optical diagnostics and modeling of different reacting and non-reacting systems saptarshi basu...
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![Page 1: Optical Diagnostics and Modeling of Different Reacting and Non-reacting Systems Saptarshi Basu Mechanical Engineering Department University of Connecticut](https://reader037.vdocuments.net/reader037/viewer/2022110322/56649d4b5503460f94a2967d/html5/thumbnails/1.jpg)
Optical Diagnostics and Modeling of Different Reacting and Non-reacting Systems
Saptarshi Basu
Mechanical Engineering Department
University of Connecticut
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Ph.D Research Projects
• Soot topography in diffusion flames
wrapped by line vortex
• Scalar mixing in vortex
• Innovative laser based non-intrusive diagnostics
in fuel cells
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Ph.D Research Projects
Hydrodynamics and heat transfer in
liquid films over rotating disk
Plasma synthesis of ceramics
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PublicationsFuel Cell Diagnostics [Experimental]
1. Basu, S., Xu, H., Renfro, M. W., and Cetegen, B. M. (2004). ASME Journal of Fuel Cell Science and Technology, Vol 3 February 2006
2. Basu, S., H. Gorgun, Renfro, M. W., and Cetegen, B. M. (2005). Journal of Power Sources, 159 (2006)
3. Basu, S., Renfro, M. W., and Cetegen, B. M. Journal of Power Sources, 162 (2006)
Patents
S.Basu, M.W Renfro, B.M Cetegen, Fiber Optic based in-situ diagnostics for PEM fuel cells. Patent pending
Vortex Dynamics [Modeling & Experimental] 4. Cetegen, B. M. and Basu, S. (2006). Combustion and Flame, 146(2006)
5. Basu, S., Barber, T and Cetegen, B. M. (2006), In Review Physics of fluids, July 2006
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Publications
Heat Transfer over Rotating Disk [Modeling]
6. Basu, S. and Cetegen, B. M. (2005). ASME Journal of Heat Transfer, Vol 128, March 2006
7. Basu, S. and Cetegen, B. M. (2005), In Press ASME Journal of Heat Transfer
Plasma Synthesis of Ceramics [Modeling & Experimental]8. Basu, S. and Cetegen, B. M. Accepted for publication in International
Journal of Heat and Mass Transfer, July 2006
9. Basu, S., E.H Jordan and Cetegen, B. M., Invited paper in Journal of Thermal Spray Technology, January 2007
10. Basu, S. and Cetegen, B. M., submitted to Acta Materialia, January 2007
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Modeling and Diagnostics of Solution Precursor Plasma Spray Process
Funding Agency ONR
Grant No. N00014-02-1-0171
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Thermal Barrier Coating
Padture et al, Science 2002• Gas Turbine Blades
• Temperature Reduction upto 300ºC
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Solution Precursor Plasma Spray Process
Precursor : Aq Soln. Zr + Yittria Salts => 7YSZ
Alumina + YSZ
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Important Parameters Affecting Coating Quality
• Initial Loading of Salts
• Droplet Size
• Plasma Temperature and Velocity Field
• Injection Velocity
• Type of Injection (Transverse or Co-axial)
• Precursor Property like 7YSZ or Alumina etc
• Standoff Distance
All affects droplet level transport
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Effect of Processing
50 m
5 m
50 m50 m
5 m5 m
Hardness: 365Density: 73 %
Hardness: 760Density: 82 %
Hardness: 1020Density: 95 % +
Droplet level transport needs to be understood
for process improvement
This improvement takes years of trial and error
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Modeling
Axial Injection
• Entire thermal history of the droplets
• Mass transport at the droplet level in the plasma
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Droplet Vaporization and Precipitation Routes
Fig.1: Solute containing droplet vaporization and precipitationroutes: (A) Uniform concentration of solute and volumeprecipitation leading to solid particles; (B) super-saturation nearthe surface followed by (1) fragmented shell formation (lowpermeability through the shell, (2) unfragmented shell formation(high permeability), (3) impermeable shell formation, internalheating, pressurization and subsequent shell break-up andsecondary atomization from the internal liquid; (C) elastic shellformation, inflation and deflation by solids consolidation
(A)
(B)
(C)
(I)
(II)
(III)
(A) Volume precipitation (B) (I) fragmented shell formation (low permeability through the shell, (II)
unfragmented shell formation (high permeability), (III) impermeable shell formation
(C) Elastic shell formation, inflation and deflation
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• Predict precipitation (surface or volume) of droplets• Model droplet level transport for better understanding of the
role of process parameters on droplet morphology • Predict shattering of shells after precipitation
SEM image of the deposition on a substrate after a single pass.
Cracked and dried Shell
Motivation
Xie et al 2003
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• High Relative Velocity
• Low Surface Tension
• Large Droplet Size
Timescale of microsecs
Timescale of millisecs
Timescale of microsecs
Three Stages of Droplet Modeling
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Aerodynamic Breakup
Aerodynamic breakup of 50 micron initial diameter 7YSZ droplets for a surface tension of 0.036 N/m
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Aerodynamic Breakup (II)
Not an issue for droplets of diameter less than 50 microns
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Heating and Vaporization (2D)
Models tried are
• 2D transient heat and species transport coupled with plasma
• Spherically symmetric heat and species transportEnergy (2D)
Tsin
sin
1
T1TrVPe5.0
T
dt
dr5.0rVPe5.0
Tr
2
22
sL
ssrL
2s
Species (2D)
sinsin
11
rVLePe5.0
dt
drLe5.0rVLePe5.0rLe
22
2
sLL
sLsrLL
2sL
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Heating and Vaporization (1D)
Energy (1D)
Species (1D)
r s2 T
0.5
drs
dtT
1
2
2 T
LeLr s2
0.5LeL
drs
dt
1
2
2
• Precipitation based on homonuclear hypothesis
• Precipitation triggered whenever solute concentration at surface reaches super saturation limit
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Heating and Vaporization (2D)
Computed droplet temperature (left) and solute mass fraction (right) for a 40 micron droplet injected into a DC arc plasma at 1 ms (top) and 3 ms (bottom)
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Precipitation (2D)
d = 5 m.
d = 10 m.
d = 20 m.
Xie et al Mater. Sci. Eng A 2003
What is shell porosity
What is the morphology/property of the shell
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Internal Pressurization
• The model of the interior of the particle is divided into three zones• Internal pressure buildup due to heating and lack of evaporation• Porosity of the shell
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Internal Pressurization
• 10 micron initial sized droplets
• Pressure rise decreases with porosity due to venting
• 40 micron initial sized droplets
• Pressure rise decreases with porosity due to venting
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Conclusions
• Droplets below 50 micron do not undergo aerodynamic breakup
• Precipitation occurs when surface concentration of solute reaches supersaturation
• Small droplets < 5 microns tend to volume precipitate
• Large droplets surface precipitate forming thin shells
• Low porosity shells fracture on further heating in the plasma
• High porosity shells do not fracture and arrive at the substrate as unpyrolized material with watery core
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Limitations
• No precipitation kinetics is modeled
• Literature show precipitation is not homonuclear
• No experimental data is available for precipitation at high heating rates
• Behavior of droplets in an array or vicinity of other droplets is not modeled
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Future Research Direction
• Physical evolution of particulate formation in droplets at rapid heating rates 105 to 107 K/s. [FUNDING NSF : CBET/ONR : Collaboration AMPAC/UCONN]
• The morphology, microstructure and chemical composition of droplets evolution as a function of time [FUNDING NSF : CBET /ONR: Collaboration AMPAC/UCONN]
• Advanced modeling with improved precipitation mechanism [FUNDING NSF : CBET /ONR : Collaboration UCONN]
• Provide general guidelines for processing routes for different types of precursors for different microstructure for advanced applications • In situ monitoring of splat dynamics and transient composition variation [FUNDING NSF : CBET /ONR]
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Future Research Direction Laser heating of droplets
Advantages• Similar heating rates as in the plasma • Similar timescales for precipitate formation• Diagnostics are easier to carry out
Similar profiles
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Future Research Direction
• High speed imaging of precipitation
• Different kinds of precursors investigated
• Ex situ analysis of morphology of collected sample using SEM, FTIR and Raman
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Future Research Direction
High Temperature resistant Fiber Optic
• In situ analysis of splat by infrared fiber optic evanascent spectrsocopy
• Transient composition variation can be monitored
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In-situ Simultaneous Measurements of Temperature and Partial Pressure in a PEM Fuel Cell under Steady and Dynamic cycles
Funding Agency
U. S. Army Research RDECOM
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Presentation Outline Development and calibration of diode laser based absorption measurement technique for
water vapor concentration measurement
Application of the measurement technique to an operating fuel cell
Theoretical method to extract temperature and partial pressure simultaneously using a single laser scan
Experimental Results of partial pressure and temperature in a PEM fuel cell under steady conditions
Experimental Results of partial pressure and temperature in a PEM fuel cell under dynamic conditions
Extensions and improvements of the measurement technique to spatially resolved measurements
Concluding Remarks
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Introduction to PEM fuel cells
At the anode the hydrogen gas ionizes releasing electrons and protons (H+).
2H2 4H+ + 4e-
This reaction releases energy. At the cathode, the oxygen reacts with electrons taken from the electrode, and H+ from the electrolyte, to form water.
O2 + 4e- + 4H+ 2H2O
Bipolar plate contains the gas channels for circulating the air and hydrogen
Courtesy : Dr. J. Fenton
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Water management in PEM fuel cells
Water diffusion from cathode to anode
Water supplied by externally humidification
Water removed by circulating hydrogen
Water produced within the cathode
Water transport due to electro-osmotic drag by protons
The depleted air leaving the fuel cell remove water
Water supplied by externally humidifying the air/O2 supply
Main Challenges
• Flooding/drying up of membrane
• Real time humidity level control in inflow gas streams
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• Proton flux through the membrane directly proportional to the current density in a MEA.
• Careful balancing of the supply and removal of water vapor to prevent FLOODING/ DRYING and BETTER PERFORMANCE and DURABILITY
Protonic conductivity of several membrane materials as a function
of relative humidity at T=100 ºC studied by Alberti et al
Water management in PEM fuel cells
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Water vapor measurements in fuel cells
Current state-of-the-art limited only to inlet and outlet measurements or expensive instrumentation
Fourier transform IR (FTIR) spectrometer Gas chromatograph Neutron Scattering
Most measurements performed at the INLET and OUTLET of the cell
Intrusive techniques require extraction of the sample from the fuel cell and sending it to the external measurement device
Both techniques provide slow, temporally and spatially averaged measurements
There is a GREAT NEED to measure water vapor concentration non-intrusively with good spatial and temporal resolution
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Water Management & Transport (DOE)
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Water Management & Transport (DOE)
Water Transport
Impurity sensor like CO sensor
Novel concepts
Cold start
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Tunable Diode Laser Absorption Spectroscopy (TDLAS)
Non-intrusive, in-situ first of its kind of measurements
Line of sight absorption in individual flow channels
Measurement time: ~seconds
Off-the-shelf telecommunications cheap lasers (~$500)
Total system cost ~$5000
Straightforward extension to other species such as CO, CO2
Ability to measure multiple channels or species simultaneously via multiplexing
Ability to measure temperature across each channel using a single laser scan
Potential use in feedback control systems
Potential use in high temperature fuel cells like SOFC
Potential use in Direct Methanol Fuel Cells
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Beer-Lambert law
b
0s
,0
i dlpexpI
I
i
s I
I
bp 0ln
1
Absorption of light by a sample
= Transmitted light intensity
= Incident light intensity
= Partial pressure of water vapor
= Absorption coefficient
iI
0I
sp
The measured partial pressure represents a path-averaged valueWavelength (nm)
1306 1308 1310 1312 1314
Lin
e In
tens
ity
(cm
/mol
)
0
10-23
2x10-23
3x10-23
4x10-23
5x10-23
6x10-23
T=300 T=400
1100 1200 1300 1400 1500 1600 1700
Lin
e In
tens
ity
(cm
/mol
)
10-23
10-22
10-21
10-20
10-19
T=300 T=400
Proper Selection of Wavelength is crucial
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Simulated signal Voigt profile simulation with HITRAN database parameters
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Test cell for system calibration Simple humidity and temperature controlled absorption cell constructed
for system calibration and validation
Signal Photodiode
DAQ
Diode Laser
AIR
Signal photodiode
Auxiliary heater
Exhaust valve
Heater controller
Windows
Absorption cellTC4
TC3
TC2
TC1
Reference Photodiode
Fiber coupler
Diode Laser
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Optically accessible bipolar plate
Same plate design for
anode and cathode
Optically accessible plates
Effective flow path is 7 cm
BIPOLAR PLATE
Measurement averaged
along channel length
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Laser system Laser temperature tuned over ~5 nm to couple with different
H2O transitions Laser current tuning affects both power and wavelength (0.4
nm) Laser power monitored by photodiode All measurements on cathode side of the fuel cell
Beamsplitter
Reference Photodiode
To experiment/Test cell
LaserCurrent Controller
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Laser current modulated by 100 Hz ramp function Single scan range of 0.4 nm Laser wavelength calibrated with a ring interferometer system Multiple scans averaged
Measurement Methodology
Test Cell
Signal Photodiode
Reference Photodiode
Current Ramp
Output Ln (sig/ Ref)
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Signal processing (1) Measurements of reference and signal photodiode are imposed on current
ramp
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Signal processing (2) Four Lorentzian profiles and a polynomial background fit to measured signal Sum of four Lorentzian represents Log(Signal/Reference)
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Partial pressure extraction• Widths of two strong transitions are assumed equal based on
HITRAN Simulation
• Intensities of two strong transitions are assumed constant multiples of one another for all Ps and T.
• Six curve fit parameters: 2 widths, 3 intensities, background
• Empirically, self-broadening and air broadening are related by:
• Partial pressure directly related to measured transition width
airwwaterw hh ,, 2.5
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Partial pressure determination Calibration experiments performed in fuel cell geometry with
controlled temperature and relative humidity
10 % Error
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Operating Fuel Cell Setup
Laser
Data Acquisition and Laser controller
Electric Load Box
Temperature Controller
Current Controller
Fuel CellControl
H2
Air
TC1
TC2 TC3Humidifiers
PD1
PD2
Scribner Fuel Cell Test Station
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Experimental conditions
• Absorption data collected twice for each current setting & averaged
• For each data set curve fit was done
• Partial Pressure predicted from measured half width using calibration line
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Measurements in active fuel cell (Cathode side)
Measured water partial pressure in operating fuel cell at inlet water partial pressures of (a) Ps = 0.19 atm and (b) Ps = 0.26 atm for a cell temperature of 80
ºC Experimental data collected show a similar increase in partial pressure with current density Diagnostic technique works for high current densities if the inlet relative humidity is less than 80 %.
Temperature insensitive measurement
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Theoretical study for the determination of temperature and partial pressure simultaneously
• Present laser source stimulated transitions insensitive to temperature
• For 20oC rise in temperature a temperature sensitivity of atleast 20 % is needed.
• 23 % variation in intensity detected for transition in the range of 1470 nm
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Calibration with new Laser for simultaneous temperatureand partial pressure detection
Partial Pressure and Temperature Calibration
• Partial Pressure calibration same as before• Temperature is calibrated from peak intensity
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Measurement Under Steady State Conditions
• Temperature and partial pressure detected from single laser scan• For a steady state cell with controlled temperature the measured temperature is about 55 ºC
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Measurement under dynamic fuel cell operation
• Partial pressure rise upto 0.3 atm from the inlet value of 0.19 atm entire dynamic cycle of 300 secs • Temperature rise is recorded for each cycle above the steady state value of 80 ºC. Temperature as high as 90 ºC is observed.
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Spatially Resolved Measurements (Steady State)
• Measurements across two channels simultaneously using a single laser scan• Difference in partial pressure between two channels increases with current load
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Spatially Resolved Measurements (Steady State)
• Difference in partial pressure between two channels increases with current load
• Temperature across both channels are similar
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Spatially Resolved Measurements (Dynamic)
• Measurements across two channels simultaneously using a single laser scan
• Load is varied sinusoidally
• Partial pressure closely follows the load profile without phase lag
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Concluding Remarks
In situ water vapor concentration measurements demonstrated using
tunable diode laser absorption spectroscopy in PEMFC
Calibration measurements permit partial pressure determination within
10% accuracy and +/- 2 ºC for temperature
Measurements in operating fuel cell show strong signals with low noise
Simultaneous detection of temperature and H2O partial pressure
Measurements in the fuel cell under dynamic and steady state conditions
Spatially resolved measurements permit simultaneous determination of
temperature and pressure across two channels
FM spectroscopy will allow higher degree of accuracy in H2O
measurements as well as allowing to measure other species such as CO,
CO2
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Acknowledgments
This work was sponsored by a grant from U. S. Army Research RDECOM, CERDEC (Fort Belvoir, VA) through Connecticut Global Fuel Cell Center (CGFCC)
I acknowledge the contributions of the following people:
Profs. B.M Cetegen (Advisor), M.W Renfro (Co-advisor), E.H Jordan (Co-advisor)
Prof. J. Fenton, Drs. M. Williams and V. Ramani for allowing us to use their fuel cell set-up
Mr. T. Mealy for technical help in machining Dr. Haluk Gorgan and Prof. F. Barbir for allowing us to use their
fuel cell set-up
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Limitations of Current Technique and Future Plans
• The spatial resolution was limited to average value along channel length. Pointwise measurements needed
• The temporal resolution of the technique inadequate for high frequency load cycle
• Cyclic loading can lead to unforeseen effects in species transport and temperature distribution.
• Timescale of load variation and species kinetics mismatch. Result malfunctioning like water logging or drying up of the cell
• The modes of failure for a cyclic load compared to steady state operation Durability will be different for same load.
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Future Research Directions (I)• Pointwise resolvable measurements across each channel
• Extension of the measurement technique to include species like CO
• Extension of the methodology to direct methanol fuel cell (DMFC)
• Improved temporal resolution of the technique to quantify the response characteristics of the gas phase subjected to high frequency load cycle
• Potential extension to include high temperature fuel cell like SOFC
• Developing novel diagnostics techniques for two-phase flow characteristics, thermal transport within the gas channels and the MEA
• Novel imaging techniques and optical sensors for fuel cell testing and real time feedback control strategy
• Extension to fuel cell stacks
• Measurements in cold weather start up
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Future Research Directions (II)
• In-situ infrared fiber evanescent wave spectroscopy using tunable laser for pointwise measurements of concentration both in the vapor and liquid phases FUNDING [CBET/DOE[EERE]/ US ARMY/ FSEC]
• High speed imaging for monitoring growth and dynamics of liquid water from the MEA at high power FUNDING [CBET/ DOE[EERE]/ PRIVATE SECTOR/COLLABORATION FSEC]
• PIV measurements to observe velocity and clogging in the channels FUNDING [CBET/ DOE[EERE]/ PRIVATE SECTOR/ COLLABORATION FSEC]
• FM Spectroscopy to increase temporal resolution of the measurements FUNDING [CBET/ DOE[EERE]/ US ARMY/ FSEC]
• 3D modeling to understand the response especially the short time transients [COLLABORATION UCONN]
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CCD
Camera
Laser Sheet
Embedded, Unclad, Flattened Optical Fiber for Evanascent Spectroscopy
Strobe Light
Water Droplets
Water Film
Water Vapor ZoneTransparent optically accessible Plate with Anti-Fog coating
Current Collector
COMPLETE UNDERSTANDING OF WATER TRANSPORT
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Frequency Modulation (FM) Spectroscopy
Laser Temperature Controller
Current Controller
Data Acquisition
Lock-in amplifier
Fuel cell
Fiber coupler
Sine wave generator
Ramp generator
Mixer
Signal Photodiode
Schematics of a single laser FM spectroscopy
• To measure weak transitions in other wavelength regions which are very sensitive to temperature
• Reduce the error band arising principally due to large background.
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Preliminary FM Spectra
Simulated Experimental
Initial data(2f) taken under ambient conditions at a temperature of 25oC at a partial pressure of 0.013 atm.
The profile looks very clean with negligible background.
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Outcomes• Complete understanding of the transport of water vapor and other species under steady and dynamic conditions
• Chemical kinetics of the of the fuel cell under high frequency load cycle as in automobile
• Inception of two phase flow
• Growth and transport of liquid water
• Simultaneous measurement of temperature
• Extension to SOFC and DMFC
• Validation of the computational models
• Partial understanding of the durability issue of the fuel cell arising through water transport
• Extension to similar measurements inside the MEA
• Measurements in fuel cell stacks
• Measurements during cold weather start up
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Combined Funding Options
• NSF [CBET: Transport and Thermal Fluids Phenomena, Energy for Sustainability]
• DOE [Office of Energy Efficiency and Renewable Energy (EERE) ]
• ONR
• U.S. Army Research, Development and Engineering Command
• Collaboration with Private Company
• Collaboration with FSEC, UCONN, CGFCC
• Startup Funding