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An Inherently-Robust 300◦C MEMS Temperature Sensor for Wireless Health Monitoring of Ball and Rolling Element Bearings Sean Scott∗ , Farshid Sadeghi† , and Dimitrios Peroulis∗ ∗ School of Electrical and Computer Engineering of Mechanical Engineering Purdue University, West Lafayette, Indiana 47907 Email: {scottsm, sadeghi, dperouli}@purdue.edu † School Abstract— Presented is an inherently-robust wireless capacitive MEMS temperature sensor capable of operating to 300◦ C. The heart of the sensor is an array of bimorph (metal-dielectric) cantilevers whose deflections are sensed by an array of appropriatelyplaced electrodes. The key advantages of this configuration are the following. First, its dielectric layer is SiO2 thermally-grown at 1,100◦ C as opposed to conventional low-temperature PECVD or sputtered films. Second, the lack of a sensing surface directly beneath the movable structures renders stiction nearly impossible. Third, the fringing-field sensing results in constant sensitivity throughout the entire temperature range. Fourth, the employed passive approach is immune to high-temperature reliability issues faced by active devices. Furthermore, the fabrication yield is over 99%, even in an academic cleanroom (Birck Nanotechnology Center at Purdue University). When configured with an inductor and wirelessly interrogated, the measured resonant frequency has a linear shift from 206 MHz at room temperature to 199 MHz at 300◦ C. as silicon carbide may seem to be a desirable option. However, these devices have reliability issues at high temperatures [2], [3], and require expensive materials and fabrication processes. A potential solution which has been explored involves two inductively-coupled coils. One of the coils is located away from the bearing, and is used for interrogation. The other is located directly on the bearing, and is connected to a temperature-sensitive capacitor which works to the necessary operating temperatures (Figure 1). I. I NTRODUCTION Knowledge of a component’s temperature or strain can be an excellent indication of the component’s overall health and remaining lifetime [1]. For example, in bearings, spalling or development of small cracks on the rolling elements will result in an increase in friction. This friction generates an increase in temperature, which will further increase as a crack propagates over time. As a result, early knowledge of this temperature increase can lead to prediction of time until failure. Currently, sensors on military aircraft monitor either the oil temperature outside of the bearing, or the housing temperature containing the entire assembly. However, because it is much closer to the point of failure, the bearing cage temperature has much faster response time and higher resolution than either of these options. As such, miniature, harsh environment sensors which can be integrated directly on the cage and read wirelessly are in high demand for real-time health monitoring. This becomes challenging, however, as this is an oily, and potentially contaminated environment, and the cage rotates at thousands of revolutions per minute. Average temperatures may vary based on the speed of rotation, but a sensor must be able to operate to at least 300◦ C. Because typical CMOS electronics are not functional at this temperature, a remotelypowered active circuit utilizing a high-bandgap material such 978-1-4244-5335-1/09/$26.00 ©2009 IEEE Fig. 1. A telemetry concept is employed to allow the temperature to be read wirelessly. A temperature sensitive capacitor is used to change the resonant frequency. MEMS bimorphs deflect downward as temperature increases, thus increasing the capacitance. This MEMS-based approach allows for much higher temperatures than commercial devices. 975 IEEE SENSORS 2009 Conference II. D ESIGN AND FABRICATION C ONSIDERATIONS A common approach employed for wireless temperature sensing involves using temperature-dependant commercial capacitors in an LC resonator configuration, which is interrogated remotely [4]. However, no commercial capacitors today simultaneously achieve small size, monotonic temperature response, and high-temperature operation (over 300◦ C). More appropriate thermal capacitors have been made with MEMS bimorph devices [5], [6]. These devices feature metaldielectric cantilevers which deflect as temperature increases. Unfortunately, these typically suffer from large creep and hysteresis at high temperatures due to a poor quality dielectric layer (typically PECVD, sputtered or other low-temperature films). These sensors usually involve a bimorph and electrode beneath to sense the capacitance in a parallel-plate topology. This technique allows for large changes in capacitance, but this increase is most significant when the beam is nearly deflected. As a result, the sensitivity at lower temperatures, and linear frequency response of the resonator are lost. By employing a bimorph made with a high-temperature dielectric in a fringing-field fashion, both of these problems are solved simultaneously, and additional benefits are gained as well. A bimorph is created by stacking two materials with differing coefficients of thermal expansion (CTE). As temperature increases, the material with the higher CTE will expand to a greater extent, and cause the structure to deflect. To generate large deflection, a metal is commonly used for the top layer, and a dielectric for the bottom. These are placed in a fringingfield configuration in which stationary electrodes are placed adjacent to the released bimorph (Figure 2). This technique helps to maintain a linear frequency response in the resonator (Figure 3). In our case, gold is used on top, and we make use of the mechanical properties of the thermally-grown oxide as our dielectric layer. Because of thermal mismatch in the processing, the beams are naturally deflected upwards at room temperature. The thicknesses of these layers and their respective CTEs will determine the amount of deflection at a specific temperature. As such, the thicknesses and materials should be selected so that the beams will be flat at the maximum desired operating temperature. In our case, about 0.5 µm of both oxide and gold yields a cantilever that lays flat at about 300◦ C. The beams used are typically several tens of µm wide and several hundreds of µm long. Because the mass of each beam is so small, the inertial effects of the bearing have virtually no impact on the sensor’s capacitance. For instance, with an acceleration of 100 Gs, the maximum tip displacement is about 90 nm, or less than 0.1% of its range. The fabrication of the MEMS bimorph capacitors is completed with a relatively-simple process, done entirely in-house at the Birck Nanotechnology Center cleanroom at Purdue University. First, an oxide is thermally grown at 1,100◦ C on a high-resistivity silicon wafer to a thickness of about 0.5 µm (Figure 4(a)). Next, the oxide is patterned using traditional lithography and a wet etch (Figure 4(b)). The metal layers Fig. 2. Depiction of difference between parallel plate sensing and fringingfield sensing. Parallel-plate sensing generates larger magnitudes for a certain area, but most of the increase is at high temperatures. Fig. 3. Simulated comparison between resonant frequency trends when parallel-plate and fringing-field sensing capacitors are coupled with inductors. Fringing-field sensing results in much more linear resonant frequency vs. temperature trends. 976 of titanium (about 50 nm for adhesion) and gold (about 0.5 µm) are then sputtered and patterned (Figure 4(c)). After this, the devices are diced into individual samples and attached and wirebonded to a commercially-available transistor outline (TO) header for packaging. The cantilevers of the device are next released with a dry-etch of the silicon using XeF2 (Figure 4(d)). The cantilevers naturally deflect upwards at room temperature due to the thermal mismatches of the films in the process. Finally, the TO can is resistively-welded to the header creating a complete, hermetically-packaged sensor (Figure 4(e)). (a) (b) (c) (d) Fig. 5. The robust fabrication process results in extremely-high fabrication yield across wafers. Around 500 individual cantilevers of 10 µm by 250 µm are shown. An advantage of the small cantilevers is that the mass is so small that inertial forces have virtually no impact on the cantilevers. (e) Fig. 4. Fabrication Process, after [7]: A thermal oxide is grown (a) and patterned (b) on a bare silicon wafer. A Ti adhesion layer and thicker Au layer are then sputtered and patterned (c). Dry etch of the silicon using XeF2 is used to release the cantilevers (d), and the devices are protected using a commercial hermetic package (e). This relatively-simple process, robust design, and dry-etch for release result in an extremely high fabrication yield, nearlyperfect across a wafer (Figure 5). The sensor is then attached to an inductor which is embedded in a plastic insert attached to the bearing cage. This plastic insert is used to isolate the wire from the metal, reducing eddy currents so significant coupling between the interrogating coil and LC can be achieved. Finally, a dummy sensor is placed opposite to dynamically balance the cage (Figure 6). Fig. 6. Image of the completed sensor integration on the bearing. A dielectric insert isolates the coil from the metallic cage, reducing eddy currents. A dummy sensor is placed opposite the original (but not connected electrically) to balance the bearing. to increase the temperature as capacitance is recorded (Figure 7). Once the packaged sensor is connected to the inductor, an interrogating coil is connected to a network analyzer (Figure 8). The two coils are placed an appropriate distance apart, at which the coupling is still large enough to see the resonance (a few cm). After this, the sensor is heated with the hotplate, while the interrogating coil remains at room temperature, and the network analyzer records the data (Figure 9). III. M EASURED R ESULTS Both the capacitance versus temperature of the individual sensor and the resonant frequency versus temperature of the resonator are measured. To measure the capacitance change as temperature increases, low capacitance probes are connected to the Analog Devices AD7746 evaluation board which is connected via USB to a PC. These probes touch measurement pads connected to each side of the device, one side to the anchor of the bimorph, the other touching the fixed electrodes. The entire silicon piece is on a ceramic hotplate, which is used IV. C ONCLUSION A new, passive, wireless temperature sensor based on a MEMS, thermally-tunable capacitance has been presented. The thermal oxide employed allows the sensor to operate to at least 300◦ C. The fringing-field method used results in a linear change in resonant frequency from 206 MHz at room temperature to 199 MHz at 300◦ C, with constant sensitivity over the entire range. In addition, the dry-etching of the substrate in the release step result in a high yield 977 Fig. 7. Measured capacitance vs. temperature for a small array of bimorphs. By scaling the number of bimorphs, the capacitance range can be scaled to obtain the best resonant frequency for the application. Here, the capacitance is only measured to 200◦ C to prevent damaging the measurement probes. Fig. 9. Measured resonant frequency vs. temperature for the MEMS capacitor attached to an inductor, and remotely read by an interrogating coil, as shown in Figure 8. ACKNOWLEDGMENT The authors would like to thank the Patuxent River Naval Air Station for financially supporting this project under grant number 103625 entitled “Disruptive MEM Sensors for Monitoring Aircraft Drivetrains”. R EFERENCES Fig. 8. Measurement setup to wirelessly record resonant frequency of resonator. An interrogating coil magnetically couples with the LC formed by the sensor and coil. The S11 of the coil determines the resonant frequency, which is tuned by the temperature dependence of the sensor. process in which stiction is virtually impossible in both the release and in operation. All of these benefits, along with the hermetic packaging of the MEMS component, give way to an industry-ready device. It is the author’s belief this is the first temperature sensor capable of surviving up to 300◦ C integrated and tested on a real-world bearing cage. Moreover, the flexibility of the process and high-quality dielectric show no signs of failure at 300◦ C, so this device will likely be a strong candidate for even higher temperatures. Although this configuration requires close-proximity operation, the MEMS can be reconfigured to operate in a far-field device as well [8], resulting in robust, multi-situational solutions for harsh environment temperature sensing. [1] A. Joshi, S. Marble and F. Sadeghi, “Bearing Cage Temperature Measurement Using Radio Telemetry”, Proceedings of the Institution of Mechanical Engineers, Vol 215, Part J. [2] Z. D. Schwartz and G. Ponchak, “High Temperature Performance of a SiC MESFET Based Oscillator”, 2005 IEEE MTT-S Int. Microwave Symp. Dig., Long Beach, CA, June 11-17, 2005. [3] M. S. Mazolla, R. Kelley, J. R. B. Casady et al, “SiC Devices for Converter and Motor Drive Applications at Extreme Temperatures”, 2006 IEEE Aerospace Conference, Big Sky, MT, March 4-11, 2006. [4] A. Kovacs, D. Peroulis and F. Sadeghi, “Early-Warning Wireless Telemeter for Harsh-Environment Bearings”, in IEEE Sensors 2007 Conference, Atlanta, Georgia, October 28-31, 2007, pp. 946-949. [5] A. DeHennis and K. D. Wise, “A Wireless Microsystem for the Remote Sensing of Pressure, Temperature, and Relative Humidity”, Journal of Microelectromechanical Systems, vol. 14, pp. 12-22, 2005. [6] I. Zine-El-Abidine, M. Okoniewski, and J. G. McRory, “RF MEMS Tunable Inductor Using Bimorph Microactuators”, Int. Conference on MEMS, NANO and Smart Systems, Bannff, Alberta, Canada, July 24-27, 2005. [7] S. Scott and D. Peroulis, “A Capacitive MEMS Slot Element for Harsh Environment Temperature Sensing”, Submitted to IEEE Microwave Theory and Techniques Journal, April, 2009. [8] S. Scott and D. Peroulis, “A Capacitively-Loaded MEMS Slot Element for Wireless Temperature Sensing of up to 300◦ C”, IEEE International Microwave Symposium 2009, Boston, MA, June, 2009. 978