Transmission Line A. Nassiri

73
Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 Lecture 2 Transmission Line A. Nassiri

Transcript of Transmission Line A. Nassiri

Page 1: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010

Lecture 2

Transmission Line

A. Nassiri

Page 2: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 2

Equations

Definitions

Processes

Reflection and Transmissions Coefficients

Complex Plane (Conformal Mapping) and Smith Chart

- Coaxial Line Arbitrary Impedance

Short Circuit

Arbitrary Impedance

Open Circuit

Matched Impedance

Page 3: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 3

Transmission Line Equations

Apply Kirchhoff’s voltage and current laws:

( ) ( ) ( ) ( )tzzt

tzizLtzziRtz ,,,, ∆+ν+

∂∂

∆+∆=ν

( ) ( ) ( ) ( )tzzit

tzzzCtzzzGtzi ,,,, ∆++

∂∆+ν∂

∆+∆+ν∆=

Divide by and taking the limit 0: z∆ z∆

( ) ( ) ( )

( ) ( ) ( )t

tzCtzG

ztzi

ttzi

LtzRiz

tz

∂ν∂

−ν−=∂

∂∂

∂−−=

∂ν∂

,,,

,,, ( ) ( ) ( )

( ) ( ) ( )zVCjGzzI

zILjRzzV

ω+−=∂

ω+−=∂

Page 4: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 4

Traveling Wave Solutions

( ) ( ) ( )zzI

LjRz

zV∂

∂ω+−=

∂∂

2

2

( ) ( ) ( )zVCjGzzI

ω+−=∂

( ) ( ) ( ) ( )[ ]zVCjGLjRz

zVω+−ω+−=

∂∂

2

2

( ) ( )( ) ( )zVCjGLjRz

zVω+ω+=

∂∂

2

2

Page 5: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 5

Traveling Wave Solutions

( ) zz eVeVzV γ−γ−+ += 00

( )( )CjGLjRj ω+ω+=β+α=γ

( ) ( ) ( )−−++ φ+β+ω+φ+β−ω=ν ztVztVtz coscos, 00

( ) zz eZV

eZV

zI γ−

γ−+

−=0

0

0

0

CjGLjR

Zω+ω+

=0

βπ

=λ2

fp λ=βω

Page 6: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 6

The Lossless Line

In many practical cases, the loss of the line is very small and socan be ignored.

LCjj ω=β=γ

CL

YZ ==0

01

LCωπ

=βπ

=λ22

LCp1

=βω

( ) zz eVeVzV γ−γ−+ += 00

( ) zz eZV

eZV

zI γ−

γ−+

−=0

0

0

0

Page 7: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 7

Field Analysis of T.L.

EB

C1

C2

S

C1and C2 are line integration contours, S is the cross-sectional surface.

Field lines on an arbitrary TEM transmission line.

4

4

:Theory Field 00 dsEEWdsHHW *

Se

*

Sm ∫∫ ⋅

ε=⋅

µ=

4

4 :Theory Circuit

20

20 VC

WIL

W em ==

mFdsEE

VCmHdsHH

IL *

S

*

S

: Inductance Self 20

20

∫∫ ⋅ε′

=⋅µ′

=

Page 8: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 8

Field Analysis of T.L.

EB

C1

C2

S

C1and C2 are line integration contours, S is the cross-sectional surface.

Field lines on an arbitrary TEM transmission line

2

l2

:Theory Field

21

c dsEEPdHHRP *

Sd

*

CC

s ∫∫ ⋅ε ′′

=⋅=+

2

2 :TheoryCircuit

20

20

cVG

PIR

P d ==

mSdsEE

VGmdHH

I

RRGR *

S

*

CC

s lmeter per 20

20 21

∫∫ ⋅ε ′′ω

=Ω⋅=+

Page 9: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 9

Example

Geometry of a coaxial line with surface resistance RS on the inner andouter conductors.

γ is the propagation constant of the line.

RS is the surface resistivity.

ε ′′−ε′=ε j.

rµµ=µ 0

( ) ρρ

= γ− ˆln

zeab

VE 0

φπρ

= γ− ˆzeI

H2

0

ρ

ab

µ,ε

RS

θ

y

x

Page 10: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 10

Example – Calculation of L

φπρ

= γ− ˆzeI

H2

0

( )

πµ

=

φρρρπ

µ=⋅

µ= ∫ ∫∫

π

ab

dddsHHI

Lb

aS

ln

*

2

12

2

0222

0

ρ

ab

µ,ε

RS

θ

y

x

Page 11: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 11

Example – Calculation of R

φπρ

= γ− ˆzeI

H2

ab

µ,ε

RS

θ

y

x

ldHHI

RR

CC

S *∫+

⋅=21

20 ( )

φ+φ

π= ∫ ∫

π

π

2

0

2

0222

112

bdb

ada

RS

+

π=

baRS 112

Page 12: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 12

Parameters for Some Common TLs

ab

µ,εRS a a

D

w

d

πµ

=ab

L ln2

( )abC

lnε′π

=2

+

π=

baR

R S 112

( )abG

lnε ′′πω

=2

πµ

= −

aD

L2

1cosh

( )( )aDC

21−ε′π

=cosh

aR

R S

π=

( )( )aDG

21−ε ′′πω

=cosh

wd

=

dwC ε′

=

wR

R S2=

dw

Gε ′′ω

=

Page 13: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 13

.5085.2ln5.12

1204.0

14.1ln2

ln2

ln

2

ln2

''

Ω==

=

===

ππ

πεεµ

πη

πεπµ

ro

o

o ab

ab

ab

CLZ

Problem : Find characteristic impedance of Coax, with a=0.4cm, b=1.14cm and εr=1.5

Page 14: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 14

.ln221

Re21

2

*

abVrdr

rV

rV

AdHEAdSP

ob

a

oo

SS abab

ηππ

η∫

∫∫∫∫

==

⋅×=⋅><=

Average Power transmitted by Coax

I

Sn

Page 15: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 15

mMVa

VE o /2max ==6102 ⋅⋅= aVo

MW.abln.a

ablnVP o 62

12051104 1222

⋅π=

ηπ=

Problem : Find max transmitted power for Coax from Problem 1

Page 16: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 16

Lossless Coaxial Line

Propagation Constant

Wave Impedance

Characteristic Impedance

Power Flow

The flow of power in a transmission line takes place entirely via the electric and magnetic fields between the two conductors; power is not transmitted through the conductors themselves.

For the case of finite conductivity, power may enter the conductors, but this power is then lost as heat and is not delivered to the load.

LCω=µεω=β

η=εµ

=βωµ

==φ

ρ

H

EZw

( )φ

ρ

π==

H

abE

IV

Z20

00

ln

**002

121

IVdsHEPS

=×= ∫

Page 17: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 17

When coaxial cable is terminated by characteristic impedance, the line is perfectly matched and the voltage is constant along the line. The VSWR=1

Coaxial line terminated by characteristic impedance.

E-field in coaxial line. Orientation depends on phase - position along the line.

Coaxial cable as a transmission line with TEM mode

Page 18: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 18

H-field in coaxial line. Orientation depends on phase - position along the line

Surface charge density induced in coaxial line. The sign depends on phase - position along the line.

Page 19: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 19

Surface current in coaxial line. Orientation depends on phase - position along the line.

Page 20: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 20

Voltage on coaxial line does not depend on time and position, because the load is matched.

Page 21: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 21

Voltage on coaxial line does not depend on time and position, because the load is matched.

Page 22: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 22

Coaxial line terminated by an impedance different than the characteristic impedance.

E-field in coaxial line. Orientation depends on phase - position along the line. The VSWR depends on reflection coefficient.

Page 23: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 23

Voltage on coaxial line depends on time and position.

Voltage on coaxial line depends on time and position, but does not go to zero.

Page 24: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 24

Coaxial line terminated by open circuit. The VSWR=indefinitely large.

Coaxial line terminated by short circuit. The VSWR=indefinitely large.

Page 25: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 25

Voltage on coaxial line depends on time and position. The VSWR=indefinitely large.

E-field in coaxial line. Orientation depends on phase - position along the line.

Page 26: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 26

Voltage on coaxial line depends on time and position, and at nodes, goes to zero .

Page 27: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 27

Page 28: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 28

Page 29: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 29

Page 30: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 30

Line length L

Page 31: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 31

Page 32: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 32

Page 33: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 33

Page 34: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 34

Page 35: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 35

Page 36: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 36

Page 37: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 37

Page 38: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 38

Page 39: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 39

Smith Chart

Smith Chart was developed in 1939 by P. Smith at the BellTelephone Laboratory.

One can develop intuition about transmission line and impedance-matching problems by learning to think in terms of the Smith Chart.

Smith Chart is essentially a plot of the voltage reflectioncoefficient, Γ, inthe complex plane.

It can be used to convert from voltage reflection coefficient ( Γ )to normalized impedances (z=Z/Z0) and admittances (y=Y/Y0), and vice versa.

Page 40: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 40

Smith Chart

Page 41: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 41

Complex Γ Plane with z Circles

The Smith Chart is a plot of the voltage reflection coefficient, Γ, on the complex plane superimposed with impedance circles.

The complex Γ plane.

The impedance circles.

jxrZZ

+==

z

jbgYY

y +==

y1

=z

Page 42: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 42

Conformal Mapping - Γand Z

If a lossless line of characteristic impedance Z0 is terminated with a loadimpedance ZL, the reflection coefficient at the load can be written as:

011

ZZ

zezz L

Lj

L

L =Γ=+−

=Γ θ where

This relation can be solved for zL in terms of Γ to give:

( )( ) LL

ir

irj

j

L jxrjj

e

ez +=

Γ−Γ−Γ+Γ+

=Γ−

Γ+= θ

θ

11

11

The real and imaginary part of the above equation can be found by multiplying the numerator and denominator by the complex conjugate of thedenominator to give:

( ) 22

22

11

ir

irLr

Γ+Γ−

Γ−Γ−=

( ) 2212

ir

iLx

Γ+Γ−

Γ=

Page 43: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 43

The rL Circles

( ) 22

22

11

ir

irLr

Γ+Γ−

Γ−Γ−=

2222 12 iriLrLrLL rrrr Γ−Γ−=Γ+Γ+Γ−

112

122 =Γ+Γ+

Γ+Γ

−Γ+ ir

r

rL

r

L rr

112

11122

22

=Γ+Γ+Γ+Γ

Γ+

+

Γ+

−Γ+ ir

r

rL

r

L

r

L

r

L rrrr

22

2

11

1

Γ+

=Γ+

Γ+

−Γr

ir

Lr

r

Page 44: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 44

The rL Circles

x

r0 0.5 1 3

Constant resistance lines in the z = r+jx

+x

-x

V

U0 0.5 1 3

Γ plane

Page 45: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 45

The xL Circles

( ) 2212

ir

iLx

Γ+Γ−

Γ=

( )L

iir x

Γ=Γ+Γ−

21 22

( )22

22 1121

=

+−Γ+Γ−

LLLir xxx

( )22

2 111

=

−Γ+Γ−

LLir xx

Page 46: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 46

The xL Circles

x3

0.51

-0.5-1

-3

r

13

-3-1

0.5

-0.5

V

U

Γ planeConstant reactance lines in (for r≥0) in the z = r+jx

Page 47: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 47

Page 48: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 48

Page 49: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 49

Page 50: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 50

Page 51: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 51

Page 52: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 52

Page 53: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 53

Page 54: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 54

Page 55: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 55

Page 56: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 56

Page 57: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 57

Page 58: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 58

Page 59: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 59

Page 60: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 60

The rL xL Circles

• •

x

r

z=j1

z=0

z=-j1

z=0+jx z=1+jx

1

z=r+j1

z=1-j1

z=1+j1

V

U

901∠=Γ

( )01 ≥+= rjrzofmapping 4634470 .. ∠=Γ

jxzofmapping +=1

jxzofmapping += 0 4634470 .. −∠=Γ

( )jVUplane

+=ΓΓ

1=Γ

1−=Γ

0=Γ

+=

+==

jxrZ

jXRZZ

z

planez

Page 61: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 61

Features of the Smith Chart

All resistance circles have centers on the horizontal Γi=0 axis and all pass through the point Γ=1.

The reactance circles have centers on the vertical Γr=1 line, and pass through the point Γ=1.

The resistance and reactance circles are orthogonal.

Smith Chart can be used to compute the normalized input impedance at a distance l away from the load.

Plot the reflection coefficient ( Γ )at the load

Rotate the point cw an amount 2βl around the center of the chart (toward the generator)

One full rotation around the center of S.C. corresponding to a phaseshift of 0.5λ . A 180°rotation corresponding to λ/4 transformation; thisfacilitate the impedance circles to be used as admittance circles.

Page 62: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 62

Features of the Smith Chart

Γ plotted directly in magnitude and phase

Outside of chart (r =0 circle) is Γ=1

Center pf chart is Γ=0 (i.e.: Z = Z0 )

Top half – inductive x or capacitive b circles

Bottom half – capacitive x or inductive b circles

Left side is short – right side is open

Position on TL? – Rotation, λ toward generator or load

Page 63: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 63

Nomograph

VSWR

Voltage Reflection Coefficient

Power Reflected (%)

Return Loss (dB)

Power Transmitted (%)

Transmission Loss (dB)

Page 64: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 64

The Z Smith Chart

Only impedance circles are plotted on the Γ-plane.

The chart looks quite “clean” but conversion between Y and Z must be done by a rotation.λ/4

Page 65: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 65

The ZY Smith Chart

Impedance and admittancecircles are both plotted on the Γ-plane.

The chart looks confusingbut conversion betweenY and z is automatic.

Page 66: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 66

standing waves result when a voltage generator of outputvoltage (VG = 1sinωt) and source impedance ZG drive a loadimpedance ZL through a transmission line having characteristicimpedance Z0, where ZG = Z0/ZL and where angular frequencyω corresponds to wavelength l (b). The values shown in Figurea result from a reflection coefficient of 0.5.

Here, probe A is located at a point at which peak voltagemagnitude is greatest—the peak equals the 1-V peak of thegenerator output, or incident voltage, plus the in-phase peakreflected voltage of 0.5 V, so on your oscilloscope you wouldsee a time-varying sine wave of 1.5-V peak amplitude (tracec). At point C, however, which is located one-quarter of awavelength (l/4) closer to the load, the reflected voltage is180° out of phase with the incident voltage and subtracts fromthe incident voltage, so peak magnitude is the 1-V incidentvoltage minus the 0.5-V reflected voltage, or 0.5 V, and youwould see the red trace. At intermediate points, you’ll seepeak values between 0.5 and 1.5 V; at B (offset l/8 from thefirst peak) in c, for example, you’ll find a peak magnitude of1 V. Note that the standing wave repeats every halfwavelength (l/2) along the transmission line. The ratio of themaximum to minimum values of peak voltage amplitudemeasured along a standing wave is the standing waveratio,SWR, SWR=3.

Figure 1

Page 67: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 67

Here, point L represents a normalizedload impedance zL = 2.5 – j1 = 0.5/18°(I chose that particular angle primarilyto avoid the need for you to interpolatebetween resistance and reactancecircles to verify the results). Therelationship of reflection coefficient andSWR depends only on the reflectioncoefficient magnitude and not on itsphase. If point L corresponds to | G | =0.5 and SWR = 3, then any point in thecomplex reflection-coefficient planeequidistant from the origin must alsocorrespond to | G | = 0.5 and SWR = 3,and a circle centered at the origin andwhose radius is the length of linesegment OL represents a locus ofconstant-SWR points. (Note that theSWR = 3 circle here shares a tangentline with the rL = 3 circle at the realaxis; this relationship between SWRand rL circles holds for all values ofSWR.)

Page 68: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 68

Using the standing-wave circle, you can determine inputimpedances looking into any portion of a transmission linesuch as Figure 1’s if you know the load impedance. Figure1, for instance, shows an input impedance Zin to bemeasured at a distance l0 from the load (toward thegenerator). Assume that the load impedance is as given bypoint L in Figure 2. Then, assume that l0 is 0.139wavelengths. (Again, I chose this value to avoidinterpolation.) One trip around the Smith chart isequivalent to traversing one-half wavelength along astanding wave, and Smith charts often include 0- to 0.5-wavelength scales around their circumferences (usuallylying outside the reflection-coefficient angle scalepreviously discussed).Such a scale is show in yellow in Figure 2, whereclockwise movement corresponds to movement away fromthe load and toward the generator (some charts also includea counter-clockwise scale for movement toward the load).Using that scale, you can rotate the red vector intersectingpoint L clockwise for 0.139 wavelengths, ending up at theblue vector. That vector intersects the SWR = 3 circle atpoint I, at which you can read Figure 1’s input impedanceZin. Point I lies at the intersection of the 0.45 resistancecircle and –0.5 reactance circle, so Zin = 0.45 – j0.5.

Figure 2

Page 69: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 69

A 100-Ω transmission line with an air dielectric is terminated by a load 50-j80Ω. Determine thevalues of the VSWR, the reflection coefficient, and the percentage of the reflected power. If thepower incident at the load is 100 mW, calculate the power in the load. If the generator frequencyis 3 GHz and the line is 73 cm long, find the input impedance at the generator. What are thevalues of the maximum and minimum impedances existing on the line?

TL

ZR=50-j80Ω

73 cm

VG100 Ω

Page 70: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 70

N M

L

• •

ZLN

ZGN

• G

P=0.56

1.68dBS=3.6

Solution

Step 1: Normalize ZLN

89050100

8050 .. jj

Z LN −=−

=

Step 2: Plot ZLN and draw VSWR circle thru ZLN.

Step 3: Mark off a length equal to thecircles’ radius on the H scale. Thereflection coefficient is P=0.56. Sameon the G scale for reflected power,P2×100=0.32×100=32%. The reflectedpower is (32/100) × 100=32 mW andthe power in the load is 100-32=68mW.

Page 71: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 71

N M

L

• •

ZLN

ZGN

• G

P=0.56

1.68dBS=3.6

Solution cont..

Notice that the reflected power is 10log(32/100)=-4.95dB w.r.t the incidentpower while the load power whencompared with the incident power is 10log(68/100)=-1.68dB

Step 4: From the center of the chartdraw a line thru ZLN and extend the lineto the peripheral scales.

cmcm

fc 10

103103

9

10=

××

==λsec/

sec/

Therefore, 73 cm is equivalent to 7.3 λ.

Page 72: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 72

N M

L

• •

ZLN

ZGN

• G

P=0.56

1.68dBS=3.6

Solution cont..

Identical impedance values on amismatched line repeat every half-wavelength, which is the distance covered byone complete revolution on the Smithchart. A distance of will require14 complete revolution together withadditional rotation of in the CWdirection toward the generator.

7.3 λ.

0.3 λ.

On the inner peripheral wavelengthscale, the distance from ZLN position tothe null position, N, is 0.118λ. We mustthen travel toward the generator afurther 0.3λ-0.118λ= 0.182λon theoutmost peripheral scale and arrive atG.

Page 73: Transmission Line A. Nassiri

Massachusetts Institute of Technology RF Cavities and Components for Accelerators USPAS 2010 73

N M

L

• •

ZLN

ZGN

• G

P=0.56

1.68dBS=3.6

Solution cont..

Step 5: Draw a line from G to the centerof chart. Point ZGN of intersectionbetween this line and the VSWR circlerepresent the normalized inputimpedance at the generator; therefore,ZGN =1.18+j1.43 and the de-normalizedvalue is 118+j143Ω. The min. and max.impedance values on the line,respectively occur at N and M. At N thenormalized value is 0.28+j0 so min.impedance is 28 Ω (Z0/S) and the M is3.6+j0 so max. impedance is 360 Ω or(S×Z0).