Anonymous
×
Create a new article
Write your page title here:
We currently have 105 articles on MOR Wiki. Type your article name above or click on one of the titles below and start writing!



MOR Wiki

Difference between revisions of "Silicon Nitride Membrane"

Line 57: Line 57:
   
 
==References==
 
==References==
[1] T. Bechtold, D. Hohfel, E. B. Rudnyi and M. Guenther, "Efficient extraction of thin-film thermal parameters from numerical models via parametric model order reduction," J. Micromech. Microeng. 20(2010) 045030 (13pp).
+
[1] T. Bechtold, D. Hohfeld, E. B. Rudnyi and M. Guenther, "Efficient extraction of thin-film thermal parameters from numerical models via parametric model order reduction," J. Micromech. Microeng. 20(2010) 045030 (13pp).
   
 
[2] J. Spannhake, O. Schulz, A. Helwig, G. Müller and T. Doll,"Design, development and operational concept of an advanced MEMS IR source for miniaturized gas sensor systems ," Proc. Sensors, 762-765, 2005.
 
[2] J. Spannhake, O. Schulz, A. Helwig, G. Müller and T. Doll,"Design, development and operational concept of an advanced MEMS IR source for miniaturized gas sensor systems ," Proc. Sensors, 762-765, 2005.

Revision as of 09:51, 19 November 2012


Description of the model

A silicon nitride membrane (SiN membrane) [1] can be a part of a gas sensor, but also a part of an infra-red sensor, a michrothruster, an optimical filter etc. This structure resembles a microhotplate similar to other micro-fabricated devices such as gas sensors [2] and infrared sources [3]. See Fig.1, the temperature profile for the silicon nitride membrane.

The governing heat transfer equation in the membrane is:

 \nabla \cdot (\kappa \nabla T)+Q - \rho c_p \cdot \frac{\partial T}{\partial t}=0

where \kappa is the thermal conductivity in W m^{-1} K^{-1}, cp is the specific heat capacity in  J kg^{-1} K^{-1}, \rho is the mass density in kg m^{-3} and T is the temperature distribution. We assume a homogeneous heat generation rate over a lumped resistor:

Q = \frac{u^2(t)}{R(T)}

with Q the heat generation rate per unit volume in W m^{-3}. We use the initial condition  T_0 = 273K , and the Dirichlet boundary condition  T = 273 K at the bottom of the computational domain.

The convection boundary condition at the top of the membrane is


q=h(T-T_{air}),

where h is the heat transfer coefficient between the membrane and the ambient air in W m^{-2} K^{-1}.

Discretization

Under the above convection boundary condition and assuming T_{air}=0, spatial discretization of the heat transfer model leads to the parametrized system as below,


(E_0+\rho c_p \cdot E_1) \dot{T} +(A_0 +\kappa \cdot A_1 +h \cdot A_2)T = B \frac{u^2(t)}{R(T)}, \quad
y=C^T T,

where the volumetric heat capacity \rho c_p, thermal conductivity \kappa and the heat transfer coefficient h between the membrane and the ambient air T_{air}, are kept as parameters.

Here R(T) is either a constant heat resistivity R(T)=R_0, or R(T)=R_0(1+\alpha T), which depends linearly on the temperature. Here we use R_0=274.94 \Omega and temperature coefficient \alpha=2.293 \pm 0.006 \times 10^{-4}. The model was created and meshed in ANSYS. It contains a constant load vector B corresponding to the constant input power of 2.49mW. The number of degrees of freedom is n=60,020.

The input function u(t) is a step function with the value 1, which disappears at the time 0.02s. This means between 0s and 0.02s input is one and after that it is zero. However, be aware that u(t) is just a factor with which the load vector B is multiplied and which corresponds to the heating power of 2.49mW. This means if one keeps u(t) as suggested above, the device is heated with 2.49mW for the time length of 0.02s and after that the heating is turned off. If for whatever reason, one wants the heating power to be 5mW, then u(t) has to be set equal to two, etc... When R(T)=R_0(1+\alpha T), it is a function of the state vector T and hence, the system has non-linear input. (It is also called a weakly nonlinear system.)

Data information

The system matrices are in MatrixMarket format (http://math.nist.gov/MatrixMarket/) and can be downloaded here File:Matrices gassensor.tgz. The files named by *.A_i, \, i=0,1,2 correspond to the system matrices A_i, \, i=0,1,2, respectively. The files named by *.E_i, \, i=0,1 correspond to E_i, \, i=0,1. The file named by *.B corresponds to the load vector B and the file named by *.C corresponds to the output matrix C.

References

[1] T. Bechtold, D. Hohfeld, E. B. Rudnyi and M. Guenther, "Efficient extraction of thin-film thermal parameters from numerical models via parametric model order reduction," J. Micromech. Microeng. 20(2010) 045030 (13pp).

[2] J. Spannhake, O. Schulz, A. Helwig, G. Müller and T. Doll,"Design, development and operational concept of an advanced MEMS IR source for miniaturized gas sensor systems ," Proc. Sensors, 762-765, 2005.

[3] M. Graf, D. Barrettino, S. Taschini, C. Hagleitner, A. Hierlemann and H. Baltes, "Metal oxide-based monolithic complementary metal oxide semiconductor gas sensor microsystem," Anal. Chem., 76:4437-4445, 2004.

Fig.1 Fig 1.png


Contact information:

Lihong Feng

Tamara Bechtold (tamara.bechtold@imtek.uni-freiburg.de)