gate ee 2003 with solutions
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answeresTRANSCRIPT
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GATE EE2003
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Q.1 - 30 Carry One Mark Each
MCQ 1.1 Figure Shows the waveform of the current passing through an inductor of resistance 1 and inductance 2 H. The energy absorbed by the inductor in the first four seconds is
(A) 144 J (B) 98 J
(C) 132 J (D) 168 J
SOL 1.1 The Correct option is (C).Energy absorbed by the inductor coil is given as
EL Pdtt
0
= #
Where power P VI= I L dtdI= b l
So, EL LI dtdI dt
t
0
= b l#For0 4t# # sec
EL 2 I dtdI dt
0
4
= b l# EL 2 ( ) 2 ( )I dt I dt3 0
0
2
2
4
= +# # ,,
,dtdI t
t
3 0 2
0 2 4< in ) diode D2 conducts and D1 will be off so the equivalent circuit is,
Vout 4 Volt= +
In the negative half cycle diode D1 conducts and D2 will be off so the circuit is,
Applying KVL 10I IV 4 10in + 0=
V20
4in+ I=
10V Vin = (Maximum value in negative half cycle)
So, I 20
10 4103 mA= + =
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V V10
in out I=
V10
10 out 103=
Vout ( )10 3= Vout 7= voltHence (D) is correct option.
MCQ 1.64 The circuit of figure shows a 555 Timer IC connected as an astable multi-vibrator. The value of the capacitor C is 10 nF. The values of the resistors RA and RB for a frequency of 10 kHz and a duty cycle of 0.75 for the output voltage waveform are
(A) 3.62 , 3.62R Rk kA B = =
(B) 3.62 , 7.25R Rk kA B = =
(C) 7.25 , 3.62R Rk kA B = =
(D) 7.25 , 7.25R Rk kA B = =
SOL 1.64 In the circuit, the capacitor charges through resistor ( )R RA B+ and discharges through RB . Charging and discharging time is given as.
TC 0.693( )R R CA B= + TD 0.693 R CB=
Frequency . ( )
fT T T R R C1 1
0 693 21
D C A B= =
+=
+
. ( )R R0 693 2 10 10
1A B
9# #+ - 10 103#=
.14 4 103# R R2A B= + ...(1)
Duty cycle TTC= .0 75=
. ( ). ( )
R R CR R C
0 693 20 693
A B
A B
++
43=
R R4 4A B+ R R3 6A B= +
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RA R2 B= ...(2)From (1) and (2) R2 A .14 4 103#= RA 7.21 k=and RB 3.60 k=Hence (C) is correct option.
MCQ 1.65 The simplified block diagram of a 10-bit A/D converter of dual slope integrator type is shown in figure. The 10-bit counter at the output is clocked by a 1 MHz clock. Assuming negligible timing overhead for the control logic, the maximum frequency of the analog signal that can be converted using this A/D converter is approximately
(A) 2 kHz (B) 1 kHz
(C) 500 Hz (D) 250 Hz
SOL 1.65 Maximum frquency of input in dual slop A/D converter is given as Tm T2n C=
where fm T1 maximum frquency of inputm"=
fC T1 clock frequencyC"=
so fm f2nC= , n 10=
1102410 kHz
6
= = (approax)
Hence (B) is correct option.
MCQ 1.66 The boolean expression X Y Z XYZ XYZ XYZ XYZ+ + + + can be simplified to(A) XZ XZ YZ+ + (B) XY YZ YZ+ +
(C) XY YZ XZ+ + (D) XY YZ XZ+ +
SOL 1.66 The Correct option is (B).Given boolean expression can be written as, F XYZ X YZ XYZ XYZ XYZ= + + + + ( ) ( )X YZ YZ X X XY Z Z= + + + + XYZ YZ XY= + + ( ) ( )( )YZ Y X X Z A BC A B A Ca= + + + = + +
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( )( )YZ Y X X X Z= + + + ( )YZ Y X Z= + + YZ YX YZ= + +
MCQ 1.67 The shift register shown in figure is initially loaded with the bit pattern 1010. Subsequently the shift register is clocked, and with each clock pulse the pattern gets shifted by one bit position to the right. With each shift, the bit at the serial input is pushed to the left most position (msb). After how many clock pulses will the content of the shift register become 1010 again ?
(A) 3 (B) 7
(C) 11 (D) 15
SOL 1.67 The Correct option is (B).
X = X X1 05 , Y X2=Serial Input [ ]Z X Y X X X1 0 25 5 5= =Truth table for the circuit can be obtain as.
Clock pulse Serial Input Shif register
Initially 1 1010
1 0 1101
2 0 0110
3 0 0011
4 1 0001
5 0 1000
6 1 0100
7 1 1010So after 7 clock pulses contents of the shift register is 1010 again.
MCQ 1.68 An X-Y flip-flop, whose Characteristic Table is given below is to be implemented
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using a J-K flip flop
(A) ,J X K Y= = (B) ,J X K Y= =
(C) ,J Y K X= = (D) ,J Y K X= =
SOL 1.68 The Correct option is (D).Characteristic table of the X-Y flip flop is obtained as.
X Y Qn Qn+10 0 0 1
0 0 1 1
0 1 0 0
0 1 1 1
1 0 0 1
1 0 1 0
1 1 0 0
1 1 0 0
Solving from k-map
Characteristic equation of X-Y flip flop is Qn 1+ Y Q XQn n= +Characteristic equation of a J-K flip-flop is given by Qn 1+ KQ J Qn n= +by comparing above two characteristic equations J Y= , K X=
MCQ 1.69 A memory system has a total of 8 memory chips each with 12 address lines and 4 data lines, The total size of the memory system is
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(A) 16 kbytes (B) 32 kbytes
(C) 48 kbytes (D) 64 kbytes
SOL 1.69 The Correct option is (A).Total size of the memory system is given by. ( )2 4 812# #= bits 2 814 #= bits 214= Bytes 16 K= bytes
MCQ 1.70 The following program is written for an 8085 microprocessor to add two bytes located at memory addresses 1FFE and 1FFFLXI H, 1FFEMOV B, MINR LMOV A, MADD BINR LMOV M, AXOR AOn completion of the execution of the program, the result of addition is found(A) in the register A
(B) at the memory address 1000
(C) at the memory address 1F00
(D) at the memory address 2000
SOL 1.70 Executing all the instructions one by one. LXI H,1FFE ( (H 1F) , L FE)H H& = = MOV B,M B& Memory [HL] Memory [1FFE]= = INR L L& ( (L 1) FF)H H= + = MOV A,M A& Memory [HL] Memory [1FFF]= = ADD B A& A B= + INR L L& ( ( (L 1) FF) 1) 00H H H= + = + = MOV M,A Memory [HL]& A= Memory [1F00] A= XOR A A& A XOR A= 0=So the result of addition is stored at memory address 1F00.Hence (C) is correct option.
MCQ 1.71 A control system with certain excitation is governed by the following mathematical equation
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dtd x
dtdx x
21
181
2
2+ + 10 5 2e et t4 5= + +
The natural time constant of the response of the system are(A) 2 sec and 5 sec (B) 3 sec and 6 sec
(C) 4 sec and 5 sec (D) 1/3 sec and 1/6 sec
SOL 1.71 Given equation
dtd x
dtdx x2
1181
2
2
+ + e e10 5 2t t4 5= + +
Taking laplace on both sides we have
( ) ( ) ( )s X s sX s X s21
1812 + + s s s
104
55
2= + + + +
( ) ( )s s X s21
1812+ +
( )( )( )( ) ( ) ( )
s s ss s s s s s
4 510 4 5 5 5 2 4= + +
+ + + + + +
System response is,
( )X s ( )( )
( )( ) ( ) ( )
s s s s s
s s s s s s
4 5 21
181
10 4 5 5 5 2 42
=+ + + +
+ + + + + +
b l
( )( )
( )( ) ( ) ( )
s s s s s
s s s s s s
4 5 31
61
10 4 5 5 5 2 4=+ + + +
+ + + + + +
b bl lWe know that for a system having many poles, nearness of the poles towards imaginary axis in s -plane dominates the nature of time response. So here time constant given by two poles which are nearest to imaginary axis.
Poles nearest to imaginary axis
s1 31= , s 6
12 =
So, time constants sec
sec
3
61
2
==
)Hence (B) is correct option
MCQ 1.72 The block diagram shown in figure gives a unity feedback closed loop control system. The steady state error in the response of the above system to unit step input is
(A) 25% (B) 0.75 %
(C) 6% (D) 33%
SOL 1.72 Steady state error for a system is given by
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ess ( ) ( )( )
limG s H ssR s
1s 0= +"
Where input ( )R s s1= (unit step)
( )G s s s153
115= + +b bl l
( )H s 1= (unity feedback)
So ess
( )( )
1
lim
s s
s s
115 1
45s 0= + + +"
b l
15 4515= + 60
15=
%ess 6015 100#= 25%=
Hence (A) is correct option.
MCQ 1.73 The roots of the closed loop characteristic equation of the system shown above (Q-5.55)
(A) 1 and 15 (B) 6 and 10
(C) 4 and 15 (D) 6 and 10
SOL 1.73 Characteristic equation is given by ( ) ( )G s H s1+ 0=Here ( )H s 1= (unity feedback)
( )G s s s153
115= + +b bl l
So, 1 s s153
115+ + +b bl l 0=
( )( )s s15 1 45+ + + 0= 16 60s s2+ + 0= ( 6)( )s s 10+ + 0= s 6,= 10Hence (C) is correct option.
MCQ 1.74 The following equation defines a separately excited dc motor in the form of a differential equation
dtd
JB
dtd
LJK
LJK Va
2 2 + + =
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The above equation may be organized in the state-space form as follows
dtd
dtd P dt
dQVa
2
2
= +
R
T
SSSSS
>V
X
WWWWW
HWhere the P matrix is given by
(A) 1 0JB
LJK2 = G (B) 0 1LJ
KJB2 = G
(C) 0 1
LJK
JB2 = G (D) 1 0JB LJK2 = G
SOL 1.74 Given equation can be written as,
dtd
2
2 J dtd
LJK
LJK Va
2 = +
Here state variables are defined as,
dtd x1=
x2=So state equation is
x1o JB x LJ
K x LJK Va1
2
2= +
x2o dtd= x1=
In matrix form
xx
1
2
o
o> H / / /B J K LJ xx K LJ V1 0 0 a2
1
2=
+> > >H H H
dtd
dtd
2
2
R
T
SSSS
V
X
WWWW P
ddt QVa
= +> HSo matrix P is
/ /B J K LJ
1 0
2 > HHence (A) is correct option.
MCQ 1.75 The loop gain GH of a closed loop system is given by the following expression
( )( )s s sK2 4+ +
The value of K for which the system just becomes unstable is(A) K 6= (B) K 8=
(C) K 48= (D) K 96=
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SOL 1.75 Characteristic equation of the system is given by GH1+ 0=
( )( )s s s
K12 4
+ + + 0=
( )( )s s s K2 4+ + + 0= s s s K6 83 2+ + + 0=Applying rouths criteria for stability
s3 1 8
s 2 6 K
s 1 K6
48
s 0 K
System becomes unstable if K 648 0 = 48K& =
Hence (C) is correct option.
MCQ 1.76 The asymptotic Bode plot of the transfer function /[1 ( / )]K s a+ is given in figure. The error in phase angle and dB gain at a frequency of 0.5a = are respectively
(A) 4.9c, 0.97 dB (B) 5.7c, 3 dB
(C) 4.9c, 3 dB (D) 5.7c, 0.97 dB
SOL 1.76 The maximum error between the exact and asymptotic plot occurs at corner frequency.Here exact gain(dB) at 0.5a = is given by
( )gain dB. a0 5=
log logKa
20 20 1 22= +
( . )
log logKaa
20 20 10 5 /
2
2 1 2
= +; E
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.logK20 0 96= Gain(dB) calculated from asymptotic plot at . a0 5 = is logK20=Error in gain (dB) 20 (20 0.96)log logK K dB= .0 96= dBSimilarly exact phase angle at 0.5a = is.
( ).
ha0 5
=
tan a1 = a k
.tan aa0 51= b l
2 .566 c=Phase angle calculated from asymptotic plot at ( 0.5 )a = is 22.5cError in phase angle . ( . )22 5 26 56c= .4 9c=Hence (A) is correct option.
MCQ 1.77 The block diagram of a control system is shown in figure. The transfer function ( ) ( )/ ( )G s Y s U s= of the system is
(A) s s18 112
13
1+ +` `j j
(B) s s27 16
19
1+ +` `j j
(C) s s27 112
19
1+ +` `j j
(D) s s27 19
13
1+ +` `j j
SOL 1.77 Given block diagram
Given block diagram can be reduced as
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Where G1
s
s
1 1
1
3=+ bb
ll
s 31= +
G2
s
s
1 1 12
1
=+ bb
ll
s 121= +
Further reducing the block diagram.
( )Y s ( )G GG G
1 2 92
1 2
1 2= +
( ) ( )
( )
s s
s s
1 2 31
121 9
2 31
121
=+ + +
+ +
b bb b
l ll l
( )( )s s3 12 18
2= + + +
s s15 54
22= + +
( 9)( 6)s s
2= + +
s s27 1 9 1 6
1=+ +a ak k
Hence (B) is correct option.
MCQ 1.78 The items in Group-I represent the various types of measurements to be made with a reasonable accuracy using a suitable bridge. The items in Group-II represent the various bridges available for this purpose. Select the correct choice of the item in Group-II for the corresponding item in Group-I from the following List-I List-IIP. Resistance in the milli- 1. Wheatstone Bridge ohm rangeQ. Low values of Capacitance 2. Kelvin Double BridgeR. Comparison of resistance 3. Schering Bridge
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which are nearly equalS. Inductance of a coil with 4. Wiens Bridge a large time-constant 5. Hays Bridge 6. Carey-Foster BridgeCodes :(A) P=2, Q=3, R=6, S=5 (B) P=2, Q=6, R=4, S=5
(C) P=2, Q=3, R=5, S=4 (D) P=1, Q=3, R=2, S=6
SOL 1.78 The Correct option is (A).Kelvin Double bridge is used for measuring low values of resistances. ( 2)P"Low values of capacitances is precisely measured by schering bridge ( 3)Q"Inductance of a coil with large time constant or high quality factor is measured by hays bridge ( 5)R"
MCQ 1.79 A rectifier type ac voltmeter of a series resistance Rs , an ideal full-wave rectifier bridge and a PMMC instrument as shown in figure. The internal. resistance of the instrument is 100 and a full scale deflection is produced by a dc current of 1 mA. The value of Rs required to obtain full scale deflection with an ac voltage of 100 V (rms) applied to the input terminals is
(A) 63.56 (B) 69.93
(C) 89.93 (D) 141.3 k
SOL 1.79 Full scale deflection is produced by a dc current of 1 mA ( )Idc fs 1= mAFor full wave reactifier
( )Idc fs I2 m= , Im"peak value of ac current
1 mA .I
3 142 m=
Im .1 57= mA
Full scale ac current
( )Irms fs . .2
1 57 1 11= = mA
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V ( )( )R R Is m rms fs= + 100 ( 100)(1.11 )R mAs= +
(1.11 )
100mA
R 100s= +
100 900# R 100s= + Rs .89 9= kHence (C) is correct option.
MCQ 1.80 A wattmeter reads 400 W when its current coil is connected in the R-phase and its pressure coil is connected between this phase and the neutral of a symmetrical 3-phase system supplying a balanced star connected 0.8 p.f. inductive load. This phase sequence is RYB. What will be the reading of this wattmeter if its pressure coil alone is reconnected between the B and Y phases, all other connections remaining as before ?(A) 400.0 (B) 519.6
(C) 300.0 (D) 692.8
SOL 1.80 The Correct option is (B).First the current coil is connected in R-phase and pressure coil is connected between this phase and the neutral as shown below
reading of wattmeter W1 cosI VP P 1= , . .cos 0 8 36 861 1& c = =
400 cosI V3
LL
1=
400 .I V3
0 8L L #= ...(1)
Now when pressure coil is connected between B and Y-phases, the circuit is
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phasor diagram
angle 2 23.14 30 .54 14c c c= + =now wattmeter reading W2 cosV IYB L 2=
from equation (1) V IL L .0 8400 3#=
so W2 . .cos0 8400 3 53 14# # c=
.519 5= W
MCQ 1.81 The inductance of a certain moving-iron ammeter is expressed as10 3 ( /4)L H2 = + , where is the deflection in radians from the zero position.
The control spring torque is 25 10 6# - Nm/radian. The deflection of the pointer in radian when the meter carries a current of 5 A, is(A) 2.4 (B) 2.0
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(C) 1.2 (D) 1.0
SOL 1.81 In a moving-iron ammeter control torque is given as
c K I ddL
21 2 = =
WhereK" control spring constant" deflection
Given that L 10 3 42
= +
ddL 3 2 H/rad
= b lSo,
(25 10 )c 6# = ( )21 5 3 2 10
2 6#
= b l 2 3 2
=
25 3& = .5
6 1 2= = rad.
Hence (C) is correct option.
MCQ 1.82 A 500A/5A, 50 Hz transformer has a bar primary. The secondary burden is a pure resistance of 1 and it draws a current of 5 A. If the magnetic core requires 250 AT for magnetization, the percentage ratio error is(A) 10.56 (B) .10 56
(C) 11.80 (D) .11 80
SOL 1.82 The Correct option is (B).
Magnetizing current Im 1250 250= = amp
Primary current Ip 500= amp Secondary current Is 5= amp
Turn ratio n II
5500 100
s
p= = =
Total primary current ( )IT [primary current(I )]p 2= + [magnetising current ( )]I 2m
IT I Ip m2 2= +
( ) ( )500 2502 2= + .559 01= amp
Turn ratio n' . .II
5559 01 111 80
s
T= = =
Percentage ratio error n3 100n
n n#= ll
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..
111 80100 111 80 100#= . %10 55=
MCQ 1.83 The voltage-flux adjustment of a certain 1-phase 220 V induction watt-hour meter is altered so that the phase angle between the applied voltage and the flux due to it is 85c(instead of 90c). The errors introduced in the reading of this meter when the current is 5 A at power factor of unity and 0.5 lagging are respectively(A) 3.8 mW, 77.4 mW (B) .3 8 mW, .77 4 mW
(C) .4 2 W, .85 1 W (D) 4.2 W, 85.1 W
SOL 1.83 The Correct option is (C).Power read by meter ( )sinP VIm 3 = Where"3 Phase angle between supply voltage and pressure coil flux." Phase angle of load
Here 3 85 , 60c c= = .cos 0 5a ="So measured power Pm ( )sin200 5 85 60# c c= sin1100 25c= .464 88= W
Actual power PO cosVI = .220 5 0 5# #= 550= W Error in measurement P Pm O= .464 88 550= .85 12= W For unity power factor cos 1= 0c=
So Pm ( )sin220 5 85 0# c c= .1095 81= W PO cos220 5 0# c= 1100=Error in Measurement .1095 81 1100= .4 19= W
MCQ 1.84 Group-II represents the figures obtained on a CRO screen when the voltage signals sinV V tx xm = and ( )sinV V ty ym = + are given to its X and Y plates respectively
and is changed. Choose the correct value of from Group-I to match with the corresponding figure of Group-II.
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Group-I
P. 0 =
Q. /2 =
R. /3 2<
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Divide both Vy and Vx equal parts and match the corresponding points on the screen. Similarly for 90c= Vx sinV txm = Vy ( 90 )sinV tym c= +
Similarly for 23 =
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we can also obtain for 0 23<
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SOL 1.86 The Correct option is ( ).
MCQ 1.87 A chopper is employed to charge a battery as shown in figure. The charging current is 5 A. The duty ratio is 0.2. The chopper output voltage is also shown in the figure. The peak to peak ripple current in the charging current is
(A) 0.48 A (B) 1.2 A
(C) 2.4 A (D) 1 A
SOL 1.87 The Correct option is (A).In the chopper during turn on of chopper V -t area across L is,
V dtLT
0
on# L dtdi dt Ldi
T
i
i
0 min
maxon= =b l# # ( )L i i L Imax min = = ^ h
V -t are applied to L is (60 12)Ton= T48 on=
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So now volt area
I LT48 on= . 0.48
20 1048 0 2 10
3
3
#
# #= =
A
MCQ 1.88 An inverter has a periodic output voltage with the output wave form as shown in figure
When the conduction angle 120c = , the rms fundamental component of the output voltage is(A) 0.78 V (B) 1.10 V
(C) 0.90 V (D) 1.27 V
SOL 1.88 The Correct option is (A).
Output voltage V0 4 /sin sin sinnV nd n t n 2
, ,
S
n 1 3 5 =
3
=b ^ ^ ^l h h h/
`RMS value of fundamental component
Vrms(fundamental) sinV d2
4 1S #
=
120c = , 120 60d d2 &c c= =
Vrms(fundamental) sinV2
4 60S # c
=
0.78 0.78V VS= =
MCQ 1.89 With reference to the output wave form given in above figure , the output of the converter will be free from 5th harmonic when(A) 72c = (B) 36c =
(C) 150c = (D) 120c =
SOL 1.89 The Correct option is (A).After removing 5th harmonic d5 , ,0 2 =
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` Pulse width , ,d2 0 52
54 = = =
, ,0 72 144c c c=
MCQ 1.90 An ac induction motor is used for a speed control application. It is driven from an inverter with a constant /V f control. The motor name-plate details are as follows (no. of poles = 2):415 :3 :50 :2850V V f NV V Hz rpmPh
The motor runs with the inverter output frequency set at 40 Hz, and with half the rated slip. The running speed of the motor is(A) 2400 rpm (B) 2280 rpm
(C) 2340 rpm (D) 2790 rpm
SOL 1.90 The Correct option is (C). NSa 3000 rpm= Na 2850 rpm=
SFL .30003000 2850 0 05= =
where by ( / )V f control
Nsb 3000 5040= b l
2400 rpm= ` N2 new running speed of motor=
1 .2400 20 05= b l
2340 rpm=
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Answer Sheet
1. (C) 19. (C) 37. (D) 55. (B) 73. (C)2. (B) 20. (D) 38. (B) 56. (D) 74. (A)3. (A) 21. (C) 39. (D) 57. (A) 75. (C)4. (A) 22. (A) 40. (B) 58. (A) 76. (A)5. (*) 23. (A) 41. (*) 59. (C) 77. (B)6. (D) 24. (A) 42. (C) 60. (D) 78. (A)7. (C) 25. (B) 43. (D) 61. (A) 79. (C)8. (D) 26. (A) 44. (D) 62. (D) 80. (B)9. (A) 27. (D) 45. (A) 63. (D) 81. (C)10. (D) 28. (D) 46. (C) 64. (C) 82. (B)11. (C) 29. (B) 47. (A) 65. (B) 83. (C)12. (B) 30. (A) 48. (B) 66. (B) 84. (A)13. (B) 31. (C) 49. (D) 67. (B) 85. (*)14. (C) 32. (C) 50. (B) 68. (D) 86. (*)15. (B) 33. (D) 51. (B) 69. (A) 87. (A)16. (C) 34. (D) 52. (A) 70 (C) 88. (A)17. (B) 35. (B) 53. (D) 71 (B) 89. (A)18. (D) 36. (B) 54. (D) 72 (A) 90. (C)