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Static response of miniature capacitive pressure sensors with square or rectangular silicon diaphragm
G. Blasquez, Y. Naciri, P. Blondel, N. Ben Moussa, Patrick Pons
To cite this version:
G. Blasquez, Y. Naciri, P. Blondel, N. Ben Moussa, Patrick Pons. Static response of miniature capac- itive pressure sensors with square or rectangular silicon diaphragm. Revue de Physique Appliquée, Société française de physique / EDP, 1987, 22 (7), pp.505-510. �10.1051/rphysap:01987002207050500�.
�jpa-00245566�
Static response of miniature capacitive pressure sensors with square
orrectangular silicon diaphragm
G.
Blasquez,
Y.Naciri,
P.Blondel,
N. Ben Moussa and P. PonsC.N.R.S.-L.A.A.S., 7,
avenue duColonel-Roche,
31077Toulouse,
France(Reçu
le 22 décembre1986, accepté
le 13 mars1987)
Résumé. 2014 La
réponse
enrégime statique
des capteurs depression capacitifs
dont l’élément sensible est unefine membrane de silicium
rectangulaire
ou carrée est étudiée dansl’hypothèse
des déformations faibles.L’équation
deLagrange
décrivant la déflexion de la membrane est résolue àpartir
du théorème des travaux virtuels et d’une solutionapprochée
dutype polynomial.
Il est montré que laréponse
peuts’exprimer
sous uneforme normalisée
qui
nedépend
que de la valeur du rapport des côtés de la membrane. Pour une surface de siliciumdonnée,
les capteurs degéométrie
carrée sont lesplus
sensibles alors que les capteursrectangulaires
sont
plus
linéaires.Enfin,
la formulationproposée
permet aussi de déterminer d’une manièrerapide
etfacile,
les quatre
paramètres géométriques
définissant ce type de capteur.Abstract. 2014 The static response of
capacitive
pressure sensors with a thinrectangular
or squarediaphragm
isstudied, assuming
small deflections.Lagrange’s equation
is solved from the virtualdisplacement
theorem andan
approximated polynomial
solution. It is shown that response can beexpressed
under a normalized formdependent only
on the value of thediaphragm
dimension ratio. For agiven
siliconsurface,
square sensors exhibit thehighest sensitivity
whereasrectangular
sensors have a more linear behaviour.Finally,
theproposed
formulation
equally
allows easy andrapid
determination of the fourgeometric
parametersdefining
this type ofsensor.
Classification
Physics
Abstracts06.30 - 07.50
1. Introduction.
Over the last
decade,
economic sectors like : theautomotive
industry,
the health and medicalservices,
domesticappliances,
have beenrequiring
an increas-ing
number ofhigh performance,
low cost, miniature pressure sensors. Thisrequirement
was metby
thedevelopment
ofpiezoresistive
sensors.Nevertheless,
the latter suffer the
major
drawback ofbeing
tem-perature-sensitive
and thereforerequire
the additionof individual
compensating systems
whichgreatly
increase their cost.
Similarly
and in order toprevent
inpart
suchdrawbacks,
W. D.Frobenius,
A. C. Sanderson and H. C. Nathanson[1]
haveproposed
miniature press-ure sensors
operating
on theprinciple
of a variablecapacitor
and with a thin silicondiaphragm
assensing
element.Intrinsically,
thistype
of device isfree of the
defects
ofpiezoresistive
sensors. Inaddition,
it is easier to manufacture.Finally,
S. K.Clark and K. D. Wise
[2]
haveproposed
a compara- tivestudy
of thesensitivity
ofpiezoresistive
andcapacitive
sensors to pressure and have shown that the latter exhibit thehighest sensitivity.
From theaforementioned considerations it may be assumed that
capacitive
pressure sensors willundergo
amajor development
in the near future.With this
perspective
inmind,
K. W. Lee and K. D. Wise[3]
havedeveloped
a simulation program known as « SENSIM », based on the finitedifference method,
to simulate the response of thin silicondiaphragm
pressure sensors. Ineffect,
the fundamen- talequation goveming
thediaphragm behaviour
is apartial differential equation
of the fourth orderwhich has no exact
analytic
solution and the sensorresponse is
given by
a doubleintegral
whose inte-grant
factor is of thehyperbolic type.
In otherwords,
theproblem
cannot be solvedanalytically.
Atpresent,
the « SENSIM » program is of restricted circulation and not available to mostpotential
users.Similarly,
the response curves which have beenpublished
refer tospecific
square structures ofgiven
dimensions.
However,
the microelectronics tech-Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/rphysap:01987002207050500
506
nology
allows the manufacture(with
the same tech-nological process)
of square orrectangular
dia-phragm
sensors whose dimensions may vary within alarge
range of values.Finally,
because the sensorresponse is
dependent
on fourparameters,
sensordesign
is not a trivialproblem.
The aim of this paper is to :
a)
demonstrate the existence of a normalized response which is more or lessindependent
of thesensors
geometric dimensions,
b)
underline therespective advantages
of rec-tangular
and square sensors,c) provide
a formulationfacilitating
thedesign
ofthese sensors.
The response is derived from a
semi-analytic
resolution of
Lagrange’s equation
based on thevirtual
displacement
method and on thechoice of
anapproximated polynomial
solution.This paper is divided into three
major headings : a) analytic study
ofdeflection,
b)
establishment of the normalized response, andc)
validation of the theoretical model from the measurements carried out on sensors realized atLAAS.
2. Deflection
study.
Consider a silicon
plate (see Fig. 1)
oflength b,
width a and thickness h. Fortechnological
reasons[4],
theplate
faces consist of(100) cristallographic planes
and its sides are(110)
oriented. Theappli-
cation of a constant and uniform pressure,
P,
on oneof its faces causes, at
point
of coordinates(x, y ),
adeflection
W (x,
y,P ).
Fig.
1. - Definition of coordinate system.It is assumed that :
a)
thediaphragm
isfully clamped
on itsedges,
.
b) diaphragm bending
is of the elastictype,
andc)
deflectionW (x, y, P )
remains small relative toh.
In these
conditions,
it is shown inappendix
thatthe deflection of the silicon
diaphragm
isgoverned by
thefollowing
differentialsystem :
where a = 0.798 and
Do
= 1.42 x101°
Pa.To obtain a
general
formulationindependent
ofthe
diaphragm geometric dimensions,
achange
invariable is introduced such that the new
integration
domain
is,
in allcases,
asquare
of unit side :x 2 a x 1 --X-- + 1 (3)
Y=2y, -1,Y,+1. 4 Solving the system (see
in Appendix)
with the
Galerkin method
[5]
leads to thefollowing approxi-
mated
analytical
solution :where
Table. z Normalized
deflection : coefficients qf
thepolynomial
solution.n, is an even
positive integer
.i, j = 0, 2, 4, 6, ..., n
r = bla
k (r )
andki, (r)
areshape
factors whose values aregiven
in the table for r= 1,
2 and3,
and n = 4.The normalized deflection for r = 1 and r = 3 is
illustrated
infigures 2,
3 and 4.x
Fig.
2. - Normalized deflection of a squarediaphragm (r =1 ).
1B
Fig.
3. - Normalized deflection of arectangular
dia-phragm (r
=3) along
the Ox axis.Y
Fig.
4. - Normalized deflection of arectangular
dia-phragm (r
=3) along
theOy
axis.3. Sensor response.
A variable
capacitor
is realized with the silicondiaphragm
and a metallizedplate.
In the absence ofapplied
pressure(P
=0 )
the distance betweenplates equals
d.Sensor
capacitance
isgiven by :
C (0) = 80 S/d (8)
where Eo stands for vacuum
permittivity,
andS = ab is the
plate
area.It has been seen that the
application
of a uniformpressure
P ~
0 on one of thediaphragm
facessensors causes, at
point (X, Y),
a deflectionW (X, Y, P ).
At thispoint,
thedistance
betweenplates
becomes d -W (X, Y, P ) (see Fig. 5).
Sensorresponse is then
given by :
a
where
W(X, Y, P )
« d.Fig.
5. - Platebending
underapplied
pressure(P 96 0).
Given the axial
symmetry
of the bentdiaphragm (see Figs. 2,
3 and4),
conditionW (X, Y, P )
d isequivalent
toW(O, 0, P) : d.
ForW(0,0,P)=
d,
a short-circuit occurs betweenplates.
The sensorbecomes
inoperative.
In thefollowing,
thespecific
value of
P,
for whichW (o, 0, P ) = d
is notedPsc.
The
analytic expression
ofPsc is easily
deducedfrom
(6) :
From
(5), (6)
and(10), expression (9)
can bewritten under the
following
normalized form :The numerical
integration
of(11)
leads to the results shown infigure 6.
The curves of thisfigure
arealmost « universal » in that
they
areindependent
of508
Fig.
6. - Normalizedresponse
ofrectangular
and square sensors.the values
of
thegeometric parameters h,
d and S. Howeverthey
remain a function of the value of thediaphragm
ratio r =b/a.
As a first
approximation,
the sensor response can bedecomposed
into twoparts :
a more or less linear section followedby
astrongly
nonlinear section.If
d,
h and S are constant, it caneasily
beshown,
from the table and
(10),
thatP sc is
anincreasing
function of r.
Hence,
thegreater
r, the wider the linear section(see Fig. 6).
On the other
hand,
the responseC (P ) computed
from
equation (10),
the values ofk(r) given
in thetable and the normalized responses, indicate that the square sensors are the most sensitive devices
(see Fig. 7).
P
( 102 Pa
1Fig. 7.
-Response
of square andrectangular
sensors(S = 4 mm2, h = 15 f.Lm, d = 5 f.Lm).
4. Model validation.
To
verify
the modelvalidity,
we have realizedsensors
which
areanalogous
to those described in[1, 3, 4, 6-8].
The fixedplated
wasdeposited
onglass
and
the diaphragm
was obtainedby anisotropic
chemical
etching
of silicon. Bothparts
wereassem-
bled
by
anodicbonding [8].
Thetypical
dimensionsof these devices were : 10 03BCm h 30 J.tm, 3 >m * d -- 10
J.tm, S
= 4mm 2@ [9].
The values of C
(P ),
C(0)
were measured with animpedance analyser (HP 4192A).
The valuePc (r) is
deduced from the
analysis
of the sensor response.Indeed,
for P =P SC the
curvesC (P )
differgreatly
from the theoretical behaviour. In
addition,
thesensor
leakage
conductance G increasesrapidly.
Theshort circuit pressure
Psc
can therefore be deter- mined from the examination ofC (P )
orG (P ).
Toobtain the best
possible determination,
these twomethods were used
simultaneously.
Nosignificant discrepancies
were noticed in the results obtained.Figures
8 and 9 show theexperimental
and theor-etical behaviours of square
(r =1 )
andrectangular (r = 3)
structures. Thegood agreement
betweentheory
andexperiments
validates themodel
and the simulation programs.Reciprocally,
it shows that it ispossible
torealize
devicesoperating
in accordancer/ rsC
Fig.
8. - Validation of the response model in the case of square sensor.P/Psc
Fig.
9. - Validation of the response model in the case ofrectangular
sensor.with fundamental
concepts. Finally,
thisstudy
con-firms the results obtained
by
other authors[4, 7]
with square
diaphragm
sensors.5. Conclusion.
A
thorough investigation
of the static response of miniature pressure sensors has been carried out forthin
square andrectangular
silicondiaphragms.
Lagrange’s
differentialequation describing
the dia-phragm
deflection has been solvedassuming :
smalldeflections and
fully clamped edges. Basically,
themethodology
relies on anapproximated
solution ofthe
polynomial type
and on the virtualdisplacement
theorem. The coefficients of these
polynomials
werecalculated
using
asemi-analytic
method in the casewhere the
edge
ratios areequal
to1,
2 and 3respectively
andby taking
into account the aniso-tropic properties
of silicon.From the
expression
ofdeflection,
the sensor response has been simulated.The
results obtainedwere
given
under a normalized form which isindependent
of :a)
thediaphragm
thickness andsurface,
b)
the distance betweenplates
withoutapplied
pressure,
c)
the absolutepressure
value.In this
model,
theinput
variable is the normalized pressure(relative
to theshort-circuit pressure).
Moreover,
thelatter
model isexpressed
under ananalytic
form. Theproposed
model hasbeen
val-idated
experimentally.
The results
presented
in this paper areinteresting
in many ways.
First,
whatever the sensor dimensions it ispossible
to foresee the sensor behaviour withouthaving
todesign
and writesophisticated
numericalprograms. Conversely from
theuser requirements (in particular
the desired response, the maximumpressure and the
value
of thecapacitor
atrest)
it ispossible
to determinedirectly
theoptimal
values ofthe sensor
geometric
dimensions(from
the nor-malized response,
expressions (8)
and(10)).
Thenormalized response and the associated
analytic
relations therefore constitute a
design
tool which canbe
easily
andrapidly implemented.
Finally,
theproposed
calculationprocedure
andmodel can
easily
beapplied
to materials other thansilicon, particularly,
to thesimple
case ofisotropic
material.
Appendix.
In terms of Cartesian
coordinates,
theequilibrium equation linking bending
moments,Mij,
withpress-
ure, can be written as
[2]
The
bending
moments are linked with deflectionsby
means of second order differential
systems [2] :
where
El, Et
and v areYoung’s modulus,
shearmodulus and Poisson’s ratio
respectively. By
sub-stituting,
the differentialsystem (A.2)
intoequation (A.1)
we obtain(1) :
where
and
The
changing
of variable definedby (6)
and(7)
allows us to write
equation (1)
under the form :where r =
b/a.
The associated
boundary
conditions aregiven by :
Because the differential
system consisting
of(A.5)
and
(A.6)
islinear,
it admits a solution of thepolynomial type :
Moreover,
this solution mustverify (A.6)
and ac-count for the axial
symmetry
of deflection. From[5]
these conditions lead to
representing ’Pii(X, Y)
under the
following
form :where
i, j
=0, 2, 4, 6,...,
n. ’To determine
Kij,
the virtualdisplacement
method
[5]
is used. It leads to thefollowing integral
system :
510
By substituting (A.8)
into(A.7)
and the resultobtained into
(A.9)
thepartial
derivates of(A.9)
canbe
expressed
under ananalytic
form.Then,
we obtain a Cramer’ssystem
in which there are doubleintegrals
which can be calculatedanalytically.
Thecalculation of these
integrals yields
analgebraic system
of linearequations
whose unknowns are the coefficientsKij. Finally,
the resolution of thissystem by
means of numerical methods allows us tospecify
the values of
Kij.
In our case,
given
thegrowing complexity
of thecalculations for
high
values of i andj,
we restrictedourselves to
solving
thesystem
for n = 4 and for the values of r= 1,
2 and 3.. The results obtained are
given
in the table under a. normalized form
(i.e.
wegive
the values ofKijIKOO).
For
writing convenience,
we letkij
=Kij/K00.
Thevalue of
K00
isgiven by (6).
It is notedW(0 ; 0)
sinceit can
easily
be demonstrated from(A.7)
and(A.8)
that
Koo
=W(0 ; 0).
Given thisremark, (A.7)
canbe written under the form :
.
where
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