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Difference between revisions of "Silicon Nitride Membrane"

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[[Category:benchmark]]
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[[Category:parametric system]]
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[[Category:linear system]]
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[[Category:first order system]]
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[[Category:physical parameters]]
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[[Category:four parameters]]
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[[Category:time invariant]]
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==Description of the device==
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A silicon nitride membrane (SiN membrane) 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 [1] and infrared sources [2].
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The governing heat transfer equation in the membrane is:
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<math> \nabla \cdot (\kappa \nabla T)+Q - \rho c p \cdot \frac{\partial T}{\partial t}=0 </math>
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where <math>\kappa </math> is the thermal conductivity in <math>W m^{−1} K^{−1}</math>, cp is the specific heat capacity in <math>J kg^{−1} K^{−1}</math>, <math>\rho</math> is the mass density in <math>kg m^{−3}</math> and <math>T</math> is the temperature distribution. We assume a homogeneous heat generation rate over a lumped resistor:
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<math>Q = \frac{U^2(t)}{R(T)}</math>
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with <math>Q</math> the heat generation rate per unit volume in <math>W m^{−3}</math>.
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==Description of the model==
  +
  +
For the silicon nitride membrane under convection boundary
  +
condition and assuming the temperature of the air to be zero, can be rewritten
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as
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(C0 + ρcp · C1)˙T + (K0 + κ · K1 + h · K2)T = F
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U2(t)
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R(T )
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y = E · T
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(11)
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where the volumetric heat capacity ρ ·cp, thermal conductivity
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κ and the heat transfer coefficient h between the membrane
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and the ambient air, are kept as parameters.
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<math>
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\nabla \cdot (\kappa \nabla T) + Q- \rho c_p \frac{\partial T}{\partial t}=0, \quad
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Q=j^2R(T), \quad (1)
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</math>
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  +
where <math>\kappa(r)</math> is the thermal conductivity in <math>W/(m*K)</math> at the position <math>r, \, c_p</math> is the
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specific heat capacity in <math>J /(kg*K), \, \rho(r)</math> is the mass density in
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<math>kg /m^3,</math> and <math>T(r,t)</math> is the temperature distribution. We assume a
  +
homogeneous heat generation rate over a lumped resistor:
  +
  +
<math>
  +
Q = \frac{u^2(t)}{R(T)}
  +
</math>
  +
  +
with unit <math>W/m^3</math>.
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We use the initial condition <math> T_0 = 273K </math>, and the
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Dirichlet boundary condition <math> T = 273 K </math> at the bottom of
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the computational domain. The convection boundary condition at the top of the membrane is
  +
  +
<math>
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q=h(T-T_{air}),
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</math>
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where <math>h</math> is the heat transfer coefficient between the membrane and the ambient air in <math>W/(m^2 K)</math>.
  +
  +
Assuming <math>T_{air}=0</math>, spatial discretization of the heat transfer model in (1) leads to the parametrized system as below,
  +
  +
<math>
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(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
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y=C^T \cdot T.
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</math>
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Here <math>R(T)</math> is either a constant heat resistivity <math>R(T)=R_0</math>, or <math>R(T)=R_0(1+\alpha T)</math>, which depends linearly on the temperature. Here we use <math>R_0=274.94 \Omega</math> and temperature coefficient <math>\alpha=1.469 \times 10^{-3}</math>. The model was created and meshed in ANSYS. It contains a constant load vector corresponding to the constant input power of <math>2.49mW</math>. The number of degrees of freedom is <math>n=60,020</math>.
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The input function <math>u(t)</math> is a step function with the value <math>1</math>, which disappears at the time <math>0.02s</math>. This means between <math>0s</math> and <math>0.02s</math> input is one and after that it is zero. However, be aware that <math>u(t)</math> is just a factor with which the load vector B is multiplied and which corresponds to the heating power of <math>2.49mW</math>. This means if one keeps <math>u(t)</math> as suggested above, the device is heated with <math>2.49mW</math> 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 <math>5mW</math>, then <math>u(t)</math> has to be set equal to two, etc...
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When <math>R(T)=R_0(1+\alpha T)</math>, it is a function of the state vector <math>T</math> and hence, the system has non-linear input. (It is also called a weakly nonlinear system.)
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==Data information==
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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 *.<math>A_i, \, i=0,1,2</math> correspond to the system matrices <math>A_i, \, i=0,1,2</math>, respectively. The files named by <math>*.E_i, \, i=0,1,2</math> correspond to <math>E_i, \, i=0,1</math>. The file named by <math>*.B</math> corresponds to the load vector <math>B</math> and the file named by <math>*.C</math> corresponds to the output matrix <math>C</math>.
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==References==
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[1] T. Bechtold, "Model Order Reduction of Electro-Thermal MEMS", PhD thesis, Department of Microsystems Engineering,
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University of Freiburg, 2005.
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[2] 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).
  +
  +
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Contact information:
  +
  +
'' [[User:Feng|Lihong Feng]] ''

Revision as of 16:26, 16 November 2012


Description of the device

A silicon nitride membrane (SiN membrane) 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 [1] and infrared sources [2].

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}.

Description of the model

For the silicon nitride membrane under convection boundary condition and assuming the temperature of the air to be zero, can be rewritten as (C0 + ρcp · C1)˙T + (K0 + κ · K1 + h · K2)T = F U2(t) R(T ) y = E · T (11) where the volumetric heat capacity ρ ·cp, thermal conductivity κ and the heat transfer coefficient h between the membrane and the ambient air, are kept as parameters.


\nabla \cdot (\kappa \nabla T) + Q- \rho c_p \frac{\partial T}{\partial t}=0, \quad
Q=j^2R(T), \quad (1)

where \kappa(r) is the thermal conductivity in W/(m*K) at the position r, \, c_p is the specific heat capacity in J /(kg*K), \, \rho(r) is the mass density in kg /m^3, and T(r,t) is the temperature distribution. We assume a homogeneous heat generation rate over a lumped resistor:


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

with unit 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).

Assuming T_{air}=0, spatial discretization of the heat transfer model in (1) 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 \cdot T.

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=1.469  \times 10^{-3}. The model was created and meshed in ANSYS. It contains a constant load vector 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=0,1,2 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, "Model Order Reduction of Electro-Thermal MEMS", PhD thesis, Department of Microsystems Engineering, University of Freiburg, 2005.

[2] 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).


Contact information:

Lihong Feng