{ "metadata": { "name": "" }, "nbformat": 3, "nbformat_minor": 0, "worksheets": [ { "cells": [ { "cell_type": "heading", "level": 1, "metadata": {}, "source": [ "Chapter 5:DC Motor Drives" ] }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.1 ,Page no:75" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\n", "\n", "#Variable declaration\n", "T=10.0 #[turns]\n", "Coil=144.0 #[no. of coils]\n", "R=0.011 #[Resitance] ohm\n", "fi=0.05 #Wb(flux per pole)\n", "N=200.0 #[Speed] rpm\n", "par_paths=2.0 #[Parallel paths] for wave winding\n", "\n", "#Calculation\n", "T_path=Coil*T/par_paths #no. of turns in each parallel path\n", "R_path=R*T_path #ohm\n", "Ra=R_path/par_paths #ohm(armature resistance)\n", "p=12.0 #poles\n", "emf=par_paths*Coil*T*p*fi*N/60.0/2.0 #V\n", "R1=1000.0 #ohm\n", "IL=emf/R1 #A\n", "Ia=IL #A\n", "T=par_paths*Coil*T*p*fi*Ia/2.0/math.pi/par_paths #N-m\n", "\n", "#Result\n", "print\"(a) Armature resistance : \",Ra,\"ohm\"\n", "print\"(b) Torque: \",round(T,2),\"N-m\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "(a) Armature resistance : 3.96 ohm\n", "(b) Torque: 396.03 N-m\n" ] } ], "prompt_number": 1 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.2 ,Page no:75" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "Ia=110.0 #[Armature current] A\n", "V=480.0 #[Volatge] volt\n", "Ra=0.2 #[Resistance] ohm\n", "p=6.0 #[poles]\n", "C=864.0 #No of conductors\n", "fi=0.05 #Wb[(flux per pole)]\n", "\n", "#Calculation\n", "back_emf=V-(Ia*Ra) #Volt\n", "N=back_emf*60.0*p/C/p/fi #rpm\n", "T=C*p*fi*Ia/2.0/math.pi/p #N-m\n", "\n", "#Result\n", "print\"Speed : \",round(N,1),\"rpm\"\n", "print\"Torque: \",round(T,1),\"N-m\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Speed : 636.1 rpm\n", "Torque: 756.3 N-m\n" ] } ], "prompt_number": 2 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.3 ,Page no:79" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "Ia=100.0 #[Current] A\n", "V=200.0 #[Voltage] volt\n", "N=600.0 #[Speed] rpm\n", "Ra=0.05 #[Resistance] ohm\n", "Eff=85.0/100.0 # [Efficiency]\n", "\n", "#Calculation\n", "Ia1=Ia*Eff #armature current in separately excited dc motor\n", "emf=V-Ia*Ra #V(motoring mode induced emf)\n", "N1=500.0 #rpm(generating mode speed)\n", "Gen_emf=emf*N1/N #V\n", "Vo=round(Gen_emf)-Ia1*Ra #V\n", "\n", "#Result\n", "print\"Voltage of source : \",Vo,\"V\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Voltage of source : 158.75 V\n" ] } ], "prompt_number": 3 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.4 ,Page no:79" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "Ia1=10.0 #[Current] A\n", "V1=200.0 #[Voltage] volt\n", "N1=1800.0 #[Speed] rpm\n", "Ra=0.6 #[Resistance] ohm\n", "Rfield=360.0 #[Field resistance] ohm\n", "V2=180.0 #[Voltage] volt\n", "I_line=20.0 #[Limit line surrent] A\n", "\n", "#Calculation\n", "#fi2=V2/V1*fi1\n", "fi2BYfi1=V2/V1 \n", "#Ia1*fi1=Ia2*fi2\n", "Ia2=Ia1/fi2BYfi1 #A\n", "Eb1=V1-Ia1*Ra #V\n", "Eb2=V2-Ia2*Ra #V\n", "#Eb1/Eb2=fi1*N1/fi2/N2\n", "N2=N1/(Eb1/Eb2*fi2BYfi1) #rpm\n", "Ifield=V2/Rfield #A\n", "Ia=I_line-Ifield\n", "#V2=Ia*(R+Ra)\n", "R=V2/Ia-Ra #ohm\n", "\n", "#Result\n", "print\"(a) Motor speed after supply voltage decreases : \",round(N2,2),\"rpm\"\n", "print\"(b) Additional resistance is: \",round(R,2),\"ohm\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "(a) Motor speed after supply voltage decreases : 1786.94 rpm\n", "(b) Additional resistance is: 8.63 ohm\n" ] } ], "prompt_number": 4 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.5 ,Page no:80" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "Ia1=10.0 #A\n", "V1=200.0 #[Supply voltage] volt\n", "N1=1800.0 #[Motor speed] rpm\n", "Ra=0.6 #[Resistance] ohm\n", "Rfield=360.0 #[Field resistace] ohm\n", "V2=180.0 #[Voltage] volt\n", "I_line=20.0 #[Limit line current] A\n", "\n", "#Calculation\n", "Ia=Ia1-V1/Rfield #A(At changeover time)\n", "emf=V1-Ia*Ra #volt\n", "Ifield=emf/Rfield #A(At changeover time)\n", "Iout=Ia1-Ifield #A\n", "Rbraking=emf/Iout #ohm(Braking Resistance)\n", "\n", "#Result\n", "print\"Braking resistance : \",round(Rbraking,3),\"ohm\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Braking resistance : 20.542 ohm\n" ] } ], "prompt_number": 5 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.6 ,Page no:80" ] }, { "cell_type": "code", "collapsed": false, "input": [ "from scipy import integrate\n", "import math \n", "#Variable declaration\n", "Ia1=10.0 #[Current] A\n", "V1=200.0 #[Voltage] volt \n", "N1=1800.0 #[Motor speed] rpm\n", "Ra=0.6 #[Resistance] ohm\n", "Rfield=360.0 #[Field resistnce] ohm\n", "V2=180.0 #[VOltage] volt\n", "I_line=20.0 #[Limit line current] A\n", "\n", "#Calculation\n", "#Part (a)\n", "Ia=Ia1-V1/Rfield #A(At changeover time)\n", "emf=V1-Ia*Ra #volt\n", "Ifield=emf/Rfield #A(At changeover time)\n", "Iout=Ia1-Ifield #A\n", "Rbraking=emf/Iout #ohm(Braking Resistance)\n", "I_initial=Iout #A(Inotial current)\n", "t=30.0 #sec(time taken to stop)\n", "I_change_rate=I_initial/t #A/s\n", "#i=I_initial-I_change_rate*t , for 0" ] }, { "output_type": "stream", "stream": "stdout", "text": [ "Resistance for dynamic braking : 9.17 ohm\n" ] } ], "prompt_number": 9 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.10 ,Page no:86" ] }, { "cell_type": "code", "collapsed": false, "input": [ " \n", "import math \n", "#Variable declaration\n", "V=240.0 #[DC voltage] V\n", "Ra=0.4 #[Resistnce] ohm\n", "N1=600.0 #[Motor speed] rpm\n", "Ifl=25.0 #[Full load current] A\n", "Radd=1.0 #[Added resistance] ohm\n", "#If1=If2\n", "#T1=T2 leads to If1*Ia1=If2*Ia2: Ia1=Ia2\n", "Ia1=25.0 #A\n", "Ia2=25.0 #A\n", "\n", "#Calculation\n", "Eb1=V-Ia1*Ra #V\n", "Eb2=V-Ia2*(Ra+Radd) #V\n", "N2=N1*Eb2/Eb1 #rpm\n", "#T3=2*T1\n", "#If3=If1\n", "Ia3=2*Ia1 #A\n", "Eb3=V-Ia3*(Ra+Radd) #V\n", "N3=N1*Eb3/Eb1 #rpm\n", "Eb4=0.0 #V(at speed zero Eb=0)\n", "Ia4=V/(Ra+Radd) #V\n", "T4ByT1=Ia4/Ia1 #(field constant)\n", "\n", "#Result\n", "print\"(a). Speed at full load torque in rpm : \",round(N2,2),\"rpm\"\n", "print\"(b) Speed at twice the full load torque : \",round(N3,2),\"rpm\"\n", "print\"(c) Stalling torque is \",round(T4ByT1,3),\" times of full load torque.\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "(a). Speed at full load torque in rpm : 534.78 rpm\n", "(b) Speed at twice the full load torque : 443.48 rpm\n", "(c) Stalling torque is 6.857 times of full load torque.\n" ] } ], "prompt_number": 10 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.11 ,Page no:87" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V=250.0 #[Voltage] V\n", "Ra=1.0 #[Resistance] ohm\n", "Ia1=25.0 #[Armature current] A\n", "N1=900.0 #Speed rpm\n", "If=2.0 #[Filed current ] A\n", "N2=1100.0 #[Increased speed [rpm]\n", "\n", "#Calculation\n", "Eb1=V-Ia1*Ra #V\n", "#If1*Ia1=If2*Ia2\n", "#Eb2=V-Ia2*Ra #V\n", "#-Ia2**2*Ra+Ia2*V-Eb1*Ia1*N2/N1=0 \n", "polynomial=[-Ra,V,-Eb1*Ia1*N2/N1] \n", "Ia2=roots(polynomial) #A\n", "Ia2=Ia2[1] #A(wide range not allowed)\n", "If2=Ia1/Ia2*If #A\n", "\n", "#Result\n", "print\"New value of field current: \",round(If2,2),\"A\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "New value of field current: 1.59 A\n" ] } ], "prompt_number": 11 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.12 ,Page no:110" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V=230.0 #[Votage] V\n", "f=50.0 #[Frequency] Hz\n", "Rf=200.0 #[Resistance] ohm\n", "Ra=0.3 #[Resiatnce] ohm\n", "T=50.0 #[Load torque] N-m\n", "N=900.0 #[Speed at load torque] rpm\n", "Kv=0.8 #[Voltage constant] V/A-rad/s\n", "Kt=0.8 #[Voltage constant] N-m/A**2\n", "\n", "from scipy import integrate \n", "#Calculation\n", "Vm=V*math.sqrt(2) #V\n", "Vf=2*Vm/math.pi #V\n", "If=Vf/Rf #A\n", "#T=Kt*If*Ia\n", "Ia=T/Kt/If #A\n", "omega=N*2*math.pi/60.0 #rad/s\n", "Eb=Kv*omega*If #V\n", "Va=Eb+Ia*Ra #V\n", "#Va=Vm/math.pi*(1+cosd(alfa_a))\n", "alfa_a=math.acos(Va/Vm*math.pi-1.0) #degree\n", "Pout=Ia*Va #W\n", "\n", "def f(t):\n", " return(1)\n", "I=integrate.quad(f,math.degrees(alfa_a),math.degrees(math.pi))\n", "\n", "Iin=math.sqrt(2/(2.0*180.0)*(Ia**2)*I[0]) \n", "VAin=V*Iin #VA\n", "pf_in=Pout/VAin #lagging\n", "\n", "#Result\n", "print\"(a) Field current:\",If,\"A\"\n", "print\"(b) Fringe angle of converter in degree : \",round(math.degrees(alfa_a),3),\"degree\"\n", "print\"(c) Power factor of convertyer(lagging) : \",round(pf_in,3)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "(a) Field current: 1.03536376358 A\n", "(b) Fringe angle of converter in degree : 94.078 degree\n", "(c) Power factor of convertyer(lagging) : 0.605\n" ] } ], "prompt_number": 12 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.13 ,Page no:111" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V=230.0 #[Voltage] V\n", "f=50.0 #[Frequency] Hz\n", "Rf=200.0 #[Resistance] ohm\n", "Ra=0.25#[Armature resistance] ohm\n", "Kv=1.1 #[Torque constant] V/A-rad/s\n", "Kt=1.1 #[Voltage constant] N-m/A**2\n", "alfa_a=45.0 #[Firing angle] degree\n", "Ia=50.0 #[Armature current] A\n", "alfa_f=0.0 \n", "\n", "#Calculation\n", "Vf=2*V*math.sqrt(2.0)/math.pi*math.cos(alfa_f) #V\n", "#Va=(2*230.0*math.sqrt(2.0)/math.pi)*math.cos(alfa_a) #V\n", "Va=(2.0*V/math.pi)\n", "If=Vf/Rf #A\n", "T=Kt*Ia*If #N-m\n", "Eb=Va-Ia*Ra-2.0 #V\n", "omega=Eb/Kv/If #rad/s\n", "N=omega*60.0/(2.0*math.pi) #rpm\n", "\n", "#Result\n", "print\"Torque developed : \",round(T,3),\"N-m\"\n", "print\"Motor speed in rpm : \",round(N,1),\"rpm \"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Torque developed : 56.945 N-m\n", "Motor speed in rpm : 1106.1 rpm \n" ] } ], "prompt_number": 13 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.14 ,Page no:111" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "\n", "V=400 #[Voltage] V\n", "Ra=0.3#Resiatnce armature inohm\n", "Rf=250 #Filed resisatnce in ohm\n", "Ia=50 #Armature current in A\n", "Kv=1.3 #Voltage constantV/A-rad/s\n", "N=1200 #Speed in rpm\n", "alfa_f=0 \n", "\n", "#Calculation\n", "Vf=3*math.sqrt(3)*V*math.sqrt(2)/math.sqrt(3)/math.pi*math.cos(alfa_f) #V\n", "If=Vf/Rf #A\n", "Eb=Kv*If*2*math.pi*N/60 #V\n", "Va=Eb+Ia*Ra #V\n", "alfa_a=math.acos(Va/3/math.sqrt(3)/V/math.sqrt(2)*math.sqrt(3)*math.pi) #degree\n", "\n", "#Result\n", "print\"Fringe angle of converter in degree : \",round(math.degrees(alfa_a),2),\"degree\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Fringe angle of converter in degree : 47.06 degree\n" ] } ], "prompt_number": 14 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.15 ,Page no:112" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\n", "\n", "#Variable declaration\n", "V=500.0 #V [Voltage]\n", "Ia=200.0 # [Armature Current] A\n", "Ra=0.1#ohm[Armature resistance]\n", "Kv=1.4 #[Voltage constant] V/A-rad/s\n", "Kt=1.4 #[torque constant] N-m/A**2\n", "If=2.0 #[Field current] A\n", "cycle=0.5 #[Duty cycle of chopper] sec\n", "\n", "#Calculation\n", "Pin=cycle*V*Ia/1000.0 #KW\n", "Va=cycle*V #V\n", "Eb=Va-Ia*Ra #V\n", "omega=Eb/Kv/2.0 #rad/s\n", "N=omega*60.0/2.0/math.pi #rpm\n", "T=Kt*2.0*Ia #N-m\n", "\n", "#Result\n", "print\"(a) Input power in KW : \",Pin,\"kW\"\n", "print\"(b) Speed in rpm : \",round(N,1),\"rpm\"\n", "print\"(c) Torque in N-m : \",T,\"N-m\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "(a) Input power in KW : 50.0 kW\n", "(b) Speed in rpm : 784.4 rpm\n", "(c) Torque in N-m : 560.0 N-m\n" ] } ], "prompt_number": 15 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.16 ,Page no:112" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "Ra=0.1#[Resistance] ohm\n", "Rb=7.5#[Braking resistance] ohm\n", "Kv=1.4 #[Volate constant] V/A-rad/s\n", "Ia=120.0 #[Armature current] A\n", "If=1.6 #[Filed current] A\n", "cycle=0.35 #[Duty cycle of chopper] sec\n", "\n", "#Calculation\n", "Vavg=Rb*Ia*(1.0-cycle) #V\n", "Pb=Ia**2*Rb*(1.0-cycle)**2 #W\n", "emf=Vavg+Ra*Ia #V\n", "omega=emf/Kv/If #rad/s\n", "N=omega*60.0/2.0/math.pi #rpm\n", "\n", "#Result\n", "print\"Average voltage across chopper : \",Vavg,\"V\"\n", "print\"Power dissipated: \",Pb,\"W\"\n", "print\"Speed : \",round(N),\"rpm\" \n", "print \"NOTE:Answer of Pb & speed is wrong in the book.\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Average voltage across chopper : 585.0 V\n", "Power dissipated: 45630.0 W\n", "Speed : 2545.0 rpm\n", "NOTE:Answer of Pb & speed is wrong in the book.\n" ] } ], "prompt_number": 16 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.17 ,Page no:113" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "%matplotlib inline\n", "#Variable declaration\n", "V=220.0 #[Voltage] V\n", "f=50.0 #[Frequency] Hz\n", "L=0.012 #[Inductance] H\n", "Ra=0.72 #[Resistance] ohm\n", "K=2.0 #[Armature constant] V/rad/s\n", "T=60.0 #[Torque characterisitc] N-m\n", "alfa=90.0 #degree\n", "\n", "#Calculation\n", "Va=(3.0*math.sqrt(3.0)*V*math.sqrt(2.0)/(2.0*math.pi))*(1.0) #V\n", "Ia=5.0 #A\n", "print\"Armature Current : \",Ia,\"A\"\n", "T1=Ia*K #N-m\n", "print\"Torque : \",T1,\"N-m\"\n", "Eb=Va-Ia*Ra #V\n", "omega=Eb/K #rad/s\n", "N1=omega*60.0/2.0/math.pi #rpm\n", "print\"Speed :\",N1,\"rpm\"\n", "\n", "Ia=10.0 #A\n", "print\"Armature Current : \",Ia,\"A\"\n", "T2=Ia*K #N-m\n", "print\"Torque : \",T2,\"N-m\"\n", "Eb=Va-Ia*Ra #V\n", "omega=Eb/K #rad/s\n", "N2=omega*60.0/(2.0*math.pi) #rpm\n", "print\"Speed : \",N2,\"rpm\" \n", "Ia=20.0 #A\n", "print\"Armature Current: \",Ia,\"A\"\n", "T3=Ia*K #N-m\n", "print\"Torque in N-m : \",T3,\"N-m\"\n", "Eb=Va-Ia*Ra #V\n", "omega=Eb/K #rad/s\n", "N3=omega*60.0/2.0/math.pi #rpm\n", "print\"Speed in rpm : \",N3,\"rpm\"\n", "Ia=30.0 #A\n", "print\"Armature Current : \",Ia,\"A\"\n", "T4=Ia*K #N-m\n", "print\"Torque: \",T4,\"N-m\"\n", "Eb=Va-Ia*Ra #V\n", "omega=Eb/K #rad/s\n", "N4=omega*60.0/2.0/math.pi #rpm\n", "print\"Speed : \",T4,\"rpm\"\n", "plot([T1,T2,T3,T4],[N1,N2,N3,N4]) \n", "title('Speed Torque Characteristics') \n", "xlabel('Torque(N-m)') \n", "ylabel('speed(RPM)') \n", "plt.ylim(0.0,1500.0)\n", "plt.xlim(0.0,60.0)\n", "plt.show()" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Populating the interactive namespace from numpy and matplotlib\n", "Armature Current : 5.0 A\n", "Torque : 10.0 N-m\n", "Speed : 1211.32800644 rpm\n", "Armature Current : 10.0 A\n", "Torque : 20.0 N-m\n", "Speed : 1194.13927258 rpm\n", "Armature Current: 20.0 A\n", "Torque in N-m : 40.0 N-m\n", "Speed in rpm : 1159.76180487 rpm\n", "Armature Current : 30.0 A\n", "Torque: 60.0 N-m\n", "Speed : 60.0 rpm\n" ] }, { "output_type": "stream", "stream": "stderr", "text": [ "WARNING: pylab import has clobbered these variables: ['f']\n", "`%pylab --no-import-all` prevents importing * from pylab and numpy\n" ] }, { "metadata": {}, "output_type": "display_data", "png": "iVBORw0KGgoAAAANSUhEUgAAAY0AAAEZCAYAAABrUHmEAAAABHNCSVQICAgIfAhkiAAAAAlwSFlz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\nEQAAAABJRU5ErkJggg==\n", "text": [ "" ] } ], "prompt_number": 17 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.18 ,Page no:114" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V=400.0 #[Thyrisotr bridge voltage] V\n", "f=50.0 #[Frequency] Hz\n", "I=50.0 #[Rated current] A\n", "Ra=0.1 #[Resustnce] ohm\n", "K=0.3 #[Voltage constant] V/rpm\n", "Ia=5.0 #[Currentarmature] A\n", "alfa=30.0 #[Firing angle] degree\n", "\n", "#Calculation\n", "Vavg=(3.0*math.sqrt(3)*V*math.sqrt(2)/(math.sqrt(3)*2.0*math.pi))*(1+math.cos(math.radians(alfa))) #V\n", "Eb=Vavg-Ia*Ra #V\n", "N=Eb/K #rpm\n", "Speed=1600.0 #rpm\n", "Eb=Speed*K #V\n", "Vin=Eb+I*Ra #V\n", "alfa=math.acos(Vin/3/math.sqrt(3)/V/math.sqrt(2)*math.sqrt(3)*2*math.pi-1.0) #degree\n", "\n", "#Result\n", "print\"No load speed : \",round(N),\"rpm\"\n", "print\"Fringe angle : \",round(math.degrees(alfa),2),\"degree\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "No load speed : 1678.0 rpm\n", "Fringe angle : 37.28 degree\n" ] } ], "prompt_number": 18 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.19 ,Page no:114" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V=230.0 #[Voltage] V\n", "f=50.0 #[Frequency] Hz\n", "Rf=200.0 #[Feild resistance] ohm\n", "Ra=0.25#[Armature resistance] ohm\n", "Kv=1.1 #[Volatge constant] V/A-rad/s\n", "Kt=1.1 #[Torque constant] N-m/A**2\n", "alfa_a=45.0 #[Firng angle] degree\n", "Ia=50.0 #[armature current] A\n", "alfa_f=0.0 #Final angle\n", "\n", "#Calculation\n", "Vf=2.0*V*math.sqrt(2.0)/math.pi*math.cos(math.radians(alfa_f)) #V\n", "Va=2.0*V*math.sqrt(2.0)/math.pi*math.cos(math.radians(alfa_a)) #V\n", "If=Vf/Rf #A\n", "T=Kt*Ia*If #N-m\n", "Eb=Va-Ia*Ra-2.0 #V\n", "omega=Eb/Kv/If #rad/s\n", "Eg=-Eb #V\n", "Va=Eg+Ia*Ra+2 #V\n", "alfa=math.acos(Va/2.0/V/math.sqrt(2.0)*math.pi) #degree\n", "\n", "P=abs(Va)*Ia #W(power fed back to source)\n", "\n", "#Result\n", "print\"Fringe angle to converter : \",round(math.degrees(alfa),2),\"degree\"\n", "print\"Power fed back to source : \",round(P),\"W (approx)\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Fringe angle to converter : 124.55 degree\n", "Power fed back to source : 5871.0 W (approx)\n" ] } ], "prompt_number": 19 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.20 ,Page no:115" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V=240.0 #[Voltage] V\n", "alfa=100.0 #degree [Firing angle] \n", "Ra=6.0# [Armature resistanec] ohm\n", "Ia=1.8 #[Armature current] A\n", "\n", "#Calculation\n", "Vm=V*math.sqrt(2.0) #V\n", "Vdc=Vm/math.pi*(1.0+math.cos(math.radians(alfa))) #Volt\n", "Eb=Vdc-Ia*Ra #V\n", "\n", "#Result\n", "print\"Back emf : \",round(Eb,2),\"V\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Back emf : 78.48 V\n" ] } ], "prompt_number": 20 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.21 ,Page no:115" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V1=230.0 #[Voltage] V\n", "N1=1500.0 #[Speed] rpm\n", "Ra=1.0 #[Armature resistance] ohm\n", "Ia=10.0 #[Armature current] A\n", "T=5.0 #[Troque] N-m\n", "#V=K*omega+Ia*Ra\n", "\n", "#Calculation\n", "K=V1/(N1*2*math.pi/60.0+Ia*Ra) #V-s/rad or N-m/A\n", "K=round(K,1)\n", "Ia=T/K #A\n", "Ia=round(Ia,2)\n", "alfa1=30.0 #degree\n", "V=(2*V1*math.sqrt(2)/math.pi)*math.cos(math.radians(alfa1)) #Volt\n", "V=round(V,1)\n", "omega=(V-Ia*Ra)/K #rad/s\n", "\n", "N=(omega*60.0)/(2.0*math.pi) #rpm\n", "print\"Parrt(a) Speed:\",N,\"rpm\"\n", "alfa=45.0 #degree\n", "N=950.0 #rpm\n", "V=(2*V1*math.sqrt(2)/math.pi)*math.cos(math.radians(alfa)) #Volt\n", "V=round(V,2)\n", "Ia=(V-K*2*math.pi/60.0*N)/Ra #A\n", "Ia=round(Ia,2)\n", "T=K*Ia #N-m\n", "print\"Part(b) Torque : \",T,\"N-m\"\n", "print\"\\nNOTE:Answer for (b) is wrong in the book.\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Parrt(a) Speed: 1198.64134927 rpm\n", "Part(b) Torque : 9.996 N-m\n", "\n", "NOTE:Answer for (b) is wrong in the book.\n" ] } ], "prompt_number": 21 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.22 ,Page no:116" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "\n", "V1=500.0 #[Voltage] V\n", "N1=1500.0 #[Speed] rpm\n", "Ia=100.0 #[Armature current] A\n", "V2=350.0 #[Voltage] V\n", "Ra=1.1 #[Resistance] ohm\n", "alfa=45.0 #[Firing angle] degree\n", "N2=1200.0 #[Motor speed] rpm\n", "#V=K*omega+Ia*Ra\n", "\n", "#Calculation\n", "K=(V1-Ia*Ra)/(N1*2*math.pi/60.0) #V-s/rad or N-m/A\n", "V=3*math.sqrt(3)*V2*math.sqrt(2.0)/2.0/math.pi/math.sqrt(3.0)*(1+math.cos(math.radians(alfa))) #Volt\n", "Ia=(V-K*N2*2*math.pi/60.0)/Ra #A\n", "Vin_rms=Ia*math.sqrt(120.0/180.0) #V\n", "Iavg=Ia/3.0 #A\n", "Irms=Ia/math.sqrt(3) #A\n", "pf_in=V*Ia/math.sqrt(3)/V2/Vin_rms #lagging\n", "\n", "#Result\n", "print\"RMS source current : \",round(Ia,2),\"A\"\n", "print\"RMS input voltage:\",round(Vin_rms,1),\"A\"\n", "print\"Average thyristor current : \",round(Iavg,2),\"A\"\n", "print\"RMS thyristor current : \",round(Irms,2),\"A\" \n", "print\"Input power factor = \",round(pf_in,3),\"lagging\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "RMS source current : 83.13 A\n", "RMS input voltage: 67.9 A\n", "Average thyristor current : 27.71 A\n", "RMS thyristor current : 48.0 A\n", "Input power factor = 0.815 lagging\n" ] } ], "prompt_number": 22 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.23 ,Page no:117" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "T1=40.0 #[Torque] N-m\n", "N1=500.0 #[Speed] rpm\n", "J=0.01 #[Inertia of drive] N-m_sec**2/rad\n", "T2=100.0 #[Troque] N-m\n", "N2=1000.0 #[Speed]rpm\n", "\n", "#Calculation\n", "#Te=J*d(omega)/dt+D*omega+TL\n", "d_omegaBYdt=(T2-T1)/J #\n", "#t=omega/d_omegaBYdt+A \n", "omega1=N1*2*math.pi/60 #rad/s\n", "t=0 #s(initial time)\n", "A=t-omega1/d_omegaBYdt #\n", "omega2=N2*2*math.pi/60 #rad/s\n", "t=omega2/d_omegaBYdt+A #s\n", "\n", "#Result\n", "print\"Time taken by the motor in sec : \",round(t,6),\"seconds\" \n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Time taken by the motor in sec : 0.008727 seconds\n" ] } ], "prompt_number": 23 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.24 ,Page no:118" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "from sympy import Symbol\n", "#Variable declaration\n", "f=400.0 #[Feed frequency] Hz\n", "V=200.0 #[Voltage] V\n", "T=30.0 #[Torque] N-m\n", "N=1000.0 #[Speed] rpm\n", "R=0.2 #[Resistance] ohm\n", "L=2.0 #[Motor resistance] mH\n", "Kv=1.5 #[Voltage constant] V-sec/rad\n", "Kt=1.5 #[Troque constant] N-m/A\n", "\n", "#Calculation\n", "Ia=T/Kt #A\n", "omega=N*2*math.pi/60.0 #rad/s\n", "Eb=Kv*omega #V\n", "alfa=(Eb+Ia*R)/V \n", "T=1.0/f*1000.0 #ms\n", "Ton=alfa*T #ms\n", "Toff=T-Ton #ms\n", "Imax=V/R*((1-math.exp(-alfa*T*10**-3*R/(L*10**-3)))/(1-math.exp(-T*10**-3*R/(L*10**-3))))-Eb/R #A\n", "\n", "#Result\n", "print\"(a) Maximum motor armature current : \",round(Imax,3),\"A\"\n", "Imin=V/R*((math.exp(alfa*T*R/L)-1)/(math.exp(T*R/L)-1))-Eb/R #A\n", "print\"(a) Minimum motor armature current : \",abs(round(Imin)),\"A\"\n", "Iexc=Imax #A\n", "print\"(b) Excursion of armature current : \",round(Iexc,3),\"A\"\n", "import sympy\n", "t_= Symbol('t`') \n", "e=Symbol('e')\n", "#yy=2*math.exp(-100*t_dash/2).expand()\n", "L=L/1000\n", "i=(round(Imax,1)*e**(-R*t_/L))\n", "i2=round((Eb/R),1)*(1.0-e**(-R*t_/L))\n", "print\"(c) Expression for armature current:\\n i=\", i,i2" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "(a) Maximum motor armature current : 39.078 A\n", "(a) Minimum motor armature current : 0.0 A\n", "(b) Excursion of armature current : 39.078 A\n", "(c) Expression for armature current:\n", " i= 39.1*e**(-100.0*t`) -785.4*e**(-100.0*t`) + 785.4\n" ] } ], "prompt_number": 26 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.25 ,Page no:128" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V=230.0 #[Voltage] V\n", "f=50.0 #[Frequency] Hz\n", "Rf=1.5 #[Frequency] ohm\n", "Kt=0.25 #[Torque constant] N-m/A\n", "T=25.0 #[Torque] N-m\n", "Kv=0.25 #[Voltage constant] V-sec/rad\n", "\n", "from scipy.optimize import fsolve\n", "#Calculation\n", "Vdc=2*math.sqrt(2)*V/math.pi #V\n", "Em=Vdc #V\n", "Ia=math.sqrt(T/Kt) #A\n", "def f(omega_m):\n", " return(1.5*Ia+Kt*omega_m*Ia-Em)\n", "omega_m=fsolve(f,1)\n", "N=omega_m*60.0/2.0/math.pi #RPM\n", "\n", "#Result\n", "print\"Average motor current: \",Ia,\"A\"\n", "print\"Motor speed : \",round(N[0],2),\"RPM\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Average motor current: 10.0 A\n", "Motor speed : 733.66 RPM\n" ] } ], "prompt_number": 27 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.26 ,Page no:128" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V1=675.0 #[Secondary voltage] V\n", "alfa1=90.5 #[Firing angle] degree\n", "N1=350.0 #[Motor speed] rpm\n", "Ia1=30.0 #[Armature current] A\n", "N2=500.0 #[Second motor speed] rpm\n", "Rf=0.22 #[Field resistance] ohm\n", "Ra=0.22 #[Armature resistance] ohm\n", "\n", "#Calculation\n", "Ia2=Ia1*N2/N1 #A\n", "Va1=V1*math.sqrt(2.0)/math.pi*(1.0+math.cos(math.radians(alfa1))) #V\n", "Eb1=Va1-Ia1*(Ra+Rf) #V\n", "#Eb1/Eb2=Ia1*N1/(Ia2*N2)\n", "#Eb2=Va2-Ia2*(Ra+Rf)\n", "Va2=Eb1*Ia2*N2/(Ia1*N1)+Ia2*(Ra+Rf) #V\n", "alfa2=math.acos(Va2/V1/math.sqrt(2.0)*math.pi-1.0) #degree\n", "\n", "#Result\n", "print\"Armature current of converter in A : \",round(Ia2,2),\"A\"\n", "print\"Fringe angle of converter in degree : \",round(math.degrees(alfa2),2),\"degree\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Armature current of converter in A : 42.86 A\n", "Fringe angle of converter in degree : 4.86 degree\n" ] } ], "prompt_number": 28 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.27 ,Page no:129" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V1=230.0 #[Voltage] V\n", "P=15.0 #[Power] hp\n", "N=1500.0 #[Speed] rpm\n", "V2=220.0 #[Voltage]] V\n", "Ke=0.03 #[emf constant] V/A-s\n", "Kt=0.03 #[torque constant] N-m/A**2\n", "alfa=45.0 #[firing angle] degree\n", "\n", "#Calculation\n", "Vm=V1*math.sqrt(2) #V\n", "omega=N*2*math.pi/60 #rad/s\n", "T=4*Kt*Vm**2*math.cos(math.radians(alfa))**2/(math.pi**2*(Ke*omega)**2) #N-m\n", "Ia=math.sqrt(T/Kt) #A\n", "\n", "#Result\n", "print\"part (a) : \"\n", "print\"Torque in N-m : \",round(T,2),\"N-m\"\n", "print\"Armature current : \",round(Ia,2),\"A\"\n", "print\"part (b) : \"\n", "Ia=Vm*(1+math.cos(math.radians(alfa)))/(math.pi*(Ke*omega)) #A\n", "T=Kt*Ia**2 #N-m\n", "print\"Armature current : \",round(Ia,1),\"A\"\n", "print\"Torque : \",round(T,4),\"N-m\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "part (a) : \n", "Torque in N-m : 28.96 N-m\n", "Armature current : 31.07 A\n", "part (b) : \n", "Armature current : 37.5 A\n", "Torque : 42.2033 N-m\n" ] } ], "prompt_number": 29 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.28 ,Page no:130" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V1=230.0 #[Voltage] V\n", "N=1000.0 #[Speed] rpm\n", "P=15.0 #[Power rating] hp\n", "Rt=0.2 #[Resistance] ohm\n", "Ke=0.03 #[emf rating] V/A-s\n", "Kt=0.03 #[torque rating] N-m/A**2\n", "alfa=30.0 #[Firng angle] degree\n", "\n", "#Calculation\n", "Vm=V1*math.sqrt(2) #V\n", "omega=N*2*math.pi/60.0 #rad/s\n", "V=Vm/math.pi*(1+math.cos(math.radians(alfa))) #V\n", "#V=Ke*Ia*omega+Ia*Rt\n", "Ia=V/(Ke*omega+Rt) #A\n", "T=Kt*Ia**2 #N-m\n", "\n", "#Result\n", "print\"Motor current : \",round(Ia,3),\"A\"\n", "print\"Torque : \",round(T,2),\"N-m\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Motor current : 57.817 A\n", "Torque : 100.28 N-m\n" ] } ], "prompt_number": 30 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.29 ,Page no:131" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V=220.0 #[Voltage] V\n", "Vin=230.0 #[input volatge] V\n", "N1=1500.0 #[Speed of motor] rpm\n", "Ia1=10.0 #[Armature current] A\n", "Ra=3.0 #[Armature resistance] ohm\n", "N2=600.0 #[Speed] rpm\n", "\n", "#Calculation\n", "E1=V-Ia1*Ra #V\n", "E2=E1*N2/N1 #V\n", "Ia2=Ia1/2.0 #A(because of Tnew=T/2)\n", "Vapp=E2+Ia2*Ra #V\n", "alfa=math.acos(Vapp*math.pi/2/math.sqrt(2)/Vin) #degree\n", "\n", "#Result\n", "print\"Firing angle of converter : \",round(math.degrees(alfa),1),\"degree\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Firing angle of converter : 63.9 degree\n" ] } ], "prompt_number": 31 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.30 ,Page no:131" ] }, { "cell_type": "code", "collapsed": false, "input": [ " \n", "import math \n", "#Variable declaration\n", "V=230.0 #[Volatge] V\n", "N=870.0 #[Motor speed] rpm\n", "Ia=100.0 #[Armaturecurrent] A\n", "Ra=0.05 #[Armature resisatce]ohm\n", "T=400.0 #[Torque] N-m\n", "\n", "#Calculation\n", "E=V-Ia*Ra #V\n", "Vgen=V+Ia*Ra #V\n", "N2=N*Vgen/E #rpm\n", "\n", "#Result\n", "print\"Motor speed in rpm : \",round(N2,2),\"rpm\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Motor speed in rpm : 908.67 rpm\n" ] } ], "prompt_number": 32 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.31 ,Page no:132" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V=220.0 #[Voltage] V\n", "P=2.2 #[Power of motor] KW\n", "N1=1000.0 #[Motor speed] rpm\n", "Ra=2.0 #[Resistance] ohm\n", "f=250.0 #[Frequency] Hz\n", "alfa=0.9 #[duty cycle] cycle\n", "N2=1200.0 #[Load torque]rpm\n", "N3=800.0 #[Final speed] rpm\n", "\n", "#Calculation\n", "Ia1=P*1000.0/V #A\n", "Ia2=Ia1*N2/N1 #A\n", "Eb2=alfa*V-Ia2*Ra #V\n", "Eb3=Eb2*N3/N2 #V\n", "Ia3=Ia1*N3/N1 #A\n", "alfa3=(Eb3+Ia3*Ra)/V #cycle\n", "ton=alfa3/f #sec\n", "\n", "#Result\n", "print\"On time of chopper %.1e\"%ton,\"sec\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "On time of chopper 2.4e-03 sec\n" ] } ], "prompt_number": 33 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.32 ,Page no:139" ] }, { "cell_type": "code", "collapsed": false, "input": [ " \n", "import math \n", "#Variable declaration\n", "V=230.0 #[Voltage]V\n", "N1=1000.0 #[Motor speed]rpm\n", "Ia1=100.0 #[Armature current]A\n", "Ra=0.1 #[Armature resistance]ohm\n", "Rf=0.1 #[Field ressiatnce]ohm\n", "N2=800.0 #[Final speed of motor]rpm\n", "\n", "#Calculation\n", "Ia2=math.sqrt(2)*Ia1 #A(As T2=2*T1 & T proportional to Ia**2)\n", "Eb1=V-Ia1*(Ra+Rf) #V\n", "Eb2=N2*Ia2/(N1*Ia1)*Eb1 #V\n", "#Eb2=Ia2*(Ra+Rf+Rbraking)\n", "Rbraking=Eb2/Ia2-Ra-Rf #ohm\n", "Ibraking=Eb2/Rbraking #A\n", "\n", "\n", "#Result\n", "print'Braking resistance : ' ,Rbraking,\"ohm\"\n", "print'Braking current : ',round(Ibraking,1),\"A\"\n", "print\"NOTE:Braking current is not calculated in the textbook but asked in the example.\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Braking resistance : 1.48 ohm\n", "Braking current : 160.5 A\n", "NOTE:Braking current is not calculated in the textbook but asked in the example.\n" ] } ], "prompt_number": 34 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.33 ,Page no:139" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "P=6.0 #poles\n", "V=220.0 #[Voltage] V\n", "f=50.0 #[Frequency] Hz\n", "Ra=0.2 #[Armature resistance] ohm\n", "Rf=150.0 #[Field resistance] ohm\n", "Z=150.0 #[no. of conductors]\n", "fi=0.02027 #[Field flux per mole]Wb(flux)\n", "alfa=0.0 #[Delay angle for field converter] degree\n", "alfa_a=45.0 #[Delay angle for armature converters] degree\n", "Ia=25.0 #[Armature current] A\n", "A=2.0 # [Area]\n", "\n", "#Calculation\n", "T=Z*P*fi*Ia/(2*math.pi*A) #N-m\n", "Vm=V*math.sqrt(2) #V\n", "Vdc=2*Vm/math.pi*math.cos(math.radians(alfa_a)) #V\n", "Eb=Vdc-Ia*Ra #V\n", "N=Eb*60*A/(Z*P*fi) #rpm\n", "Pout=Vdc*Ia #W\n", "pf=Pout/V/Ia #lagging\n", "\n", "#Result\n", "print\"Totque : \",round(T,3),\"N-m\"\n", "print\"Speed : \",round(N,2),\"rpm\"\n", "print'Power factor : ',round(pf,4),\"Lagging\"\n", "\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Totque : 36.293 N-m\n", "Speed : 888.38 rpm\n", "Power factor : 0.6366 Lagging\n" ] } ], "prompt_number": 35 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.34 ,Page no:140" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#Variable declaration\n", "R=0.1 #Armature resistance in [ohm]\n", "V1=220.0 #Voltage in [V]\n", "N1=1000.0 #speed in [rpm]\n", "I=100.0 #Current in [A]\n", "V2=200.0 #Dropped voltage in [V]\n", "\n", "#Calculation\n", "Eb2=V2-I*R\n", "Eb1=V1-I*R \n", "N2=Eb2*N1/Eb1 #Motor speed after drop\n", "\n", "#Result\n", "print\"Motor speed after voltage drop is\",round(N2,2),\"rpm\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Motor speed after voltage drop is 904.76 rpm\n" ] } ], "prompt_number": 36 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.35 ,Page no:140" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\n", "V1=200.0 #[Voltage] V\n", "N1=940.0 #[Speed] rpm\n", "Ra=0.02 #[Armature resistance] ohm\n", "Ia=100.0 #[Armature current] A\n", "N2=500.0 #[Speed] rpm\n", "\n", "#Calculation\n", "Eb1=V1-Ia*Ra #V\n", "#Eb1/Eb2=N1/N2\n", "#Eb2=V2-Ia*Ra #V\n", "V2=Eb1*N2/N1+Ia*Ra #V\n", "cycle=V2/V1 \n", "\n", "#Result\n", "print\"Duty cycle : \",round(cycle,4)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Duty cycle : 0.5366\n" ] } ], "prompt_number": 37 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.36 ,Page no:141" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V1=220.0 #[Voltage] V\n", "Ra=0.05 #[Armature resistance]ohm\n", "N1=1000.0 #[Speed]rpm\n", "Ia=100.0 #[Armature current]A\n", "N2=500.0 #[Speed]rpm\n", "\n", "#Calculation\n", "Eb=V1-Ia*Ra #V\n", "Ib=2*Ia #A\n", "Rb=(V1+Eb)/Ib-Ra #ohm\n", "Tb=Eb/(N1*2*math.pi/60.0)*Ib #N-m\n", "Eb2=Eb*N2/N1 #V\n", "Ib2=(V1+Eb2)/(Ra+Rb) #A\n", "Tb2=Eb2/(N2*2*math.pi/60.0)*Ib2 #N-m\n", "\n", "#Result\n", "print\"Resistance to be added:\",Rb,\"ohm\"\n", "print\"Initial braking torque : \",round(Tb,2),\"N-m\"\n", "print\"Initial braking torque: \",round(Tb2,1),\"N-m\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Resistance to be added: 2.125 ohm\n", "Initial braking torque : 410.62 N-m\n", "Initial braking torque: 309.1 N-m\n" ] } ], "prompt_number": 38 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.37 ,Page no:142" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V1=230.0 #[Voltage] V\n", "N1=870.0 #[Speed] rpm\n", "Ia=100.0 #[Armature current] A\n", "Ra=0.05 #[Armature resistance] ohm\n", "T=400.0 #[Torqu] N-m\n", "\n", "#Calculation\n", "Eb=V1-Ia*Ra #V\n", "Vgen=V1+Ia*Ra #V\n", "N2=N1*Vgen/Eb #rpm\n", "\n", "#Result\n", "print\"Speed : \",round(N2,2),\"rpm\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Speed : 908.67 rpm\n" ] } ], "prompt_number": 39 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.38 ,Page no:142" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "P=10.0 #[Power] KW\n", "V1=230.0 #[Voltage] V\n", "N1=1200.0 #[Speed] rpm\n", "Ra=0.5 #[Armature resistance] ohm\n", "Ke=0.182 #[emf constant] V/rpm\n", "V2=260.0 #[Voltage]V\n", "alfa=30.0 #[Firing angle] degree\n", "Ia=30.0 #[Armature current] A\n", "\n", "#Calculation\n", "Vm=V2*math.sqrt(2) #V\n", "Vdc=2*Vm/math.pi*math.cos(math.radians(alfa)) #V\n", "Eb=Vdc-Ia*Ra #V\n", "Kt=Ke*60/2/math.pi #N-m/A\n", "T=Kt*Ia #N-m\n", "N2=Eb/Ke #rpm\n", "Pout=Vdc*Ia #W\n", "pf=Pout/V2/Ia #lagging power factor\n", "\n", "#Result\n", "print\"Torque in N-m : \",round(T,2),\"N-m\"\n", "print\"Speed in rpm : \",round(N2,2),\"rpm\"\n", "print\"Power factor : \",round(pf,3),\"lagging\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Torque in N-m : 52.14 N-m\n", "Speed in rpm : 1031.43 rpm\n", "Power factor : 0.78 lagging\n" ] } ], "prompt_number": 40 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.39 ,Page no:143" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration \n", "P=2.2 #[Power] KW\n", "V=220 #[Voltage] V\n", "N1=1000 #[Speed] rpm\n", "Ra=2 #[Resistance armature] ohm\n", "f=250 #[frequency] Hz\n", "alfa=0.9 #duty cycle\n", "N2=1200 #[Speed]rpm\n", "N3=800 #[Motor sped] rpm\n", "\n", "#Calculation\n", "Ia1=P*1000/V #A\n", "Ia2=Ia1*N2/N1 #A\n", "Eb1=alfa*V-Ia2*Ra #V\n", "Eb2=Eb1*N3/N2 #V\n", "Ia3=Ia1*N3/N1 #A\n", "alfa3=(Eb2+Ia3*Ra)/V #cycle\n", "ton=alfa3/f #sec\n", "\n", "#Result\n", "print'On time of chopper : ',ton*1000,\"milli seconds\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "On time of chopper : 2.4 milli seconds\n" ] } ], "prompt_number": 41 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.40,Page no:143" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V=220.0 #[Voltage] V\n", "Eff1=85/100.0 #Efficiency\n", "Eff2=80/100.0 #Efficiency\n", "Load=400.0 #[Load in Kg\n", "t=2.5 #[time] ms\n", "Ra=0.1 #[Armature resistance] ohm\n", "g=9.81 #constant for gravity acceleration\n", "\n", "#Calculation\n", "Pout=Load*g*t #W\n", "IL=Pout/V/Eff1/Eff2 #A\n", "Eb=V-IL*Ra #V\n", "R=(V+Eb)/IL-Ra #ohm\n", "\n", "#Result\n", "print\"Current drawn : \",round(IL,3),\"A\"\n", "print\"Resistance to be added : \",round(R,2),\"ohm\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Current drawn : 65.575 A\n", "Resistance to be added : 6.51 ohm\n" ] } ], "prompt_number": 42 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example:5.41 ,Page no:144" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "#Variable declaration\n", "V1=220.0 #[Voltage] V\n", "N1=1500.0 #[Speed] rpm\n", "I=10.0 #[Current] A\n", "Ra=3.0 #[Armature resistance] ohm\n", "V2=230.0 #[Voltage]V\n", "N2=600.0 #[Speed] rpm\n", "\n", "#Calculation\n", "Eb1=V1-I*Ra #V\n", "Eb2=Eb1*N2/N1 #V\n", "Ia=I/2 #A(at half rated torque)\n", "Vm=V1*math.sqrt(2) #V\n", "alfa=math.acos((Eb2+Ia*Ra)*math.pi/2/Vm) #degree\n", "\n", "#Result\n", "print\"Firing angle : \",round(math.degrees(alfa),2),\"degree\"\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Firing angle : 62.65 degree\n" ] } ], "prompt_number": 43 } ], "metadata": {} } ] }