DESULFURIZATION OF LOGISTIC FUELS FOR FUEL CELL APUs

Similar documents
TARDEC Technology Integration

UNCLASSIFIED: Dist A. Approved for public release. GVPM Non-primary Power Systems Overview Kevin Centeck and Darin Kowalski 10 Aug 2011

UNCLASSIFIED: Dist A. Approved for public release. GVPM Track & Suspension Overview Mr. Jason Alef & Mr. Geoff Bossio 11 Aug 2011

Alternative Fuels: FT SPK and HRJ for Military Use

TARDEC Robotics. Dr. Greg Hudas UNCLASSIFIED: Dist A. Approved for public release

UNCLASSIFIED: Dist A. Approved for public release. GVPM Energy Storage Overview Mr. David Skalny & Dr. Laurence Toomey 10 August 2011

Robot Drive Motor Characterization Test Plan

Energy Storage Requirements & Challenges For Ground Vehicles

Evaluation of SpectroVisc Q3000 for Viscosity Determination

Energy Storage Commonality Military vs. Commercial Trucks

U.S. Army/CERDEC's Portable Fuel Cell Evaluation and Field Testing 2011 Fuel Cell Seminar & Expo Orlando, FL 31 Oct 2011

Vehicle Systems Engineering and Integration Activities - Phase 3

TARDEC OVERVIEW. Tank Automotive Research, Development and Engineering Center. APTAC Spring Conference Detroit 27 March, 2007

US ARMY POWER OVERVIEW

GM-TARDEC Autonomous Safety Collaboration Meeting

Tank Automotive Research, Development and Engineering Command (TARDEC) Overview

Feeding the Fleet. GreenGov Washington D.C. October 31, 2011

An Advanced Fuel Filter

Up-Coming Diesel Fuel and Exhaust Emissions Regulations For Mobile Sources. Parminder Khabra RDECOM-TARDEC TACOM LCMC March 22, 2006 JSEM

Automatic Air Collision Avoidance System. Auto-ACAS. Mark A. Skoog Dryden Flight Research Center - NASA. AutoACAS. Dryden Flight Research Center

AFRL-RX-TY-TM

U.S. Army s Ground Vehicle Energy Storage R&D Programs & Goals

Servicing Hawker Vehicle Batteries with Standard Battery Charging and Test Equipment

Navy Coalescence Test on Camelina HRJ5 Fuel

Additives to Increase Fuel Heat Sink Capacity

UNCLASSIFIED: Distribution A. Approved for Public Release TACOM Case # 21906, 26 May Vehicle Electronics and Architecture

Vehicle Systems Engineering and Integration Activities - Phase 4

High efficiency variable speed versatile power air conditioning system for military vehicles

TARDEC --- TECHNICAL REPORT ---

TARDEC Hybrid Electric Program Last Decade

Navy Coalescence Test on Petroleum F-76 Fuel with Infineum R655 Lubricity Improver at 300 ppm

EXPLORATORY DISCUSSIONS - PRE DECISIONAL

Evaluation of Single Common Powertrain Lubricant (SCPL) Candidates for Fuel Consumption Benefits in Military Equipment

UNCLASSIFIED: DIST A. APPROVED FOR PUBLIC RELEASE. ARMY GREATEST INVENTIONS CY 2009 PROGRAM MRAP Overhead Wire Mitigation (OWM) Kit

FINAL REPORT FOR THE C-130 RAMP TEST #3 OF A HYDREMA MINE CLEARING VEHICLE

REMOTE MINE AREA CLEARANCE EQUIPMENT (MACE) C-130 LOAD CELL TEST DATA

REPORT DOCUMENTATION PAGE

Joint Light Tactical Vehicle Power Requirements

Cadmium Repair Alternatives on High-Strength Steel January 25, 2006 Hilton San Diego Resort 1775 East Mission Bay Drive San Diego, CA 92109

2011 NDIA GROUND VEHICLE SYSTEMS ENGINEERING AND TECHNOLOGY SYMPOSIUM POWER AND MOBILITY (P&M) MINI-SYMPOSIUM AUGUST 9-11 DEARBORN, MICHIGAN

Hydro-Piezoelectricity: A Renewable Energy Source For Autonomous Underwater Vehicles

INTELLIGENT ENERGY MANAGEMENT IN A TWO POWER-BUS VEHICLE SYSTEM. DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.

Open & Evolutive UAV Architecture

DSCC Annual Tire Conference CATL UPDATE. March 24, 2011 UNCLASSIFIED: Dist A. Approved for public release

SIO Shipyard Representative Bi-Weekly Progress Report

EVALUATING VOLTAGE REGULATION COMPLIANCE OF MIL-PRF-GCS600A(ARMY) FOR VEHICLE ON-BOARD GENERATORS AND ASSESSING OVERALL VEHICLE BUS COMPLIANCE

Presented by Mr. Greg Kilchenstein OSD, Maintenance. 29August 2012

Predator B: The Multi-Role UAV

Evaluation of Digital Refractometers for Field Determination of FSII Concentration in JP-5 Fuel

FTTS Utility Vehicle UV2 Concept Review FTTS UV2 Support Variant

Helicopter Dynamic Components Project. Presented at: HCAT Meeting January 2006

Application of Airbag Technology for Vehicle Protection

Dual Use Ground Vehicle Condition-Based Maintenance Project B

Transparent Armor Cost Benefit Study

HIGH REPETITION RATE CHARGING A MARX TYPE GENERATOR *

Monolithically Integrated Micro Flapping Vehicles

LESSONS LEARNED WHILE MEASURING FUEL SYSTEM DIFFERENTIAL PRESSURE MARK HEATON AIR FORCE FLIGHT TEST CENTER EDWARDS AFB, CA 10 MAY 2011

TRANSIENT MAGNETIC FLUX DENSITY MEASUREMENT RESULTS ON A FUSELAGE-LIKE TEST SETUP AND INVESTIGATION OF THE EFFECTS OF APERTURES

Portable Fluid Analyzer

Transparent Armor Cost Benefit Study

US Army Non - Human Factor Helicopter Mishap Findings and Recommendations. Major Robert Kent, USAF, MC, SFS

Does V50 Depend on Armor Mass?

Predator Program Office

Fuel Efficient ground vehicle Demonstrator (FED) Vision

INLINE MONITORING OF FREE WATER AND PARTICULATE CONTAMINATION OF JET A FUEL

Robust Fault Diagnosis in Electric Drives Using Machine Learning

Development of Man Portable Auxiliary Power Unit using Advanced Large Format Lithium-Ion Cells

Power Technology Branch Army Power Division US Army RDECOM CERDEC C2D Fort Belvoir, Virginia

Joint Oil Analysis Program Spectrometer Standards VHG Labs Inc. Qualification Report For D19-0, D3-100 and D12-XXX Series Standards

DISTILLATE FUEL PROCESSING FOR MARINE FUEL CELL APPLICATIONS. G. Steinfeld, R. Sanderson, H. Ghezel-Ayagh, S. Abens

Impact of 200 ppm HiTEC 4898C Lubricity Improver Additive (LIA) on F-76 Fuel Coalescence

Multilevel Vehicle Design: Fuel Economy, Mobility and Safety Considerations, Part B

BALANCE OF PERFORMANCE PARAMETERS FOR SURVIVABILITY AND MOBILITY IN THE DEMONSTRATOR FOR NOVEL DESIGN (DFND) VEHICLE CONCEPTS

F100 ENGINE NACELLE FIRE FIGHTING TEST MOCKUP DRAWINGS

Membrane Wing Aerodynamics for µav Applications

U.S. Army s Ground Vehicle Energy Storage R&D Programs & Goals

Joint Oil Analysis Program Spectrometer Standards SCP Science (Conostan) Qualification Report For D19-0, D3-100, and D12-XXX Series Standards

Quarterly Progress Report

Additional Transit Bus Life Cycle Cost Scenarios Based on Current and Future Fuel Prices

Center for Ground Vehicle Development and Integration

PERFORMANCE OF A DIESEL, JP-8 REFORMER. Subir Roychoudhury*, Dennis Walsh Precision Combustion Inc., 410 Sackett Point Road, North Haven, CT 06473;

REPORT DOCUMENTATION PAGE

DEVELOPMENT OF COMPACT VARIABLE- VOLTAGE, BI-DIRECTIONAL 100KW DC-DC CONVERTER

GVSET Power & Energy Preview Mr. Chuck Coutteau Associate Director (Acting) Ground Vehicle Power & Mobility 19 August 2009

Power Distribution System for a Small Unmanned Rotorcraft

Hybrid Components: Motors and Power Electronics

Research Development and Engineering Command TARDEC/NAC

NDCEE National Defense Center for Energy and Environment

REPORT DOCUMENTATION PAGE

ONR Manhattan Project Montana Tech Butte, MT March 18, 2011 Kevin Centeck. Unclassified

IMPACT OF FRICTION REDUCTION TECHNOLOGIES ON FUEL ECONOMY FOR GROUND VEHICLES G. R. Fenske, R. A. Erck, O. O. Ajayi, A. Masoner, and A. S.

Tank-Automotive Research, Development, and Engineering Center

US Army CERDEC: Fuel Cell Testing Update

Program Overview. Chris Mocnik Robotic Vehicle Control Architecture for FCS ATO Manager U.S. Army RDECOM TARDEC

ITC-Germany Visit. Chuck Coutteau, Associate Director Ground Vehicle Power and Mobility Overview 10 November 2011

REPORT DOCUMENTATION PAGE

A GENERAL PURPOSE VEHICLE POWERTRAIN MODELING AND SIMULATION SOFTWARE - VPSET

NoFoam Unit Installation, Evaluation and Operations Manual

EXPERIMENTAL VALIDATION AND COMBUSTION MODELING OF A JP-8 SURROGATE IN A SINGLE CYLINDER DIESEL ENGINE

Developing a Methodology for the Evaluation of Hybrid Vehicle Thermal Management Systems

Transcription:

DESULFURIZATION OF LOGISTIC FUELS FOR FUEL CELL APUs Gökhan Alptekin*, Ambalavanan Jayaraman, Margarita Dubovik, Matthew Schaefer, John Monroe, and Kristin Bradley TDA Research, Inc Wheat Ridge, CO, 33 ABSTRACT The sulfur level in logistic fuels is very high; up to 3, ppmw S for jet fuels (JP-, JP-5) and 1, ppmw S for naval distillate (NATO F-7) compared to the commercial gasoline (3 ppmw S) and diesel (15 ppmw S). The effective utilization of logistic fuels in fuel cell applications requires removal of refractory sulfur species (organosulfur compounds) to below.1 ppm. Sulfur removal is critical for fuel cells and adsorption is a promising technology for reducing the sulfur content to such low levels. TDA has developed a sorbent-based fuel desulfurization system that can easily be integrated with any fuel cell fuel processor. TDA's desulfurizer removes all of the refractory organic sulfur compounds in a regenerable manner from the military fuels (both JP-5 and JP-) while it is still in the liquid phase, and reduces the total fuel sulfur content to subppm levels (e.g., less than.1 ppmw). TDA has built a - bed prototype jet fuel desulfurization system that could be integrated with a 1.5 kw fuel cell powered APU. Demonstration of the desulfurizer is being carried out with two types of jet fuels i.e., JP-5 (from ONR Fuel Cell Research Program, NAVAIR) and JP- (from Wright- Patterson Air Force Base in Ohio) fuels. We will be presenting test data from demonstration of the prototype desulfurization system in the conference. 1. INTRODUCTION The effective utilization of logistic fuels in fuel cell applications requires removal of refractory sulfur species (organosulfur compounds) to below.1 ppm. Low temperature fuel cells (e.g. PEM) require clean (essentially pure) hydrogen feed to prevent the poisoning of the anode catalyst. Even the more robust high temperature fuel cells (e.g., solid oxide fuel cells) are poisoned with low levels of sulfur contaminants. Sulfur removal is critical for fuel cells and adsorption is a promising technology for accomplishing such low levels of sulfur. TDA has developed a sorbent-based fuel desulfurization system that can easily integrate with any fuel cell fuel processor. TDA's desulfurizer removes all of the refractory organic sulfur compounds from military fuels (both JP-5 and JP-) while they are still in the liquid phase and reduces the total fuel sulfur content to sub-ppm levels (e.g., less than.1 ppmw). In order to increase the utilization of the sorbent and minimize the logistics burden and manpower associated with frequent replacements, the desulfurization system operates in a regenerable manner.. JET FUEL DESULFURIZATION We observed that at higher adsorption temperatures the interaction between the sorbent and the sulfur species are stronger than the interaction between the sorbent and the unsaturated hydrocarbons. This resulted in removal of some of the hydrocarbons from the surface at higher temperature and increased the number of sorbent sites available for sulfur removal. Figure 1 shows the impact of temperature on the sulfur removal performance of the sorbent. At 9 o C, the sulfur uptake of the sorbent improved significantly. However, a further increase in temperature to o C did not improve the sulfur capacity any further. It is anticipated that at higher temperatures the affinity of the sulfur species to the sorbent is also reduced. Sulfur Concn., ppmw 1 1 1 T = 5C T = 9C T = C 1 3 5 Figure 1. The impact of adsorption temperature on SulfaTrap TM -D1 performance. 51 ppmw sulfur containing JP- fuel spiked with 7 ppmw of benzothiophene and 7 ppmw of -methyl benzothiophene. LHSV = 1. h -1. We tested our SulfaTrap TM -D1 sorbent with different JP-5 fuels containing varying levels of sulfur species in them (11, 5 and 5 ppmw S). Figure 1

Report Documentation Page Form Approved OMB No. 7-1 Public reporting burden for the collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington Headquarters Services, Directorate for Information Operations and Reports, 15 Jefferson Davis Highway, Suite, Arlington VA -3. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to a penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. 1. REPORT DATE DEC. REPORT TYPE N/A 3. DATES COVERED -. TITLE AND SUBTITLE Desulfurization Of Logistic Fuels For Fuel Cell Apus 5a. CONTRACT NUMBER 5b. GRANT NUMBER 5c. PROGRAM ELEMENT NUMBER. AUTHOR(S) 5d. PROJECT NUMBER 5e. TASK NUMBER 5f. WORK UNIT NUMBER 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) TDA Research, Inc Wheat Ridge, CO, 33. PERFORMING ORGANIZATION REPORT NUMBER 9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES) 1. SPONSOR/MONITOR S ACRONYM(S). DISTRIBUTION/AVAILABILITY STATEMENT Approved for public release, distribution unlimited 11. SPONSOR/MONITOR S REPORT NUMBER(S) 13. SUPPLEMENTARY NOTES See also ADM17. Proceedings of the Army Science Conference (th) Held in Orlando, Florida on 1- December 1. ABSTRACT 15. SUBJECT TERMS 1. SECURITY CLASSIFICATION OF: 17. LIMITATION OF ABSTRACT UU a. REPORT b. ABSTRACT c. THIS PAGE 1. NUMBER OF PAGES 19a. NAME OF RESPONSIBLE PERSON Standard Form 9 (Rev. -9) Prescribed by ANSI Std Z39-1

shows the impact of fuel sulfur level on the sulfur removal performance of the sorbent. The sorbent achieved very high sulfur adsorption capacities and could remove sulfur from JP-5 fuels of varying concentrations and reduce it to sub ppm levels. The sorbent could desulfurize ~ 15 ml/g of low sulfur JP-5. Hence, SulfaTrap TM -D1 could be used as an expendable polishing sorbent downstream of a bulk desulfurizer. A comparison of the sorbent performance in the two types of jet fuels JP- and JP-5 is shown in Figure 3. The sorbent showed better performance in JP-5 than JP-. JP- 5 typically has slightly lower aromatic content than JP-, though the US military specification is the same < 5% for both. JP- could also have slightly more polyaromatic hydrocarbons (PAHs) than JP-5. The presence of additives, moisture, PAHs and organo-nitrogen compounds in jet fuels can all affect the desulfurization of liquid fuels by adsorption. 3. DIESEL DESULFURIZATION We also carried out desulfurization of ultra low sulfur diesel (ULSD) containing 1.5 ppmw S with TDA-SulfaTrap TM -D1. The results are provided in Figure. The sorbent could desulfurize 1 L of ULSD per kg of sorbent with 9+% removal efficiency. The sorbent performance improved significantly with increases in adsorption temperature and pressure. As shown in Figure 5, the sorbent was able to achieve 9+% removal efficiency while desulfurizing 3 L of ULSD per kg of sorbent (which corresponds to 15 ml/ml sorbent) and +% removal efficiency for 75 L of ULSD per kg sorbent (which corresponds to ml/ml of sorbent). Hence, the sorbent could be used as an expendable sorbent for diesel fuel (ULSD) powered fuel cell APUs with the sorbent replacement being carried out during routine servicing of the heavy-duty vehicle. 5 Sulfur Concentration, ppmw 3 1 Low S JP5 (5 ppmw S) JP5 (5 ppmw S) JP5/Cu (11 ppmw S) 5 1 15 Figure. The impact of fuel sulfur level on SulfaTrap TM - D1 performance. JP-5 fuel. T = o C. LHSV = 1. h -1. Sulfur Concentration, ppmw 1 1 ULSD breakthrough on TDA SulfaTrap - Liquid Phase Sorbent TDA- SulfaTrap Selexsorb 3 9 Figure. Diesel fuel breakthrough on TDA-SulfaTrap TM - D1 sorbent. T = o C. LHSV = 1. h -1. total sulfur (ppmw) 1 1 JP JP5 TDA- SulfaTrap TM - D1 (3-7 Mesh) JP Vs JP5 at o C JP- JP-5 1 ml fuel desulfurized/g of sorbent ppmw sulfur 1 1 ULSD - 1.1 ppmw S (inlet) on SulfaTrap TM -D1(P = 5 psig) cumulative average sulfur in effluent Fuel Adsorption Temp. 1 3 35 3 5 15 1 5 Temperature, o C ml Fuel Desulfurized/mL of Sorbent Figure 3. Comparison of sorbent performance in JP- and JP-5. Figure 5. Diesel fuel breakthrough on TDA-SulfaTrap TM - D1 sorbent at higher temperatures. P = 5 psig. LHSV =. 1.9 h -1.

. MULTIPLE CYCLE TESTS A regenerable system could benefit from high temperature adsorption since it reduces the time required for heating and cooling transitions. Further, TDA SulfaTrap TM -D1 sorbent showed better desulfurization performance at higher temperatures. Hence, we carried out the multiple cycle tests at an adsorption temperature of o C. Figure shows the impact of various regeneration gases on desulfurization of jet fuel (JP-5). We observed that the sorbent could be regenerated either in air and/or a reducing gas at -5 o C. We also carried out a multiple cycle test (9 cycles) of SulfaTrap TM -D1 sorbent with air regeneration. The use of air regeneration allowed us to cool the system rapidly and minimized the cooling time. Figure 7 shows the summary of the results from the 9-cycle test. The sorbent showed a stable breakthrough capacity of.9-1.1 ml/g over 9 cycles in a 5 ppmw S JP-5 fuel. We optimized the regeneration time and temperature during these experiments and found that a regeneration time of - hrs at o C was sufficient to remove the adsorbed sulfur compounds. Sulfur concn. (ppmw S) 1 1 1 1 TDA SulfaTrap (1/1" pellets) Optimization of Regen Gas @ -5 o C Cycling Data - JP-5 with 5 ppmw S Regenerations in %H /He Cycle # -1 Regenerations in air Cycle # 7-7 Regenerations in air & %H /He Cycle # 15-.5 1 1.5.5 3 ml Fuel Desulfurized/g of Sorbent Figure. The impact of regeneration gas on desulfurization of jet fuel by SulfaTrap TM -D1. T = o C. LHSV =. h -1. Sulfur concn. (ppmw S) 5 15 1 5 TDA SulfaTrap TM -D1 (1/1" pellets) Cycling Data with air regeneration @ o C Cycle #1 - Cycle #9 #17 #1 #3 # #15 #5, 9 #, 51, 53 #5 #19.5 1 1.5 ml Fuel Desulfurized/g of Sorbent Figure 7. Multiple cycle test results with JP-5 (5 ppmw S) on TDA-SulfaTrap TM -D1 sorbent. T = o C. LHSV =. h -1. 3

Figure. TDA s -bed prototype jet fuel desulfurization system. 5. TDA s PROTOTYPE LOGISTIC FUEL DESULFURIZATION SYSTEM TDA has built a -bed prototype jet fuel desulfurization system that could be integrated with a 1.5 kw fuel cell powered APU. Figure shows the picture of TDA s -bed prototype desulfurization system. The system was designed for easy access and modification and is therefore far larger than a commercial unit; note that the unit is virtually all empty space. The desulfurizer system is sized to treat up to 1 ml/min fuel flow rate with sulfur contamination levels up to 3, ppmw. The sorbent beds are 1.5L in volume each. The system is equipped with various pumps, valves and heaters and is operated using LabView control software. Demonstration of the desulfurizer is being carried out with two types of jet fuels i.e., JP-5 (from ONR Fuel Cell Research Program, NAVAIR) and JP- (from Wright- Patterson Air Force Base in Ohio) fuels. We will be presenting test data from demonstration of the prototype desulfurization system in the conference. CONCLUSIONS TDA s liquid fuel desulfurization system reduces the sulfur level in the logistic fuels to sub ppm levels making them suitable for use in military fuel cells. TDA s desulfurization technology will enable the deployment of fuel cell powered APUs in the field for silent and other strategic missions. ACKNOWLEDGMENTS We acknowledge the funding provided by DOD Phase II SBIR Grant (Contract No. W5HZV-5-C- 1) for this research and valuable inputs from Mr. Kevin Mills of TARDEC, U.S. Army.