Добавил:
Upload Опубликованный материал нарушает ваши авторские права? Сообщите нам.
Вуз: Предмет: Файл:

Книги2 / 1993 P._Lloyd,__C._C._McAndrew,__M._J._McLennan,__S._N

.pdf
Скачиваний:
51
Добавлен:
11.03.2016
Размер:
14.08 Mб
Скачать

J. Lorenz et a1.: The STORM Technology CAD System

177

1.2xl0

16

LASER

+ BOOae

anneal

,-.....

 

 

1.0

0

 

 

 

 

C\l

 

 

 

 

I

S

 

 

Np=const

 

 

 

 

 

0.8

 

 

 

 

()

 

 

 

 

Np=f(t)

~

 

 

 

 

 

()

0.6

 

 

 

 

 

 

q

 

 

 

 

 

 

0

 

 

 

 

 

 

 

 

()

0.4

 

 

 

 

B

-+->

 

 

 

 

 

Q)

 

 

 

 

 

 

 

 

Q)

 

 

 

 

 

 

 

,.q

0.2

 

 

 

 

 

 

rn

 

 

 

 

 

 

 

 

 

0.0

10°

101

102

103

104

 

 

 

 

annealing time (min)

Figure 6: Sheet carrier concentration vs. implanted specimens with dose 1·1016cm-3 treatment

annealing time at 800°C for Sb and B and laser annealed before the isothermal

than this, significant implant-induced nonequilibrium defect populations are present for most of the anneal time and influence dopant diffusion. Defects generated by ion implantation are in general represented either as an initial amount of vacancies and interstitials located in the bulk at the same place as the dopants, or as dislocations at the boundary of the amorphised silicon, or as amounts of defects which decrease with time independently from diffusion and recombination phenomena. The algorithm implemented in STORM is robust enough for all these cases. The influence of defects on dopant diffusion was shown even at temperatures as low as 850°C.

5.1.3Dopant-Dopant Interactions

The precipitation kinetics of boron and antimony in silicon at high concentrations are accurately modelled by the LAMEL SOLMI model incorporated into the STORM code by CNETj the model also simulates very high concentration As precipitation. In STORM, the model has been combined with the MMG model described above. In order to take the precipitation into account, an additional term P(x,t) which acts as a source or sink for the dopant has been added to the diffusion equation. P(x,t) is the amount of dopant going to or leaving the precipitates in the interval dt:

P(x, t) =411"· D(C) [C(x, t) - Csol]· rp(x, t) Np(x, t)

(10)

This source term depends on the dopant solubility Cso!, and the number Np and radius rp of precipitates. Csol is a function of temperature and co-diffusing dopant

178

J. Lorenz et al.: The STORM Technology CAD System

concentration only. Np remains constant with time at the initial critical nuclei density Np(x,O):

(11)

rp grows from the initial nucleus size rp(x,O) to rp(x,t) by a diffusion limited growth rate:

(12)

Here, Cp is the dopant concentration in the precipitate, a is the surface free energy between precipitate and matrix, and Knl the only fitting parameter, is related to the density of available nucleation sites.

In Fig. 6, a comparison of the simulated and measured electrical conductivity of Band Sb oversaturated silicon as a function of the anneal time is shown. In the simulations, both a constant precipitate density Np and a precipitate density Np(t) decreasing with time are considered. Good agreement between experiment and simulation is obtained.

5.2Diffusion in and from Polycrystalline Materials

As in some other simulators, STORM can approximate diffusion in polycrystalline materials by using a (high) constant diffusion co~fficient, and for some applications, this is a fast and satisfactory approach. However, in many cases, the microstructure of the material must be taken into account, and in STORM this option is available through the incorporation of the GMMT physically-based polysilicon model. This model has also been used by IMEC, with adjusted parameters, to simulate dopant diffusion in and from CoSb.

5.2.1Diffusion in and from Polysilicon

The polysilicon model incorporated into the STORM code is the most sophisticated 2D model currently available. The basic model, described elsewhere [33, 34, 35], uses a local homogenisation approach to solve simultaneously the grain growth and the dopant diffusion in grain boundaries, in the grain interior and along interfaces, and the segregation at grain boundaries and at interfaces. It has been successful in predicting a wide range of experimentally observed profiles. The influence of doping concentration and temperature on grain growth, dopant diffusion and dopant segregation is accurately modelled. The principles of the model are summarized in Fig. 7 and Fig. 8.

The model described above has been extended for true simulation of non-planar microstructures by including a modification of the Mei model [36] for grain growth with a term related to the local curvature at each location inside the polysilicon layer, determined from the mathematical divergence of the columnar orientation vector function stored for each point. The effect of the curvature is to enhance growth rates at convex corners and to reduce it at convace corners, through a change in the total free energy per unit volume.

Another extension of the model consists in the inclusion of epitaxial alignment, using the basic mechanism proposed earlier [34], to define a nucleation time for slits to

182

J. Lorenz et &1.: The STORM Technology CAD System

6.1Diffusion and Reaction of Oxidizing Species

For the diffusion and reaction of the oxidizing species a straight-forward generalization of the well known Deal & Grove model [37] is used, which assumes stationary diffusion with an effective diffusivity Deff in the oxide

 

div (Deff .

grad C) = 0

(13)

and the boundary condition

 

 

ac

=kJ" (C - C*)

on the free surface

(14)

Deff · an

ac

= k• . C

on the Si/Si02 interface

(15)

Deff . an

ac

=0

on the Si02 /SiaN4 interface

(16)

an

 

 

 

Here, e· is the surface concentration resulting from Henry's law, and k, and k. are the transfer coefficient at the free surface and the reaction rate at the Si/Si02 interface, respectively. Diffusion and reaction coefficient depend on temperature, Hel concentration and stress:

Deff

= De!J,o· DHc1 exp (-(Vcto +P . Vdp / kT)

(17)

k.

= k.o · kHC1 . exp (-(VlcO +0""" . Vkp/ kT)

(18)

Here, P is the hydrostatic pressure, and 0""" is the normal stress along the Si/Si02 interface. The model parameters used in eqs. (14-18) have been taken from literature.

The diffusion-reaction equations are solved numerically by using a standard finiteelement method with piecewise linear shape functions and numerical quadrature rules.

6.2Oxide growth near Si/Si02 interfaces

During a time step 6..t, an infinitesimal new oxide layer with thickness 6 is grown:

6 = 6..t . C . k./Nl

(19)

For the calculation of the movement of the interface between Si and Si02 , two different approaches are being used. In the first one, the interface between Si and Si02 is displaced by the incremental additional oxide thickness 6. Afterwards, suitable equations of motion are solved to express the mechanical reaction of the silicon. In the second approach, the interface is displaced by 0.44 ·6 to express the consumption of the silicon, and the dilatation of the layers is considered afterwards. In this latter case, a mesh is built in the newly formed oxide in each time step. This also decreases the numerical noise otherwise resulting from unstructured triangular meshes. In contrast to the first approach this one also correctly includes that part of the stress which results from ID oxidation, whereas the first approach includes 2D extra stress only. Both principles are shown in Fig. 11.

6.3Displacement resulting from surface tension and dilatation forces

Following the approaches described above, the oxidation kinetics either leads to Dirichlet boundary conditions on velocities at the interface between rigid Si and Si02 ,

184

J. Lorenz et al.: The STORM Technology CAD System

G

 

E

(21)

2 (1 + v)

 

 

 

 

vE

(22)

 

(l+zi) (1-2v)

 

 

The components of the stress tensor 0"

are given by

 

 

). [l-vaV + aVy]

 

v

x

ay

=

ax

). [l-VaVy + av ]

 

v

ay

x

 

ax

=

G [avx + aVy]

 

 

ay

ax

 

Shear stress and pressure are deduced from the stress tensor as follows:

(23)

(24)

(25)

(26)

 

(O"xx +O"yy)2 +O";y

(27)

p

O"xx +O"yy

= -~\7 . if

(28)

 

2

2v

 

and the normal stress along any boundary or interface depends on the normal component Vn and the tangential component VT of the velocity via

_). [1 -v aVn

a~]

(29)

O"nn -

v

an

+ aT

 

The boundary conditions are that if is zero in rigid materials, O"nn is zero on the free surface, and Vx is zero at the left and right sides of the structure. For the interfaces between Si02 and silicon,

if = -0.56 . ii . C . k./Nl

(30)

Here, N1 is the number of oxidizing molecules incorporated into a unit volume of the oxide layer.

In STORM, the elastic model outlined here is used as the default one for silicon nitride, and also recommended for oxide layers at temperatures below 1000°C.

The link between viscosity and elasticity coefficients in silicon dioxide is achieved by introducing a relaxation time T, which is applied to cumulative stresses in the expressions of diffusivity and reaction rate. The Maxwell viscoelastic model is assumed for the shear modulus G and the viscosity f.L:

f.L = T . G

(31 )

J. Lorenz et al.: The STORM Technology CAD System

185

In STORM, thermal dilatation is accounted for during thermal ramps (under oxidizing or inert ambients) by simulating the different expansion between bulk silicon and the other materials. Thermal stresses are computed in all materials defined as elastic or visco-elastic. The internal forces which result from temperature variations lead to an additional term in the elasticity or visco-elastic equations; from first principles, the internal pressure is given as CithK 6T, where Cith is the volume expansion coefficient, K is the bulk modulus, and 8T denotes the temperature variation.

6.3.2Visco-elastic Model

Alternatively, a viscoelastic model may be used in STORM. In this model, the components of the strain tensor e depend on the components of the stress tensor 0' via the stress deviator 0", the hydrodynamic pressure p, the shear stress modulus G, the viscosity J-l and the components Dx and Dy of the dilatation force:

 

 

exx

 

1/2G . dO'~x/dt +O'~x/2J-l

 

 

exy

=

1/2G· dO'~y/dt +O'~y/2J-l

 

 

eyy

=

1/2G . dO'~y/dt +O'~y/2J-l

 

 

,

 

 

O'xx

=

O'xx -

P

 

 

O'~y

=

O'yy -

P

 

 

,

 

O'xy

 

 

 

O'xy

 

 

aO'xx

+

aO'XY

=

Dx

 

ax

7fY

 

aO'xy

 

aO'yy

 

Dy

 

7h + 7fY

 

 

 

 

 

(32)

(33)

(34)

(35)

(36)

(37)

(38)

(39)

In addition to the boundary condition (30) of the elastic model, the surface tension at the free surface is inversely proportional to the local curvature radius R:

p. = ,/R

(40)

This condition has negligible influence in case of thermal oxidation, but is the driving force for glass reflow.

In this model, the pressure is computed as a piecewise constant solution and is used a a Lagrange multiplier for expressing the uncompressibility of the materials at a fixed temperature. A modified version of the well-known Uzawa algorithm is used to combine this uncompressibility, the elastic term in eqs. (32-34), and the different dilatation forces.

6.3.3Stress-reduced Viscosity

In STORM, stress reduced viscosity has been expressed according to the work by Suturdja and Oldham [40]:

J-l = J-lo' exp( Ep./kT ). J-l/sinh(T/)

(41)

with

186

J. Lorenz et al.: The STORM Technology CAD System

 

", =VI" (J'.heo.r/ kT

(42)

Here, P is the local viscosity, (J'.heo.r is the shear stress, and the parameters VI" Po, and EI' are taken from literature [41).

6.3.4 Viscosity of BPSG Glasses

The viscosity parameters referred to above are valid for thermal oxidation. For planarization, materials with much lower viscosity are used, such as phospho-silicate and boro-phospho-silicate glasses. For BPSG, the preexponential term Po has been expressed versus boron concentration for different deposition processes, whereas EI' shows no clear dependence on process conditions.

6.3.5Finite Element Simulation of Dilatation Forces

Dilatation forces result either from the transformation of Si into Si02 or from thermal dilatation. They can be expressed as gradient of a scalar function d. This fits well to the Finite Element approach to solve the oxidation problem. If some silicon is not treated as a rigid body, the full stress tensor needs to be evaluated, including 1D stress occuring during full wafer oxidation. In this case, the scalar function d in the new oxide layer is

d =(A + 2 G) ( 1 - p)/ p

(43)

Otherwise, only extra stress resulting from local 2D effects is simulated.

Furthermore, at each time step the thermal dilatation is simulated, depending on the dilatation coefficient 0th of each material:

 

d=K(Tt

 

(44)

TITAN-6

Locos simulation

Temperature=920'C

PAD-oxide thickness= I 00 Ang.

Tlme=300 min.

Nitride thikness= 1300 Ang.

 

 

 

~--..---- .-

 

/ .

__ simulation

 

-- -"

without stress effect

 

 

_

simulation

 

 

with stress effect

 

 

VkP=2SA 3 • Vdp-SO 'A3

 

 

• experiment

 

 

II!

 

 

 

T~~~~r-~~~~~~~~~~~~~r4

0.0

'.t

1.0

1 0

Figure 12: Comparison between experiment and STORM/TITAN simulatiom of local oxidation at 920°C for 300 min