Output characteristics , Other Engineering

Assignment Help:

OUTPUT CHARACTERISTICS:

Figure shows a "Common Emitter" amplifier stage.

2319_OUTPUT CHARACTERISTICS.png

Common Emitter Amplifier Stage

With no base/emitter bias applied, there will be no collector current flowing.  The output voltage VCE will be equal to the supply voltage (40V).  As the collector current  IC flows through resistor RL there will be a voltage drop (IC x RL) across the resistor.  The collector voltage will depend upon the collector current i.e.  40V minus IC x RL  volts.

If  IC  is zero, then VCE must be 40v. VCE  could be reduced to zero by a value of  IC  of 40/RL amperes.  If we assume RL to have a value of 18 ohms, then VCE will be zero for an IC of approximately 2.2 amperes.

Figure shows a graph plotting collector current against collector/emitter voltage
for different values of base current.

 

The straight line from the collector/emitter voltage axis to the collector current axis is the "Load Line" and indicates the only values of VCE and IC which are possible for that circuit.  Obviously, if a different value of RL is used, we would get a different load line with a different slope.

1834_OUTPUT CHARACTERISTICS1.png

For amplifiaction to take place we must first apply an initial bias voltage to the base.  With 1.3 VBE applied the IB will be 25mA giving an IC of 1.4A which would produce an output of 15V (VCE).  If we now apply a sinusoidal input signal of 0.6V, the base current would vary between 15 --35mA, which in turn would vary the IC between 1.1 - 1.7A, giving a voltage output between 10 - 20V.

This produces an amplifier gain of 0.6A/25mA = 30.  Figure shows the voltage/current waveforms of these variations.

 


Related Discussions:- Output characteristics

Embedded system, do u do embedded system assignment?

do u do embedded system assignment?

Propeller governing mode, Propeller governing mode: The speed lever is ...

Propeller governing mode: The speed lever is placed in the high position. The engine is operating at 97 percent. As the power lever is advanced ahead of the flight idle deten

K-map, simplify using k-map f=sum(0,4,5,6,9,10,12)+d(1,15)

simplify using k-map f=sum(0,4,5,6,9,10,12)+d(1,15)

NIRAN, Why spiral model is called meta model?

Why spiral model is called meta model?

Survey, what are the obstacles which are likely to encounter chain survey a...

what are the obstacles which are likely to encounter chain survey and how to overcome them.

Engineering Risk and Reliability , The demand placed on a system is describ...

The demand placed on a system is described by a lognormally distributed random variable with mean 50 and standard deviation of 10. The capacity of the system is modeled by a Weibul

Fire risk assessment process, Fire risk assessment process: This is th...

Fire risk assessment process: This is the main part of the FRA process.    Here we consider the risk, measure it against what we consider acceptable and, if we consider that t

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd