02-02-2010 dept of aeronautical enggineering s.m.m. rahman mist direct current limitations:...
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02-02-2010 Dept of Aeronautical Enggineering S.M.M. Rahman
MIST
Direct Current
Limitations:• Transmission Loss• No Amplification• Power Distribution Lim.•Expensive
02-02-2010 Dept of Aeronautical Enggineering S.M.M. Rahman
MIST
DC or AC ?
”A different type of Power System is needed to overcome the limitations”
Should we try with Alternating Current (AC) system?
Solution?
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Generation of Alternating Current
90 180 270 360
“The direction of current flowing in a circuit is constantly being reversed back and forth”
“the light bulb still lights but the electron current is constantly reversing directions”
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Alternating Current
Oscillatory Current
Periodic Current
Alternating Current
i = I0+ I1 sin (ωt+α1)+ I2 sin (2ωt+α2)+.........
i = I1 sin (ωt+α1)+ I2 sin (2ωt+α2)+.........
Alternating current is a periodic current, the average of of which over a period is zero
A periodic current is a oscillating current the values of which at equal interval
An oscillatory current is a current which alternately increases and decreases In magnitude with repect to time according to some definite law
time
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Period and Frequency
The time for one complete cycle is defined as Period ( T ).
Freqency ( f )is the number of cycles per second
frequency, f = 1/T
A complete cycle corresponded to 2π electrical radians or 360 degrees. Therefore the Angular Velocity,
ω = 2 π/T = 2 πf We use 50 Hz AC sytem
Period(T)
Time(t)/angle(α)
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Alternating Current/Voltage - Sine Wave
Triangular wave
Square wave
Im
t
ωt = π
ωt = 2π
i= Im sin ωtori=Im sinα
”In practice, many AC waves approximate a sine wave very closely and therefore its calculations are based on sine waves”
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Phase
i= Im sin (ωt+Ө)
Ө phase angle
”Phase is the fractional part of a period through which time or the associated time angle ωt has advanced from an arbitrary reference”
i= Im sin (ωt+Ө) represents a sine wave of current with phase angle Ө
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Phase Difference
Applied voltage is, v = Vm sin ωt
Due to nature of circuit parameters the current comes to a certain point before the voltage wave by degrees to that point, then the current can be expressed as
i= Im sin (ωt+Ө)
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Phase Difference
To further describe the phase relationship between two sine waves, the terms Lead and Lag are used. The amount by which one sine wave leads or lags another sine wave is measured in degrees.
The positive maximum of the leading quantity occurs before the positive maximumof the lagging quantity
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Impedance
“Electrical impedance extends the concept of resistance to AC circuits, describing not only the relative amplitude of the voltage and current, but also the relative phases”
Impedance is represented by, Z∟Ө Z define the ratio of Vm to Im
Ө define their relative phase differenceZ
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Impedance
C
R Circuit L Circuit C Circuit
RLC CircuitRC CircuitRL Circuit
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Resistive Element
Applied voltage v= Vm sinωt
Current i= Im sinωt
Instantaneous Power is given by,
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Inductive Element
A sinusoidal voltage is applied to a pure inductor
Integrating both sides
The constant c1 will be considered to be zero, then the expression for i reduces to
Vm/Im= ωL and i lags v by 90 degree.Therefore, the impedance of L branch is
Here ωL is called inductive reactance
XL= ωL = 2πfL
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Inductive Element
The instantaneous power delivered to the pure inductance is
•The power variation is symmetrical andThe average power absorbed is equal to zero
• positive and negative power exist for a purelyInductive circuit
02-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Inductive Element
The inductive element receives energy from source during one quarter of the applied voltage And returns exactly the same amount of energy to the driving source during the next one-quarter of a cycle.
The energy delivered to the circuit during a quarter of a cycle is
03-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Capacitive Element
CA sinusoidal voltage is applied to a pure inductor
Differentiating the equation with respect to time
Vm/Im= 1/ωc and i leads v by 90 degree.Therefore, the impedance of C branch is
Here 1/ωC is called capacitive reactance
Xc= 1/ωC = 1/2πfC
03-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Capacitive Element
C
The instantaneous power delivered to the pure capacitor is
•The power variation is symmetrical andThe average power absorbed is equal to zero
• positive and negative power exist for a purelyInductive circuit
03-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Capacitive Element
C
The capacitive element receives energy from source during one quarter of the applied voltage and returns exactly the same amount of energy to the driving source during the next one-quarter of a cycle.
The energy received by the capacitor during a quarter of a cycle is
03-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
RL Branch
Resistane R and Inductance L are connected in series and a sinusoidal sinusoidal Current Imsin ωt flows in the circuit, then
03-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
RL Branch
03-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
RL BranchThe instantaneous power of delivered to the RL circuit is
Average Power
03-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
RL Branch
Instantaneous power delivered to the RL branch
The equation has two components, real and reactive component
Instantaneous Real power Instantaneous Reactive power
Real Power Reactive Power
The real and reactive power may be combined to yield the volt-ampere of the circuit
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
RLC Branch
A sinusoidal current flows to the RLC series circuitThe voltage accross R, L and C become
The sum of the three component voltages
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
RLC Branch
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
RLC Branch
Impedance:
• Inductive and capacitive branch cause exactly opposite phase displacement of current with respect to voltage.• ωL is positive quantity and 1/ωC is negative quantity
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
RLC Branch
i= Im sinωt and v=Vm sin(ωt+Ө)Instantanous power delivered to the RLC branch
Real power delivered to the RLC branch is
Reactive power delivered to the RLC branch is
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Effective Current and Voltage
DC AC
”An alternating current which produces heat in a given resistance at the same average rate as I amperes of direct current is said to have a value of I ”
The average rate of producing heat by direct current isThe average rate of producing heat by AC current during one cycle is
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Root Mean Square Value
The RMS value is the effective value of a varying voltage or current. It is the equivalent steady DC (constant) value which gives the same effect.
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Average Value
Average value of a ac wave is zero, however, average value of a ac wave means the average of either the positive or negative loop of the wave
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
RMS Value of a Sinusoidal Wave
Root mean square value of a sinusoidal wave is 0.7 of the peak value
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Average Value of a Sinusoidal Wave
Therefore, average value of a sinusoidal wave is 0.636 of the peak value
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Form Factor
Form Factor= RMS Value/ Average Value
Form factor is the ratio of the effective voltage to the average value of the wave
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Peak Factor
e = Em sin ωt + (5/12) Em sin 5ωt Form factor= 1.11
Pure sine waveForm factor=0.707 Vm/0.636 Vm = 1.11
•Form factor of both waves are same •It gives no certain indication of wave shape or wave form •Give some indication of relative hysteresis loss• use in determining induced effective voltage when non sinusoidal flux wave is present in the iron core
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Peak Factor
Peak factor is the ratio of the maximum value to the effective value of a wave
Pure sine wavePeak factor= Em/0.707Em = 1.41
e = Em sin ωt + (5/12) Em sin 5ωt Peak factor= 1.85
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Peak Factor
•The purpose of the crest factor calculation is to give an analyst a quick idea of how much impacting is occurring in a waveform
• For dielectric test a knowledge of crest factor is required
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Form Factor and Crest Factor of Different Waves
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Vector Representation of a Sine Wave
• AC computations are often based upon the assumption of sine waves of voltage and current
• It is cumbersome to handle instantaneous values in the form of equations of the waves
• Vector/ Phasor method could be used to represent sine waves
• It simplifies certain kinds of calculations
• The phasor/vector representations of sine functions may be manipulated instead of the sine functions themselves to secure the desired result
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Vector Representation of a Sine Wave
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Vector Representation of a Sine Wave
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Vector Representation of a Sine Wave
• The lengths of two the vectors represent maximum values of the waves respectively, the resultant vector will represent the maximum value of the two waves
• Effective or rms value could be used instead of maximum values
• The vector can be considered to represent effective values
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Vector Representation of a Sine Wave
• A convanient reference axis should be established• Counterclockwise is considered the positive direction of rotation of axis
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Vector Representation of a Sine Wave
• For a pure resistance applied voltage is in phase with the current
• For a pure inductance circuits, the voltage drop accross the inductor leads the current by 90 degree
• For a pure capacitance circuits, the voltage drop accross the capacitor lags the current by 90 degree
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Vector Representation of a Sine Wave
09-02-2010 Dept of Aeronautical Engineering S.M.M. Rahman
MIST
Vector Representation of a Sine Wave