PPPP Hans-EliasP andPoster Session, Thursday, June 17Theme F686 - N1123Hydroflown: A MEMS Based Underwater Acoustic Particle Velocity Sensor123M. Berke Gür,Pde BreePUTuncay AkalUP P*PDepartment of Mechatronics Eng<strong>in</strong>eer<strong>in</strong>g, Bahçeehir University, stanbul 34353, TurkeyPMicroflown Technologies, Han University of Applied Sciences, Arhhem 6826, The Netherlands3PSUASIS Ltd., TUBITAK MRC Campus, Gebze-Kocaeli 41470, Turkey21Abstract-An acoustic field is fully described by two different but related variables: the scalar acoustic pressure and the vector valued acousticparticle velocity. Conventional hydrophones measure the acoustic pressure variable only. However, it is the particle velocity that carriesdirectional <strong>in</strong>formation and provides a more complete description of the acoustic field. Hydroflown is a novel MEMS based underwater acousticparticle velocity sensor under development, when comb<strong>in</strong>ed with a MEMS hydrophone is capable of completely measur<strong>in</strong>g the underwateracoustic field. Unlike conventional accelerometer based underwater acoustic particle velocity sensors, the sensor will not exhibit resonance andis expected to have a flat frequncy response from dc to 20 kHz.An underwater acoustic wave is a propagat<strong>in</strong>g energypacket which causes a disturbance <strong>in</strong> the ambient pressure and<strong>in</strong>duces a small volumetric motion (whose rate is termed theparticle velocity). Although the amplitudes of the acousticpressure and particle velocity are related, the latter is a vectorvalued and hence, carries directional <strong>in</strong>formation regard<strong>in</strong>gacoustic energy propagation. While the scalar valued acousticpressure is easily measured us<strong>in</strong>g a hydrophone, low costsensors capable of accurately measur<strong>in</strong>g the particle velocityhas rema<strong>in</strong>ed a major challenge. Several underwater sensorsdesigned for this purpose (all which are not commerciallyavailable) rely on accelerometers that are packaged such thatthe sensor is naturally buoyant <strong>in</strong> water [1,2,3].Recently, a novel MEMS based acoustic particle velocitysensor, called the Microflown, capable of measur<strong>in</strong>g theparticle velocity <strong>in</strong> air was developed [4]. This paper outl<strong>in</strong>esthe prelim<strong>in</strong>ary concepts and work done for extend<strong>in</strong>g theMicroflown sensor to underwater applications. The newsensor is termed appropriately the Hydroflown. TheMicroflown measures the particle velocity us<strong>in</strong>g two paralleloriented plat<strong>in</strong>um wire resistances. The wires are 200 nm th<strong>in</strong>and 5m wide (see Figure 1). When voltage is applied acrossthe wire term<strong>in</strong>als the wires heat up to 300°C. An acousticwave propagat<strong>in</strong>g perpendicular to the wires results <strong>in</strong> atemperature difference between the wires. The upstream wirewill cool down more compared to the downstream wire due toconvective heat transfer, which will result <strong>in</strong> a change <strong>in</strong> theresistance of the wires. The particle velocity is proportional tothe voltage change <strong>in</strong>duced by the change <strong>in</strong> the resistance.The sensor has a flat frequency response from dc up to 20kHz.The Hydroflown sensor is to be manufactured by firstdeposit<strong>in</strong>g a 300nm layer of Silicon Nitride (SiR3RNR4R) on aSilicon wafer followed by the deposition of a photoresist. ThisSilicon Nitride layer is used as a mask for the wet chemicaletch<strong>in</strong>g process <strong>in</strong> the follow<strong>in</strong>g steps. Next, a 200nmPlat<strong>in</strong>um layer is added us<strong>in</strong>g the sputter technique. Theresistive wires and the term<strong>in</strong>als are patterned from thisPlat<strong>in</strong>um layer us<strong>in</strong>g the lift-off technique. Afterphotolithography, the Silicon Nitride layer is removed us<strong>in</strong>greactive ion etch<strong>in</strong>g. F<strong>in</strong>ally, the Silicon wafer is etched withanisotropic wet chemical etch<strong>in</strong>g us<strong>in</strong>g Potassium Hydroxide(KOH) to create the channel and the bridge.Although the work<strong>in</strong>g pr<strong>in</strong>ciple of the Hydroflown sensor isTable 1. A comparison of the acoustic properties of air andseawater.Property Air SeawaterSpeed of Sound (m/s) 340 1500Density (kg/m 3 ) 1,2 1025Acoustic Impedence (Pa s/m) 415 1,54×10 6Specific Heat (kJ/kg/K) 1,0 4,0Thermal Conductivity (W/m/K) 0,025 0,596similar to the Microflown sensor, the former is designed towork underwater. S<strong>in</strong>ce water will start to boil above 100°C,the sensor is required to be encapsulated <strong>in</strong> an acousticallytransparent package filled with another fluid with a higherboil<strong>in</strong>g temperature. A comparison of the acoustic propertiesof air and seawater are presented <strong>in</strong> Table 1.In summary, Hydroflown, a novel underwater sensor formeasur<strong>in</strong>g the acoustic particle velocity is <strong>in</strong>troduced. Thework<strong>in</strong>g pr<strong>in</strong>ciples of the sensor are def<strong>in</strong>ed. The lab tests ofthe sensor are currently <strong>in</strong> progress and the first sea trials arescheduled for the summer of 2010. The Hydroflown sensor isexpected to provide higher quality measurements with fewersensors compared to conventional pressure measur<strong>in</strong>ghydrophone based systems. Initial applications of the sensorare planned for uniform l<strong>in</strong>e arrays. This work is supported bythe EUROSTARS Programme grant E!-4224 Hydroflown.*Correspond<strong>in</strong>g author: tuakal@suasis.comFigure 1. A scann<strong>in</strong>g electron microscope image of a bridgetype Microflown MEMS acoustic particle velocity sensor clearlyshow<strong>in</strong>g the Plat<strong>in</strong>um resistive wires and the term<strong>in</strong>als.[1] K. J. Bastyr et al., J. Acoust. Soc. Am. 106, 6 (1999).[2] W. D. Zhang et al., Sensors 9 (2009).[3] V. Shchurov, Vector Acoustics of the Ocean, engl. transl. (2006).[4] H.-E. de Bree, Acoust. Aust. 31 (2003).6th Nanoscience and Nanotechnology Conference, zmir, 2010 687
Poster Session, Thursday, June 17Theme F686 - N1123Implementation of DSMC Method to Nano Knudsen CompressorsNevsan engilEDA Ltd., Silikon Blok,No:22, ODTÜ Teknokent,06531, Ankara, TürkiyeAbstract- If density is low or characteristic length is micro/nano scale, it can be said that gas is rarefied. In rarefied gas conditions, gas startsflow<strong>in</strong>g slowly from cold to hot. This phenomenon is called thermal creep or transpiration. Us<strong>in</strong>g thermal creep phenomenon, Knudsencompressors are built. In this study various properties of a nano scale Knudsen compressors are analyzed with direct simulation Monte Carlo(DSMC) method.Lately, a number of Micro/Nano Electro MechanicalSystems (MEMS/NEMS) have been developed. Thesedevices sometimes <strong>in</strong>clude mechanical systems work withthe fluids such as micro/nano size gas compressors. Thesecompressors have much potential <strong>in</strong> the area ofchromatography, spectroscopy, micro plasmamanufactur<strong>in</strong>g and chemical sensors [1,2].If two gas reservoirs with different pressures andtemperatures are connected with a channel, gas startsflow<strong>in</strong>g from high-pressure side to low-pressure side.When the reservoir pressures get equal, gas flow stopseven if reservoir temperatures are different. In micro/nanoscale lengths, gas is rarefied even if pressure isatmospheric. If gas is rarefied and a temperature gradientexists, gas flows slowly from cold region to hot region. Itis called thermal creep or transpiration phenomenon [3].Us<strong>in</strong>g this phenomenon, it is possible to construct variousmicro/nano size Knudsen compressors.The theoretical efficiencies of Knudsen pumps are highcompared to conventional vacuum pumps. Besides theyare very reliable because they <strong>in</strong>clude no mov<strong>in</strong>g parts.Recent technological development <strong>in</strong> the area of thermalisolation on MEMS/NEMS, enable to use high temperaturegradients to obta<strong>in</strong> high volume rates [1].Gas flows related with the MEMS/NEMS devices havehigh Knudsen numbers (Kn) similar to rarefied gases ofhigh atmosphere flights. Rarefied gas flows with highKnudsen number ( Kn 0.1) depart from local thermalequilibrium because of the <strong>in</strong>adequate molecule collisions.Consequently, the l<strong>in</strong>ear relations between not only shearstress and velocity gradient but also heat conduction andtemperature gradient are lost. As a result cont<strong>in</strong>uum basedNavier-Stokes and Euler equations cannot be used becausethese equations use l<strong>in</strong>ear constitutive equations [4].In rarefied gas flows with high Knudsen number( Kn 0.1) , both cont<strong>in</strong>uum equations with high ordernon-l<strong>in</strong>ear constitutive equations, like Burnett equations,and molecular based methods can be used. Burnettequations are not used widely because these equations aredifficult to solve and have both stability and complicatedboundary condition problems. In rarefied gas flows,generally molecular methods are preferred. Molecularmethods are based on the Boltzmann equation, which is amathematical model and difficult to solve both analyticallyand numerically. Only its simplified versions can besolved. Molecular dynamic (MD) is the best-knownphysical molecular method [3]. MD is generally used toanalyze liquid and dense gas flows. Because of the hugenumber of the molecules, only very small flow volumescan be analyzed for very small time durations. Directsimulation Monte Carlo (DSMC) is another physicalmolecular model. In this method molecule movements andcollisions are decoupled and one DSMC moleculerepresents many physical molecules [5]. DSMC consists offour ma<strong>in</strong> steps. The first step is “molecule movement”step. In this step, molecules move <strong>in</strong>side the flow area. Thesecond step is “molecule <strong>in</strong>dex<strong>in</strong>g” step. Molecules are<strong>in</strong>dexed based on their cell <strong>in</strong>formation. The third step is“molecule collisions” step. Here molecules <strong>in</strong> the samecells undergo collisions with each other. The fourth step is“calculation of macroscopic properties” step. In this step,us<strong>in</strong>g microscopic molecule <strong>in</strong>formation, macroscopicvalues <strong>in</strong> each cell are calculated.In this study one stage and multi-stage Knudsencompressors are analyzed with DSMC method. Pump<strong>in</strong>gspeeds and maximum pressure ratios of Knudsencompressors will be reported together with boundaryconditions used.Figure 1. Reservoir pressure decreases with thermaltranspiration.sengiln@itu.edu.tr[1] S. McNamara and Y.B. Gianchandani, J., 2005. On-ChipVacuum Generated by Micro Mach<strong>in</strong>ed Knudsen Pump,Microelectromech. Syst. 14, 4:741-745.[2] E.P. Muntz and S.E. Vargo, 2002. Microscale VacuumPumps <strong>in</strong> The MEMS Handbook, M. Gad-el-Hak, Ed. BocaRaton, FL: CRC.[3] G.E. Karniadakis and A. Beskok, 2002. Micro FlowsFundementals and Simulation, Spr<strong>in</strong>ger-Verlag, New York.[4] S. Chapman and T.G. Cowl<strong>in</strong>g, 1970. The MathematicalTheory of Non-Uniform Gases, Cambridge University Press,New York.[5] G.A. Bird, 1994. Molecular Gas Dynamics and the DirectSimulation of Gas Flows, Clarendon Press, Oxford.6th Nanoscience and Nanotechnology Conference, zmir, 2010 688
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