2.1. Model of Vacuum Degradation
In vacuum packaged MEMS sensors, vacuum degree is degraded mainly due to the release of gas inside the cavity [
13], including gas molecules adsorbed on the inner wall of the cavity, gas molecules in the material inside the cavity, etc. High temperatures are the main source of sensitive stress [
14]. It is generally true that vacuum-packaged MEMS sensors have resonant structures, which can be used as a measure of the level of vacuum inside the cavity of the package [
15]. Hence, this paper first establishes a mathematical model for predicting the degradation of the Q-factor of vacuum packaged MEMS sensors when exposed to high temperatures. Here is a description of how the mathematical model is constructed.
Material outgassing from vacuum-packaged MEMS sensors is considered an unsteady process, and the diffusion coefficient in different directions is regarded as a constant. Based on Fick’s second law:
In this formula,
n represents the number of gas molecules per unit cross-sectional area,
t represents the diffusion time, and
D represents the diffusion coefficient. The Gilliland formula can be used to express the diffusion coefficient
D as follows:
where
T denotes the thermodynamic temperature,
p is the total pressure,
μ is the molecular weight, and
V is the liquid gram molar volume of the gas at its normal boiling point.
After vacuum packaging, the MEMS sensor cannot maintain an absolute vacuum state in its cavity, so there will be a certain amount of gas in the initial state, which is directly related to the initial Q-factor of the samples. Considering this, assuming there are
N0 gas molecules in the sealed cavity at the beginning, and
Ntot is the total number of gas molecules released, the boundary condition for the number of molecules inside the cavity
N(
t) over time is:
Based on the above conditions, the Fourier series method may be used to calculate the diffusion equation as follows:
As a result, the number of free gas molecules can be expressed as follows:
MEMS sensors that are vacuum packaged can be described by the following vacuum degradation model:
In the formula, a = 1/Q0 + A × Ntot, b = A × Ntot, c = DT, and the physical meanings of model parameters a, b, and c are as follows:
Parameter a represents the final total number of gases inside the sample cavity, which determines the final Q-factor of the sample. Depending on parameter b, the degree of degradation of the sample is determined by the number of gases released inside the sample cavity. Parameter c characterizes the degradation speed of the sample, which is related to temperature.
With time, the vacuum degree of the vacuum-packaged MEMS sensor decays exponentially. By fitting the experimental data to the above-mentioned model, parameters a, b, and c can be obtained. The above analysis also reveals that 1/(a−b) is the initial value of the Q-factor of the sample.
2.2. Experiment of Reliability Evaluation
2.2.1. Sample
As it is difficult to detect and activate the MEMS microstructure of the MEMS products electrically, we customized a batch of samples. It is typical to find MEMS gyroscopes in commercial applications. The structure of the device must be in a resonant state, and it is usually packaged in a vacuum. In order to investigate vacuum degradation of vacuum packaged MEMS devices, this paper selects the sensitive structure of a MEMS gyroscope as the subject of experimental research.
As shown in
Figure 1b, MEMS gyroscopes have comb structures as their internal structure. During the operation of the gyroscope, the position of the combs will change, as will the capacitance between them. It is possible to determine the value based on the change in capacitance. As a result, the vacuum encapsulated gyroscope will have difficulty moving the comb, which will adversely affect the gyroscope’s performance.
As shown in
Figure 1a, three types of device-level packaged MEMS gyroscopes were customized with different vacuum degrees.
Table 1 provides information regarding the vacuum packaging of the samples. There were a total of 18 samples, which were divided into three groups. Samples that were highly vacuum packaged were H1 and H6, medium vacuum packaged samples were M1 and M6, and low vacuum packaged samples were L1 and L6.
2.2.2. Test Method and System
Considering that the Q-factor can be used to characterize the vacuum of a MEMS cavity, the Q-factor of our sample was evaluated. As shown in
Figure 2, we developed a Q-factor test method based on transient excitation [
16] for the above-mentioned test samples with different levels of vacuum.
Q value measurement is based on the oscillating principle [
17]. Labview software, an NI PXI 4461 acquisition card, an analog circuit, and a MEMS sensor are included in the test system. A part of the test process is as follows: by applying excitation signals to the resonant structure of the MEMS sensor using the acquisition card, Labview software causes the sensor to enter the steady state. After stopping the excitation, the sensor is in a state of damped vibration. As a final step, the acquisition card collects the transient response voltage signal and passes it to Labview for analysis and processing. Using Labview software, it is possible to determine the resonant frequency and Q value rapidly by using wave peak detection technology, the cycle average method, and exponential fitting algorithm.
2.2.3. Experiment
The environment has a significant impact on the reliability of vacuum-packaged MEMS sensors. It has been reported that the Q-factor of vacuum packaged MEMS gyroscopes will degrade with time at room temperature [
13]. Based on theory and analysis, it has been tentatively determined that temperature affects the outgassing of internal materials.
At the beginning of the research, a vacuum packaged MEMS gyroscope was baked at three different high temperatures and the Q-factor was monitored over time. According to
Figure 3, the Q-factor of the MEMS gyroscope dropped sharply at high temperatures. Accordingly, the analysis of the theoretical and experimental results indicates that high temperature is the main stress contributing to the degree of vacuum degradation of MEMS sensors packaged in a vacuum.
At different temperatures, we conducted accelerated degradation experiments on the samples using the high-temperature accelerated test method based on MIL-STD-883. As shown in
Table 2, samples with high vacuum, medium vacuum, and low vacuum were tested at three temperatures of 85 °C, 105 °C, and 125 °C.
In order to conduct a reliability test, the following steps must be followed:
(1) Prior to the test, the Q-factor of the samples is measured at room temperature;
(2) Incubator temperature is raised to the specified temperature, and samples are placed in the incubator after the temperature reaches the specified temperature;
(3) The samples are baked at a high temperature, and then taken out of the incubator after t1 min;
(4) The Q-factor of the samples is determined after they have stood at room temperature for two hours;
(5) After the measurements have been completed, the samples are placed back into the incubator;
(6) Repeat steps (3) and (4) until the test is complete.