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Patterson, Bailey - Solid State Physics Introduction to theory

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5.8 Electromigration (EE, MS) 285

the momentum of the electron before and after collision, and pa and Pa be the momentum of the ion before and after. By momentum and energy conservation we have:

 

 

p + pa = P + Pa ,

 

(5.49)

p2

 

p2

P2

 

P2

 

 

 

+

a

=

 

+

a

+V

,

(5.50)

 

 

 

 

2m

 

2ma

2m

 

0

 

 

 

 

2ma

 

 

where V0 is the magnitude of the potential hole the ion is in before collision, and m and ma are the masses of the electron and the ion, respectively. Solving for Pa and P in terms of pa and p, retaining only the physically significant roots and assuming m << ma:

P = ( p + p

a

) +

p2 2mV ,

(5.51)

a

 

0

 

P = − p2 2mV .

(5.52)

0

 

In order to move the ion, the electron’s kinetic energy must be greater than V0 as perhaps is obvious. However, the process by which ions are started in motion is surely more complicated than this description, and other phenomena, such as the presence of vacancies are involved. Indeed, electromigration is often thought to occur along grain boundaries.

For the simplest model, we may as well start by setting V0 equal to zero. This makes the collisions elastic. We will assume that the ions are pushed along by the electron wind, but there are other forces that cancel out the wind force, so that the flow is in steady state. The relevant conservation equations become:

Pa = pa + 2 p , P = −p.

We will consider motion in one dimension only. The ions drift along with a momentum pa. The electrons move back and forth between the drifting ions with momentum p. We assume the electron’s velocity is so great that the ions are stationary in comparison. Assume the electric field points along the −x-axis. Electrons moving to the right collide and increase the momentum of the ions, and those moving to the left decrease their momentum. Because of the action of the electric field, electrons moving to the right have more momentum so the net effect is a small increase in the momentum of the ions (which, as mentioned, is removed by other effects to produce a steady-state drift). If E is the electric field, then in time τ, (the time taken for electrons to move between ions), an electron of charge −e gains momentum

= eEτ ,

(5.53)

if it moves against the field, and it loses a similar amount of momentum if it goes in the opposite direction. Assume the electrons have momentum p when they are

286 5 Metals, Alloys, and the Fermi Surface

halfway between ions. The net effect of collisions to the left and to the right of the ion is to transfer an amount of momentum of

= 2eEτ .

(5.54)

This amount of momentum is gained per pair of collisions. Each ion experiences such pair collisions every 2τ. Thus, each ion gains on average an amount of momentum eEτ in time τ. If n is the electron density, v the average velocity of electrons and σ the cross section, then the number of collisions per unit time is nvσ, and the net force is this times the momentum transferred per collision. Since the mean free path is λ = , we find for the magnitude of the wind force

F = eEτ n(λ /τ)σ = eEnλσ .

(5.55)

W

 

If Ze is the charge of the ion, then the net force on the ion, including the electron wind and direct Coulomb force can be written

F = −Z eE ,

(5.56)

where the effective charge of the ion is

 

Z = nλσ Z ,

(5.57)

and the sign has been chosen so a positive electric field gives a negative wind force (see Borg and Dienes, op cit). The subject is of course much more complicated that this. Note also, if the mobility of the ions is μ, then the ion flux under the wind force has magnitude Z*naμE, where na is the concentration of the ions. For further details, see, e.g., Lloyd [5.18]. See also Sorbello [5.28]. Sorbello summarizes several different approaches. Our approach could be called a rudimentary ballistic method.

5.9 White Dwarfs and Chandrasekhar’s Limit (A)

This Section is a bit of an excursion. However, metals have electrons that are degenerate as do white dwarfs, except the electrons here are at a much higher degeneracy. White dwarfs evolve from hydrogen-burning stars such as the sun unless, as we shall see, they are much more massive than the sun. In such stars, before white-dwarf formation, the inward pressure due to gravitation is balanced by the outward pressure caused by the “burning” of nuclear fuel.

Eventually the star runs out of nuclear fuel and one is left with a collection of electrons and ions. This collection then collapses under gravitational pressure. the electron gas becomes degenerate when the de Broglie wavelength of the electrons becomes comparable with their average separation. Ions are much more massive. Their de Broglie wavelength is much shorter and they do not become degenerate. The outward pressure of the electrons, which arises because of the Pauli principle and the electron degeneracy, balances the inward pull of gravity and eventually the star

5.9 White Dwarfs and Chandrasekhar’s Limit (A)

287

 

 

reaches stability. However, by then it is typically about the size of the earth and is called a white dwarf.

A white dwarf is a mass of atoms with major composition of C12 and O16. We assume the gravitational pressure is so high that the atoms are completely ionized, so the white dwarf is a compound of ions and degenerate electrons.

For typical conditions, the actual temperature of the star is much less than the Fermi temperature of the electrons. Therefore, the star’s electron gas can be regarded as an ideal Fermi gas in the ground state with an effective temperature of absolute zero.

In white dwarfs, it is very important to note that the density of electrons is such as to require a relativistic treatment. A nonrelativistic limit does not put a mass limit on the white dwarf star.

Some reminders of results from special relativity: The momentum p is given by

 

p = mv = m0γv ,

(5.58)

where m0 is the rest mass.

 

 

 

 

 

β =

v

 

(5.59)

 

c

 

 

 

 

γ = (1 β 2 )1/ 2

(5.60)

E = K + m c2

= kinetic energy plus rest energy

 

0

 

 

 

 

= γm0c2

 

 

 

(5.61)

=mc2 = p2c2 + m02c4 .

5.9.1Gravitational Self-Energy (A)

If G is the gravitational constant, the gravitational self-energy of a mass M with radius R is

 

M

2

 

(5.62)

U = −Gα

 

.

 

R

 

 

 

 

 

 

 

For uniform density, α = 3/5, which is an oversimplification. We simply assume α = 1 for stars.

5.9.2 Idealized Model of a White Dwarf (A)5

We will simply assume that we have N electrons in their lowest energy state, which is of such high density that we are forced to use relativistic dynamics. This

5 See e.g. Huang [5.12]. See also Shapiro and Teukolsky [5.26].

288 5 Metals, Alloys, and the Fermi Surface

leads to less degeneracy pressure than in the nonrelativistic case and hence collapse. The nuclei will be assumed motionless, but they will provide the gravitational force holding the white dwarf together. The essential features of the model are the Pauli principle, relativistic dynamics, and gravity.

We first need to calculate the relativistic pressure exerted by the Fermi gas of electrons in their ground state. The combined first and second laws of thermodynamics for open systems states:

dU = TdS pdV + μdN .

(5.63)

As T 0, U E0, so

 

 

 

 

 

p = −

E

0

 

.

(5.64)

 

 

 

V

N ,T =0

 

 

For either up or down spin, the electron energy is given by

 

ε

p

= ( pc)2 + (m c2 )2

,

(5.65)

 

e

 

 

where me is the rest mass of the electrons. Including spin, the ground-state energy

of the Fermi gas is given by (with p =

k)

 

 

E

 

= 2

( kc)2 + (m c2 )2

=

V

kF k 2

( kc)2 + (m c2 )2 dk . (5.66)

 

0

k <kF

e

 

π 2

0

e

The Fermi momentum kF is determined from

 

 

 

kF3 V

= N ,

 

 

 

3π3

 

 

 

 

 

where N is the number of electrons, or

 

 

 

kF

 

3π 2 N 1/ 3

 

=

V

.

 

 

 

 

 

 

 

 

 

 

 

From the above we have

 

 

 

 

 

E0

kF mec x2

1+ x2 dx ,

N

0

 

 

 

 

where x = k/mec. The volume of the star is related to the radius by

V = 34 πR3

(5.67)

(5.68)

(5.69)

(5.70)

5.9 White Dwarfs and Chandrasekhar’s Limit (A)

289

 

 

and the mass of the star is, neglecting electron mass and assuming the neutron mass equals the proton mass (mp) and that there are the same number of each

M = 2mp N .

(5.71)

Using (5.64) we can then show for highly relativistic conditions (xF >> 1) that

p0 β2 β,

(5.72)

where

 

 

 

 

β

M

2 / 3

.

(5.73)

R2

 

 

 

We now want to work out the conditions for equilibrium. Without gravity, the work to compress the electrons is

R p0 4πr2

dr .

(5.74)

 

 

Gravitational energy is approximately (with α = 1)

GM 2

.

(5.75)

R

 

 

 

If R is the equilibrium radius of the star, since gravitational self-energy plus work to compress = 0, we have

R p0 4πr2

dr

+

GM 2

 

= 0 .

(5.76)

 

 

 

 

 

 

 

R

 

 

 

 

Differentiating, we get the condition for equilibrium

 

 

 

p0

M 2

.

 

 

 

(5.77)

 

 

R

 

 

 

 

 

 

 

 

 

 

 

 

Using the expression for p0 (5.72) with xF >> 1, we find

 

 

1/ 3

 

 

 

M

2

 

 

R M

1

 

 

 

 

,

(5.78)

 

 

M 0

 

 

 

 

 

 

 

 

 

 

where

 

 

 

 

 

 

 

 

 

 

M 0 Msun ,

 

 

 

(5.79)

and this result is good for small R (and large xF). A more precise derivation pre-

dicts M0 1.4Msun. Thus, there is no white dwarf star with mass M M0 Msun. See Fig. 5.8. M0 is known as the mass for the Chandrasekhar limit. When the mass

is greater than M0, the Pauli principle is not sufficient to support the star against gravitational collapse. It may then become a neutron star or even a black hole, depending upon the mass.

290 5 Metals, Alloys, and the Fermi Surface

R

M/Msun

0.80

0.85

0.90

0.95

1.00

Fig. 5.8. The Chandrasekhar limit

5.10 Some Famous Metals and Alloys (B, MET)6

We finish the chapter on a much less abstract note. Many of us became familiar with the solid-state by encountering these metals.

Iron

This, of course, is the most important metal. Alloying with carbon,

 

steel of much greater strength is produced.

Aluminum

The second most important metal. It is used everywhere from alumi-

 

num foil to alloys for aircraft.

Copper

Another very important metal used for wires because of its high

 

conductivity. It is also very important in brasses (copper-zinc al-

 

loys).

Zinc

Zinc is widely used in making brass and for inhibiting rust in steel

 

(galvanization).

Lead

Used in sheathing of underground cables, making pipes, and for the

 

absorption of radiation.

Tin

Well known for its use as tin plate in making tin cans. Originally, the

 

word “bronze” was meant to include copper-tin alloys, but its use

 

has been generalized to include other materials.

Nickel

Used for electroplating. Nickel steels are known to be corrosion resis-

 

tant. Also used in low-expansion “Invar” alloys (36% Ni-Fe alloy).

6 See Alexander and Street [5.1].

Problems 291

Chromium Chrome plated over nickel to produce an attractive finish is a major use. It is also used in alloy steels to increase hardness.

Gold Along with silver and platinum, gold is one of the precious metals. Its use as a semiconductor connection in silicon is important.

Titanium Much used in the aircraft industry because of the strength and lightness of its alloys.

Tungsten Has the highest melting point of any metal and is used in steels, as filaments in light bulbs and in tungsten carbide. The hardest known metal.

Problems

5.1For the Hall effect (metals-electrons only), find the Hall coefficient, the effec-

tive conductance jx/Ex, and σyx. For high magnetic fields, relate σyx to the Hall coefficient. Assume the following geometry:

y, Ey

jy

z, Bz

Reference can be made to Sect. 6.1.5 for the definition of the Hall effect.

5.2(a) A twodimensional metal has one atom of valence one in a simple rectan-

gular primitive cell a = 2, b = 4 (units of angstroms). Draw the First Brillouin zone and give dimensions in cm–1.

(b)Calculate the areal density of electrons for which the free electron Fermi surface first touches the Brillouin zone boundary.

5.3For highly relativistic conditions within a white dwarf star, derive the rela-

tionship for pressure p0 as a function of mass M and radius R using p0 =

− ∂E0/∂V.

5.4Consider the current due to metal-insulator-metal tunneling. Set up an expression for calculating this current. Do not necessarily assume zero temperature. See, e.g., Duke [5.6].

5.5Derive (5.37).

6 Semiconductors

Starting with the development of the transistor by Bardeen, Brattain, and Shockley in 1947, the technology of semiconductors has exploded. With the creation of integrated circuits and chips, semiconductor devices have penetrated into large parts of our lives. The modern desktop or laptop computer would be unthinkable without microelectronic semiconductor devices, and so would a myriad of other devices.

Recalling the band theory of Chap. 3, one could call a semiconductor a narrowgap insulator in the sense that its energy gap between the highest filled band (the valence band) and the lowest unfilled band (the conduction band) is typically of the order of one electron volt. The electrical conductivity of a semiconductor is consequently typically much less than that of a metal.

The purity of a semiconductor is very important and controlled doping is used to vary the electrical properties. As we will discuss, donor impurities are added to increase the number of electrons and acceptors are added to increase the number of holes (which are caused by the absence of electrons in states normally electron occupied – and as discussed later in the chapter, holes act as positive charges). Donors are impurities that become positively ionized by contributing an electron to the conduction band, while acceptors become negatively ionized by accepting electrons from the valence band. The electrons and holes are thermally activated and in a temperature range in which the charged carriers contributed by the impurities dominate, the semiconductor is said to be in the extrinsic temperature range, otherwise it is said to be intrinsic. Over a certain temperature range, donors can add electrons to the conduction band (and acceptors can add holes to the valence band) as temperature is increased. This can cause the electrical resistivity to decrease with increasing temperature giving a negative coefficient of resistance. This is to be contrasted with the opposite behavior in metals. For group IV semiconductors (Si, Ge) typical donors come from column V of the periodic table (P, As, Sb) and typical acceptors from column III (B, Al, Ga, In).

Semiconductors tend to be bonded tetrahedrally and covalently, although binary semiconductors may have polar, as well as covalent character. The simplest semiconductors are the nonpolar semiconductors from column 4 of the Periodic Table: Si and Ge. Compound III-V semiconductors are represented by, e.g., InSb and GaAs while II-VI semiconductors are represented by, e.g., CdS and CdSe. The pseudobinary compound Hg(1–x)Cd(x)Te is an important narrow gap semiconductor whose gap can be varied with concentration x and it is used as an infrared detector. There are several other pseudobinary alloys of technical importance as well.

294 6 Semiconductors

As already alluded to, there are many applications of semiconductors, see for example Sze [6.42]. Examples include diodes, transistors, solar cells, microwave generators, light-emitting diodes, lasers, charge-coupled devices, thermistors, strain gauges, and photoconductors. Semiconductor devices have been found to be highly economical because of their miniaturization and reliability. We will discuss several of these applications.

The technology of semiconductors is highly developed, but cannot be discussed in this book. The book by Fraser [6.14] is a good starting point for a physics oriented discussion of such topics as planar technology, information technology, computer memories, etc.

Table 6.1 and Table 6.2 summarize several semiconducting properties that will be used throughout this chapter. Many of the concepts within these tables will become clearer as we go along. However, it is convenient to collect several values all in one place for these properties. Nevertheless, we need here to make a few introductory comments about the quantities given in Table 6.1 and Table 6.2.

In Table 6.1 we mention bandgaps, which as already stated, express the energy between the top of the valence band and the bottom of the conduction band. Note that the bandgap depends on the temperature and may slowly and linearly decrease with temperature, at least over a limited range.

In Table 6.1 we also talk about direct (D) and indirect (I) semiconductors. If the conduction-band minimum (in energy) and the valence-band maximum occur at the same k (wave vector) value one has a direct (D) semiconductor, otherwise the semiconductor is indirect (I). Indirect and direct transitions are also discussed in Chap. 10, where we discuss optical measurement of the bandgap.

In Table 6.2 we mention several kinds of effective mass. Effective masses are used to take into account interactions with the periodic lattice as well as other interactions (when appropriate). Effective masses were defined earlier in Sect. 3.2.1 (see (3.163)) and discussed in Sect. 3.2.2 as well as Sect. 4.3.3. They will be further discussed in this chapter as well as in Sect. 11.3. Hole effective masses are defined by (6.65).

When, as in Sect. 6.1.6 on cyclotron resonance, electron-energy surfaces are represented as ellipsoids of revolution, we will see that we may want to represent them with longitudinal and transverse effective masses as in (6.103). The relation of these to the so-called ‘density of states effective mass’ is given in Sect. 6.1.6 under “Density of States Effective Electron Masses for Si.” Also, with certain kinds of band structure there may be, for example, two different E(k) relations for holes as in (6.144) and (6.145). One may then talk of light and heavy holes as in Sect. 6.2.1.

Finally, mobility, which is drift velocity per unit electric field, is discussed in Sect. 6.1.4 and the relative static dielectric constant is the permittivity over the permittivity of the vacuum.

The main objective of this chapter is to discuss the basic physics of semiconductors, including the physics necessary for understanding semiconductor devices. We start by discussing electrons and holes—their concentration and motion.

6.1 Electron Motion

295

 

 

Table 6.1. Important properties of representative semiconductors (A)

Semiconductor

Direct/indirect,

Lattice con-

Bandgap (eV)

crystal struct.

stant

 

 

 

 

D/I

300 K (Ǻ)*

0 K

300 K

 

 

 

 

 

Si

I, diamond

5.43

1.17

1.124

Ge

I, diamond

5.66

0.78

0.66

InSb

D, zincblende

6.48

0.23

0.17

GaAs

D, zincblende

5.65

1.519

1.424

CdSe

D, zincblende

6.05

1.85

1.70

GaN

D, wurtzite

a = 3.16,

3.5

3.44

 

 

c = 5.12

 

 

* Adapted from Sze SM (ed), Modern Semiconductor Device Physics, Copyright © 1998, John Wiley & Sons, Inc, New York, pp. 537-540. This material is used by permission of John Wiley & Sons, Inc.

Table 6.2. Important properties of representative semiconductors (B)

Semi-

Effective masses

 

Mobility (300 K)

Relative static di-

conductor

(units of free electron mass)

(cm2/Vs)

 

electric constant

 

Electron*

Hole**

Electron

Hole

 

Si

ml

= 0.92

mlh

= 0.15

1450

505

11.9

 

mt

= 0.19

mhh

= 0.54

 

 

 

Ge

ml

= 1.57

mlh

= 0.04

3900

1800

16.2

 

mt

= 0.082

mhh

= 0.28

 

 

 

InSb

0.0136

mlh

= 0.0158

77 000

850

16.8

 

 

 

mhh

= 0.34

 

 

 

GaAs

0.063

mlh

= 0.076

9200

320

12.4

 

 

 

mhh

= 0.50

 

 

 

CdSe

0.13

0.45

 

800

––

10

GaN

0.22

0.96

 

440

130

10.4

*ml is longitudinal, mt is transverse.

**mlh is light hole, mhh is heavy hole.

Adapted from Sze SM (ed), Modern Semiconductor Device Physics, Copyright © 1998, John Wiley & Sons, Inc, New York, pp. 537-540. This material is used by permission of John Wiley & Sons, Inc.

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