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

Architectural Design and Drawing, how can I improve my G+4 apartment with r...

how can I improve my G+4 apartment with rendering with pen and ink

Flight dynamics - introduction, In the Aircraft Performance course, the air...

In the Aircraft Performance course, the aircraft was assumed to be in a steady-state (e.g. steady  cruise, climb, turn, glide), with the forces and moments balanced. The subject of

Hydraulics.., A pump delivers 40 lpm to a 100 mm bore/25 mm rod cylinder to...

A pump delivers 40 lpm to a 100 mm bore/25 mm rod cylinder to move a load of 22 kN. A throttle is introduced on the rod end, and return flow with a 10 lpm flow rate. A 70 bar press

Types of engine, TYPES OF ENGINE: The internal combustion engines for the ...

TYPES OF ENGINE: The internal combustion engines for the automotive use may be classified according to the following considerations: Engine cycle Number of strokes F

Causes of unbalance - aircraft design, Causes of unbalance Unbalance ma...

Causes of unbalance Unbalance may be caused by a variety of factors occurring singly or in combination with others. These factors include:- a) Eccentricity Eccentricity

Matlab assignment, can you formulate a program using only bubblesort for as...

can you formulate a program using only bubblesort for assigning grades in an array?

URGENT, Suppose an investor acquired 1 Round lot of Walden stock at $30/sha...

Suppose an investor acquired 1 Round lot of Walden stock at $30/share last year. If the investor received a $1.00 per share dividend during the year and sells the shares at year-en

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