Introduction to Electrical and Electronics Engineering. Module 2, module 2.

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Contents · Electromagnetic induction: Faraday's laws and Lenz's law
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Electromagnetic induction: Faraday's laws and Lenz's law

Syllabus: Electromagnetic Induction

  • Faraday's laws, Lenz's law
  • Statically induced and dynamically induced emf
  • Self-inductance and mutual inductance, coefficient of coupling (numerical problems not needed)

Concept of Electromagnetic Induction

Electromagnetic Induction

Electromagnetic induction is the phenomenon in which an electromotive force (emf) is induced in a conductor or a coil whenever the magnetic flux linking with it changes. This phenomenon was discovered by Michael Faraday in 1831 and forms the operating principle of generators, transformers, and induction motors.

Magnetic Flux Linkage (ψ\psi)

If a coil has NN turns and a magnetic flux ϕ\phi (in webers, Wb) passes through each turn, the total flux linkage ψ\psi is the product of the number of turns and the flux linking each turn:

ψ=Nϕ(in weber-turns, Wb-turns)\psi = N\phi \quad \text{(in weber-turns, Wb-turns)}

Faraday's Laws of Electromagnetic Induction

Faraday summarized the principles of electromagnetic induction into two fundamental laws:

Faraday's First Law

Whenever the magnetic flux linking a closed circuit or conductor changes, an electromotive force (emf) is induced in the conductor. If the conductor forms part of a closed circuit, an induced current flows through it for as long as the change in flux continues.

Faraday's Second Law

The magnitude of the induced emf in a coil is directly proportional to the rate of change of magnetic flux linkages with the coil.

If a coil has NN turns and the magnetic flux linking it changes from ϕ1\phi_1 to ϕ2\phi_2 in a small time interval dtdt, the magnitude of the induced emf ee in volts is given in differential form by:

∣e∣=dψdt=Ndϕdt(volts)|e| = \frac{d\psi}{dt} = N \frac{d\phi}{dt} \quad \text{(volts)}

If the flux changes uniformly from ϕ1\phi_1 to ϕ2\phi_2 in time tt seconds:

∣e∣=Nϕ2−ϕ1t(volts)|e| = N \frac{\phi_2 - \phi_1}{t} \quad \text{(volts)}

Lenz's Law

Lenz's Law

Proposed by Heinrich Lenz in 1834, Lenz's law states that the direction of an electromagnetically induced emf (and hence the induced current in a closed circuit) is always such that it opposes the very cause that produces it—namely, the change in magnetic flux.

Incorporating Lenz's law into Faraday's second law gives the complete mathematical expression for induced emf:

e=−Ndϕdt(volts)e = -N \frac{d\phi}{dt} \quad \text{(volts)}

Here, the negative sign indicates that the induced emf sets up a current whose magnetic field opposes the change in the original magnetic flux ϕ\phi.

Lenz's Law and Conservation of Energy

Lenz's law is a direct consequence of the law of conservation of energy:

  1. Suppose the North pole of a permanent magnet is moved toward a closed coil. The magnetic flux linking the coil increases.
  2. By Lenz's law, the induced current in the coil flows in a direction (counter-clockwise when viewed from the magnet side) that makes the near face of the coil behave like a North pole.
  3. The two North poles repel each other. Therefore, external mechanical work must be done against this force of repulsion to push the magnet toward the coil.
  4. This mechanical work done by the external agent is converted directly into electrical energy (and eventually dissipated as heat I2RtI^2Rt in the coil). If the induced current aided the motion instead of opposing it, the magnet would accelerate on its own without any energy input, violating conservation of energy.

Types of Induced EMF

An emf can be induced in a conductor by changing the flux linkage in two fundamental ways:

Code
                   Induced EMF
                        |
        +---------------+---------------+
        |                               |
Dynamically Induced EMF        Statically Induced EMF
(Conductor moves OR            (Both conductor and magnet
 field moves physically)        are stationary; flux magnitude
                                varies with time)
                                        |
                        +---------------+---------------+
                        |                               |
               Self-Induced EMF               Mutually Induced EMF
               (In the same coil)             (In a neighboring coil)

Dynamically Induced EMF

Dynamically Induced EMF

When the magnetic field is stationary (constant in time) and the conductor moves across the magnetic flux lines—or when the conductor is stationary and the magnetic field system moves physically past it—the emf induced in the conductor is called dynamically induced emf (or motional emf). Examples include DC generators and AC synchronous generators (alternators).

Expression for Dynamically Induced EMF:

  1. Consider a straight conductor of active length ll meters moving with a uniform velocity vv m/s in a uniform magnetic field of flux density BB tesla (Wb/m2\text{Wb/m}^2).
  2. Let the conductor move in a direction making an angle θ\theta with the direction of the magnetic field lines.
  3. In a small time interval dtdt, the conductor moves a distance dx=v dtdx = v \, dt. The component of displacement perpendicular to the magnetic field is dx⊥=v dtsin⁡θdx_{\perp} = v \, dt \sin\theta.
  4. The area swept by the conductor perpendicular to the flux lines in time dtdt is: dA=l⋅vsin⁡θ dtdA = l \cdot v \sin\theta \, dt
  5. Therefore, the magnetic flux cut by the conductor in time dtdt is: dϕ=B⋅dA=Blvsin⁡θ dtd\phi = B \cdot dA = B l v \sin\theta \, dt
  6. By Faraday's law, the magnitude of the induced emf in the single conductor is: e=dϕdt=Blvsin⁡θ(volts)e = \frac{d\phi}{dt} = B l v \sin\theta \quad \text{(volts)}
  • Case 1 (Conductor moves parallel to the field, θ=0∘\theta = 0^\circ): sin⁡0∘=0  ⟹  e=0 V\sin 0^\circ = 0 \implies e = 0\text{ V}. No flux lines are cut.
  • Case 2 (Conductor moves perpendicular to the field, θ=90∘\theta = 90^\circ): sin⁡90∘=1  ⟹  e=Blv V\sin 90^\circ = 1 \implies e = Blv\text{ V} (maximum induced emf).

Fleming's Right-Hand Rule

The direction of dynamically induced emf is found using Fleming's Right-Hand Rule: Hold the thumb, forefinger, and middle finger of the right hand mutually perpendicular to one another. If the Forefinger points in the direction of the magnetic Field (North to South), and the Thumb points in the direction of Motion of the conductor (relative to the field), then the Middle finger points in the direction of the Induced EMF (or current).

Statically Induced EMF

Statically Induced EMF

When both the conductor (coil) and the magnetic field system are completely stationary, and the magnetic flux linking the coil is changed purely by varying the magnitude of the electric current producing the flux, the induced emf is called statically induced emf (or transformer emf). An example is the electrical transformer.

Statically induced emf is further classified into two types:

  1. Self-induced emf: Induced in a coil due to the change of flux produced by its own current.
  2. Mutually induced emf: Induced in a coil due to the change of flux produced by a current flowing in a neighboring magnetically coupled coil.

Comparison: Dynamically vs. Statically Induced EMF

FeatureDynamically Induced EMFStatically Induced EMF
Physical movementRelative physical motion exists between conductor and magnetic fieldBoth conductor and magnetic field system remain stationary
Cause of flux changeConductor physically cuts across magnetic flux linesMagnitude of current producing the flux varies with time
Formulae=Blvsin⁡θe = Blv\sin\thetae=−Ndϕdte = -N \frac{d\phi}{dt}
Rule for directionFleming's Right-Hand RuleLenz's Law
Practical exampleDC generator, AC alternatorTransformer

Summary

  • Faraday's First Law: A changing magnetic flux linking a conductor induces an emf in it.
  • Faraday's Second Law & Lenz's Law: e=−Ndϕdte = -N \frac{d\phi}{dt}, where the negative sign shows opposition to the change in flux.
  • Dynamically induced emf: e=Blvsin⁡θe = Blv\sin\theta, produced by relative motion between conductor and field.
  • Statically induced emf: Produced by time-varying current in a stationary coil system.

Self-inductance, mutual inductance and coefficient of coupling

Self-Inductance (LL)

Self-Induced EMF

When a time-varying current ii flows through a coil of NN turns, it sets up a time-varying magnetic flux ϕ\phi through the coil itself. By Faraday's law, this changing flux induces an emf in the very same coil that opposes the change in current. This emf is called self-induced emf.

Self-Inductance (Coefficient of Self-Induction)

Self-inductance (LL) is the property of a coil by virtue of which it opposes any change in the magnitude or direction of electric current flowing through it by inducing an emf in itself. The SI unit of inductance is the henry (H).

Expressions for Self-Inductance

Assuming the magnetic core has constant permeability (no magnetic saturation), the flux ϕ\phi is directly proportional to the current ii:

  1. In terms of flux linkage per unit current: ψ=Nϕ∝i  ⟹  Nϕ=Li\psi = N\phi \propto i \implies N\phi = L i L=Nϕi(henrys, H)L = \frac{N\phi}{i} \quad \text{(henrys, H)} Definition: A coil has a self-inductance of 1 henry if a current of 1 ampere flowing through it produces a flux linkage of 1 weber-turn.

  2. In terms of self-induced emf: By Faraday's law, the magnitude of self-induced emf is: eL=Ndϕdt=ddt(Nϕ)=ddt(Li)e_L = N \frac{d\phi}{dt} = \frac{d}{dt}(N\phi) = \frac{d}{dt}(Li) Since LL is constant for an air core or unsaturated magnetic core: eL=Ldidt(volts)e_L = L \frac{di}{dt} \quad \text{(volts)} (Taking opposition into account, eL=−Ldidte_L = -L \frac{di}{dt}.) Definition: A coil has a self-inductance of 1 henry if a current changing at the rate of 1 ampere per second induces an emf of 1 volt in the coil.

  3. In terms of physical dimensions and magnetic reluctance: From magnetic circuit theory, flux ϕ=MMFReluctance=NiS\phi = \frac{\text{MMF}}{\text{Reluctance}} = \frac{Ni}{\mathcal{S}}, where reluctance S=lμ0μrA\mathcal{S} = \frac{l}{\mu_0 \mu_r A}. Substituting ϕ\phi into L=NϕiL = \frac{N\phi}{i}: L=Ni(NiS)=N2SL = \frac{N}{i} \left(\frac{Ni}{\mathcal{S}}\right) = \frac{N^2}{\mathcal{S}} L=μ0μrAN2l(henrys, H)L = \frac{\mu_0 \mu_r A N^2}{l} \quad \text{(henrys, H)} where NN is the number of turns, AA is the cross-sectional area of the core (m2\text{m}^2), ll is the mean length of the magnetic path (m\text{m}), μ0=4π×10−7 H/m\mu_0 = 4\pi \times 10^{-7}\text{ H/m}, and μr\mu_r is the relative permeability of the core.

Mutual Inductance (MM)

Mutually Induced EMF

Consider two coils, Coil 1 (having N1N_1 turns) and Coil 2 (having N2N_2 turns), placed close to each other so that a portion of the magnetic flux produced by one coil links with the other:

Code
   i1 -->  +--------+           +--------+
           | Coil 1 |  Phi_12   | Coil 2 |  --> Induced emf e_M2
           | (N1)   | ========> | (N2)   |
           +--------+           +--------+

When a time-varying current i1i_1 flows in Coil 1, it produces a total flux ϕ1\phi_1. A part of this flux, denoted ϕ12\phi_{12}, links with Coil 2. As i1i_1 changes, ϕ12\phi_{12} changes, inducing an emf eM2e_{M2} in Coil 2. This is called mutually induced emf.

Mutual Inductance (Coefficient of Mutual Induction)

Mutual inductance (MM) between two coils is defined as the property by which a change of current in one coil induces an emf in the neighboring coil. Its SI unit is also the henry (H).

Expressions for Mutual Inductance

  1. In terms of mutual flux linkage per unit current: The flux linkage in Coil 2 due to current i1i_1 in Coil 1 is N2ϕ12N_2 \phi_{12}, which is proportional to i1i_1: N2ϕ12=Mi1  ⟹  M=N2ϕ12i1(H)N_2 \phi_{12} = M i_1 \implies M = \frac{N_2 \phi_{12}}{i_1} \quad \text{(H)} Similarly, if current i2i_2 flows in Coil 2 and produces flux ϕ21\phi_{21} linking Coil 1: M=N1ϕ21i2(H)M = \frac{N_1 \phi_{21}}{i_2} \quad \text{(H)} For a linear (unsaturated) magnetic medium, M12=M21=MM_{12} = M_{21} = M.

  2. In terms of mutually induced emf: By Faraday's second law, the magnitude of mutually induced emf in Coil 2 when current i1i_1 changes in Coil 1 is: eM2=N2dϕ12dt=ddt(N2ϕ12)=ddt(Mi1)e_{M2} = N_2 \frac{d\phi_{12}}{dt} = \frac{d}{dt}(N_2 \phi_{12}) = \frac{d}{dt}(M i_1) eM2=Mdi1dt(volts)e_{M2} = M \frac{di_1}{dt} \quad \text{(volts)} Definition: Two coils have a mutual inductance of 1 henry if a current changing at the rate of 1 ampere per second in one coil induces an emf of 1 volt in the other coil.

  3. In terms of magnetic circuit parameters: If both coils are wound on the same core of reluctance S=lμ0μrA\mathcal{S} = \frac{l}{\mu_0 \mu_r A} and all the flux of Coil 1 links Coil 2 (ϕ12=ϕ1=N1i1S\phi_{12} = \phi_1 = \frac{N_1 i_1}{\mathcal{S}}): M=N2i1(N1i1S)=N1N2S=μ0μrAN1N2l(H)M = \frac{N_2}{i_1}\left(\frac{N_1 i_1}{\mathcal{S}}\right) = \frac{N_1 N_2}{\mathcal{S}} = \frac{\mu_0 \mu_r A N_1 N_2}{l} \quad \text{(H)}

Coefficient of Coupling (kk)

Coefficient of Coupling

The coefficient of coupling (kk) between two magnetically coupled coils is defined as the fraction of the total magnetic flux produced by one coil that actually links with the second coil. It is a dimensionless number between 00 and 11 (0≤k≤10 \le k \le 1).

Derivation of M=kL1L2M = k\sqrt{L_1 L_2}:

  1. Let current i1i_1 in Coil 1 (N1N_1 turns) produce total flux ϕ1\phi_1. The self-inductance of Coil 1 is: L1=N1ϕ1i1— (Equation 1)L_1 = \frac{N_1 \phi_1}{i_1} \quad \text{--- (Equation 1)}
  2. If kk is the coefficient of coupling, the flux linking Coil 2 is ϕ12=kϕ1\phi_{12} = k \phi_1. Therefore, the mutual inductance is: M=N2ϕ12i1=N2(kϕ1)i1— (Equation 2)M = \frac{N_2 \phi_{12}}{i_1} = \frac{N_2 (k \phi_1)}{i_1} \quad \text{--- (Equation 2)}
  3. Similarly, let current i2i_2 in Coil 2 (N2N_2 turns) produce total flux ϕ2\phi_2. The self-inductance of Coil 2 is: L2=N2ϕ2i2— (Equation 3)L_2 = \frac{N_2 \phi_2}{i_2} \quad \text{--- (Equation 3)}
  4. A fraction kk of ϕ2\phi_2 links with Coil 1, so ϕ21=kϕ2\phi_{21} = k \phi_2. Expressing MM from Coil 2 to Coil 1: M=N1ϕ21i2=N1(kϕ2)i2— (Equation 4)M = \frac{N_1 \phi_{21}}{i_2} = \frac{N_1 (k \phi_2)}{i_2} \quad \text{--- (Equation 4)}
  5. Multiplying Equation 2 and Equation 4 together: M×M=(kN2ϕ1i1)(kN1ϕ2i2)=k2(N1ϕ1i1)(N2ϕ2i2)M \times M = \left(\frac{k N_2 \phi_1}{i_1}\right) \left(\frac{k N_1 \phi_2}{i_2}\right) = k^2 \left(\frac{N_1 \phi_1}{i_1}\right) \left(\frac{N_2 \phi_2}{i_2}\right)
  6. Substituting L1L_1 and L2L_2 from Equations 1 and 3: M2=k2L1L2M^2 = k^2 L_1 L_2 M=kL1L2⟺k=ML1L2M = k \sqrt{L_1 L_2} \quad \Longleftrightarrow \quad k = \frac{M}{\sqrt{L_1 L_2}}

Special Cases of Coupling:

  • Tightly coupled coils (k≈1k \approx 1): Nearly 100% of the flux of one coil links the other (e.g., transformer windings wound on a common iron core, where k≈0.98 to 0.99k \approx 0.98\text{ to }0.99). For ideal coupling (k=1k = 1), Mmax⁡=L1L2M_{\max} = \sqrt{L_1 L_2}.
  • Loosely coupled coils (k<0.5k < 0.5): Only a small fraction of flux links the second coil (e.g., air-core radio-frequency coils separated in space).
  • Magnetically isolated coils (k=0k = 0): Coils are placed far apart or perpendicular to each other so that ϕ12=0\phi_{12} = 0 and M=0M = 0.

Comparison: Self-Inductance vs. Mutual Inductance

ParameterSelf-Inductance (LL)Mutual Inductance (MM)
Number of coilsAssociated with a single coilAssociated with a pair of magnetically coupled coils
Flux linkage formulaL=NϕiL = \frac{N\phi}{i}M=N2ϕ12i1=N1ϕ21i2M = \frac{N_2 \phi_{12}}{i_1} = \frac{N_1 \phi_{21}}{i_2}
Induced EMF formulaeL=Ldidte_L = L \frac{di}{dt}eM2=Mdi1dte_{M2} = M \frac{di_1}{dt}
Physical formulaL=N2S=μ0μrAN2lL = \frac{N^2}{\mathcal{S}} = \frac{\mu_0 \mu_r A N^2}{l}M=kN1N2S=kL1L2M = \frac{k N_1 N_2}{\mathcal{S}} = k\sqrt{L_1 L_2}

Summary

  • Self-inductance: L=Nϕi=N2SL = \frac{N\phi}{i} = \frac{N^2}{\mathcal{S}}, and self-induced emf eL=Ldidte_L = L\frac{di}{dt}.
  • Mutual inductance: M=N2ϕ12i1M = \frac{N_2 \phi_{12}}{i_1}, and mutually induced emf eM2=Mdi1dte_{M2} = M\frac{di_1}{dt}.
  • Coefficient of coupling: k=ϕ12ϕ1=ML1L2k = \frac{\phi_{12}}{\phi_1} = \frac{M}{\sqrt{L_1 L_2}}, with 0≤k≤10 \le k \le 1.

Alternating current fundamentals: Generation and waveform representation

Syllabus: Alternating Current Fundamentals

  • Generation of alternating voltages
  • Representation of sinusoidal waveforms: frequency, period, average value, RMS value and form factor - numerical problems

Alternating Quantity vs. Direct Quantity

  • Direct Current (DC): An electric current or voltage whose magnitude and direction (polarity) remain constant with time (e.g., output of a storage battery).
  • Alternating Current (AC): An electric current or voltage whose magnitude changes continuously with time and whose direction reverses periodically at regular intervals. The most standard and widely used alternating waveform is the sinusoidal waveform (sine wave).

Generation of Alternating Voltage

An alternating voltage is generated based on Faraday's law of electromagnetic induction either by rotating a rectangular coil with constant angular velocity inside a uniform stationary magnetic field, or by rotating a magnetic field inside a stationary set of coils (as in large commercial alternators).

Code
      N-Pole                     S-Pole
     +------+       (b)         +------+
     |      |        o          |      |
     |      |       /           |      |
     |  B   |  --->  O  omega   |  B   |
     |      |       /           |      |
     |      |      o            |      |
     +------+      (a)          +------+
            Axis of coil rotation

Derivation of the Sinusoidal EMF Equation:

  1. Consider a rectangular coil of NN turns and cross-sectional area A m2A\text{ m}^2 placed in a uniform magnetic field of flux density BB tesla (Wb/m2\text{Wb/m}^2).
  2. Let the coil rotate counter-clockwise at a uniform angular velocity of ω\omega radians per second (rad/s\text{rad/s}).
  3. At time t=0t = 0, assume the plane of the coil is perpendicular to the magnetic field lines (i.e., the normal to the coil plane is parallel to B⃗\vec{B}, so angle θ=0\theta = 0). At this instant, the magnetic flux passing through the coil is maximum: Φm=B⋅A(webers)\Phi_m = B \cdot A \quad \text{(webers)}
  4. After time tt seconds, the coil has rotated through an angle θ=ωt\theta = \omega t radians. The component of magnetic flux perpendicular to the plane of the coil at instant tt is: ϕ(t)=BAcos⁡θ=Φmcos⁡(ωt)\phi(t) = B A \cos\theta = \Phi_m \cos(\omega t)
  5. By Faraday's law of electromagnetic induction, the instantaneous emf ee induced in the coil of NN turns is: e=−Ndϕdt=−Nddt(Φmcos⁡ωt)e = -N \frac{d\phi}{dt} = -N \frac{d}{dt} \left(\Phi_m \cos\omega t\right) e=−NΦm(−ωsin⁡ωt)=ωNΦmsin⁡(ωt)e = -N \Phi_m (-\omega \sin\omega t) = \omega N \Phi_m \sin(\omega t)
  6. The induced emf reaches its maximum (peak) value EmE_m when sin⁡(ωt)=1\sin(\omega t) = 1, i.e., when θ=ωt=90∘\theta = \omega t = 90^\circ (at this position, the plane of the coil is parallel to the magnetic field lines and the coil sides cut the flux lines at maximum rate): Em=ωNΦm=2πfNBA(volts)E_m = \omega N \Phi_m = 2\pi f N B A \quad \text{(volts)}
  7. Substituting EmE_m gives the standard equation for instantaneous alternating emf: e(t)=Emsin⁡(ωt)=Emsin⁡θ(volts)e(t) = E_m \sin(\omega t) = E_m \sin\theta \quad \text{(volts)}

Key Terminology of Sinusoidal Waveforms

A general sinusoidal voltage or current is written as:

v(t)=Vmsin⁡(ωt+ϕ)ori(t)=Imsin⁡(ωt+ϕ)v(t) = V_m \sin(\omega t + \phi) \quad \text{or} \quad i(t) = I_m \sin(\omega t + \phi)
  1. Instantaneous Value (vv or ii): The value of an alternating quantity at any particular instant of time tt. It is denoted by lowercase letters (e,v,ie, v, i).
  2. Maximum Value / Peak Value / Amplitude (VmV_m or ImI_m): The highest positive or negative value attained by an alternating quantity during one half-cycle. The peak-to-peak value is Vp−p=2VmV_{p-p} = 2V_m.
  3. Cycle: One complete set of positive and negative values of an alternating quantity before it repeats itself. One complete cycle corresponds to 360∘360^\circ or 2π2\pi electrical radians.
  4. Time Period (TT): The time taken in seconds by an alternating quantity to complete one full cycle.
  5. Frequency (ff): The number of cycles completed per second. Its SI unit is hertz (Hz) (or cycles/second). f=1TandT=1ff = \frac{1}{T} \quad \text{and} \quad T = \frac{1}{f} (In India, the standard AC power supply frequency is f=50 Hzf = 50\text{ Hz}, giving T=150=0.02 s=20 msT = \frac{1}{50} = 0.02\text{ s} = 20\text{ ms}.)
  6. Angular Frequency (ω\omega): The rate of change of angle in radians per second. Since one cycle equals 2π2\pi radians in time TT: ω=2πT=2πf(rad/s)\omega = \frac{2\pi}{T} = 2\pi f \quad \text{(rad/s)}
  7. Electrical Angle vs. Mechanical Angle: In an AC machine having PP magnetic poles, one complete mechanical revolution (360∘360^\circ mechanical) produces P/2P/2 complete electrical cycles. Therefore: θelectrical=P2θmechanicalandf=PN120\theta_{\text{electrical}} = \frac{P}{2} \theta_{\text{mechanical}} \quad \text{and} \quad f = \frac{PN}{120} where NN is the rotational speed in revolutions per minute (rpm).

Worked Example 1

Problem: A rectangular coil of 200200 turns having dimensions 30 cm×20 cm30\text{ cm} \times 20\text{ cm} is rotated at a constant speed of 1500 rpm1500\text{ rpm} in a uniform magnetic field of flux density 0.1 T0.1\text{ T}. Calculate: (a) Frequency and time period of the generated voltage, (b) Maximum value of induced emf, (c) Equation of the instantaneous emf, and (d) Instantaneous emf at t=2 mst = 2\text{ ms} from the start of the cycle.

Solution:

  1. Identify given data:

    • Number of turns, N=200N = 200
    • Area of coil, A=0.30 m×0.20 m=0.06 m2A = 0.30\text{ m} \times 0.20\text{ m} = 0.06\text{ m}^2
    • Speed, n=1500 rpmn = 1500\text{ rpm} (for a basic 2-pole field, 1 rev=1 cycle1\text{ rev} = 1\text{ cycle})
    • Flux density, B=0.1 TB = 0.1\text{ T}
  2. Calculate frequency (ff) and time period (TT): f=n60=150060=25 Hzf = \frac{n}{60} = \frac{1500}{60} = 25\text{ Hz} T=1f=125=0.04 s=40 msT = \frac{1}{f} = \frac{1}{25} = 0.04\text{ s} = 40\text{ ms} Angular frequency: ω=2πf=2π×25=50π≈157.08 rad/s\omega = 2\pi f = 2\pi \times 25 = 50\pi \approx 157.08\text{ rad/s}

  3. Calculate maximum induced emf (EmE_m): Em=ωNBA=157.08×200×0.1×0.06=188.5 VE_m = \omega N B A = 157.08 \times 200 \times 0.1 \times 0.06 = 188.5\text{ V}

  4. Write the equation of instantaneous emf: e(t)=Emsin⁡(ωt)=188.5sin⁡(157.08t) Ve(t) = E_m \sin(\omega t) = 188.5 \sin(157.08 t)\text{ V}

  5. Calculate instantaneous emf at t=2 ms=0.002 st = 2\text{ ms} = 0.002\text{ s}: ωt=157.08×0.002=0.31416 rad=18∘\omega t = 157.08 \times 0.002 = 0.31416\text{ rad} = 18^\circ e(0.002)=188.5sin⁡(18∘)=188.5×0.3090=58.25 Ve(0.002) = 188.5 \sin(18^\circ) = 188.5 \times 0.3090 = 58.25\text{ V}

Answer: (a) f=25 Hz,T=0.04 sf = 25\text{ Hz}, T = 0.04\text{ s}; (b) Em=188.5 VE_m = 188.5\text{ V}; (c) e(t)=188.5sin⁡(157.08t) Ve(t) = 188.5\sin(157.08t)\text{ V}; (d) e=58.25 Ve = 58.25\text{ V}.

Summary

  • Instantaneous sinusoidal emf: e(t)=Emsin⁡(ωt)e(t) = E_m \sin(\omega t), where Em=2πfNBAE_m = 2\pi f N B A.
  • Frequency f=1/Tf = 1/T and angular frequency ω=2πf rad/s\omega = 2\pi f\text{ rad/s}.
  • For a PP-pole machine rotating at N rpmN\text{ rpm}, f=PN120 Hzf = \frac{PN}{120}\text{ Hz}.

Average value, RMS value, form factor and peak factor

Average Value (IavgI_{\text{avg}} or VavgV_{\text{avg}})

Definition of Average Value

The average value of an alternating current is defined as that steady (DC) current which transfers across any circuit the same amount of electric charge in a given time interval as is transferred by the alternating current in the same time interval.

For a symmetrical alternating waveform (like a pure sine wave), the positive half-cycle is identical in area to the negative half-cycle. Hence, the average value over one complete cycle is always zero. Therefore, for symmetrical waveforms, the average value is always defined over a half-cycle (from θ=0\theta = 0 to θ=π\theta = \pi).

In general, for a waveform i(θ)i(\theta) over an interval of base length BB:

Iavg=Area under the curve over the intervalBase length of the interval=1B∫0Bi(θ) dθI_{\text{avg}} = \frac{\text{Area under the curve over the interval}}{\text{Base length of the interval}} = \frac{1}{B} \int_{0}^{B} i(\theta) \, d\theta

Derivation of Average Value for a Sinusoidal Waveform:

  1. Consider a sinusoidal current i=Imsin⁡θi = I_m \sin\theta.
  2. Integrating over one positive half-cycle (θ=0\theta = 0 to θ=π\theta = \pi, so base B=πB = \pi): Iavg=1π∫0πImsin⁡θ dθ=Imπ[−cos⁡θ]0πI_{\text{avg}} = \frac{1}{\pi} \int_{0}^{\pi} I_m \sin\theta \, d\theta = \frac{I_m}{\pi} \Big[ -\cos\theta \Big]_{0}^{\pi}
  3. Substituting the limits (cos⁡π=−1\cos\pi = -1 and cos⁡0=1\cos 0 = 1): Iavg=Imπ[−(−1)−(−1)]=2Imπ≈0.637ImI_{\text{avg}} = \frac{I_m}{\pi} \left[ -(-1) - (-1) \right] = \frac{2 I_m}{\pi} \approx 0.637 I_m Similarly, for a sinusoidal voltage:
Vavg=2Vmπ≈0.637VmV_{\text{avg}} = \frac{2 V_m}{\pi} \approx 0.637 V_m

Root Mean Square (RMS) or Effective Value (IrmsI_{\text{rms}} or VrmsV_{\text{rms}})

Definition of RMS (Effective) Value

The RMS (Root Mean Square) or effective value of an alternating current is defined as that steady (DC) current which, when flowing through a given resistance for a given time, produces the exact same amount of heat energy as is produced by the alternating current when flowing through the same resistance for the same time.

(Note: All standard AC voltmeters and ammeters are calibrated to read RMS values, and domestic supply ratings like "230 V230\text{ V} AC" always specify the RMS value unless stated otherwise.)

Mathematically, for a periodic waveform i(θ)i(\theta) of period TT (or 2π2\pi radians):

Irms=1T∫0T[i(t)]2 dt=12π∫02π[i(θ)]2 dθI_{\text{rms}} = \sqrt{\frac{1}{T} \int_{0}^{T} [i(t)]^2 \, dt} = \sqrt{\frac{1}{2\pi} \int_{0}^{2\pi} [i(\theta)]^2 \, d\theta}

Derivation of RMS Value for a Sinusoidal Waveform:

  1. Consider a sinusoidal current i=Imsin⁡θi = I_m \sin\theta. Because [i(θ)]2=Im2sin⁡2θ[i(\theta)]^2 = I_m^2 \sin^2\theta is identical over both positive and negative half-cycles, the mean of the square over a half-cycle (00 to π\pi) is the same as over a full cycle (00 to 2π2\pi).
  2. Taking the integral over 00 to π\pi: Irms2=1π∫0πIm2sin⁡2θ dθI_{\text{rms}}^2 = \frac{1}{\pi} \int_{0}^{\pi} I_m^2 \sin^2\theta \, d\theta
  3. Using the trigonometric identity sin⁡2θ=1−cos⁡2θ2\sin^2\theta = \frac{1 - \cos 2\theta}{2}: Irms2=Im22π∫0π(1−cos⁡2θ) dθ=Im22π[θ−sin⁡2θ2]0πI_{\text{rms}}^2 = \frac{I_m^2}{2\pi} \int_{0}^{\pi} (1 - \cos 2\theta) \, d\theta = \frac{I_m^2}{2\pi} \left[ \theta - \frac{\sin 2\theta}{2} \right]_{0}^{\pi}
  4. Since sin⁡(2π)=0\sin(2\pi) = 0 and sin⁡(0)=0\sin(0) = 0: Irms2=Im22π(π−0)=Im22I_{\text{rms}}^2 = \frac{I_m^2}{2\pi} (\pi - 0) = \frac{I_m^2}{2}
  5. Taking the square root on both sides: Irms=Im2≈0.707ImI_{\text{rms}} = \frac{I_m}{\sqrt{2}} \approx 0.707 I_m Similarly, for a sinusoidal voltage:
Vrms=Vm2≈0.707VmV_{\text{rms}} = \frac{V_m}{\sqrt{2}} \approx 0.707 V_m

Form Factor (KfK_f) and Peak (Crest) Factor (KpK_p)

Form Factor (KfK_f)

The form factor of an alternating waveform is defined as the ratio of its RMS value to its average value:

Form Factor (Kf)=RMS ValueAverage Value=IrmsIavg\text{Form Factor } (K_f) = \frac{\text{RMS Value}}{\text{Average Value}} = \frac{I_{\text{rms}}}{I_{\text{avg}}}

For a pure sinusoidal waveform:

Kf=Im/22Im/π=π22≈1.11K_f = \frac{I_m / \sqrt{2}}{2 I_m / \pi} = \frac{\pi}{2\sqrt{2}} \approx 1.11

Peak Factor / Crest Factor / Amplitude Factor (KpK_p)

The peak factor (or crest factor) of an alternating waveform is defined as the ratio of its maximum (peak) value to its RMS value:

Peak Factor (Kp)=Maximum (Peak) ValueRMS Value=ImIrms\text{Peak Factor } (K_p) = \frac{\text{Maximum (Peak) Value}}{\text{RMS Value}} = \frac{I_m}{I_{\text{rms}}}

For a pure sinusoidal waveform:

Kp=ImIm/2=2≈1.414K_p = \frac{I_m}{I_m / \sqrt{2}} = \sqrt{2} \approx 1.414

Summary Table for Standard Waveforms

Waveform TypeAverage ValueRMS ValueForm Factor (KfK_f)Peak Factor (KpK_p)
Pure Sine Wave (or full-wave rectified sine)2Vmπ=0.637Vm\frac{2 V_m}{\pi} = 0.637 V_mVm2=0.707Vm\frac{V_m}{\sqrt{2}} = 0.707 V_m1.111.112=1.414\sqrt{2} = 1.414
Half-Wave Rectified Sine WaveVmπ=0.318Vm\frac{V_m}{\pi} = 0.318 V_mVm2=0.5Vm\frac{V_m}{2} = 0.5 V_mπ2=1.57\frac{\pi}{2} = 1.572.02.0
Symmetrical Square Wave (peak ±Vm\pm V_m)VmV_mVmV_m1.01.01.01.0
Triangular / Sawtooth Wave (peak VmV_m)Vm2=0.5Vm\frac{V_m}{2} = 0.5 V_mVm3=0.577Vm\frac{V_m}{\sqrt{3}} = 0.577 V_m23=1.155\frac{2}{\sqrt{3}} = 1.1553=1.732\sqrt{3} = 1.732

Worked Example 1

Problem: An alternating voltage is given by v(t)=325.27sin⁡(314t) Vv(t) = 325.27 \sin(314 t)\text{ V}. Find: (a) Maximum voltage, (b) RMS voltage, (c) Average voltage, (d) Frequency, (e) Time period, and (f) Form factor.

Solution:

  1. Compare v(t)=325.27sin⁡(314t)v(t) = 325.27 \sin(314 t) with v(t)=Vmsin⁡(ωt)v(t) = V_m \sin(\omega t):
    • (a) Maximum voltage: Vm=325.27 VV_m = 325.27\text{ V}
    • Angular frequency: ω=314 rad/s\omega = 314\text{ rad/s}
  2. (b) RMS voltage: Vrms=Vm2=325.271.4142=230 VV_{\text{rms}} = \frac{V_m}{\sqrt{2}} = \frac{325.27}{1.4142} = 230\text{ V}
  3. (c) Average voltage over a half-cycle: Vavg=2Vmπ=0.637×325.27=207.2 VV_{\text{avg}} = \frac{2 V_m}{\pi} = 0.637 \times 325.27 = 207.2\text{ V}
  4. (d) Frequency: f=ω2π=3142×3.1416=50 Hzf = \frac{\omega}{2\pi} = \frac{314}{2 \times 3.1416} = 50\text{ Hz}
  5. (e) Time period: T=1f=150=0.02 s=20 msT = \frac{1}{f} = \frac{1}{50} = 0.02\text{ s} = 20\text{ ms}
  6. (f) Form factor: Kf=VrmsVavg=230207.2=1.11K_f = \frac{V_{\text{rms}}}{V_{\text{avg}}} = \frac{230}{207.2} = 1.11

Answer: Vm=325.27 VV_m = 325.27\text{ V}, Vrms=230 VV_{\text{rms}} = 230\text{ V}, Vavg=207.2 VV_{\text{avg}} = 207.2\text{ V}, f=50 Hzf = 50\text{ Hz}, T=0.02 sT = 0.02\text{ s}, Kf=1.11K_f = 1.11.

Worked Example 2

Problem: Find the average value, RMS value, and form factor of a periodic voltage waveform that increases linearly from 0 V0\text{ V} to 100 V100\text{ V} in 0.01 s0.01\text{ s} and then drops instantly to 0 V0\text{ V}, repeating with a time period T=0.01 sT = 0.01\text{ s} (a sawtooth waveform).

Solution:

  1. Write the equation of the waveform for one period (0≤t≤T0 \le t \le T): With Vm=100 VV_m = 100\text{ V} and T=0.01 sT = 0.01\text{ s}, the straight line through the origin is: v(t)=VmTtv(t) = \frac{V_m}{T} t
  2. Calculate the average value (VavgV_{\text{avg}}): Vavg=1T∫0T(VmTt)dt=VmT2[t22]0T=Vm2=1002=50 VV_{\text{avg}} = \frac{1}{T} \int_{0}^{T} \left(\frac{V_m}{T} t\right) dt = \frac{V_m}{T^2} \left[\frac{t^2}{2}\right]_{0}^{T} = \frac{V_m}{2} = \frac{100}{2} = 50\text{ V}
  3. Calculate the RMS value (VrmsV_{\text{rms}}): Vrms=1T∫0T(VmTt)2dt=Vm2T3[t33]0T=Vm3=1001.732=57.74 VV_{\text{rms}} = \sqrt{\frac{1}{T} \int_{0}^{T} \left(\frac{V_m}{T} t\right)^2 dt} = \sqrt{\frac{V_m^2}{T^3} \left[\frac{t^3}{3}\right]_{0}^{T}} = \frac{V_m}{\sqrt{3}} = \frac{100}{1.732} = 57.74\text{ V}
  4. Calculate the form factor (KfK_f): Kf=VrmsVavg=57.7450=1.155K_f = \frac{V_{\text{rms}}}{V_{\text{avg}}} = \frac{57.74}{50} = 1.155

Answer: Vavg=50 VV_{\text{avg}} = 50\text{ V}, Vrms=57.74 VV_{\text{rms}} = 57.74\text{ V}, Kf=1.155K_f = 1.155.

Summary

  • For a sine wave: Iavg=2Imπ=0.637ImI_{\text{avg}} = \frac{2I_m}{\pi} = 0.637 I_m and Irms=Im2=0.707ImI_{\text{rms}} = \frac{I_m}{\sqrt{2}} = 0.707 I_m.
  • Form factor Kf=RMSAverage=1.11K_f = \frac{\text{RMS}}{\text{Average}} = 1.11 (for sine wave).
  • Peak factor Kp=PeakRMS=1.414K_p = \frac{\text{Peak}}{\text{RMS}} = 1.414 (for sine wave).

Phasor representation of sinusoidal quantities

Syllabus: AC Circuits – Phasor Representation

  • Phasor representation of sinusoidal quantities
  • Trigonometric, Rectangular, Polar and complex forms

Concept of a Phasor

Phasor

A phasor is a directed line segment (rotating vector) rotating counter-clockwise in the complex plane with a constant angular velocity ω\omega equal to the angular frequency of the sinusoidal quantity it represents.

  • The length of the phasor represents either the maximum value (VmV_m) or, by standard engineering convention, the RMS value (V=Vm/2V = V_m/\sqrt{2}) of the sinusoid.
  • The angle (ϕ\phi) that the phasor makes with the positive real (reference) axis at t=0t = 0 represents the phase angle of the sinusoid.
  • The projection of a rotating phasor of length VmV_m on the vertical (imaginary) axis at any instant tt gives the instantaneous value v(t)=Vmsin⁡(ωt+ϕ)v(t) = V_m \sin(\omega t + \phi).

Phase and Phase Difference

Phase

The phase of an alternating quantity at any instant is the fraction of a time period (or the angle in radians/degrees) that has elapsed since the quantity last passed through its zero reference position in the positive direction. In v(t)=Vmsin⁡(ωt+ϕ1)v(t) = V_m \sin(\omega t + \phi_1), the argument (ωt+ϕ1)(\omega t + \phi_1) is the phase at time tt, and ϕ1\phi_1 is the initial phase angle at t=0t = 0.

Phase Difference

When two alternating quantities of the same frequency ω\omega are given by:

v(t)=Vmsin⁡(ωt+ϕ1)andi(t)=Imsin⁡(ωt+ϕ2)v(t) = V_m \sin(\omega t + \phi_1) \quad \text{and} \quad i(t) = I_m \sin(\omega t + \phi_2)

the difference between their phase angles, ϕ=ϕ1−ϕ2\phi = \phi_1 - \phi_2, is called the phase difference, which remains constant with time:

  1. In Phase (ϕ1−ϕ2=0∘\phi_1 - \phi_2 = 0^\circ): Both quantities pass through their zero and peak values of the same polarity at the exact same instant. Their phasors are collinear and point in the same direction.
  2. Leading (ϕ1>ϕ2\phi_1 > \phi_2): Voltage v(t)v(t) reaches its positive zero and positive peak earlier in time by angle ϕ=ϕ1−ϕ2\phi = \phi_1 - \phi_2 than current i(t)i(t). We say vv leads ii by angle ϕ\phi. In a phasor diagram (where rotation is counter-clockwise), the phasor V\mathbf{V} lies ahead of I\mathbf{I} in the counter-clockwise direction by angle ϕ\phi.
  3. Lagging (ϕ1<ϕ2\phi_1 < \phi_2): Current i(t)i(t) reaches its peak behind voltage v(t)v(t) by angle ϕ\phi. We say ii lags behind vv by angle ϕ\phi (located clockwise relative to V\mathbf{V}).
Code
      Imaginary (+j)
          ^
          |      / V (Leads I by phi)
          |     /
          |    /  phi1
          |   /    \  phi2
   -------+--o----------------> Real (Reference Axis)
          |   \
          |    \ I (Lags V)

Mathematical Forms of a Phasor

Using the RMS value V=Vm/2V = V_m/\sqrt{2} and phase angle ϕ\phi, a sinusoidal quantity v(t)=2Vsin⁡(ωt+ϕ)v(t) = \sqrt{2} V \sin(\omega t + \phi) is represented as a complex phasor V\mathbf{V} in four equivalent mathematical forms:

  1. Polar Form: Specifies the RMS magnitude VV and the phase angle ϕ\phi (usually in degrees): V=V∠ϕ\mathbf{V} = V \angle \phi

  2. Exponential (Complex) Form: Based on Euler's identity ejϕ=cos⁡ϕ+jsin⁡ϕe^{j\phi} = \cos\phi + j\sin\phi, where j=−1j = \sqrt{-1} is the imaginary operator in electrical engineering (used instead of ii to avoid confusion with current): V=Vejϕ\mathbf{V} = V e^{j\phi}

  3. Trigonometric Form: Expanding the exponential form using Euler's identity: V=V(cos⁡ϕ+jsin⁡ϕ)\mathbf{V} = V (\cos\phi + j\sin\phi)

  4. Rectangular (Cartesian) Form: Expresses the phasor in terms of its real (in-phase) component aa and imaginary (quadrature) component bb in the complex plane: V=a+jb\mathbf{V} = a + jb where: a=Vcos⁡ϕandb=Vsin⁡ϕa = V \cos\phi \quad \text{and} \quad b = V \sin\phi

Conversions Between Rectangular and Polar Forms

  • Polar to Rectangular (V∠ϕ⟶a+jbV \angle \phi \longrightarrow a + jb): a=Vcos⁡ϕ,b=Vsin⁡ϕa = V \cos\phi, \qquad b = V \sin\phi

  • Rectangular to Polar (a+jb⟶V∠ϕa + jb \longrightarrow V \angle \phi): V=a2+b2,ϕ=tan⁡−1(ba)V = \sqrt{a^2 + b^2}, \qquad \phi = \tan^{-1}\left(\frac{b}{a}\right) (Care must be taken with the signs of aa and bb to place ϕ\phi in the correct quadrant: if a<0a < 0 and b>0b > 0, ϕ=180∘−tan⁡−1∣b/a∣\phi = 180^\circ - \tan^{-1}|b/a|; if a<0a < 0 and b<0b < 0, ϕ=−180∘+tan⁡−1∣b/a∣\phi = -180^\circ + \tan^{-1}|b/a|.)

Properties of the jj-Operator and Phasor Arithmetic

  • Properties of jj:

    • j=−1=1∠90∘j = \sqrt{-1} = 1\angle 90^\circ (multiplying a phasor by jj rotates it counter-clockwise by 90∘90^\circ).
    • j2=−1=1∠180∘j^2 = -1 = 1\angle 180^\circ
    • j3=−j=1∠270∘=1∠−90∘j^3 = -j = 1\angle 270^\circ = 1\angle -90^\circ
    • j4=+1=1∠0∘j^4 = +1 = 1\angle 0^\circ
    • 1j=−j=1∠−90∘\frac{1}{j} = -j = 1\angle -90^\circ (dividing by jj or multiplying by −j-j rotates a phasor clockwise by 90∘90^\circ).
  • Addition and Subtraction (best done in Rectangular Form): If V1=a1+jb1\mathbf{V}_1 = a_1 + jb_1 and V2=a2+jb2\mathbf{V}_2 = a_2 + jb_2: V1±V2=(a1±a2)+j(b1±b2)\mathbf{V}_1 \pm \mathbf{V}_2 = (a_1 \pm a_2) + j(b_1 \pm b_2)

  • Multiplication and Division (best done in Polar Form): If V1=V1∠ϕ1\mathbf{V}_1 = V_1 \angle \phi_1 and V2=V2∠ϕ2\mathbf{V}_2 = V_2 \angle \phi_2: V1⋅V2=(V1V2)∠(ϕ1+ϕ2)\mathbf{V}_1 \cdot \mathbf{V}_2 = (V_1 V_2) \angle (\phi_1 + \phi_2) V1V2=(V1V2)∠(ϕ1−ϕ2)\frac{\mathbf{V}_1}{\mathbf{V}_2} = \left(\frac{V_1}{V_2}\right) \angle (\phi_1 - \phi_2)

Worked Example 1

Problem: Express the sinusoidal voltage v(t)=141.42sin⁡(314t−30∘) Vv(t) = 141.42 \sin(314t - 30^\circ)\text{ V} as an RMS phasor in Polar, Exponential, Trigonometric, and Rectangular forms.

Solution:

  1. Find the RMS magnitude and phase angle:
    • Peak voltage Vm=141.42 VV_m = 141.42\text{ V}
    • RMS voltage V=141.422=100 VV = \frac{141.42}{\sqrt{2}} = 100\text{ V}
    • Phase angle ϕ=−30∘=−π6 rad\phi = -30^\circ = -\frac{\pi}{6}\text{ rad}
  2. Write the four forms:
    • Polar form: V=100∠−30∘ V\mathbf{V} = 100 \angle -30^\circ\text{ V}
    • Exponential form: V=100e−j30∘ V=100e−jπ/6 V\mathbf{V} = 100 e^{-j30^\circ}\text{ V} = 100 e^{-j\pi/6}\text{ V}
    • Trigonometric form: V=100[cos⁡(−30∘)+jsin⁡(−30∘)]=100(cos⁡30∘−jsin⁡30∘) V\mathbf{V} = 100 \left[\cos(-30^\circ) + j\sin(-30^\circ)\right] = 100 (\cos 30^\circ - j\sin 30^\circ)\text{ V}
    • Rectangular form: a=100cos⁡(−30∘)=100×0.866=86.6 Va = 100 \cos(-30^\circ) = 100 \times 0.866 = 86.6\text{ V} b=100sin⁡(−30∘)=100×(−0.5)=−50 Vb = 100 \sin(-30^\circ) = 100 \times (-0.5) = -50\text{ V} V=(86.6−j50) V\mathbf{V} = (86.6 - j50)\text{ V}

Answer: Polar: 100∠−30∘ V100\angle -30^\circ\text{ V}; Exponential: 100e−j30∘ V100e^{-j30^\circ}\text{ V}; Trigonometric: 100(cos⁡30∘−jsin⁡30∘) V100(\cos 30^\circ - j\sin 30^\circ)\text{ V}; Rectangular: (86.6−j50) V(86.6 - j50)\text{ V}.

Worked Example 2

Problem: Two alternating currents entering a node are given by i1(t)=102sin⁡(ωt+30∘) Ai_1(t) = 10\sqrt{2}\sin(\omega t + 30^\circ)\text{ A} and i2(t)=202sin⁡(ωt−45∘) Ai_2(t) = 20\sqrt{2}\sin(\omega t - 45^\circ)\text{ A}. Find the total current i(t)=i1(t)+i2(t)i(t) = i_1(t) + i_2(t) in time-domain sinusoidal form.

Solution:

  1. Convert i1(t)i_1(t) and i2(t)i_2(t) to RMS Polar and Rectangular forms:
    • I1=10∠30∘=10(cos⁡30∘+jsin⁡30∘)=8.66+j5.0 A\mathbf{I}_1 = 10\angle 30^\circ = 10(\cos 30^\circ + j\sin 30^\circ) = 8.66 + j5.0\text{ A}
    • I2=20∠−45∘=20(cos⁡45∘−jsin⁡45∘)=14.14−j14.14 A\mathbf{I}_2 = 20\angle -45^\circ = 20(\cos 45^\circ - j\sin 45^\circ) = 14.14 - j14.14\text{ A}
  2. Add the two phasors in rectangular form: I=I1+I2=(8.66+14.14)+j(5.0−14.14)=22.80−j9.14 A\mathbf{I} = \mathbf{I}_1 + \mathbf{I}_2 = (8.66 + 14.14) + j(5.0 - 14.14) = 22.80 - j9.14\text{ A}
  3. Convert I\mathbf{I} back to polar form: I=(22.80)2+(−9.14)2=519.84+83.54=603.38=24.56 AI = \sqrt{(22.80)^2 + (-9.14)^2} = \sqrt{519.84 + 83.54} = \sqrt{603.38} = 24.56\text{ A} ϕ=tan⁡−1(−9.1422.80)=−21.84∘\phi = \tan^{-1}\left(\frac{-9.14}{22.80}\right) = -21.84^\circ I=24.56∠−21.84∘ A\mathbf{I} = 24.56 \angle -21.84^\circ\text{ A}
  4. Write the time-domain expression (Im=2II_m = \sqrt{2} I): i(t)=24.562sin⁡(ωt−21.84∘)=34.73sin⁡(ωt−21.84∘) Ai(t) = 24.56\sqrt{2} \sin(\omega t - 21.84^\circ) = 34.73 \sin(\omega t - 21.84^\circ)\text{ A}

Answer: i(t)=34.73sin⁡(ωt−21.84∘) Ai(t) = 34.73 \sin(\omega t - 21.84^\circ)\text{ A}.

Summary

  • A sinusoid v(t)=2Vsin⁡(ωt+ϕ)v(t) = \sqrt{2}V\sin(\omega t + \phi) is represented as an RMS phasor V=V∠ϕ=V(cos⁡ϕ+jsin⁡ϕ)=a+jb\mathbf{V} = V\angle\phi = V(\cos\phi + j\sin\phi) = a + jb.
  • Use rectangular form for addition/subtraction and polar form for multiplication/division.
  • Multiplying by jj advances the phase by +90∘+90^\circ; multiplying by −j-j (or dividing by jj) retards the phase by −90∘-90^\circ.

Analysis of simple AC circuits: Purely resistive, inductive and capacitive circuits

Syllabus: Analysis of Simple AC Circuits

  • Purely resistive, inductive & capacitive circuits
  • Inductive and capacitive reactance, concept of impedance - numerical problems

1. AC Circuit with a Pure Resistor (RR)

Consider an AC voltage source v(t)=Vmsin⁡(ωt)v(t) = V_m \sin(\omega t) connected across a pure resistor of resistance RR ohms.

Code
         i(t) --->
      +-----/\/\/\-----+
      |       R        |
     (~) v(t)          |
      |                |
      +----------------+
  1. Current Equation: By Ohm's law, the instantaneous current is: i(t)=v(t)R=Vmsin⁡(ωt)R=Imsin⁡(ωt)i(t) = \frac{v(t)}{R} = \frac{V_m \sin(\omega t)}{R} = I_m \sin(\omega t) where peak current Im=VmRI_m = \frac{V_m}{R} and RMS current I=VRI = \frac{V}{R}.
  2. Phase Relationship: Comparing v(t)=Vmsin⁡(ωt)v(t) = V_m \sin(\omega t) and i(t)=Imsin⁡(ωt)i(t) = I_m \sin(\omega t), the phase angle between voltage and current in a pure resistor is zero (ϕ=0∘\phi = 0^\circ). Voltage and current are in phase.
  3. Phasor Relation and Complex Impedance: If V=V∠0∘\mathbf{V} = V\angle 0^\circ, then I=I∠0∘\mathbf{I} = I\angle 0^\circ. ZR=VI=R∠0∘=R+j0(Ω)\mathbf{Z}_R = \frac{\mathbf{V}}{\mathbf{I}} = R\angle 0^\circ = R + j0 \quad (\Omega)
  4. Instantaneous and Average Power: p(t)=v(t)⋅i(t)=(Vmsin⁡ωt)(Imsin⁡ωt)=VmImsin⁡2(ωt)p(t) = v(t) \cdot i(t) = (V_m \sin\omega t)(I_m \sin\omega t) = V_m I_m \sin^2(\omega t) Using sin⁡2(ωt)=1−cos⁡(2ωt)2\sin^2(\omega t) = \frac{1 - \cos(2\omega t)}{2} and VmIm=2VIV_m I_m = 2VI: p(t)=VI(1−cos⁡2ωt)=VI−VIcos⁡(2ωt)p(t) = V I (1 - \cos 2\omega t) = V I - V I \cos(2\omega t) Since the average of cos⁡(2ωt)\cos(2\omega t) over a full cycle is zero, the average power consumed over a cycle is: P=VI=I2R=V2R(watts, W)P = V I = I^2 R = \frac{V^2}{R} \quad \text{(watts, W)}

2. AC Circuit with a Pure Inductor (LL)

Consider an AC voltage source v(t)=Vmsin⁡(ωt)v(t) = V_m \sin(\omega t) connected across a pure (lossless, R=0R = 0) inductor of inductance LL henrys.

  1. Current Equation: By KVL and Faraday's law, the applied voltage equals the self-induced voltage drop across the inductor: v(t)=Ldidt=Vmsin⁡(ωt)v(t) = L \frac{di}{dt} = V_m \sin(\omega t) Integrating both sides with respect to tt: i(t)=VmL∫sin⁡(ωt) dt=−VmωLcos⁡(ωt)i(t) = \frac{V_m}{L} \int \sin(\omega t) \, dt = -\frac{V_m}{\omega L} \cos(\omega t) Using −cos⁡(ωt)=sin⁡(ωt−90∘)-\cos(\omega t) = \sin(\omega t - 90^\circ): i(t)=Imsin⁡(ωt−90∘)=Imsin⁡(ωt−π2)i(t) = I_m \sin(\omega t - 90^\circ) = I_m \sin\left(\omega t - \frac{\pi}{2}\right) where the peak current is Im=VmωL=VmXLI_m = \frac{V_m}{\omega L} = \frac{V_m}{X_L}.
  2. Inductive Reactance (XLX_L): The opposition offered by an inductor to the flow of alternating current is called inductive reactance (XLX_L), measured in ohms (Ω\Omega): XL=ωL=2πfL(Ω)X_L = \omega L = 2\pi f L \quad (\Omega)
    • XLX_L is directly proportional to frequency ff. For DC (f=0f = 0), XL=0 ΩX_L = 0\ \Omega, so a pure inductor acts as a short circuit to steady DC.
  3. Phase Relationship: In a pure inductor, the current lags behind the applied voltage by 90∘90^\circ (π/2 rad\pi/2\text{ rad}), or equivalently, voltage leads current by 90∘90^\circ.
  4. Phasor Relation and Complex Impedance: If V=V∠0∘\mathbf{V} = V\angle 0^\circ, then I=I∠−90∘\mathbf{I} = I\angle -90^\circ. ZL=VI=V∠0∘I∠−90∘=XL∠90∘=jXL=jωL(Ω)\mathbf{Z}_L = \frac{\mathbf{V}}{\mathbf{I}} = \frac{V\angle 0^\circ}{I\angle -90^\circ} = X_L \angle 90^\circ = j X_L = j\omega L \quad (\Omega)
  5. Instantaneous and Average Power: p(t)=v(t)⋅i(t)=(Vmsin⁡ωt)(−Imcos⁡ωt)=−VmIm2sin⁡(2ωt)=−VIsin⁡(2ωt)p(t) = v(t) \cdot i(t) = (V_m \sin\omega t)\left(-I_m \cos\omega t\right) = -\frac{V_m I_m}{2} \sin(2\omega t) = -V I \sin(2\omega t) The instantaneous power is a double-frequency sine wave (2f2f) that alternates equally between positive (energy absorbed from source to build magnetic field, 12Li2\frac{1}{2}Li^2) and negative (energy returned completely to the source when magnetic field collapses). Therefore, the average power consumed over a complete cycle is zero: P=0 WP = 0\text{ W}

3. AC Circuit with a Pure Capacitor (CC)

Consider an AC voltage source v(t)=Vmsin⁡(ωt)v(t) = V_m \sin(\omega t) connected across a pure capacitor of capacitance CC farads.

  1. Current Equation: The instantaneous charge on the capacitor is q(t)=Cv(t)q(t) = C v(t), so the current is: i(t)=dqdt=Cdvdt=Cddt(Vmsin⁡ωt)=ωCVmcos⁡(ωt)i(t) = \frac{dq}{dt} = C \frac{dv}{dt} = C \frac{d}{dt} \left(V_m \sin\omega t\right) = \omega C V_m \cos(\omega t) Using cos⁡(ωt)=sin⁡(ωt+90∘)\cos(\omega t) = \sin(\omega t + 90^\circ): i(t)=Imsin⁡(ωt+90∘)=Imsin⁡(ωt+π2)i(t) = I_m \sin(\omega t + 90^\circ) = I_m \sin\left(\omega t + \frac{\pi}{2}\right) where the peak current is Im=ωCVm=Vm1/(ωC)=VmXCI_m = \omega C V_m = \frac{V_m}{1/(\omega C)} = \frac{V_m}{X_C}.
  2. Capacitive Reactance (XCX_C): The opposition offered by a capacitor to the flow of alternating current is called capacitive reactance (XCX_C), measured in ohms (Ω\Omega): XC=1ωC=12πfC(Ω)X_C = \frac{1}{\omega C} = \frac{1}{2\pi f C} \quad (\Omega)
    • XCX_C is inversely proportional to frequency ff. For DC (f=0f = 0), XC=∞ ΩX_C = \infty\ \Omega, so a capacitor acts as an open circuit to steady DC.
  3. Phase Relationship: In a pure capacitor, the current leads the applied voltage by 90∘90^\circ (π/2 rad\pi/2\text{ rad}), or equivalently, voltage lags behind current by 90∘90^\circ.
  4. Phasor Relation and Complex Impedance: If V=V∠0∘\mathbf{V} = V\angle 0^\circ, then I=I∠+90∘\mathbf{I} = I\angle +90^\circ. ZC=VI=V∠0∘I∠90∘=XC∠−90∘=−jXC=1jωC(Ω)\mathbf{Z}_C = \frac{\mathbf{V}}{\mathbf{I}} = \frac{V\angle 0^\circ}{I\angle 90^\circ} = X_C \angle -90^\circ = -j X_C = \frac{1}{j\omega C} \quad (\Omega)
  5. Instantaneous and Average Power: p(t)=v(t)⋅i(t)=(Vmsin⁡ωt)(Imcos⁡ωt)=VmIm2sin⁡(2ωt)=VIsin⁡(2ωt)p(t) = v(t) \cdot i(t) = (V_m \sin\omega t)(I_m \cos\omega t) = \frac{V_m I_m}{2} \sin(2\omega t) = V I \sin(2\omega t) Energy stored in the electrostatic field (12Cv2\frac{1}{2}Cv^2) during one quarter-cycle is returned completely to the source during the next quarter-cycle. Hence, the average power consumed over a complete cycle is zero: P=0 WP = 0\text{ W}

Concept of Impedance (Z\mathbf{Z})

In general AC circuits containing resistance RR and reactance XX, impedance (Z\mathbf{Z}) is defined as the complex ratio of the voltage phasor V\mathbf{V} to the current phasor I\mathbf{I}:

Z=VI=R+jX=Z∠ϕ(Ω)\mathbf{Z} = \frac{\mathbf{V}}{\mathbf{I}} = R + jX = Z \angle \phi \quad (\Omega)

where the magnitude of impedance is Z=R2+X2Z = \sqrt{R^2 + X^2} and the phase angle is ϕ=tan⁡−1(X/R)\phi = \tan^{-1}(X/R).

Comparison of Pure R, Pure L, and Pure C Circuits

ParameterPure Resistor (RR)Pure Inductor (LL)Pure Capacitor (CC)
Opposition to ACResistance RR (independent of ff)Reactance XL=2πfLX_L = 2\pi f L (∝f\propto f)Reactance XC=12πfCX_C = \frac{1}{2\pi f C} (∝1f\propto \frac{1}{f})
Complex Impedance (Z\mathbf{Z})R=R∠0∘R = R\angle 0^\circ+jXL=XL∠+90∘+jX_L = X_L\angle +90^\circ−jXC=XC∠−90∘-jX_C = X_C\angle -90^\circ
Phase of I\mathbf{I} relative to V\mathbf{V}I\mathbf{I} is in phase with V\mathbf{V} (ϕ=0∘\phi = 0^\circ)I\mathbf{I} lags V\mathbf{V} by 90∘90^\circ (ϕ=+90∘\phi = +90^\circ)I\mathbf{I} leads V\mathbf{V} by 90∘90^\circ (ϕ=−90∘\phi = -90^\circ)
Average Power (PP)P=VI=I2RP = VI = I^2 RP=0 WP = 0\text{ W}P=0 WP = 0\text{ W}

Worked Example 1

Problem: A pure inductor of L=0.15 HL = 0.15\text{ H} is connected across a 230 V,50 Hz230\text{ V}, 50\text{ Hz} AC supply. Find: (a) Inductive reactance, (b) RMS current, (c) Peak current, and (d) Equation for instantaneous current if v(t)=2302sin⁡(314t) Vv(t) = 230\sqrt{2}\sin(314t)\text{ V}.

Solution:

  1. (a) Inductive reactance: XL=2πfL=2π×50×0.15=47.12 ΩX_L = 2\pi f L = 2\pi \times 50 \times 0.15 = 47.12\ \Omega
  2. (b) RMS current: I=VXL=23047.12=4.88 AI = \frac{V}{X_L} = \frac{230}{47.12} = 4.88\text{ A}
  3. (c) Peak current: Im=2I=1.414×4.88=6.90 AI_m = \sqrt{2} I = 1.414 \times 4.88 = 6.90\text{ A}
  4. (d) Since current lags voltage by 90∘90^\circ in a pure inductor: i(t)=6.90sin⁡(314t−90∘) Ai(t) = 6.90 \sin(314t - 90^\circ)\text{ A}

Answer: XL=47.12 ΩX_L = 47.12\ \Omega, I=4.88 AI = 4.88\text{ A}, Im=6.90 AI_m = 6.90\text{ A}, i(t)=6.90sin⁡(314t−90∘) Ai(t) = 6.90\sin(314t - 90^\circ)\text{ A}.

Worked Example 2

Problem: A 50 μF50\ \mu\text{F} capacitor is connected across a 200 V,50 Hz200\text{ V}, 50\text{ Hz} single-phase AC supply. Calculate: (a) Capacitive reactance, (b) RMS current, and (c) Maximum power delivered by the source at any instant.

Solution:

  1. (a) Capacitive reactance: XC=12πfC=12π×50×50×10−6=63.66 ΩX_C = \frac{1}{2\pi f C} = \frac{1}{2\pi \times 50 \times 50 \times 10^{-6}} = 63.66\ \Omega
  2. (b) RMS current: I=VXC=20063.66=3.14 AI = \frac{V}{X_C} = \frac{200}{63.66} = 3.14\text{ A}
  3. (c) Instantaneous power is p(t)=VIsin⁡(2ωt)p(t) = VI\sin(2\omega t). Its maximum value (when sin⁡2ωt=1\sin 2\omega t = 1) is: Pinst, max=VI=200×3.14=628 WP_{\text{inst, max}} = V I = 200 \times 3.14 = 628\text{ W} (Note: Average power over a full cycle is 0 W0\text{ W}.)

Answer: XC=63.66 ΩX_C = 63.66\ \Omega, I=3.14 AI = 3.14\text{ A}, Pinst, max=628 WP_{\text{inst, max}} = 628\text{ W}.

Summary

  • Pure RR: ZR=R∠0∘\mathbf{Z}_R = R\angle 0^\circ, I\mathbf{I} in phase with V\mathbf{V}, P=VIP = VI.
  • Pure LL: ZL=jXL=ωL∠90∘\mathbf{Z}_L = jX_L = \omega L \angle 90^\circ, I\mathbf{I} lags V\mathbf{V} by 90∘90^\circ, P=0P = 0.
  • Pure CC: ZC=−jXC=1ωC∠−90∘\mathbf{Z}_C = -jX_C = \frac{1}{\omega C} \angle -90^\circ, I\mathbf{I} leads V\mathbf{V} by 90∘90^\circ, P=0P = 0.

RL, RC and RLC series AC circuits

Syllabus: RL, RC and RLC Series Circuits

  • RL, RC and RLC series circuits
  • Power factor, active, reactive and apparent power - simple numerical problems

1. Series RL Circuit

Consider a resistor RR and an inductor LL connected in series across an AC supply v(t)=Vmsin⁡(ωt)v(t) = V_m \sin(\omega t). Since the circuit is in series, the same current I=I∠0∘\mathbf{I} = I\angle 0^\circ (taken as the reference phasor) flows through both elements.

Code
         I --->      V_R          V_L
      +-----------/\/\/\-------uuuuuu-------+
      |             R            L          |
     (~) V                                  |
      |                                     |
      +-------------------------------------+
  1. Component Voltage Phasors:
    • Voltage drop across RR: VR=IR∠0∘=VR+j0\mathbf{V}_R = I R \angle 0^\circ = V_R + j0 (in phase with I\mathbf{I}).
    • Voltage drop across LL: VL=I(jXL)=IXL∠+90∘=jVL\mathbf{V}_L = I (j X_L) = I X_L \angle +90^\circ = j V_L (leads I\mathbf{I} by 90∘90^\circ).
  2. Total Supply Voltage and Voltage Triangle: By Kirchhoff's Voltage Law (KVL) in phasor form: V=VR+VL=VR+jVL=I(R+jXL)\mathbf{V} = \mathbf{V}_R + \mathbf{V}_L = V_R + j V_L = I(R + jX_L) Magnitude of supply voltage: V=VR2+VL2=IR2+XL2V = \sqrt{V_R^2 + V_L^2} = I \sqrt{R^2 + X_L^2}
  3. Impedance (Z\mathbf{Z}) and Impedance Triangle: Z=VI=R+jXL=Z∠+ϕ\mathbf{Z} = \frac{\mathbf{V}}{\mathbf{I}} = R + j X_L = Z \angle +\phi where magnitude Z=R2+XL2Z = \sqrt{R^2 + X_L^2} and phase angle ϕ=tan⁡−1(XLR)=tan⁡−1(VLVR)\phi = \tan^{-1}\left(\frac{X_L}{R}\right) = \tan^{-1}\left(\frac{V_L}{V_R}\right).
  4. Phase Relationship: Since ϕ\phi is positive (0∘<ϕ<90∘0^\circ < \phi < 90^\circ), the supply voltage V\mathbf{V} leads the current I\mathbf{I} by angle ϕ\phi, or current I\mathbf{I} lags behind voltage V\mathbf{V} by angle ϕ\phi.
Code
   Voltage Triangle (RL)             Impedance Triangle (RL)
          /|                                /|
       V / | V_L = I*X_L                 Z / | X_L
        /  |                              /  |
       /phi|                             /phi|
      +----+                            +----+
     V_R = I*R                            R

2. Series RC Circuit

Consider a resistor RR and a capacitor CC connected in series carrying reference current I=I∠0∘\mathbf{I} = I\angle 0^\circ.

  1. Component Voltage Phasors:
    • Voltage drop across RR: VR=IR∠0∘=VR\mathbf{V}_R = I R \angle 0^\circ = V_R (in phase with I\mathbf{I}).
    • Voltage drop across CC: VC=I(−jXC)=IXC∠−90∘=−jVC\mathbf{V}_C = I (-j X_C) = I X_C \angle -90^\circ = -j V_C (lags behind I\mathbf{I} by 90∘90^\circ).
  2. Total Supply Voltage: V=VR+VC=VR−jVC=I(R−jXC)\mathbf{V} = \mathbf{V}_R + \mathbf{V}_C = V_R - j V_C = I(R - jX_C) Magnitude: V=VR2+VC2=IR2+XC2V = \sqrt{V_R^2 + V_C^2} = I \sqrt{R^2 + X_C^2}
  3. Impedance (Z\mathbf{Z}): Z=VI=R−jXC=Z∠−ϕ\mathbf{Z} = \frac{\mathbf{V}}{\mathbf{I}} = R - j X_C = Z \angle -\phi where magnitude Z=R2+XC2Z = \sqrt{R^2 + X_C^2} and phase angle Magnitude ϕ=tan⁡−1(XCR)=tan⁡−1(VCVR)\phi = \tan^{-1}\left(\frac{X_C}{R}\right) = \tan^{-1}\left(\frac{V_C}{V_R}\right) (or θZ=tan⁡−1(−XC/R)=−ϕ\theta_Z = \tan^{-1}(-X_C/R) = -\phi).
  4. Phase Relationship: The supply voltage V\mathbf{V} lags behind I\mathbf{I} by angle ϕ\phi, or current I\mathbf{I} leads the supply voltage V\mathbf{V} by angle ϕ\phi (0∘<ϕ<90∘0^\circ < \phi < 90^\circ).

3. Series RLC Circuit

Consider a resistor RR, an inductor LL, and a capacitor CC connected in series across an AC supply V\mathbf{V}, carrying a common reference current I=I∠0∘\mathbf{I} = I\angle 0^\circ.

Code
         I --->    V_R       V_L       V_C
      +----------/\/\/\----uuuuuu------||------+
      |            R         L         C       |
     (~) V                                     |
      +----------------------------------------+
  1. Phasor KVL Equation:
    • VR=IR\mathbf{V}_R = I R (along +x+x axis, in phase with I\mathbf{I})
    • VL=+jIXL\mathbf{V}_L = +j I X_L (along +j+j axis, leading I\mathbf{I} by 90∘90^\circ)
    • VC=−jIXC\mathbf{V}_C = -j I X_C (along −j-j axis, lagging I\mathbf{I} by 90∘90^\circ) Since VL\mathbf{V}_L and VC\mathbf{V}_C are 180∘180^\circ out of phase with each other, they partially or fully cancel: V=VR+VL+VC=VR+j(VL−VC)=I[R+j(XL−XC)]\mathbf{V} = \mathbf{V}_R + \mathbf{V}_L + \mathbf{V}_C = V_R + j(V_L - V_C) = I \left[ R + j(X_L - X_C) \right] Magnitude of supply voltage: V=VR2+(VL−VC)2V = \sqrt{V_R^2 + (V_L - V_C)^2}
  2. Total Complex Impedance (Z\mathbf{Z}): Z=R+j(XL−XC)=R+jX=Z∠ϕ\mathbf{Z} = R + j(X_L - X_C) = R + jX = Z \angle \phi where net reactance is X=XL−XCX = X_L - X_C, impedance magnitude is: Z=R2+(XL−XC)2Z = \sqrt{R^2 + (X_L - X_C)^2} and phase angle is: ϕ=tan⁡−1(XL−XCR)=tan⁡−1(VL−VCVR)\phi = \tan^{-1}\left(\frac{X_L - X_C}{R}\right) = \tan^{-1}\left(\frac{V_L - V_C}{V_R}\right)

Three Operating Cases of an RLC Series Circuit:

ConditionNet Reactance (X=XL−XCX = X_L - X_C)Circuit NaturePhase of Current I\mathbf{I} relative to V\mathbf{V}Power Factor (cos⁡ϕ\cos\phi)
Case 1: XL>XCX_L > X_C (VL>VCV_L > V_C)Positive (+X+X)Predominantly InductiveI\mathbf{I} lags V\mathbf{V} by ϕ\phiLagging
Case 2: XL<XCX_L < X_C (VL<VCV_L < V_C)Negative (−X-X)Predominantly CapacitiveI\mathbf{I} leads V\mathbf{V} by $\phi
Case 3: XL=XCX_L = X_C (VL=VCV_L = V_C)Zero (X=0X = 0)Purely Resistive (Series Resonance)I\mathbf{I} is in phase with V\mathbf{V} (ϕ=0∘\phi = 0^\circ)Unity (cos⁡ϕ=1\cos\phi = 1)

(Note: At series resonance, XL=XC  ⟹  2πfrL=12πfrCX_L = X_C \implies 2\pi f_r L = \frac{1}{2\pi f_r C}, giving the resonant frequency fr=12πLCf_r = \frac{1}{2\pi\sqrt{LC}}, where impedance is minimum Z=RZ = R and current is maximum I=V/RI = V/R.)

Worked Example 1

Problem: A coil having a resistance of 12 Ω12\ \Omega and an inductance of 0.05 H0.05\text{ H} is connected in series with a 100 μF100\ \mu\text{F} capacitor across a 230 V,50 Hz230\text{ V}, 50\text{ Hz} AC supply. Calculate: (a) Inductive reactance, capacitive reactance, and total impedance, (b) RMS current and its phase angle with respect to supply voltage, and (c) Voltage drops across the coil and across the capacitor.

Solution:

  1. Calculate reactances and total impedance:

    • XL=2πfL=2π×50×0.05=15.71 ΩX_L = 2\pi f L = 2\pi \times 50 \times 0.05 = 15.71\ \Omega
    • XC=12πfC=12π×50×100×10−6=31.83 ΩX_C = \frac{1}{2\pi f C} = \frac{1}{2\pi \times 50 \times 100 \times 10^{-6}} = 31.83\ \Omega
    • Net reactance: X=XL−XC=15.71−31.83=−16.12 ΩX = X_L - X_C = 15.71 - 31.83 = -16.12\ \Omega (capacitive since XC>XLX_C > X_L)
    • Complex impedance: Z=12−j16.12 Ω\mathbf{Z} = 12 - j16.12\ \Omega
    • Magnitude of impedance: Z=122+(−16.12)2=144+259.85=403.85=20.10 ΩZ = \sqrt{12^2 + (-16.12)^2} = \sqrt{144 + 259.85} = \sqrt{403.85} = 20.10\ \Omega
    • Impedance angle: ϕ=tan⁡−1(−16.1212)=−53.34∘  ⟹  Z=20.10∠−53.34∘ Ω\phi = \tan^{-1}\left(\frac{-16.12}{12}\right) = -53.34^\circ \implies \mathbf{Z} = 20.10 \angle -53.34^\circ\ \Omega
  2. Calculate RMS current (taking V=230∠0∘ V\mathbf{V} = 230\angle 0^\circ\text{ V}): I=VZ=230∠0∘20.10∠−53.34∘=11.44∠+53.34∘ A\mathbf{I} = \frac{\mathbf{V}}{\mathbf{Z}} = \frac{230\angle 0^\circ}{20.10\angle -53.34^\circ} = 11.44 \angle +53.34^\circ\text{ A} Thus, RMS current is 11.44 A11.44\text{ A} and it leads the supply voltage by 53.34∘53.34^\circ.

  3. Calculate voltage across the coil (RR and LL together) and across the capacitor (CC):

    • Impedance of the coil: Zcoil=R2+XL2=122+15.712=19.77 ΩZ_{\text{coil}} = \sqrt{R^2 + X_L^2} = \sqrt{12^2 + 15.71^2} = 19.77\ \Omega
    • Voltage across coil: Vcoil=I⋅Zcoil=11.44×19.77=226.17 VV_{\text{coil}} = I \cdot Z_{\text{coil}} = 11.44 \times 19.77 = 226.17\text{ V}
    • Voltage across capacitor: VC=I⋅XC=11.44×31.83=364.14 VV_C = I \cdot X_C = 11.44 \times 31.83 = 364.14\text{ V}

Answer: (a) XL=15.71 Ω,XC=31.83 Ω,Z=20.10∠−53.34∘ ΩX_L = 15.71\ \Omega, X_C = 31.83\ \Omega, \mathbf{Z} = 20.10\angle -53.34^\circ\ \Omega; (b) I=11.44 AI = 11.44\text{ A} (leading by 53.34∘53.34^\circ); (c) Vcoil=226.17 V,VC=364.14 VV_{\text{coil}} = 226.17\text{ V}, V_C = 364.14\text{ V}.

Summary

  • Series RL: Z=R+jXL=R2+XL2∠+ϕ\mathbf{Z} = R + jX_L = \sqrt{R^2 + X_L^2}\angle +\phi, current lags voltage by ϕ=tan⁡−1(XL/R)\phi = \tan^{-1}(X_L/R).
  • Series RC: Z=R−jXC=R2+XC2∠−ϕ\mathbf{Z} = R - jX_C = \sqrt{R^2 + X_C^2}\angle -\phi, current leads voltage by ϕ=tan⁡−1(XC/R)\phi = \tan^{-1}(X_C/R).
  • Series RLC: Z=R+j(XL−XC)\mathbf{Z} = R + j(X_L - X_C), Z=R2+(XL−XC)2Z = \sqrt{R^2 + (X_L - X_C)^2}, V=VR2+(VL−VC)2V = \sqrt{V_R^2 + (V_L - V_C)^2}.

Power in AC circuits: Power factor, active, reactive and apparent power

Instantaneous and Average Power in a General AC Circuit

Let the voltage applied across a general single-phase AC circuit and the resulting current be:

v(t)=Vmsin⁡(ωt)andi(t)=Imsin⁡(ωt−ϕ)v(t) = V_m \sin(\omega t) \quad \text{and} \quad i(t) = I_m \sin(\omega t - \phi)

where ϕ\phi is the phase angle between voltage and current.

Derivation of Instantaneous and Average Power:

  1. The instantaneous power p(t)p(t) is the product of instantaneous voltage and instantaneous current: p(t)=v(t)⋅i(t)=VmImsin⁡(ωt)sin⁡(ωt−ϕ)p(t) = v(t) \cdot i(t) = V_m I_m \sin(\omega t) \sin(\omega t - \phi)
  2. Using the trigonometric identity 2sin⁡Asin⁡B=cos⁡(A−B)−cos⁡(A+B)2\sin A \sin B = \cos(A - B) - \cos(A + B): p(t)=VmIm2[cos⁡ϕ−cos⁡(2ωt−ϕ)]p(t) = \frac{V_m I_m}{2} \left[ \cos\phi - \cos(2\omega t - \phi) \right]
  3. Since V=Vm/2V = V_m/\sqrt{2} and I=Im/2I = I_m/\sqrt{2}, we have VmIm2=VI\frac{V_m I_m}{2} = V I: p(t)=VIcos⁡ϕ−VIcos⁡(2ωt−ϕ)p(t) = V I \cos\phi - V I \cos(2\omega t - \phi)
  4. The instantaneous power consists of two parts:
    • A constant part VIcos⁡ϕV I \cos\phi, which is independent of time.
    • A pulsating cosine term VIcos⁡(2ωt−ϕ)V I \cos(2\omega t - \phi) that oscillates at twice the supply frequency (2f2f) and whose average value over one complete cycle is zero.
  5. Therefore, the average power (real or active power) PP over a complete cycle is: P=12π∫02πp(ωt) d(ωt)=VIcos⁡ϕ(watts, W)P = \frac{1}{2\pi} \int_{0}^{2\pi} p(\omega t) \, d(\omega t) = V I \cos\phi \quad \text{(watts, W)}

The Three Types of AC Power

In an AC circuit, power is characterized by three related quantities that form a right-angled triangle called the Power Triangle:

Code
             /|
            / |
   S = VI  /  | Q = VI sin(phi)  [Reactive Power, VAR]
  [VA]    /   |
         /phi |
        +-----+
     P = VI cos(phi)  [Active Power, W]
  1. Active Power / Real Power / True Power (PP): The actual power consumed or dissipated in the resistive part of the circuit that does useful work (converted into heat, light, or mechanical work). P=VIcos⁡ϕ=I2R(Unit: watt, W or kilowatt, kW)P = V I \cos\phi = I^2 R \quad \text{(Unit: watt, W or kilowatt, kW)}

  2. Reactive Power / Quadrature Power (QQ): The power that continuously surges back and forth between the AC source and the magnetic field of inductors or electric field of capacitors without doing net useful work. Q=VIsin⁡ϕ=I2X=I2(XL−XC)(Unit: volt-ampere reactive, VAR or kVAR)Q = V I \sin\phi = I^2 X = I^2 (X_L - X_C) \quad \text{(Unit: volt-ampere reactive, VAR or kVAR)} -By convention, an inductive circuit (XL>XCX_L > X_C) absorbs positive reactive power (+Q+Q, lagging VAR), whereas a capacitive circuit (XC>XLX_C > X_L) supplies reactive power (−Q-Q, leading VAR).

  3. Apparent Power (SS): The product of the RMS voltage VV and the RMS current II supplied to the circuit, without considering the phase angle. Electrical equipment such as transformers and AC generators are rated in terms of apparent power (SS). S=VI=I2Z=P2+Q2(Unit: volt-ampere, VA or kilovolt-ampere, kVA)S = V I = I^2 Z = \sqrt{P^2 + Q^2} \quad \text{(Unit: volt-ampere, VA or kilovolt-ampere, kVA)}

(Note: Complex Power is written as S=VI∗=P+jQ=S∠ϕ VA\mathbf{S} = \mathbf{V} \mathbf{I}^* = P + jQ = S\angle\phi\text{ VA}.)

Power Factor (cos⁡ϕ\cos\phi)

Definitions of Power Factor

The power factor (pf) of an AC circuit can be defined in three equivalent ways:

  1. Cosine of the phase angle between the supply voltage V\mathbf{V} and supply current I\mathbf{I}: Power Factor=cos⁡ϕ\text{Power Factor} = \cos\phi
  2. Ratio of Resistance to Impedance (from the impedance triangle): cos⁡ϕ=RZ\cos\phi = \frac{R}{Z}
  3. Ratio of Active Power to Apparent Power (from the power triangle): cos⁡ϕ=Active Power (P)Apparent Power (S)=VIcos⁡ϕVI\cos\phi = \frac{\text{Active Power }(P)}{\text{Apparent Power }(S)} = \frac{V I \cos\phi}{V I}

Nature and Range of Power Factor:

  • Since −90∘≤ϕ≤+90∘-90^\circ \le \phi \le +90^\circ for passive circuits, 0≤cos⁡ϕ≤10 \le \cos\phi \le 1.
  • Lagging power factor: Occurs in inductive circuits (XL>XCX_L > X_C), where current lags voltage.
  • Leading power factor: Occurs in capacitive circuits (XC>XLX_C > X_L), where current leads voltage.
  • Unity power factor (cos⁡ϕ=1\cos\phi = 1): Occurs in purely resistive circuits or RLC circuits at resonance (XL=XCX_L = X_C), where ϕ=0∘\phi = 0^\circ.
  • Zero power factor (cos⁡ϕ=0\cos\phi = 0): Occurs in pure inductive or pure capacitive circuits (ϕ=±90∘\phi = \pm 90^\circ).

Significance of Power Factor: For a fixed active power PP to be delivered at a constant supply voltage VV, the line current required is: I=PVcos⁡ϕI = \frac{P}{V \cos\phi} If the power factor cos⁡ϕ\cos\phi is low, the circuit draws a much larger current II from the supply to deliver the same real power PP. This causes higher I2RI^2R copper losses in transmission lines, larger voltage drops, and requires higher kVA ratings of generators and transformers.

Worked Example 1

Problem: A single-phase AC motor takes a current of 20 A20\text{ A} from a 230 V,50 Hz230\text{ V}, 50\text{ Hz} supply at a lagging power factor of 0.80.8. Calculate: (a) Apparent power in kVA, (b) Active power in kW, (c) Reactive power in kVAR, and (d) Resistance and inductive reactance of the motor (modeled as a series RL circuit).

Solution:

  1. Given data: V=230 VV = 230\text{ V}, I=20 AI = 20\text{ A}, cos⁡ϕ=0.8 (lagging)\cos\phi = 0.8\text{ (lagging)}.
    • Phase angle: ϕ=cos⁡−1(0.8)=36.87∘\phi = \cos^{-1}(0.8) = 36.87^\circ
    • sin⁡ϕ=sin⁡(36.87∘)=0.6\sin\phi = \sin(36.87^\circ) = 0.6
  2. (a) Apparent power (SS): S=VI=230×20=4600 VA=4.6 kVAS = V I = 230 \times 20 = 4600\text{ VA} = 4.6\text{ kVA}
  3. (b) Active power (PP): P=VIcos⁡ϕ=4600×0.8=3680 W=3.68 kWP = V I \cos\phi = 4600 \times 0.8 = 3680\text{ W} = 3.68\text{ kW}
  4. (c) Reactive power (QQ): Q=VIsin⁡ϕ=4600×0.6=2760 VAR=2.76 kVARQ = V I \sin\phi = 4600 \times 0.6 = 2760\text{ VAR} = 2.76\text{ kVAR}
  5. (d) Equivalent series RR and XLX_L:
    • Impedance magnitude: Z=VI=23020=11.5 ΩZ = \frac{V}{I} = \frac{230}{20} = 11.5\ \Omega
    • Resistance: R=Zcos⁡ϕ=11.5×0.8=9.2 ΩR = Z \cos\phi = 11.5 \times 0.8 = 9.2\ \Omega
    • Inductive reactance: XL=Zsin⁡ϕ=11.5×0.6=6.9 ΩX_L = Z \sin\phi = 11.5 \times 0.6 = 6.9\ \Omega

Answer: (a) S=4.6 kVAS = 4.6\text{ kVA}; (b) P=3.68 kWP = 3.68\text{ kW}; (c) Q=2.76 kVARQ = 2.76\text{ kVAR}; (d) R=9.2 Ω,XL=6.9 ΩR = 9.2\ \Omega, X_L = 6.9\ \Omega.

Worked Example 2

Problem: A voltage v(t)=2002sin⁡(314t+20∘) Vv(t) = 200\sqrt{2}\sin(314t + 20^\circ)\text{ V} applied across an AC circuit produces a current i(t)=102sin⁡(314t−10∘) Ai(t) = 10\sqrt{2}\sin(314t - 10^\circ)\text{ A}. Find the phase angle, power factor, active power, reactive power, and apparent power.

Solution:

  1. Extract RMS values and phase angles:
    • V=200 VV = 200\text{ V}, ϕv=+20∘\phi_v = +20^\circ
    • I=10 AI = 10\text{ A}, ϕi=−10∘\phi_i = -10^\circ
  2. Calculate phase difference (ϕ\phi) and power factor: ϕ=ϕv−ϕi=20∘−(−10∘)=30∘(current lags voltage by 30∘)\phi = \phi_v - \phi_i = 20^\circ - (-10^\circ) = 30^\circ \quad (\text{current lags voltage by } 30^\circ) Power factor=cos⁡30∘=0.866 (lagging)\text{Power factor} = \cos 30^\circ = 0.866\text{ (lagging)}
  3. Calculate SS, PP, and QQ:
    • Apparent power: S=VI=200×10=2000 VA=2 kVAS = V I = 200 \times 10 = 2000\text{ VA} = 2\text{ kVA}
    • Active power: P=VIcos⁡30∘=2000×0.866=1732 W=1.732 kWP = V I \cos 30^\circ = 2000 \times 0.866 = 1732\text{ W} = 1.732\text{ kW}
    • Reactive power: Q=VIsin⁡30∘=2000×0.5=1000 VAR=1 kVARQ = V I \sin 30^\circ = 2000 \times 0.5 = 1000\text{ VAR} = 1\text{ kVAR}

Answer: ϕ=30∘\phi = 30^\circ, pf=0.866 (lagging)\text{pf} = 0.866\text{ (lagging)}, P=1732 WP = 1732\text{ W}, Q=1000 VARQ = 1000\text{ VAR}, S=2000 VAS = 2000\text{ VA}.

Summary

  • Active power: P=VIcos⁡ϕ=I2R (W)P = VI\cos\phi = I^2R\text{ (W)}.
  • Reactive power: Q=VIsin⁡ϕ=I2X (VAR)Q = VI\sin\phi = I^2X\text{ (VAR)}.
  • Apparent power: S=VI=I2Z=P2+Q2 (VA)S = VI = I^2Z = \sqrt{P^2 + Q^2}\text{ (VA)}.
  • Power factor: cos⁡ϕ=RZ=PS\cos\phi = \frac{R}{Z} = \frac{P}{S}.

Three-phase AC systems: Generation, advantages and balanced connections

Syllabus: Three-Phase AC Systems

  • Generation of three-phase voltages, advantages of three-phase systems
  • Star and delta connections (balanced only)
  • Relation between line and phase voltages, line and phase currents - numerical problems

Generation of Three-Phase Voltages

A three-phase AC system consists of three identical single-phase AC voltage sources of the same frequency and same amplitude, displaced from one another in phase by 120∘120^\circ electrical (2π/3 radians2\pi/3\text{ radians}).

Principle of Generation:

  1. Consider three identical armature coils RR-R′R', YY-Y′Y', and BB-B′B' (representing the Red, Yellow, and Blue phases) mounted on the stator of an alternator such that their magnetic axes are physically displaced from one another in space by 120∘120^\circ.
  2. When a magnetic rotor is rotated at a constant angular velocity ω\omega inside these three coils, sinusoidal emfs of equal maximum value EmE_m and equal frequency f=ω/(2π)f = \omega / (2\pi) are induced in all three coils.
  3. Because of the 120∘120^\circ spatial displacement, the emf in phase YY reaches its positive peak 120∘120^\circ after phase RR, and the emf in phase BB reaches its positive peak 120∘120^\circ after phase YY (i.e., 240∘240^\circ after phase RR, or 120∘120^\circ before phase RR).

Instantaneous and Phasor Equations (for RYBRYB Phase Sequence):

  • Time-domain expressions: eR(t)=Emsin⁡(ωt)e_R(t) = E_m \sin(\omega t) eY(t)=Emsin⁡(ωt−120∘)e_Y(t) = E_m \sin(\omega t - 120^\circ) eB(t)=Emsin⁡(ωt−240∘)=Emsin⁡(ωt+120∘)e_B(t) = E_m \sin(\omega t - 240^\circ) = E_m \sin(\omega t + 120^\circ)

  • RMS Phasor expressions (where Eph=Em/2E_{ph} = E_m/\sqrt{2}): ER=Eph∠0∘\mathbf{E}_R = E_{ph} \angle 0^\circ EY=Eph∠−120∘\mathbf{E}_Y = E_{ph} \angle -120^\circ EB=Eph∠−240∘=Eph∠+120∘\mathbf{E}_B = E_{ph} \angle -240^\circ = E_{ph} \angle +120^\circ

Code
             E_B (120 deg)
               \
                \  120 deg
                 \
                  o------------> E_R (0 deg)
                 /
                /  120 deg
               /
             E_Y (-120 deg)

Important Property: At every instant of time, the algebraic sum of the three balanced instantaneous three-phase voltages is zero, and their phasor sum is also zero: eR(t)+eY(t)+eB(t)=0andER+EY+EB=0e_R(t) + e_Y(t) + e_B(t) = 0 \quad \text{and} \quad \mathbf{E}_R + \mathbf{E}_Y + \mathbf{E}_B = 0

Phase Sequence: The order in which the voltages in the three phases attain their positive maximum values is called the phase sequence. The standard (positive) phase sequence is R→Y→BR \to Y \to B; reversing the direction of rotation (or interchanging any two line leads) gives the reverse (negative) sequence R→B→YR \to B \to Y.

Advantages of Three-Phase Systems over Single-Phase Systems

  1. Constant Instantaneous Power and Uniform Torque: In a single-phase system, instantaneous power pulsates at twice the supply frequency (2f2f), causing vibration in motors. In a balanced three-phase system, the total instantaneous power ptotal(t)=pR(t)+pY(t)+pB(t)=3VphIphcos⁡ϕp_{\text{total}}(t) = p_R(t) + p_Y(t) + p_B(t) = 3 V_{ph} I_{ph} \cos\phi is completely constant at every instant, resulting in smooth, pulsation-free torque in three-phase motors.
  2. Higher Output Rating for a Given Frame Size: A three-phase alternator or motor has about 1.51.5 times the power output of a single-phase machine of the same physical frame size and weight.
  3. Economy in Transmission Conductor Material: To transmit the same amount of power over a fixed distance at the same voltage and power loss, a three-phase system requires only about 75%75\% of the conductor weight (copper/aluminium) required by a single-phase system.
  4. Self-Starting Capability of Three-Phase Motors: Three-phase currents flowing in three spatially displaced windings produce a uniform rotating magnetic field (RMF), making three-phase induction motors inherently self-starting without auxiliary starting windings or capacitors.
  5. Availability of Two Voltages (in 3-Phase, 4-Wire Star System): A star-connected system with a neutral wire provides two voltage levels simultaneously: phase voltage (230 V230\text{ V}) between any line and neutral for domestic single-phase loads, and line voltage (3×230≈400 V\sqrt{3} \times 230 \approx 400\text{ V}) between any two lines for industrial three-phase loads.

Balanced Three-Phase System and Basic Definitions

  • Balanced Supply and Balanced Load: Three-phase voltages are balanced if they are equal in magnitude and displaced by 120∘120^\circ in phase. A three-phase load is balanced if the impedances in all three phases are identical in both magnitude and phase angle (ZR=ZY=ZB=Zph∠ϕ\mathbf{Z}_R = \mathbf{Z}_Y = \mathbf{Z}_B = Z_{ph} \angle \phi).
  • Phase Voltage (VphV_{ph}): The voltage across any single phase winding or single load impedance branch.
  • Line Voltage (VLV_L): The voltage measured between any two of the three line conductors (VRYV_{RY}, VYBV_{YB}, or VBRV_{BR}).
  • Phase Current (IphI_{ph}): The current flowing through any single phase winding or single load impedance branch.
  • Line Current (ILI_L): The current flowing through any of the three external transmission line conductors (IRI_R, IYI_Y, or IBI_B).

1. Balanced Star (Wye, Y) Connection

In a Star (Y) connection, the similar ends (starting ends or finishing ends) of the three phase impedances are joined together at a common point NN called the neutral point (or star point), and the other three ends are connected to the three line conductors RR, YY, and BB.

Code
   Line R ------>----+   I_L = I_ph
                     |
                    [Z_ph]  (V_ph = V_RN)
                     |
   Neutral N --------*-------------------- (Neutral Wire)
                    / \
     (V_YN) [Z_ph] /   \ [Z_ph] (V_BN)
                  /     \
   Line Y ------>+       +<------ Line B

Derivation of Line-to-Phase Relations in Star Connection:

  1. Current Relation: Since each line conductor is connected directly in series with its respective phase winding, the line current is identical to the phase current: IL=IphI_L = I_{ph} (In a balanced 4-wire star system, the neutral current is IN=IR+IY+IB=0\mathbf{I}_N = \mathbf{I}_R + \mathbf{I}_Y + \mathbf{I}_B = 0.)

  2. Voltage Relation: Let the balanced phase voltages with respect to the neutral NN be: VRN=Vph∠0∘,VYN=Vph∠−120∘,VBN=Vph∠+120∘\mathbf{V}_{RN} = V_{ph} \angle 0^\circ, \qquad \mathbf{V}_{YN} = V_{ph} \angle -120^\circ, \qquad \mathbf{V}_{BN} = V_{ph} \angle +120^\circ Applying KVL between line RR and line YY, the line voltage VRY\mathbf{V}_{RY} (potential of RR with respect to YY) is the phasor difference between VRN\mathbf{V}_{RN} and VYN\mathbf{V}_{YN}: VRY=VRN−VYN=VRN+(−VYN)\mathbf{V}_{RY} = \mathbf{V}_{RN} - \mathbf{V}_{YN} = \mathbf{V}_{RN} + (-\mathbf{V}_{YN})

    • On the phasor diagram, −VYN-\mathbf{V}_{YN} has magnitude VphV_{ph} at an angle of −120∘+180∘=+60∘-120^\circ + 180^\circ = +60^\circ with respect to VRN\mathbf{V}_{RN}.
    • Therefore, the angle between VRN\mathbf{V}_{RN} (0∘0^\circ) and −VYN-\mathbf{V}_{YN} (+60∘+60^\circ) is α=60∘\alpha = 60^\circ.
    • Using the parallelogram law of vector addition for two equal phasors of length VphV_{ph} separated by 60∘60^\circ: VL=VRY=Vph2+Vph2+2VphVphcos⁡60∘=Vph2+Vph2+2Vph2(0.5)=3Vph2V_L = V_{RY} = \sqrt{V_{ph}^2 + V_{ph}^2 + 2 V_{ph} V_{ph} \cos 60^\circ} = \sqrt{V_{ph}^2 + V_{ph}^2 + 2 V_{ph}^2 (0.5)} = \sqrt{3 V_{ph}^2} VL=3Vph≈1.732VphV_L = \sqrt{3} V_{ph} \approx 1.732 V_{ph}
    • Also, the resultant phasor VRY\mathbf{V}_{RY} bisects the 60∘60^\circ angle between VRN\mathbf{V}_{RN} and −VYN-\mathbf{V}_{YN}, so each line voltage leads its corresponding phase voltage by 30∘30^\circ: VRY=3Vph∠+30∘,VYB=3Vph∠−90∘,VBR=3Vph∠+150∘\mathbf{V}_{RY} = \sqrt{3} V_{ph} \angle +30^\circ, \quad \mathbf{V}_{YB} = \sqrt{3} V_{ph} \angle -90^\circ, \quad \mathbf{V}_{BR} = \sqrt{3} V_{ph} \angle +150^\circ

2. Balanced Delta (Mesh, Δ\Delta) Connection

In a Delta (Δ\Delta) connection, the finishing end of one phase impedance is connected to the starting end of the next phase impedance to form a closed triangular loop, and the three line conductors RR, YY, and BB are connected to the three junction points.

Code
   Line R (I_R) ---------->---------*
                                   / \
                                  /   \
                   (I_BR) [Z_ph] /     \ [Z_ph] (I_RY = I_ph)
                                /       \
   Line B (I_B) ------>--------*---------*--------<------ Line Y (I_Y)
                                  [Z_ph]
                                  (I_YB)

Derivation of Line-to-Phase Relations in Delta Connection:

  1. Voltage Relation: Since each phase impedance is connected directly across a pair of line conductors, the line voltage is equal to the phase voltage: VL=VphV_L = V_{ph}

  2. Current Relation: Let the three balanced phase currents inside the delta loop be: IRY=Iph∠0∘,IYB=Iph∠−120∘,IBR=Iph∠+120∘\mathbf{I}_{RY} = I_{ph} \angle 0^\circ, \qquad \mathbf{I}_{YB} = I_{ph} \angle -120^\circ, \qquad \mathbf{I}_{BR} = I_{ph} \angle +120^\circ Applying Kirchhoff's Current Law (KCL) at junction RR: IR+IBR=IRY  ⟹  IR=IRY−IBR=IRY+(−IBR)\mathbf{I}_R + \mathbf{I}_{BR} = \mathbf{I}_{RY} \implies \mathbf{I}_R = \mathbf{I}_{RY} - \mathbf{I}_{BR} = \mathbf{I}_{RY} + (-\mathbf{I}_{BR})

    • On the phasor diagram, −IBR-\mathbf{I}_{BR} has magnitude IphI_{ph} at an angle of +120∘−180∘=−60∘+120^\circ - 180^\circ = -60^\circ with respect to IRY\mathbf{I}_{RY} (0∘0^\circ).
    • The angle between IRY\mathbf{I}_{RY} and −IBR-\mathbf{I}_{BR} is 60∘60^\circ.
    • Using the parallelogram law of vector addition for two equal phasors of magnitude IphI_{ph} separated by 60∘60^\circ: IL=IR=Iph2+Iph2+2IphIphcos⁡60∘=3Iph2I_L = I_R = \sqrt{I_{ph}^2 + I_{ph}^2 + 2 I_{ph} I_{ph} \cos 60^\circ} = \sqrt{3 I_{ph}^2} IL=3Iph≈1.732IphI_L = \sqrt{3} I_{ph} \approx 1.732 I_{ph}
    • Also, the line current IR\mathbf{I}_R bisects the angle between IRY\mathbf{I}_{RY} (0∘0^\circ) and −IBR-\mathbf{I}_{BR} (−60∘-60^\circ), so each line current lags behind its corresponding phase current by 30∘30^\circ: IR=3Iph∠−30∘\mathbf{I}_R = \sqrt{3} I_{ph} \angle -30^\circ

Summary of Star and Delta Relations

  • Star (Y) connection: IL=IphI_L = I_{ph} and VL=3VphV_L = \sqrt{3} V_{ph}.
  • Delta (Δ\Delta) connection: VL=VphV_L = V_{ph} and IL=3IphI_L = \sqrt{3} I_{ph}.

Power in balanced three-phase circuits and worked problems

Power Expressions in a Balanced Three-Phase Circuit

In any balanced three-phase circuit (whether connected in Star or Delta), each of the three identical phases has phase voltage VphV_{ph}, phase current IphI_{ph}, and phase angle ϕ\phi between VphV_{ph} and IphI_{ph} (where cos⁡ϕ=Rph/Zph\cos\phi = R_{ph}/Z_{ph}).

Therefore, the active power consumed per phase is Pph=VphIphcos⁡ϕP_{ph} = V_{ph} I_{ph} \cos\phi, and the total three-phase active power PP is three times the single-phase power:

P=3Pph=3VphIphcos⁡ϕ(watts, W)P = 3 P_{ph} = 3 V_{ph} I_{ph} \cos\phi \quad \text{(watts, W)}

Expressing Three-Phase Power in Terms of Line Quantities (VLV_L and ILI_L):

  1. For a Balanced Star (Y) Connection: Substitute Vph=VL3V_{ph} = \frac{V_L}{\sqrt{3}} and Iph=ILI_{ph} = I_L: P=3(VL3)ILcos⁡ϕ=3VLILcos⁡ϕ(W)P = 3 \left(\frac{V_L}{\sqrt{3}}\right) I_L \cos\phi = \sqrt{3} V_L I_L \cos\phi \quad \text{(W)}

  2. For a Balanced Delta (Δ\Delta) Connection: Substitute Vph=VLV_{ph} = V_L and Iph=IL3I_{ph} = \frac{I_L}{\sqrt{3}}: P=3VL(IL3)cos⁡ϕ=3VLILcos⁡ϕ(W)P = 3 V_L \left(\frac{I_L}{\sqrt{3}}\right) \cos\phi = \sqrt{3} V_L I_L \cos\phi \quad \text{(W)}

Thus, the expressions for Total Active, Reactive, and Apparent Power in terms of line voltage VLV_L and line current ILI_L are identical for both Star and Delta connections:

  • Total Active Power (PP): P=3VphIphcos⁡ϕ=3VLILcos⁡ϕ=3Iph2Rph(W)P = 3 V_{ph} I_{ph} \cos\phi = \sqrt{3} V_L I_L \cos\phi = 3 I_{ph}^2 R_{ph} \quad \text{(W)}
  • Total Reactive Power (QQ): Q=3VphIphsin⁡ϕ=3VLILsin⁡ϕ=3Iph2Xph(VAR)Q = 3 V_{ph} I_{ph} \sin\phi = \sqrt{3} V_L I_L \sin\phi = 3 I_{ph}^2 X_{ph} \quad \text{(VAR)}
  • Total Apparent Power (SS): S=3VphIph=3VLIL=P2+Q2(VA)S = 3 V_{ph} I_{ph} = \sqrt{3} V_L I_L = \sqrt{P^2 + Q^2} \quad \text{(VA)}

(Important Note: In all these formulas, ϕ\phi is always the phase angle between the phase voltage Vph\mathbf{V}_{ph} and the phase current Iph\mathbf{I}_{ph}, i.e., cos⁡ϕ=Rph/Zph\cos\phi = R_{ph}/Z_{ph}, NOT the angle between VLV_L and ILI_L.)

Comparison: Balanced Star vs. Balanced Delta Connection

ParameterStar (Y) ConnectionDelta (Δ\Delta) Connection
Voltage relationVL=3VphV_L = \sqrt{3} V_{ph}VL=VphV_L = V_{ph}
Current relationIL=IphI_L = I_{ph}IL=3IphI_L = \sqrt{3} I_{ph}
Phase current (IphI_{ph})Iph=VL3ZphI_{ph} = \frac{V_L}{\sqrt{3} Z_{ph}}Iph=VLZphI_{ph} = \frac{V_L}{Z_{ph}}
Line current (ILI_L)IL(star)=VL3ZphI_{L(\text{star})} = \frac{V_L}{\sqrt{3} Z_{ph}}IL(delta)=3VLZph=3 IL(star)I_{L(\text{delta})} = \frac{\sqrt{3} V_L}{Z_{ph}} = 3 \, I_{L(\text{star})}
Total Active Power (PP)P=3VLILcos⁡ϕP = \sqrt{3} V_L I_L \cos\phiP=3VLILcos⁡ϕ=3 PstarP = \sqrt{3} V_L I_L \cos\phi = 3 \, P_{\text{star}} (for same ZphZ_{ph} and VLV_L)
Neutral pointAvailable (permits 3-phase 4-wire supply)Not available (3-phase 3-wire only)

Worked Example 1 (Star-Connected Load)

Problem: Three identical coils, each having a resistance of 15 Ω15\ \Omega and an inductance of 0.04 H0.04\text{ H}, are connected in star across a 400 V,50 Hz400\text{ V}, 50\text{ Hz}, three-phase balanced AC supply. Calculate: (a) Phase voltage, (b) Impedance and power factor of each phase, (c) Phase current and line current, and (d) Total active power, reactive power, and apparent power absorbed by the load.

Solution:

  1. Identify given data: VL=400 VV_L = 400\text{ V}, f=50 Hzf = 50\text{ Hz}, Rph=15 ΩR_{ph} = 15\ \Omega, Lph=0.04 HL_{ph} = 0.04\text{ H} (Star connected).
  2. (a) Calculate phase voltage (VphV_{ph}): Vph=VL3=4001.732=230.94 VV_{ph} = \frac{V_L}{\sqrt{3}} = \frac{400}{1.732} = 230.94\text{ V}
  3. (b) Calculate phase impedance (ZphZ_{ph}) and power factor (cos⁡ϕ\cos\phi):
    • Inductive reactance per phase: Xph=2πfLph=2π×50×0.04=12.57 ΩX_{ph} = 2\pi f L_{ph} = 2\pi \times 50 \times 0.04 = 12.57\ \Omega
    • Impedance per phase: Zph=Rph2+Xph2=152+12.572=225+158.0=383.0=19.57 ΩZ_{ph} = \sqrt{R_{ph}^2 + X_{ph}^2} = \sqrt{15^2 + 12.57^2} = \sqrt{225 + 158.0} = \sqrt{383.0} = 19.57\ \Omega
    • Power factor: cos⁡ϕ=RphZph=1519.57=0.7665 (lagging)\cos\phi = \frac{R_{ph}}{Z_{ph}} = \frac{15}{19.57} = 0.7665\text{ (lagging)} ϕ=cos⁡−1(0.7665)=39.96∘,sin⁡ϕ=XphZph=12.5719.57=0.6423\phi = \cos^{-1}(0.7665) = 39.96^\circ, \qquad \sin\phi = \frac{X_{ph}}{Z_{ph}} = \frac{12.57}{19.57} = 0.6423
  4. (c) Calculate phase current (IphI_{ph}) and line current (ILI_L): Iph=VphZph=230.9419.57=11.80 AI_{ph} = \frac{V_{ph}}{Z_{ph}} = \frac{230.94}{19.57} = 11.80\text{ A} For a star connection: IL=Iph=11.80 AI_L = I_{ph} = 11.80\text{ A}
  5. (d) Calculate total PP, QQ, and SS:
    • Total Active Power: P=3VLILcos⁡ϕ=1.732×400×11.80×0.7665=6266 W=6.266 kWP = \sqrt{3} V_L I_L \cos\phi = 1.732 \times 400 \times 11.80 \times 0.7665 = 6266\text{ W} = 6.266\text{ kW}
    • Total Reactive Power: Q=3VLILsin⁡ϕ=1.732×400×11.80×0.6423=5251 VAR=5.251 kVARQ = \sqrt{3} V_L I_L \sin\phi = 1.732 \times 400 \times 11.80 \times 0.6423 = 5251\text{ VAR} = 5.251\text{ kVAR}
    • Total Apparent Power: S=3VLIL=1.732×400×11.80=8175 VA=8.175 kVAS = \sqrt{3} V_L I_L = 1.732 \times 400 \times 11.80 = 8175\text{ VA} = 8.175\text{ kVA}

Answer: (a) Vph=230.94 VV_{ph} = 230.94\text{ V}; (b) Zph=19.57 Ω,cos⁡ϕ=0.7665 (lag)Z_{ph} = 19.57\ \Omega, \cos\phi = 0.7665\text{ (lag)}; (c) Iph=IL=11.80 AI_{ph} = I_L = 11.80\text{ A}; (d) P=6.266 kW,Q=5.251 kVAR,S=8.175 kVAP = 6.266\text{ kW}, Q = 5.251\text{ kVAR}, S = 8.175\text{ kVA}.

Worked Example 2 (Delta-Connected Load)

Problem: If the same three coils of Worked Example 1 (Rph=15 ΩR_{ph} = 15\ \Omega, Lph=0.04 HL_{ph} = 0.04\text{ H}) are reconnected in delta across the same 400 V,50 Hz400\text{ V}, 50\text{ Hz} three-phase supply, calculate: (a) Phase voltage, (b) Phase current, (c) Line current, and (d) Total active power consumed.

Solution:

  1. From Worked Example 1, per-phase impedance and power factor remain unchanged: Zph=19.57 Ωandcos⁡ϕ=0.7665 (lagging)Z_{ph} = 19.57\ \Omega \quad \text{and} \quad \cos\phi = 0.7665\text{ (lagging)}
  2. (a) Phase voltage (VphV_{ph}) in Delta: Vph=VL=400 VV_{ph} = V_L = 400\text{ V}
  3. (b) Phase current (IphI_{ph}): Iph=VphZph=40019.57=20.44 AI_{ph} = \frac{V_{ph}}{Z_{ph}} = \frac{400}{19.57} = 20.44\text{ A}
  4. (c) Line current (ILI_L): IL=3Iph=1.732×20.44=35.40 AI_L = \sqrt{3} I_{ph} = 1.732 \times 20.44 = 35.40\text{ A} (Notice that IL(delta)=35.40 A=3×11.80 A=3IL(star)I_{L(\text{delta})} = 35.40\text{ A} = 3 \times 11.80\text{ A} = 3 I_{L(\text{star})}.)
  5. (d) Total Active Power (PP): P=3VLILcos⁡ϕ=1.732×400×35.40×0.7665=18.80 kWP = \sqrt{3} V_L I_L \cos\phi = 1.732 \times 400 \times 35.40 \times 0.7665 = 18.80\text{ kW} (Notice that Pdelta=18.80 kW=3×6.266 kW=3PstarP_{\text{delta}} = 18.80\text{ kW} = 3 \times 6.266\text{ kW} = 3 P_{\text{star}}.)

Answer: (a) Vph=400 VV_{ph} = 400\text{ V}; (b) Iph=20.44 AI_{ph} = 20.44\text{ A}; (c) IL=35.40 AI_L = 35.40\text{ A}; (d) P=18.80 kWP = 18.80\text{ kW}.

Worked Example 3

Problem: A balanced three-phase delta-connected load draws a total active power of 12 kW12\text{ kW} at a lagging power factor of 0.80.8 from a 415 V,50 Hz415\text{ V}, 50\text{ Hz} three-phase supply. Find the line current, phase current, and the resistance and reactance of each phase of the load.

Solution:

  1. Calculate line current (ILI_L): P=3VLILcos⁡ϕ  ⟹  IL=P3VLcos⁡ϕ=120001.732×415×0.8=20.87 AP = \sqrt{3} V_L I_L \cos\phi \implies I_L = \frac{P}{\sqrt{3} V_L \cos\phi} = \frac{12000}{1.732 \times 415 \times 0.8} = 20.87\text{ A}
  2. Calculate phase current (IphI_{ph}) for Delta: Iph=IL3=20.871.732=12.05 AI_{ph} = \frac{I_L}{\sqrt{3}} = \frac{20.87}{1.732} = 12.05\text{ A}
  3. Calculate phase impedance (ZphZ_{ph}), resistance (RphR_{ph}), and reactance (XphX_{ph}):
    • For Delta, Vph=VL=415 VV_{ph} = V_L = 415\text{ V}.
    • Zph=VphIph=41512.05=34.44 ΩZ_{ph} = \frac{V_{ph}}{I_{ph}} = \frac{415}{12.05} = 34.44\ \Omega
    • Rph=Zphcos⁡ϕ=34.44×0.8=27.55 ΩR_{ph} = Z_{ph} \cos\phi = 34.44 \times 0.8 = 27.55\ \Omega
    • Since cos⁡ϕ=0.8\cos\phi = 0.8, sin⁡ϕ=0.6\sin\phi = 0.6: Xph=Zphsin⁡ϕ=34.44×0.6=20.66 ΩX_{ph} = Z_{ph} \sin\phi = 34.44 \times 0.6 = 20.66\ \Omega

Answer: IL=20.87 AI_L = 20.87\text{ A}, Iph=12.05 AI_{ph} = 12.05\text{ A}, Rph=27.55 ΩR_{ph} = 27.55\ \Omega, Xph=20.66 ΩX_{ph} = 20.66\ \Omega.

Summary

  • In both Star and Delta balanced 3-phase circuits: P=3VLILcos⁡ϕP = \sqrt{3} V_L I_L \cos\phi, Q=3VLILsin⁡ϕQ = \sqrt{3} V_L I_L \sin\phi, and S=3VLILS = \sqrt{3} V_L I_L.
  • When three identical impedances are switched from Star to Delta across the same line voltage VLV_L, both the line current drawn and the total power consumed increase by a factor of 33 (IL(Δ)=3IL(Y)I_{L(\Delta)} = 3I_{L(Y)} and PΔ=3PYP_{\Delta} = 3P_Y).

Suggested reading

Textbooks

  1. D. P. Kothari and I. J. Nagrath, Basic Electrical Engineering, Tata McGraw Hill, 4th ed., 2019.
  2. J. J. Cathey and Syed A. Nasar, Schaum's Outline of Basic Electrical Engineering, Tata McGraw Hill, 3rd ed., 2010.
  3. D. P. Kothari and I. J. Nagrath, Basic Electrical and Electronics Engineering, McGraw Hill, 2nd ed., 2020.

Reference Books

  1. D. C. Kulshreshtha, Basic Electrical Engineering, Tata McGraw Hill, 2nd ed., 2019.
  2. V. Del Toro, Electrical Engineering Fundamentals, Pearson Education, 2nd ed., 2019.
  3. T. K. Nagsarkar and M. S. Sukhija, Basic Electrical Engineering, Oxford Higher Education, 3rd ed., 2017.