
 
membrane approximates a linear function, as it 
steadily decreases with increasing pyramid size. The 
upper graph in Fig. 5 shows the membrane 
deflection for different pyramid sizes. One important 
aspect to point out is the constant maximum 
deflection value for the membrane, not at a single 
point, but under the complete pyramid base area. 
This last effect cannot be modelled by using the 
mathematical formulation presented in Section 3, 
even if we modify it to increase its accuracy in order 
to get closer to the results obtained by FE analysis. 
Fig. 4 and Fig. 5 also show that the presence of a 
pyramid on top of the membrane of our capacitive 
MEMs pressure sensor produces a smaller deflection 
than expected in the fault-free case. Thus, this faulty 
condition implies a sensitivity loss of the sensor that 
can compromise its reliability, which is a critical 
issue for implantable devices. 
Therefore, it is important to count on an accurate 
behavioural model for its main component, the 
membrane, valid for both fault-free and faulty 
conditions. As said before, its deflection can have an 
acceptable analytical solution in the fault-free case. 
However, in this work we have proven that this 
mathematical formulation is no longer valid for 
modelling the membrane with certain kinds of faults 
as, for example, the formation of pyramids on top of 
the membrane. Therefore it is necessary to create 
additional mathematical models that accurately 
describe the behaviour of the membrane under faulty 
conditions, considering the deflection results 
obtained through FE simulations. Especially for 
those faulty cases which significantly affect the 
geometry and/or material properties of the 
membrane. 
5 CONCLUSIONS 
In this work test-related problems for implantable 
capacitive MEMS pressure sensors for the early 
detection of in-stent restenosis have been presented. 
 The typical failure mechanisms and defects that can 
give raise to the faulty behaviour of a 
microelectromechanical system have also been 
explained. 
The deflection problem of circular membranes 
has been proven to be analytically or numerically 
solvable for a fault-free case, in order to build a 
behavioural model of the sensor. Nevertheless, this 
mathematical model is not valid to describe certain 
faulty conditions where the geometry or the material 
properties of the membrane are seriously affected. 
So as to obtain a realistic fault model in these cases a 
finite-element analysis must be performed. 
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