AUTOMATION AND GENERATION OF SUSTAINABLE ENERGY SUPPLY USING BLADE LESS WIND TURBINE Dissertation Submitted For PARTIAL FULFILLMENT OF THE REQUIREMENT FOR THE AWARD OF THE DEGREE OF MASTER OF TECHNOLOGY IN MECHANICAL ENGINEERING Specialization Manufacturing Technology and Automation Submitted By ANKIT KUMAR Enrolment no.:2102219001 Under the guidance of Prof. (Dr.) Dilip Kumar (Assistant Professor) School of Engineering and Information Technology Sanskriti University,Mathura,U.P. (281401) 1 In dedication to my parents for making me who I am, and for supporting me all the way! 2 Acknowledgement I am extremely fortunate to be involved in an exciting and challenging project on “Automation and Generation of Sustainable energy supply using Bladeless wind Turbine”. It has enriched my intellect, giving me an opportunity to look at the horizon of technology with a wide view and to come in contact with people endowed with many superior qualities. I would like to express my deep gratitude and respect to my Mentor/Guide Dr. Dilip Kumar (Assistant Professor, Dept. of Mechanical Engineering) for his excellent guidance, suggestions and constructive criticism. I feel proud that I am one of his post graduate students. The charming personality of Dr. Dilip Kumar has been unified perfectly with knowledge that creates a permanent impression in my mind. I consider myself extremely lucky to be able to work under the guidance of such a dynamic personality. It would be a crime not to thank my beloved senior Rahul Kumar (JRF, ,Mechanical Engineering, Sanskriti university) who stood by me whenever the need arose, be it problem formulation, coding, results or drafting and most importantly through the odds and evens of my life. He is the one true partner in research I had the good fortune of having. I also like to convey my special thanks to Dr. Rahul Kumar (Assistant Professor & Coordinator ,Mechanical Department) for sharing his valuable knowledge and also want to thank Professor BALLU, (Head of Department, Mechanical Engineering). I would also like to extend my sincere thanks to all the staff members of Mechanical Engineering Department, SU, MATHURA for their valuable suggestions and timely support. This thesis is a fruit of the fathomless love and affection of all the people around me – my parents, my supervisor and my friends. If there is anything in this work that is of value – the credit goes entirely to them. Ankit kumar M.Tech (Mechanical Engineering) Splz: Manufacturing Technology and Automation Enrolment no:- 2102219001 3 CERTIFICATE Date: May 4, 2023 This is to certify that the thesis entitled “AUTOMATION AND GENERATION OF SUSTAINABLE ENERGY SUPPLY USING BLADE LESS WIND TURBINE” being submitted by Ankit Kumar (2102219001) for the partial fulfilment of the requirement of Master of Technology degree in Mechanical Engineering (Specialization: Manufacturing Technology & Automation) is a bona-fide thesis work done in the Department of Mechanical Engineering, Sanskriti University Mathura, India under our supervision and guidance. The results presented in this thesis have not been submitted elsewhere for the award of any other degree. Dr. Rahul Kumar Course Co-ordinator(M.E.) Dept. of Mechanical Engineering Sanskriti University (Mathura) Prof.(Dr.) Dilip Kumar Project Supervisor Dept. of Mechanical Engineering Sanskriti University (Mathura) 4 Table of Contents: 1. Abstract……………………………………………………………………………………….6 2. Introduction…………………………………………………………………………………7 3. Literature Review…………………………………………………………………………8 4. Objective………………………………………………………………………………………9 5. Working Principle…………………………………………………………………………10 6. Working Methodology………………………………………………………………….13 7. Observation Table……………………………………………………………………….19 8. Mathematical Calculation ……………………………………………………………31 9. Applications…………………………………………………………………………………34 10. Advantages………………………………………………………………………………..35 11. Future scope of work………………………………………………………………….35 12. Few snaps of observation of our model………………………………………36 13. Conclusion………………………………………………………………………………….37 References…………………………………………………………………………………..38 5 1. ABSTRACT Bladeless wind power generation uses a radically new approach to capture wind energy. The device captures the energy of vorticity, an aerodynamic effect that has plagued structural engineers and architects for ages (vortex shedding effect). As the wind strikes or passes the mast of the bladeless power generator, it will create vortex also known as the spinning motion of air. The vortex then exerts forces with certain frequency on the mast. When the frequency of the forces equals the natural frequency of the mast, resonance will occur and eventually the mast will vibrate and start oscillating. This phenomenon is known as Vortex Induced Vibration (VIV). The vibration of the mast will create kinetic energy and this energy will be transformed into electrical energy with the help of alternator. Naturally, the design of such devices is completely different from a traditional wind turbine. Instead of the usual tower, nacelle and blades, the device has a fixed mast, a power generator and a hollow, light weight and semi rigid fibreglass cylinder on top. This puts the technology at the very low range of capital intensity for such projects, it also makes it highly competitive not only against generations of alternative or renewable energy, but even compared to conventional technologies. Key words: Vorticity, Aerodynamic effect, VIV 6 2. INTRODUCTION The vortex flow wind turbine uses a radically new approach to capture wind energy. The device captures the energy of vortex, an aerodynamic effect that has troubled engineers and designers for a long period of time. As the wind bypasses a fixed structure, its flow changes and generates a cyclic pattern of vortices. Once these forces are strong enough, the fixed structure starts oscillating due to the vortices formed around the structure and spring placed at the bottom of the mast. The fundamental principle of our design is that instead of preventing the losses of this aerodynamic effect it maximizes the resulting oscillation and captures that energy. Naturally, the design of such device is completely different from a traditional turbine. Instead of the usual tower, blades, gear box and motor mounted on it, the device has fixed mast, spring to support mast on top of it, magnets, conductor coil(with proper insulation), charging circuit etc. Therefore the technology becomes at the very low range of capital investment, it also makes it highly competitive not only against generations of alternative or renewable energy, but even compared to conventional technologies. This proposal has been chosen due to its low initial setup cost, less maintenance, easy installation, easy to fabricate, use of vortex in flowing wind. The changes that it will bring about are the quick transportation unlike the conventional wind turbines. Construction and assembly are also simplified which are required for the wind industry. The impact on the life of birds will also be less since it won’t take as much space as the conventional wind turbine. There will also be significant impact on the efficiency of such turbines as it will have lesser components and so the losses will be less. We had theoretical knowledge of vortex concept i.e. a whirling mass of fluid or air which actually brings about loss to any moving object once it comes in vortex region, it tries to pull it towards the centre, so people whenever designed anything they always took vortex in a negative perspective. But we knew that moving vortex carries some momentum and energy with it, so we decided to use the energy of vortex for the oscillation of mast. 7 3. LITERATURE REVIEW The nature of the circulation regions around a bluff body in a cross flow can vary considerably from the normal von Karman vortex-shedding mode when subjected to external excitations. Krishnan et al.[1] correlated the spectral content and characteristics of the force coefficients for a square cylinder externally excited by inline sinusoidal pulsation, to near body vortical events. The effect of natural frequency of structure vortex induced vibration cylindrical structure in twodimensional unsteady flow studied by simulation of circular cylinder in cross flow conditions. Effect of natural frequency of structure on its vortex-induced vibration had been studied.[2] Numerical analysis of cylinder shows that maximum response occurs at frequency ratio close to unity and reduced velocity (inverse of the oscillator natural frequency) ranging 4-10. This zone is referred as lock-in zone. Sareen A et al. [3] in their paper discussed that the effect of transverse rotation on the vortex induced vibration response of sphere. The axis of rotation was perpendicular to the flow direction. Unlike cylinder, the VIV response of the sphere reduced gradually and steadily with increase in the rotation ratio. Khan N.B. et al. [4] discussed in their paper that – - large amplitude vibration through wake body synchronization. - Noble wake pattern under fixed rotation. Bourget R. et al. [5] observed that free oscillations of the rotating cylinder may also develop in the absence of vortex shedding. The symmetry breaking due to the rotation is shown to directly impact the selection of the higher harmonics appearing in the fluid force spectra. The rotation also influences the mechanism of phasing between the force and the structural response. D. J. Milborrow [6] in his article ‘Performance of arrays in wind turbines’ assesses the power produced from the cluster or array of traditional wind turbines and results from these studies are reviewed and compared and it is shown that there is reasonable agreement between the estimates for the power loss due to interactive effects in a cluster generating 1000 MW (about 25% is lost, if the rotors are spaced 10 m diameters apart). 8 4. OBJECTIVE Present technological advancement requires high demand of electricity. Also at the same time it is to keep in mind that due to high demand of electricity, environment must not be affected by more and more consumption of fossil fuels and coals. Since the availability of fossil fuel and coal is limited in nature. Therefore it is very much important to search for some alternative and renewable source of energy. Wind energy is available abundantly in the earth. Traditional wind turbines are the devices which extract energy from wind, however this proven set up has got some drawbacks. Firstly, it is not economical in view of installation, running and maintenance, secondly, substantial wind is required to rotate the blades, thirdly, heavy noise produced by rotor blades, which reduces the efficiency of the system, and also becomes vulnerable for the birds. It’s one of the areas that researchers and developers are looking to make more efficient so that a greater current of electricity can be produced at slower speeds. Our objective of the present study to design and fabricate a model that is able to generate electricity from wind energy as well as from different modes of vibration. The proposed model is easy to install and very economical. Also it can be placed over or near the area where vibration is present such as offshore, beside railway tracks, beside highways etc. The proposed model is having a very simple construction and made up of easily available materials. The model is based on fundamental principle of Von Karman vortex-shedding effect which states that when an oscillating flow takes place when a fluid such as, air or water flow past a bluff body at certain velocities, depending on the size and shape of the body. In this flow, vortices are created at the back of the body and detached periodically from either side of the body. Due to this effect, if any object placed in the direction of wind it oscillates. Due to relative motion between the upper and lower part of the model, any vibration from base also can be utilized to generate electricity through the alternator. Also, the proposed model can be designed in such a way so that not only the flow of fluid but also the other types of vibration (on shore, railway tracks, etc.) can be used to vibrate the mast. 9 5. WORKING PRINCIPLE 5.1 Vortex Shedding Effect: Vortex shedding is an oscillating flow that takes place when a fluid such as air or water flows past a bluff (as opposed to streamlined) body at certain velocities, depending on the size and shape of the body. In this flow, vortices are created at the back of the body and detach periodically from either side of the body. The fluid flow past the object creates alternating low pressure vortices on the downstream side of the object. The object will tend to move towards the low pressure zone if the bluff structure is not mounted rigidly and the frequency of vortex shedding matches the resonance frequency of the structure, then the structure can being to resonate vibrating with harmonic oscillations driven by the energy of the flow. This phenomenon is known as Vortex Induced Vibration (VIV). Figure1. Vortex shedding behind a circular cylinder 5.2 Von Karman Vortex Street: In fluid dynamics, a Von Karman vortex street is a repeating pattern of swirling vortices, caused by a process known as vortex shedding which is responsible for the unsteady separation of flow of a fluid around blunt bodies. Figure 2 : Von Karman street 10 5.3 Boundary layer separation: Boundary layer separation is the detachment of a boundary layer from the surface into a broader wake. Boundary layer separation occurs when the portion of the boundary layer closest to the wall or leading edge reverses in flow direction. The separation point is defined as the point between the forward and backward flow, where the shear stress is zero. The overall boundary layer initially thickens suddenly at the separation point and is then forced off the surface by the reversed flow at its bottom. Figure 3: Boundary layer separation Figure 4: Boundary layer separation in a cylindrical bluff body Figure 4 shows the flow past a circular cylinder, in an infinite medium. 11 Up to θ = 900 , the flow area is like a constricted passage and the flow behaviour is like that of a nozzle. Beyond θ = 900 the flow area is diverged, therefore, the flow behaviour is much similar to a diffuser This dictates the inviscid pressure distribution on the cylinder which is shown by a firm line in Fig.4. Here P∞ : pressure in the free stream , the cylinder. U∞ : velocity in the free stream and p : is the local pressure on 5.4 Faraday’s law of electromagnetic Induction: First law- First Law of Faraday's Electromagnetic Induction state that whenever a conductor are placed in a varying magnetic field emf are induced which is called induced emf, if the conductor circuit are closed current are also induced which is called induced current. Second law- Second law of Faraday’s law of electromagnetic induction state that the induced emf is equal to the rate of change of flux linkages. Figure 5: Electromagnetic Induction Mathematically, = - N d/dt , = BAcosө where, = Instantaneous induced voltages in volts , B= Magnetic field N = Number of turns in the coil , A= Area of coil = Magnetic flux in Webers, Ө=Angle between A and B t = Time in Seconds 12 6. WORKING METHODOLOGY 6.1 Basic components of the model i) Selection of mast- The mast that may be selected must fulfill certain requirements. The important properties are listed belowa) Light weight – The weight will play a significant role in the balancing of the whole device. Slight variation in weight may cause failure of the device. b) Rigidity- The mast must be having light weight but at the same time it must be rigid enough to sustain the pressure exerted on its surface by blowing wind. c) High heat transfer- The device would be in open and so it will experience a wide range of temperature. If the material is having high heat transfer capability, it would easily conduct heat to the surroundings. The perfect choice of material for the mast can be carbon fiber or any polymer. ii) Helical spring – Helical springs have been used to get lateral vibration. The springs have been chosen in accordance with the mass of the mast. The stiffness of the spring is a important factor and the mass of the mast will be adjusted according to the stiffness of the spring. Besides length of the active spring is also a important factor for oscillation. iii) Coil & Ring magnets - It is a part of tuning system and the current would be generated from the relative motion of coil and magnets. A series of magnets is used to enhance the current output. Figure 6 : Copper Coil Figure 7: Ring Magnet 13 6.2 Oscillation of Mast The working principle of the proposed model is based on fundamental principle of Von Karman vortex shedding effect. Vortex shedding phenomenon, unlike other dynamic phenomena such as fluttering or galloping are easily formed in circular section bodies. In the proposed model, the mast considered as solid body, if placed in wind flow, the wind would strike on the surface of mast. The vortex, usually present in the wind at higher altitudes will act on the periphery of surface and the wake vortex will detach periodically. After a certain point of time, the mast will start oscillating since the vortex carries some momentum with it. As the wind strikes or passes the mast of the bladeless turbine it will create vortex also known as the spinning motion of air. The vortex then exerts force with certain frequency on the mast. When the frequency of the forces equals the natural frequency of the mast, resonance will occur and eventually the mast will vibrate and start oscillating. This phenomenon is known as Vortex Induced Vibration (VIV).The vibration of the mast will create kinetic energy and this energy will be transformed into electrical energy with the help of alternator. For the proposed model, mathematical calculations is done for finding frequency and time period of the oscillation. Special care is taken for adjusting the center of gravity of the mast since any little imbalance can cause buckling of the mast. As the frequency of vortex shedding is proportional to wind speed which is not constant, we need a tuning system for a sustained and continuous vibration over a period of time. Two pairs of permanent magnets have been added to the damped harmonic oscillator. The same poles are facing each other. The oscillating mast has placed in between one pair of magnet at a distance of 230mm above the base and another is placed at a distance of 320mm from the base. Both pair of magnets are perpendicular to each other. Two pair of copper coil has mounted on hollow steel road and the centre of each pair of magnet and coil are collinear. The magnetic force that appears between two permanent magnets is inversely proportional to the square of the average distance between their poles, in a way that they behave like a compression spring with non-constant elasticity dependent on the displacement. The recent study started with basic observation of lateral spring mass movement and is found that there was a significant oscillations being observed during motion. So if the stand and light weight mast pivoted, such that it oscillates on its axis, that can drive the electrical alternator connected with it and a significant amount of electricity generated at the output. The current at output will be DC .By use of filters or rectifiers that can be changed to AC current which can be used at spot or may be kept in storage for future use. During design and development of the system the following two things have to be maintained. 1) At equilibrium the centre of gravity of the system should lie on the axis of the system. 2) The set-up should start oscillating with a minimal amount of air flow hitting the mast. Proposed model will be like the bottom portion of spring will be fixed to the base and hollow steel rod is placed above top portion of the spring , will support the mast.The spring, which will help in oscillating the mast as well as provide support for the rod to be straight. The proposed plan is technically feasible since it will utilize the maximum amount of wind energy from the surrounding to 14 produce electricity. When wind passes one of the cylindrical object, it shears off the downward side of the cylinder in a spinning whirlpool or vortex. That vortex then exerts force on the cylinder, causing it to vibrate/oscillate. This kinetic energy of oscillating cylinder can be converted to electricity through a linear generator similar to those used to harness wave energy. This wind generator generates electricity through systems of coil and magnet. During wind flow, if obstruction is created, wind energy is creating a natural vortex in way of the obstruction area. Due to which the obstruction (if kept fixed at the bottom, i.e. it will act as a cantilever) will create a random oscillation in the horizontal plane at top (say x-y plane). Faraday’s Law of electromagnetism has been used for generation of induced emf and the circuit is made closed for flow of current. Insulated copper coils are used during experiment in the Basic Physics Lab (at Asansol Engineering College, Asansol, West Bengal) up to 147.83mA current was generated with 4 coil of diameter 80 mm each with 160 turns and permanent magnet of magnetic strength of 37 Gauss. Also the experiment was conducted with improper insulation to cross verify the Faraday’s experiment. Based on the experiment, it was decided to make an array of system of coil and magnets to generate more electricity. Below is the list of components used in model:(A) Base: To provide strong foundation to mast. (B) Spring: To support the load acting on it and for oscillation of mast. (C) Mast: made up of glass fibre or polymer sheet due to its low weight. (D) Hollow steel rod – To support the mass. (E) Permanent ring magnets and Copper coil: For generating electricity. (F) Full wave rectifier: To convert the output a.c. current to d.c. (G) Charging circuit: The charging circuit use the micro controller which compare the generated voltage with a predefined value and controls the relays. The relays act as a switch which helps in charging only when power is adequate to charge the battery. (H) Battery: It stores the charge when power is being generated and gives power to any load connected to it. (I) Load: It can be anything, depends on how much power is stored. In our case, it’s LED bulb. The wind generator does not have any moving parts in contact, which eliminates the need for lubrication and reduces the wear and tear. The design completely eliminates mechanical elements that can suffer wear and tear due to friction leading to a reduction in maintenance cost compared to the conventional wind turbine with blades. There is a huge scope of scaling up the model geometrically, kinematically and kinetically with the help of dimensional and model analysis. The dimensional scale up will depend upon the height of installation of turbine. If it’s is installed on high rise buildings , even if the height of the mast is not more, higher output may be expected at higher elevation, where wind speed will be high. This project has three main advantages(1) Utilizing less area; (2) generation of green electricity; (3) economical. 15 Figure 8: Prototype of new model 6.3 Tuning system As assessed, the frequency of vortex shedding is proportional to the wind speed which is not constant. On the other hand, the range of wind velocities within the structure resonates is narrow due to the fact that the normal oscillation frequency of a structure is single one. To increase the number of equivalent working hours per year, we have to increase this range of useful wind velocities. An available strategy to increase the range of working wind velocities isTwo pairs of permanent magnets have been added to the damped harmonic oscillator. The same poles are facing each other. The oscillating mast has placed in between one pair of magnet at a distance of 230mm above the base and another is placed at a distance of 320mm from the base. Both pair of magnets are perpendicular to each other. Two pair of copper coil has mounted on hollow steel road and the centre of each pair of magnet and coil are collinear. The magnetic force that appears between two permanent magnets is inversely proportional to the square of the average distance between their poles, in a way that they behave like a compression spring with non-constant elasticity dependent on the displacement. As coils get closer to the respective magnets, the change in magnetic flux occurs. Thus, the output is optimized. 16 Figure 9: Tuning system Fig 10: circuit diagram showing orientations of magnets Fig 11: Circuit diagram showing magnetic field lines 17 6.4 Previous models 6.4.1 First Model The work started with this model. The material of the mast was a hard paper. The mast stood on a helical spring. There were certain drawbacks of this model which compelled us to review the concept again. We got output of 0.00325 watt power in one oscillation. This model has some drawbacks. The drawbacks werea) The dynamic balancing was not achieved which sometimes led to buckling. b) Bar magnets were used which were not fit to be used in this model. This led to the problem of positioning of magnets. c) The orientation was not proper for coil and magnets. Figure 12: 3D drawing of first model 18 6.4.2 Second Model The work started with this model. The material of the mast was a PVC polymer of thickness 0.75 mm. The mast stood on a helical spring. There were certain drawbacks of this model which compelled us to review the concept again. We got output of 0.02629 watt in one oscillation. We found drawbacks here also. The drawbacks werea) As there is a lack of proper shape and size of mast , required balance was not achieved. b) The orientation was not proper for coil and magnets. Figure 13: 3D drawing of first model 19 7. OBSERVATION TABLE Table 1: Table of Load voltage, Wind velocity and Displacement at constant load = 0.6 ohm 1. At Morning around 7:00 – 8:00 AM LOAD VOLTAGE (mv) WIND VELOCITY (m/s) 5.2 4.8 1.4 4.6 6.4 6.9 3.5 3.5 3.3 2.2 4.2 3.5 0.6 2.7 6.9 8.9 0.7 2.3 2.9 9.1 6.1 6.5 5.4 9.5 3.3 6.7 4.6 4.8 1.3 4.7 1.7 4.4 2.98 2.65 2.65 2.65 2.65 2.95 2.92 2.9 2.9 3.06 3.06 3.06 3.06 3.0.5 3.11 3.21 1.13 3.11 3.11 2.64 2.64 2.65 2.54 2.74 2.47 2.47 1.92 1.92 1.92 1.92 1.92 1.57 DISPLACEMENT (cm) 2 1.5 1.5 2 1.5 1.5 2 1.5 1.5 1.5 1.5 0.5 1.5 1.5 2 2 0.5 1.5 1.5 2.5 2 2 1.5 2.5 1.5 2 1.5 1.5 1.5 1.5 1.5 1.5 LOAD VOLTAGE (mv) WIND VELOCITY (m/s) 6.6 6.2 6 4.8 5.6 1.6 3.1 5.8 1.7 2.9 2.8 6.3 5.5 2.5 1.5 4.2 1.3 7.5 1.8 5.5 0.7 2.3 2.9 1.8 2.2 3.4 2.8 6.3 7.6 1.1 6 2.9 2.93 2.63 1.93 1.83 1.93 1.93 1.53 2.25 1.92 1.92 2.36 2.36 2.36 2.36 2.36 2.35 2.35 2.35 1.97 1.97 1.97 2.17 2.17 2.17 2.45 2.45 2.00 2.45 2.45 2.45 2.45 2.57 20 DISPLACEMENT (cm) 2 2 1.5 1.5 2 1.5 1.5 2 1.5 1.5 1.5 2 2 1.5 1.5 1.5 1.5 2 1.5 2 0.5 1.5 1.5 1.5 1.5 1.5 1.5 1.5 2 15 2 1.5 3.2 1.57 1.5 3.9 2.57 1.5 4.7 4.7 39.1 15.2 16.5 15.5 15.4 22.8 2.5 6.9 7.2 10.5 2.1 7.4 17 11.8 12.1 15.8 7.7 9.3 7.5 2.5 3.1 2.6 9.7 6.9 2.9 1.5 7 18.6 12.2 4.9 7.7 7 3.6 1.4 6.4 15.2 16.5 15.5 15.4 3.5 3.4 3.6 3.4 2.6 3.6 3.5 3.4 3.26 3.26 3.26 3.11 3.11 2.39 3.59 3.53 3.79 3.79 3.79 3.79 3.14 3.14 3.14 3.14 3.22 2.22 2.65 2.65 3.99 2.62 2.16 2.16 2.27 2.27 2.79 2.79 2.79 2.75 2.75 2.75 2.75 1.5 1.5 5.5 3.5 3.5 3.5 3.5 5 1.5 2 2 2.5 1.5 2 4.5 2.5 2.5 3.5 2 2.5 2 1.5 1.5 1.5 2.5 2 1.5 1 2 4.5 2.5 1.5 2 2 1.5 1 2 3 3 3.5 3.5 2. At Evening around 5:00 – 6:00 3 0.8 5 7.3 3.6 4.8 2.9 1.7 2.2 6.5 2.8 3.01 9.2 5.2 2.5 3.1 4.3 1.7 5 1 4.8 2.8 2.1 4.5 3.2 8 3.5 8.1 4.5 8.9 4.8 5.3 2.7 2.9 2.1 3.1 14.7 11.2 16.8 20.7 26.8 3.5 3.4 3.6 3.92 3.92 3.92 3.92 3.92 3.13 3.53 2.3 2.3 2.3 2.3 2.3 3.46 3.46 3.38 3.38 3.38 3.37 3.2 3.2 3.52 3.52 2.52 3.52 3.52 2.62 3.65 3.65 3.65 3.55 3.55 3.55 2.6 2.85 2.35 2.2 3.02 3.5 1.5 0.5 2 2 1.5 1.5 1.5 1 1.5 2 1.5 1.5 2.5 2 1.5 1.5 1.5 0.5 2 0.5 1.5 1.5 1.5 1.5 1.5 2.5 1.5 2.5 1.5 2.5 2 2 1.5 1.5 1 1.5 3.5 2.5 3.5 4.5 5 21 6.5 15.7 27.7 16.8 9 8.9 3.1 1.3 6.2 0.84 7.8 17.6 4.7 39.1 32.1 35.5 34.3 7.8 9.6 19.6 9.2 9.3 13.4 2.05 2.3 3.01 2.56 2.25 2.25 2 2 2.5 1.25 3.25 2.26 2.01 4.52 4.52 4.52 4.52 2.51 2.52 3.01 2.05 2.05 2.75 2 3.5 4 3.5 2.5 2.5 1.5 0.5 2 0.5 2 3.5 1.5 5.5 5 5.5 5.5 2 2.5 4 2 2.5 2.5 22.8 12.8 15 16.5 25.5 13.5 46 3.9 4.3 5.8 14.5 16.5 19.4 16.5 20.5 12.6 14.6 15.8 20.5 19.6 15.8 0.4 2.6 2.52 2.52 2.52 2.52 3.25 2.52 4.62 2.52 2.52 1.75 2.45 3.45 2.45 2.45 3.56 2.56 2.51 2.5 3.45 2.46 2.45 2.65 2.65 Table 2: Table of no of oscillation, time, time period No of Oscillation 20 Time taken(sec) 21 26 14 21.9 24.8 31.8 25 29.2 16.2 19.4 45.4 26.9 17.5 18.9 16.7 Time period 1.2 1.34 0.7 1.095 1.24 1.59 1.25 1.46 0.81 0.97 2.27 1.34 0.86 0.945 0.835 22 4 2.5 3 3.5 5 3 5.5 3.5 1.5 2 3 3.5 3.5 3 4 2.5 2.5 3.5 5 4 3.5 3.5 1.5 27.9 21.6 27 28 16.2 19 18.3 26.8 27 27.3 18.9 15.2 19.6 27.8 1.44 1.08 1.35 1.28 0.84 0.96 0.915 1.34 1.42 1.45 0.945 0.6 0.97 1.39 Table 3: Table of wind velocity and current WIND VELOCITY CURRENT 0.3 1.2 0.5 2.2 0.5 3.5 0.5 2.5 0.51 3.0 0.52 3.8 0.6 19.5 0.61 20.8 0.65 9.3 0.84 27.5 0.84 19.2 0.84 12.8 0.88 3.2 0.89 5.7 0.88 1.8 WIND VELOCITY CURRENT WIND VELOCITY CURRENT 0.92 2.8 1.26 16.8 0.97 25.8 1.26 28.3 0.97 12.7 1.26 1.8 0.98 15.2 1.26 27.0 1.04 12.5 1.26 19.3 1.05 10.5 1.26 9.0 1.06 4.5 1.28 18.2 1.06 28.0 1.28 15.8 1.06 1.0 1.28 12.7 1.13 1.2 1.28 20.2 1.13 3.7 1.28 13.3 1.15 14.3 1.28 6.3 1.18 21.6 1.28 3.8 1.2 4.7 1.28 4.2 1.2 3.5 1.29 6.8 23 0.88 2.7 0.92 12.2 0.92 6.0 0.92 8.0 0.92 4.8 0.92 3.8 1.2 14.8 1.3 4.7 1.22 1.6 1.3 5.0 1.24 3.5 1.3 15.3 1.25 1.4 1.3 8.7 1.25 13.0 1.3 4.2 1.25 1.3 1.3 15.3 Table 4: Table of oscillating frequency and induced emf OSCILLATING FREQUENCY INDUCED EMF 11.5 0.47 13.1 7.5 1.6 9.1 7.7 3.6 7.6 6.1 11.7 0.62 3.4 7.3 15.5 3 16.5 16.8 1.7 1.3 1.9 0.8 0.3 2.9 0.6 5 1.1 4.8 2.7 0.44 0.63 0.68 0.69 0.69 0.70 0.75 0.75 0.75 0.77 0.80 0.81 0.83 0.83 0.83 0.98 1.03 1.03 1.04 1.11 1.16 1.19 1.19 1.19 1.19 1.23 1.25 1.43 1.67 24 Table 5: Table of wind velocity and oscillating frequency WIND VELOCITY 0.4 0.5 0.5 0.5 0.52 0.52 0.6 0.6 0.6 0.84 0.84 0.84 0.89 0.89 0.89 0.89 0.92 0.92 0.92 0.92 0.92 1.05 1.19 1.25 1.27 1.29 1.30 1.32 1.35 1.94 2.56 3.25 4.54 5.0 5.5 OSCILLATING FREQUENCY 0.44 0.63 0.68 0.69 0.69 0.70 0.75 0.75 0.75 0.77 0.80 0.81 0.83 0.83 0.83 0.98 1.03 1.03 1.04 1.11 1.16 2.12 2.59 3.19 4.59 5.23 7.25 9.43 11.58 17.008 28.311 55.670 110.675 125.756 130.388 Some collected avg. data from above observations table 25 Table of Load Voltage, Wind Velocity, Current and Induced EMF Resistance=0.6Ω S.L. No. Load voltage (mV) Wind velocity (m/s) Current (mA) Induced Emf (mV) 1 5 2 7.5 0.5 3.5 0.981 5.7 2.933 5.3 0.89 1.35 3 12.5 3.527 4 15.2 1.58 15.36 4.525 5 1.3 1.94 20.36 7.56 6 16.8 2.56 25.625 10.56 7 1.9 3.25 30.16 20.36 8 1.8 4.54 32.6 37.4 9 5.5 5.0 9.28 28 10 5.7 5.5 9.5 25 Table of Induced EMF and Oscillating frequency S.L. NO. INDUCED EMF (mV) OSCILLATING FREQUENCY (Hz) 1 0.0 1.072 2 0.6 9.778 3 2.4 11.58 4 4.0 13.889 5 6.5 17.008 6 9.4 28.311 7 15.7 55.670 8 23.8 110.675 9 28.5 125.756 10 39.1 130.388 Table of Oscillating frequency and wind velocity 26 S.L. NO. OSCIILATING FREQUENCY(Hz) WIND VELOCITY(m/s) 1 1.072 0.5 2 9.778 3 11.58 0.89 1.35 4 13.889 1.58 5 17.008 1.94 6 28.311 2.56 7 55.670 3.25 8 110.675 4.54 9 125.756 5.0 10 130.388 5.5 Variation of Induced Emf with Wind Velocity 40 Induced Emf (mV) 35 30 25 20 15 10 5 0 0 1 2 3 4 5 6 Wind velocity (m/s) Fig 14: Variation of induced emf with wind velocity for a particular spring 27 Variation of current with wind velocity 40 35 Current(mA) 30 25 20 15 10 5 0 0 1 2 3 4 5 6 Wind velocity (m/s) Fig 15: Variation of generated current with wind velocity for a particular spring Variation of induced emf with oscillating frequency 45 (mv) 35 Induced emf 40 25 30 20 15 10 5 0 0 20 40 60 80 100 120 140 Oscillating frequency (hz) Fig 16: Variation of induced emf with oscillating frequency for a particular spring 28 Variation of Oscilating Frequency with Wind Velocity) Osciilating frequency(hz) 140 120 100 80 60 40 20 0 0 1 2 3 4 5 6 Wind velocity(m/s) Fig 17: Variation of oscillating frequency with wind velocity for a particular spring Calculation of power generated in one oscillation: Average Velocity, vavg= 2.90 m/s Average current, I = 14.63mA Resistance of one coil = 0.6 Ω Total no. of coils = 04 Total resistance, R = 2.4 Ω Power generated (P) = I2 R = 0.0005137 W (approx.) 8. MATHEMATICAL CALCULATION Kinematic equation of motion of mast; Let, x=displacement of mast in horizontal direction t=time period of oscillation g=acceleration due to gravity l=length of mast k=spring constant 29 m=mass of mast When force applied on the mast, then it deflects in other side due to weight of the mast but due to spring it deflects in another side and thus oscillating motion takes place. Balancing the forces; Bending force (force due to wind + force due to mast weight)-Restoring force (spring force) = 0 𝑑 𝑥 𝑑𝑡 + 𝑑 𝑥 𝑥− 𝑥 =0 + 𝑎𝑥 − 𝑏𝑥 = 0 𝑑𝑡 and b = Here, a = Let, v= Then, 𝑑 𝑥 𝑣 𝑑𝑣 𝑑𝑥 =𝑣 𝑑𝑡 𝑑𝑣 𝑑𝑥 + ax-bx2=0 V.dv= (bx2-ax).dx 𝑣 𝑏𝑥 𝑎𝑥 = − +𝑐 2 3 2 At, t=0, x=0 Therefore v=0, c=0 𝑣 𝑏𝑥 𝑎𝑥 = − 2 3 2 Putting, v= 𝑑𝑥 √2𝑏 = √𝑥 − (√𝑎)𝑥 𝑑𝑡 3 𝑑𝑥 √2𝑏 3 √𝑥 − (√𝑎)𝑥 𝑑𝑥 √2𝑏 𝑥 − (√𝑎)𝑥 3 √ √ ∫ √ √ (√ ) * √ = 𝑑𝑡 = √ (√ ) √ (√ ) 30 𝑑𝑡 =∫ 𝑑𝑡 √2𝑏 𝑥 + √𝑎 𝑥. 𝑑𝑥 3 √ 2𝑏 𝑥 − 𝑎𝑥 3 √ √ ∫ √ ∫ √ √ 𝑑𝑡 .dx=∫ 𝑑𝑡 √ . 𝑑𝑥+∫ = 𝑑𝑥 = ∫ 𝑑𝑡 Solving 1st part of equation √2𝑏 𝑥 3 √ 2𝑏 𝑥 − 𝑎𝑥 3 . 𝑑𝑥 √ =∫ . 𝑑𝑥 √ √ =∫ √ ( ) . 𝑑𝑥 Let, x=t2 Then, dx=2t.dt . =∫ . . 𝑑𝑡 =√ ∫ =√ * =√ * ∗ ln +c1 √ +c1 ln √ Solving 2nd part of the equation 3 √2𝑏 𝑑𝑥 3𝑎 𝑥 − 𝑥 2𝑏 =∫ √ 𝑑𝑥 31 3 𝐴 𝐵 √2𝑏 = + 3𝑎 𝑥 𝑥 − 3𝑎 𝑥 𝑥− 2𝑏 2𝑏 Solving above equation A=- √ And, B= 3 √2𝑏 𝑑𝑥 = 3𝑎 𝑥 𝑥− 2𝑏 ∫ √ −√2𝑏 𝑎 𝑑𝑥 + 𝑥 √ 𝑑𝑥 = √ ln 𝑥 + √ √2𝑏 𝑎 𝑑𝑥 3𝑎 𝑥− 2𝑏 ln(𝑥 − )+C2 Therefore, 𝑑𝑥 𝑑𝑡 = t=√ * ln √ √ √2𝑏 𝑥 − (√𝑎)𝑥 3 √ + √ ln 𝑥 + √ ln(𝑥 − )+C3 Where C3 is constant of integration 9. APPLICATIONS The developed equipment can be brought to use at many places such as – Outdoor lighting – for lighting up streets, parks etc. For auxiliary purpose. It can be installed at on-shore and off-shore where there is significant vibration from any source. For pumping water at higher altitude for irrigation purpose. It can be stored for future use or can be send to power grid. It can be installed beside railway tracks. It can also be used to some extent in very small scale industries for some work. It can also be installed on either sides of roads in highways etc. It can be used in remote areas with high air flow and vibration, where a lesser amount of electricity is available. 32 10. ADVANTAGE The impact on the bird population is expected to be much smaller Reduction in maintenance costs compared to traditional wind turbine and easy installation It does not have moving parts in contact, which eliminates the need for lubrication and reduces the wear and tear. Since, it is lighter in weight, transportation would be easier. 11. FUTURE SCOPE OF WORK To scale up the model dimensionally for increase in power output. To study the CFD analysis of the model and working on every component precisely and optimizing it. To do testing for power output in an open field. To form cluster or array of similar models and install it together for increase in net power output. In a study by D.J. Milborrow, he assessed that there is a loss in power output (about 25% of the total output) if the rotors diameter is less than 10 m and they are placed together. On basis of this study, we are concluding that since our model doesn’t have any rotors like in traditional wind turbine, there won’t be any loss in power output. Instead the net output may increase in array as in the below figure it can been seen that the pathline of the breeze is such that the shedding which is formed at the first device will go on increasing and in the last row, the vortex shedding will be maximum. Figure 18: An array of system 33 12. FEW SNAPS OF OBSERVATION OF OUR MODEL 34 13. CONCLUSION Today, there are lot of research and study going on across the globe in renewable energy sector. This is the sector which is also growing at very fast rate. May be today the purpose of electricity generation is being fulfilled with fossil fuels and natural gases. But it is need of the hour where we have to realize that with the increase in power consumption and introduction of automation across all the sectors, we have to leverage the sources of electricity generation. In this regard wind energy can become a significant source of unlimited power generation. The major contribution of our model is that it can give us significant power generation with less occupying area, less number of components and can even work under low average wind speed. The allure of the model is its wide range of installation points. It can be installed on the sides of highways, besides railway tracks and can also be installed on the off-shore. For its optimization the model can be scaled up dimensionally and the strength of components can be varied accordingly. As of now we are not aiming to increase the power output, rather focus on auxiliary demands and for household purposes. To conclude, this developed model can become challenging in the power sector of India if proper scaling up is done. 35 REFERENCES 1. Krishnan H, Agrawal A, Sharma A, Thompson M, Sheridan J, Characteristics of force coefficients and energy transfer for vortex shedding modes of a square cylinder subjected to inline excitation. Journal of Fluids and Structures 2018; 81:270-288. 2. 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