are satisfying, the real drivetrain will be constructed and tested. In order to imitate the turbine behaviour, a motor with specified speed and torque inputs will instead be connected to the drivetrain. With respect to the given results, further improvements will be suggested. 3.4.1 Design of control system The control system should be designed to be both efficient and allow a wide range of speed control in order to allow more degrees of freedom in future fish behaviour studies. The speed control required for future fish behaviour studies has been chosen to be separated from the proposed maximum power point tracking system. Since the fish behaviour studies will likely take place during a reasonably short time span, it will not affect the total generated power in such a high degree. Therefore, a mechanical manual braking system is instead proposed to control the turbine during fish studies. This results in a decreased power output during the time of the studies, but since the time frame is limited, there is a small effect on the total energy output. Due to the generally small output 14 of the turbine, the mechanical torque is fairly small and the breaking system can be dimensioned accordingly. During the period of mechanical control, the regular control system will be disconnected to avoid disturbances. The aim of the actual control system that is going to be in place during normal operation is instead to generate maximum power at all water flow velocities. The whole circuit in its entity in Simulink is presented in Figure 5 below. Figure 5. Simulink model of a Gorlov turbine and PMSG connected to a DC load The aim of the control system is to control the switch of the boost converter and thereby the output voltage and current of the PMSG. By measuring the power output on the DCside and considering the power-speed characteristics of the generator, the rotor speed reference can be determined. The estimated power-speed characteristics for the Gorlov turbine is found in section 4.3 and Figure 13.The error between the actual speed and the reference speed is then fed to a PI controller to obtain the reference torque, expressed as [14] ππ,πππ = (πΎπΞ© + πΎπΞ© ) (Ξ©ref β Ξ©) π (3.5) where ππ,πππ is the reference electromagnetic torque, πΎπΞ© and πΎπΞ© are the proportional and integral gains for the speed control, and Ξ©ref is the reference rotor speed. The values for the proportional and integral gain are chosen experimentally and the results are presented in section X. From the torque reference, the DC current reference is calculated by using (2.10) and (2.15) 15 πΌπ·πΆ,πππ = π Μm 3β6Ξ¨ ππ,πππ (3.6) The DC current reference is then compared with the actual DC current and the error is finally provided to a hysteresis controller. Thus, when the error between the reference and actual current is too large, a signal will be transmitted to the switch in the boost converter. The inner current loop controller is used to ensure a higher level of robustness and a quicker response. The control circuit in its entity in Simulink is illustrated in Figure 6. Figure 6. The simple control circuit used in Simulink for the PMSG To avoid the need of measuring the speed of the PMSG, a speed estimation block is connected. The speed estimation block is derived by using (2.12) and is found in Figure 7. Figure 7. Speed estimation block in Simulink for the PMSG 3.4.2 Simulations The performed simulations use the water speed profile from Figure 15 as input to the previously presented Simulink model. The simulation output was chosen to 5000 points per second, with a total of 100 000 points in 20 seconds. This resolution is believed to be enough to observe the system and controller behavior and performance. The Power 16 Systems Toolbox is used in Simulink for the electrical components, as well as the PMSG block for the generator. The simulations are performed to both examine the potential of the drivetrain and to control that the proposed control system is operating properly. To examine whether the control is fast enough, simulations are performed for a step and a filtered water speed profile with shrunk time axis. The reason of using this shrunk time axis is to make it more challenging for the control. Furthermore, the properties and functionality of the speed estimation block is examined. In order to observe the difference for with and without control, the control block is turned on first after 10 seconds for the filtered speed profile case, whereas it is always on for the step responses. The following four different simulations are performed in order to examine the control system: A. 1 to 1.5m/s step with measured speed B. 1 to 1.5m/s step with estimated speed C. Filtered water speed profile and measured speed D. Filtered water speed profile and estimated speed 17 4 Results In the following section the results from the water measurements, the parameterization of the motor, and the Simulink simulations are presented. The results are further analysed and discussed in the next section. 4.1 Water measurements Figure 8 show the water speed results from the measurements in Säveån for a depth of 0.5 meters. These measurements were performed on the first opening to the right of the largest bridge opening, for reference see Figure 2. To reduce the noise of the measurements, a cubic SavitzkyβGolay filter with a moving average of 99 elements has been implemented [15]. The moving average is illustrated by the red line in the figure. The average water speed value of the measurement is calculated to 0.198 m/s. 0.4 0.35 Water speed [m/s] 0.3 0.25 0.2 0.15 0.1 0.05 0 Measurement data Filtered data 50 100 150 200 250 Time [s] Figure 8. Water measurement plot from Säveån, 2015-09-16. Blue line is measured data points and red line is the filtered water speed Another measurement was performed the 15th October 2015 with an estimated average water speed value of 0.369 m/s. Figure 9 shows the speed measurements for this date with the same moving average as previous. The water flow from this figure will later be used in the upcoming simulations and an added constant will used to simulate a river with a higher water velocity. 18 0.6 0.55 Speed [m/s] 0.5 0.45 0.4 0.35 0.3 0.25 0 200 400 600 800 1000 1200 1400 1600 Time [s] Figure 9. Water measurement plot from Säveån, 2015-10-15. Blue line is measured data points and red line is the filtered water speed The water flow in the Säveån measurement point, Figure 3, in cubic meter per second was found by using the SMHI application βSMHI Vattenwebb β Hydrologiskt nulägeβ [16]. During the date of the first measurement the flow at the southern water power station in Floda was measured to 8.7 π3 /π [16]. During the date of the second measurement the flow at the southern water power station in Floda was measured to 8.1 π3 /π [16]. By assuming a linear relationship between these values and the estimated average values from the actual measurements in Säveån, a reference value for the water velocity can be found. Monthly water flow data for the southern power station is presented in Table 1 together with the estimated average water speed, average power for an assumed turbine, and the possible energy generation per month. The estimated water average speed in Säveån near Nääs castle is also found in Figure 10. 19 Table 1. Monthly water flow of Säveån in Floda and estimated values of water speed and energy generation for Nääs castle [16] Average Estimated Average Average Power of Energy Water Flow Water Speed power Generated* Month Water Flow in Floda in Floda Generated* [W/m2] [kWh/month] [m³/s] [m/s] [W/m2] Jan 32.88 1.12 712.13 178.03 129.96 Feb 30.16 1.03 549.61 137.40 100.30 Mar 25.25 0.86 322.59 80.64 58.87 Apr 23.03 0.78 244.85 61.20 44.67 May 16.62 0.56 92.12 23.03 16.81 Jun 11.85 0.40 33.33 8.33 6.08 Jul 11.67 0.39 31.87 7.96 5.81 Aug 11.06 0.37 27.13 6.78 4.95 Sep 11.44 0.39 30.06 7.51 5.48 Oct 14.78 0.50 64.76 16.19 11.81 Nov 21.44 0.73 197.58 49.39 36.06 Dec 27.79 0.95 430.11 107.53 78.49 499.34 Total generation* [kWh/year]: * Assuming a turbine- and drivetrain total efficiency of 25 % efficiency and a swept area of 1 m2 1.2 Water Speed [m/s] 1 0.8 0.6 0.4 0.2 0 Jan Feb Mar Apr May Jun Jul Aug Sep Oct Figure 10. Estimated average water speed for Nääs castle 20 Nov Dec 4.2 Parameterization results and values for simulation In the following section, the results from the parameterization of the PMSG are presented. Furthermore, the values chosen for the Simulink model and control are presented. 4.2.1 Generator measurements The results from the inductance measurements are presented in Table 2. As can be found in the table, the value of the inductance is varying somewhat between the measurements and to determine what value is most correct is hard to state. Due to the lower variation in the results for the no vibration cases, the average of these values will be used in the simulations. Table 2. Results from the inductance measurements Inductance (No vibration) Measurement Conditions I [A] U [V] L [mH] 2 2.1 2.31 2.3 2.3 0.36 0.356 0.381 0.407 0.34 0.263 0.245 0.2376 0.258 0.207 Average 0.242 The measured speed-voltage characteristics of the generator are found in Figure 11. By evaluating the slope, the flux linkage can be estimated and the value is presented in Table 2. 21 20 18 16 Voltage [V] 14 12 10 8 6 4 2 50 100 150 200 250 Rotor Speed [rmp] 300 350 400 Figure 11. Voltage-speed characteristics for the measured PMSG 4.2.2 Efficiency and Power-Speed curves The πΆπ -vs-π curve is found by using experimental values from [4] and adding two fictional points (marked with black rings in Figure 12) to the experimental values. This is made so that the control strategy can be made analogous to a wind turbine controller. From these points, a fitted curve for a theoretical πΆπ -vs-π curve is found. The fitted curve will be later used to find the power-speed characteristics of the turbine. Cp vs. lambda FIT 0.25 Cp 0.2 0.15 0.1 0.05 0 0 0.5 1 1.5 2 2.5 ο¬ Figure 12. Estimated πΆπ -vs-π curve for a Gorlov turbine 22 3 The πΆπ -vs-π curve is found and can be mathematically stated as πΆπ,πππ‘π‘ππ = 0.2713 β π (πβ2.06) 2 ) ) (β( 0.7059 + 0.03035π (πβ2.724) 2 ) ) (β( 0.252 (4.1) Using the πΆπ -vs-π curve from Figure 12, the power-speed characteristics is generated for turbine at different water velocities. This power-speed curve (see Figure 13) is later used in the simulations together with the measured DC power to find the reference value of the turbine speed. Figure 13. Power-Speed characteristics of for a Gorlov Helical Turbine This equation for the power-speed curve is found by taking the maximum value of each water velocity and fitting a curve with fourth order polynomial which can be mathematically stated as ππππ€ππ_π ππππ = β0.07083 β Ξ©πππ 4 + 16 β Ξ©πππ 3 β 1.069 β Ξ©πππ 2 + 0.8488 β Ξ©πππ β 0.1778 23 (4.2) 4.2.3 Values and parameters for simulations The data to be used in the Simulink simulations are summarized in Table 3. Note that the values for system inertia and viscous damping are estimated, and that the values for proportional and integral gain are experimentally gathered. The values of the boost converter are deducted experimentally to suit the application. Table 3. Summarized table of measured and estimated values to be used in simulations Generator Controller Turbine Converter Parameter Estimated values Resistance [β¦] 0.071 Inductance [mH] 0.242 Flux linkage [Wb] 0.4643 Pole pairs [-] 8 System Inertia [kgβm2] 40 Viscous damping [Ns/m] 0.006 Proportional gain Speed C. 3000 Integral gain Speed C. 30 Radius of turbine [m] 1 Height of turbine [m] 0.5 Forward voltage rectifier [V] 0.3 Boost converter inductor [mH] 200 Boost converter capacitor [µH] 10 24 4.3 Simulink simulations In the following section, the results from the Simulink simulations are presented. The water flow is simulated by using the data from Figure 9 with an added constant of 1 m/s. The measurement device was operated at 1 measurement/s and this is believed not to be demanding enough for the control, and therefore the time axis will be reduced to match the Simulink simulation time. Thus, the time data is scaled down with a 1/80 factor. The compressed water speed used in the simulation is found in Figure 14. The step water profile is shown in Figure 15. Figure 14. Filtered water curve used for the upcoming simulations, with a compressed time axis to match the simulation time. Figure 15. Step water speed profile for performed simulations. 25 A. Step water speed profile and measured speed Figure 16 shows the πΆπ evolution. As seen, it can easily follow the reference, and the πΆπ gets back to the optimal value within a short period of time, around 1.5s. As for the generated power, illustrated in Figure 17, there is a steady state error, but the shape is of a first order response, which is the expected from the proposed PI controller. Figure 16. πΆπ -value with step water speed profile with speed sensor. Figure 17. Power with step water speed profile with speed sensor. Actual DC power in blue, maximum theoretical value in red. 26 B. Step water speed profile and estimated speed The πΆπ evolution is displayed in Figure 18. In this case, there is an overshoot every time the control is started or a new step is applied. However, is it not due to integrator windup or a second order system control, but due to the πΆπ -curve. The step takes the operation point to a lambda value smaller than the optimal, arrow 1 in Figure 19. This way, the controller has to move the operation point to the optimal, arrows 2 and 3, but owing to the speed estimation, it does not stop there and continues to a lower πΆπ , arrow 4. As for the generated power, illustrated in Figure 20, there is a steady state error, but the shape is of a first order response, which is the expected from the proposed PI controller. Figure 18. πΆπ -value with step water speed profile with speed estimation. 0.25 3 2 0.2 Cp 4 Cp vs. lambda FIT 1 0.15 0.1 0.05 0 0 0.5 1 1.5 2 2.5 3 ο¬ Figure 19. πΆπ -trajectory during step change from Figure 15. 27 Figure 20. Power with step water speed profile with speed estimation. Actual DC power in blue, maximum theoretical value in red. C. Filtered water speed profile and measured speed Figure 21 illustrates the change of the πΆπ -value over time in the case of using the filtered water speed profile and speed sensor. The controller is turned on at π‘ = 10, and as can be seen in the figure the control succeed to significantly improve the πΆπ -value. Figure 21. πΆπ -value with filtered water speed profile with speed sensor. In Figure 22 the optimal and actual output power output are illustrated. In the figure, it is clearly seen that the difference between the optimal and actual power are significantly 28 reduced once the controller is turned on at π‘ = 10. It is also possible to distinguish a steady-state error between the optimal and actual output power. Figure 22. Power with filtered water speed profile with speed sensor. Actual DC power in blue, maximum theoretical value in red. D. Filtered water speed profile and estimated speed When the speed sensor is disabled and the control uses speed estimation, results get altered, mainly due to the fact that the speed estimation is not as accurate in lower speeds. Figure 23 shows the πΆπ -value at estimated speed. Figure 23. πΆπ -value with filtered water speed profile with speed estimation. 29 In Figure 24 the optimal and actual output power output with estimated speed are illustrated. In the figure, it is clearly seen that the difference between the optimal and actual power are significantly reduced once the controller is turned on at π‘ = 10. However, due to the speed estimation, the output DC power is somewhat reduced. Figure 24. Power with filtered water speed profile with speed estimation. Actual DC power in blue, maximum theoretical value in red. 5 Analysis The water flow is found to varying significantly during the year, with the lowest water flow during June to September and the highest during December to Mars. Furthermore, the results show that the extractable power is almost non-existent during large periods of the year and the estimated total energy generated during one year for the proposed turbine would only be 500 kWh. This number is also based on the assumption of an efficiency of 25 % for the whole drivetrain. However, due to the low water velocity and therefore the low speed of the turbine, the efficiency of the generator might be decreased significantly. When this generated energy during one year is compared with the consumption of an electric bus, with 4 daily 2-way trips between Floda train station and Nääs castle, 5.5km, for 100 days per year, it found seen that the turbine does not suffice to cope for the busβ consumption. The used parameter for traction consumption is 0.072 kWh/km·ton [17]. A bus with a mass of 19 ton would thus require a yearly consumption of 6019.2 kWh. Hence, 12 Gorlov turbines like the studied one would be needed. The established linear relationship between the water measurements and the data from the power station in Floda might also be a source of uncertainty. The first measurement registered a water velocity of 0.198 m/s whilst the power flow at Floda was found to be 8.7 m3/s. During the second measurement, the water velocity was measured to 0.369 m/s whilst the power flow was found to be 8.1 m3/s. Therefore, the positive linear relationship between the water velocity at Nääs and the water flow in Floda cannot be proved with 30 this data. However, due to the time constraints of the project no more measurements could be performed to further verify this. Due to the undesirable results of the water measurements, the simulation and design of the drivetrain was instead performed with a hypothetical river in consideration. Furthermore, since no Gorlov turbine was available for testing, several of the parameters for the simulation had to be estimated. For example, the πΆπ -curves and the resulting power-speed characteristics had to be estimated from previous experiments and parameter values such as the system inertia and viscous damping had to be estimated. Thus, for future setups and installations, these values would have to be reconsidered. The results from the Simulink model show that the simple controller and the drivetrain is generally working well. In figures 16 - 24, the controller is tested for a filtered and a step water speed profiles, and for the scenarios with or without the proposed speed sensor. In all the filtered scenarios, the controller is activated after 10 seconds. In the step simulations, the control is always activated. Generally, the πΆπ -value is found to be significantly increased when the control is activated in all simulations. Furthermore, the results show that, despite that the water velocity varies significantly in the filtered water speed profile, the controller has no problem of responding to these variations. Therefore, it can be concluded that the controller is well adapted to handle quick changes in the water speed. However, there is a somewhat decrease in the efficiency of the controller when the speed estimation block is connected. At lower speeds the estimation block is found to not estimate the speed perfectly. In the case when the speed sensor is connected, the πΆπ -value is increased from 75% to 95% of the optimal πΆπ -value. Though, in the case when instead the speed estimation block is connected the πΆπ -value is increased only up to 92% of the optimal πΆπ -value. Therefore, it is possible to conclude that the speed estimation is generally operating well, but is somewhat misjudging the actual speed. However, this would probably be acceptable for most setups as speed measurement devices generally are both rather expensive and require some maintenance. For all simulations, a steady state error between the optimal power output and the actual generated power output is found. This steady state error is believed to be a result of both the limits of the controller and due to losses in the drivetrain. As the controller is designed as a hysteresis-controller, the operating point of the system will always be close to the desired, but never perfect. Furthermore, the losses in the boost converter and the rectifier will also contribute to the discrepancies. 6 Conclusions The water flow in Säveån close to Nääs castle is found to be considerably too small to for it to be feasible to install a Gorlov turbine. A river with both a higher and more consistent water flow would be desirable. 31 Due to the lacking results of the water measurements, the simulation and design of the drivetrain were performed on a theoretical setup instead. The simple and robust drivetrain and control were found to be adapting well to the applied simulations, and the power output was significantly increased with the controller implemented. The system has a first order response, which was expected to have with the PI tuning that was performed. The operation with a speed estimation block instead of a speed measurement was found to be generally working well, however, with a small decrease in the power output. 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