45

Final presentation( sajjad)

Embed Size (px)

Citation preview

  1. 1. Group members Roll NO.Sajjad Ahmed ( Group leader) 26Ghulam Sarwar 14Nasir Ali 07Abdul Baqi 09Shoaib Ahmed 23Shafique Rehman 01Project advisor: Engr. Bashir Ahmed Leghari
  2. 2. Overview The engine used for the demonstration of Stirling cycle inthe thesis presented in Department of MechanicalEngineering BUET Khuzdar during 2011 was operated byCNG/LPG gas. we wanted to operate that with direct solarradiation using concentrating convex lens.
  3. 3. Introduction Convex lens is used to converge the solar radiation to a singlepoint so that high amount of heat energy is obtained. This heat energy is used to heat the displacer cylinder of thestirling engine. When the air inside the cylinder is heated its pressure increasesthat pushes the displacer. The displacer is connected to theflywheel by the help of a connecting rod. The reciprocating motion of the displacer is converted intorotational energy of the flywheel by the help of crank. This mechanical energy can further be used to produce electricpower.
  4. 4. Objective Of the StudyThe objective of this project is closely linked to the energyproblem with a specific focus on electricity generation usingsolar power To reduce the Grid dependence by building a residentialbased cost effective and renewable power supply. To provide for relief work in disaster affected areas likeearthquake, flood etc. To avoid burning of fossil fuel for power generation andprovide a environment friendly power technology.
  5. 5. Solar Energy Solar energy is the heat energy obtained from the Sun In sheer size, solar energy has the potential to supply allenergy needs: electric, thermal, transportation etc It is regarded as the solution for reducing the use of fossiland nuclear fuels and for a cleaner environment. Solar energy is very diffuse and is scattered, it therefore,needs systems and components to capture and concentrateit efficiently for conversions to any of the uses.
  6. 6. Solar-Electric Conversion SystemsThere are many differenttypes of solar energysystems that will convert thesolar resource into a usefulform of energy. CSP systems use lenses ormirrors and tracking systemsto focus a large area ofsunlight into a small beam. PV converts light intoelectric current using thephotoelectric effect.
  7. 7. Concentrated Solar PowerConcentrated solar power (CSP) technologies use lens ormirrors to reflect and concentrate sunlight onto receivers.The receivers collect the concentrated solar energy andconvert it to high-temperature heat that can drive either heat engine domestic heating create steam to drive a turbine desalination
  8. 8. Different CSP techniquesSolar Parabolic TroughFresnel lensConcentrated Photovoltaic
  9. 9. Cont Solar Power Tower Solar Dish-EngineSystems
  10. 10. Stirling Engine A Stirling engine is a heat engine operating by cycliccompression and expansion of air or other gas. Theworking fluid, at different temperature levels such thatthere is a net conversion of heat energy to mechanicalwork. The external combustion aspect enables a Stirling Engineto operate equally well on multiple types of fuel, such asnatural gas, gasoline, diesel, or even heat from the sun
  11. 11. Cont The Stirling engine is notedfor its high efficiency (up to40%). It operates Quietly and theease with which it can usealmost any heat source. In this case the sun's heat isused for operating the engine. Stirling engine is a closed-cycleregenerative heatengine permanently workingon gaseous fluid.
  12. 12. Stirling engine configurations Alpha enginesIt has two pistons inseparate cylinders which areconnected in series by aheater, regenerator andcooler. Seals are provided on boththe hot and cold pistons toprevent the escape of gasfrom the engine cylinders.
  13. 13. Cont Beta Engines The Beta engine has both thedisplacer and the piston arein the single cylinder.A beta Stirling has a singlepower piston arranged withinthe same cylinder on thesame shaft as a displacerpiston.
  14. 14. Cont Gamma Engines A gamma Stirling engineis simply like a beta typebut the power piston ismounted in a separate cylinderadjacent tothe displacer piston cylinder. both pistons are connected tothe same flywheel. The gas in the two cylinderscan flow freely between them.
  15. 15. Operation /working cycle 1-2 const. Volume heating 2-3 isothermal expansionof the gas 3-4 const. Volume coolingof the gas. 4-1-Iso thermalcompression of the gas.
  16. 16. Major Components of the StirlingEngine Displacer- To shift the volume of gas from one end ofcylinder to an other. Power Piston - The work of the power piston is tocompress the gas at low temperature to expansion space. Bush - Used to align the displacer rod and connecting rod. Flywheel - It is used to store energy during theexpansion of displacer and provide the same energyduring compression to the power piston. Sealing- To reduce leakage of gas and maintaining thepressure.
  17. 17. Cont Regenerator- It captures the heat from the gas afterexpansion and provide this heat to the gas when it movesfrom cold end to the hot end of the engine. Connecting rods- It transmits the mechanical work of thedisplacer to the flywheel. Cooling fins- Fins are made over the cold end displacercylinder for dissipation of heat to the sink. Pressure Regulating Screw- It is used to regulate thepressure.
  18. 18. The Solar Concentrator It is used to refract light, converging the beam. A simple lens consists of a single optical element. A compound lens is an array of simple lenses (elements)with a common axis. The use of multiple elements allowsmore optical aberrations to be corrected than is possiblewith a single element.
  19. 19. Types of simple lenses Lenses are classified by the curvature of the two opticalsurfaces.
  20. 20. Convex Lenses Typically made of glass or transparent plastic, a convexlens has at least one surface that curves outward like theexterior of a sphere. it is the most commonly used. A convex lens is also known as a converging lens. Aconverging lens is a lens that converge rays of light thatare traveling parallel to its principal axis
  21. 21. Concentration of light throughconvex lens
  22. 22. Site Characteristic This residential based power generation system ismade for the District Khuzdar. The overall directnormal solar radiation in Pakistan is shown:
  23. 23. Geographic location of Khuzdar Geographic coordinates of Khuzdar, PakistanLatitude: 27.74N , Longitude: 66.64EElevation above sea level: 1218 m = 3996 ft
  24. 24. Average monthly climate conditions forThe year 2012 in KhuzdarMonths T TM Tm PP V VMJan 10.1 17.1 2.4 14.74 2.1 6.7Feb 11.7 19.6 3.8 0 3.8 9.4March 19.6 26.1 10.8 13.97 4.5 12.4April 24.1 29.7 17 27.17 5.2 13.7May 29.8 36.4 22.6 23.88 5.7 15.1June 31.5 37.5 24.3 2.03 7.1 17.4July 32 38.9 24.7 5.33 5.4 15Aug 32 37.5 25.6 1.02 1.5 12.7Sep 26.7 32.4 20.7 54.09 3.5 12.8Oct 22.9 30.5 13.9 0.76 4.9 14.4Nov 18.1 25.8 9.3 0 4.4 13.4Dec 12.5 19.4 4.5 25.91 2.7 10.2
  25. 25. Solar Parameters The solar parameters are taken for 3rd july inselected site where the maximum temp is 41.5 C LabelsHGloCS- Horizontal clear sky Global RadiationHDifCS- Horizontal clear sky Diffuse RadiationHBmCS- Horizontal clear sky Beam RadiationThe sum of the diffuse and beam irradiance isequal to the global irradiance.
  26. 26. Legal Time HGloCS W/m2 HDifCS W/m2 HBmCS W/m206am 14 11 307am 192 43 14908am 432 69 36409am 660 90 57010am 852 107 74511am 990 119 87212noon 1067 125 942
  27. 27. Legal Time HGloCS W/m2 HDifCS W/m2 HBmCS W/m201pm 1076 126 95002 pm 1016 121 89503 pm 892 110 78204 pm 713 95 61805 pm 492 75 41806 pm 252 50 20107 pm 42 20 22
  28. 28. Design Specifications Our objective is to operate the stirling engine andproduce electric power using solar energy by thehelp of convex lens to avoid the use of fossil fuelsand develop a renewable energy technology. Since the amount of heat energy produced by aconvex lens is comparatively less than that of fossilfuels so we had to make the design changed. Theparameters that we worked on are as follows:
  29. 29. Data for the Already ExistingStirling EngineDimensions and temperature data Inner diameter of displacer cylinder, Di = 32mm Length of stroke, l = 36mm Temperature of source, T1= 250C0 Temperature of sink, T2 =100C0 Swept Volume, Vs=28.95X10-6 m3 Clearance Volume, Vc = 8.84X10-6 m3 Compression ratio, r = Vs/Vc = 3.27 Total Volume, Vt = Vc + Vs= 37.74X10-6 m3
  30. 30. Cont Heat Rejected to Sink, Q4-1=-126.99KJ/Kg(Compression) Heat supplied from hot source, Q2-3 = 177.80 KJ/Kg Net work done, Wn= Heat supplied heat rejected=50.81 KJ/Kg Efficiency, = 28.6 % Minimum Speed (at the start) = 80 r.p.m Maximum Speed (at the peak revolutions)= 422 r.p.m
  31. 31. Design Specifications Hot side temperature T1 Cold End temperature T2 Swept Volume Vs Clearance volume Vc Compression ratio r Heat rejected to the sinkQ4-1 Heat supplied to the hot end,Q2-3 Reduce Losses ( Leakage,conduction and convection)
  32. 32. ContHot side temperature ( T1) Since T1 depends on heat energy supplied from thesource. It depends on the solar concentrator (lens).Like: Area of the lens No of lens Concentration ratio
  33. 33. ContCold end temperature (T2) The cold end temperature is reduced by increasing the finsurface area and number of fins to increase the heatdissipation.Swept Volume (Vs)Vs =(/4) D2lD = inner diameter of the displacer cylinderl = length of strokeIncreased swept volume by increasing the Diameter of displacer and lengthof stoke.
  34. 34. ContClearance volume (Vc)Vc =(/4) D2 l1l1= clearance lengthBy reducing the clearance length l1 we reduced theclearance volume.Heat supplied to the hot side(Q2-3)Q2-3 = R T1 ln ( Vs/Vc)By increasing T1, Vs and decreasing Vc the amount of heatenergy supplied is increased.
  35. 35. Reduce Losses Leakage losses- Air leakage is a big problem at theheating section. To prevent leakage we used O-Ringsbetween support collar and expansion cylinder. Conduction lossesTo reduce conduction losses the heat cap and thedisplacer cylinder is made as thin as possible. Convection lossesConvection from hot side to the surrounding is verydifficult to stop but by placing the engine in a certainarea where the natural air circulation is comparativelylow the convection loss of heat is prevented.
  36. 36. Modified design specificationInner diameter of the displacer cylinder, Di = 48.5mmLength of stroke, l = 38 mmClearance length , l1 = 10 mmHot end Temperature, T1 = 200CCold end temperature, T2 = 50CSwept volume, Vs = 70.2x10-6 m3Clearance volume, Vc = 18.5x10-6 m3Total volume, Vt = 88.7x10-6Compression ratio, r = Vs/Vc = 3.80Heat supplied to hot end Q2-3 =180.8 KJ/KgThen heat rejected to the sink, Q4-1= -123.7 KJ/KgNet Work done Wn = 57.1 KJ/KgThermal Efficiency of the engine =31.7%
  37. 37. Solar concentratorFor concentrating the solar energy onto the receiving section of thestirling engine to heat it up we used convex lens. Parameters for theconvex lens are given below:Type of lens used is biconvexDiameter of the lens, d= 130 mmFocal length, L = 20cmArea of lens, A= (/4) d2= 0.0153m2Diameter of the beam at the focal point, di = 10 mmConcentration ratio, C = d/di= 130/10 = 13
  38. 38. ContIn our site selected ( Khuzdar) the average horizontal clear sky Global irradiancefrom 7.am to 6.pm is calculated to be=720 W/m2The amount of solar radiation intensity that can strike our lens is:= 720x area of the lens=720x0.0153= 11.01 W/ lensSince the concentration ratio is,C= 13then the amount of solar energy produced by the lens at the focal point is=11.01x13= 143.2 W/lens
  39. 39. Test ResultsTime HGloCS W/m2Temperature at hotend (C0)Angular Speed(RPM)Thermaleffiiency7:00 am 192 17 0 08:00 am 432 20 0 09:00 am 660 72 150 6.3%10:00 am 852 180 180 28.6%11:00 am 990 191 262 30.0%12:00 pm 1067 195 280 30.9%1:00 pm 1076 199 303 31.5%2:00 pm 1016 197 250 31%3:00 pm 892 194 230 30.7%4:00 pm 713 140 175 21.7%5:00 pm 492 124 65 18.6%6:00 pm 252 65 0 4.43%
  40. 40. Test Results
  41. 41. Test Results
  42. 42. ConclusionOld Design Modified Design Source of energy inputFossil fuel Net work doneWn = 50.81 KJ/Kg Thermal efficiency = 28.6 % Source of energy inputDirect solar thermal energy (convex lens) Net work doneWn = 57.1 KJ/Kg Thermal efficiency = 0.317 = 31.7%
  43. 43. Future RecommendationThe following recommendations are given for futurework:- That the Fresnel lens which is made of plastic can be moresuccessful. That it is also recommended that helium gas is usedinstead of air due to its better thermodynamic properties. The overall efficiency can be improved, if increase the sizeof the lens used in the system. The efficiency of the system can be improved by usingautomatic tracking.