Homogeneous Charge Compression Ignition (HCCI) Engines Gajendra Singh.
A High Efficiency Spark Assisted Compression Ignition 1 ...• GT POWER simulations • Parametric...
Transcript of A High Efficiency Spark Assisted Compression Ignition 1 ...• GT POWER simulations • Parametric...
A High Efficiency Spark Assisted Compression Ignition
1 KWe Generator System with
Integrated Waste Energy Recovery
Air Squared Inc., Purdue University, Argonne National Laboratory,
Mississippi State University
PI: Bryce Shaffer (ASI), CTO
Revision 4
Team
System Integration
and Design
SACI Development
WER Development
Technology
Proposed ICE Improvements -
• Spark Assisted Compression Ignition (SACI) combustion of
NG.
• High compression ratios.
• EGR dilution - Increased specific heat ratios.
• Low combustion temperatures - Lower heat losses.
• ICE down-speeding - Higher torque operation.
GENSET with greater than 40% fuel-to-electricity
conversion efficiency.
• Develop a high efficiency (35%) natural
gas (NG) internal combustion engine.
Organic Rankine Cycle flow diagram.
• Proposed ORC System Improvements
• Regenerator for working fluid
preheat
• Superheat working fluid from
exhaust heat.
• Expander-Pump integration.
• Compact size
• Fewer components
• Lower cost
• Increased reliability
T-S plot for the ORC system. (Purdue)
• Develop a novel bottoming Organic Rankine
Cycle (ORC) with appropriate working fluid
for optimal (6%) Waste Energy Recovery
(WER)
Expander-Pump Assembly
Technical Progress – ICE
• GT POWER simulations
• Parametric studies on the effects of
compression ratios, valve timing, phi
(Φ), intake boost, and EGR quantified
at diff. spark timings.
• Engine Selection and Procurement
• Marathon engine - liquid cooled
NG Spark Ignited.
• Engine Testing
• Test setup fabrication and
functional testing.
Marathon engine test setup. (ANL)
Exhaust
Process Water
Marathon Engine
TestStand
Starter System: Battery
Data Acquisition
Exhaust Heat Exchanger
WaterBrake Dyno
Natural Gas
Intake System
Estop#2: TestStand
Dyno LoadControl
Dyno ReservoirExhaust
Condensate Collector
Marathon engine best baseline at 1200 rpm. (MSU)
Technical Progress – ORC/WER
• ORC Working Fluid Selection
• R1233zd(E)
• Operating Conditions Optimization
• Max η1st Law = 16%
• Predictive Performance Modeling
• Pre-Alpha Expander Testing
• ORC Architecture Layout
• Process and Instrumentation
• Test Stand Design
• CAD Modeling for Test Stand
Construction
ORC test setup schematic. (Purdue)
ORC Test Setup CAD Model
Technical Progress – ORC/WER• Expander
• Operating conditions
• Designing
• Fabrication/Assembly
• Testing
Operating Conditions
Inlet Pressure 2400 [KPa]
Inlet Temperature 275 [C]
Outlet Pressure 240 [KPa]
Mass Flow Rate 0.00308 [Kg/s]
Work Output 120 [Watt]
Specifications
Rotational Speed 1800 [RPM]
Suction Volume 0.8 [CC]
Volume Ratio 6.5 [-]Scroll expander mounted on the test setup. (ASI)
Pre-Alpha Scroll Expander Model
Technical Progress – System• System Thermal Analysis
• Use engine and ORC
simulation data
• Optimize working
conditions
• Preliminary CAD model
• Component solid models
• Component packaging
System CAD model showing outer shell and component packaging.
Lessons Learned
• Scroll Expander Design
• Design improvements to reduce leakage losses
• Single stage might be more suitable for low power & high pressure
application.
• System Transient Operation
• WER System - Start Up/
Shut Down
• Clutch/Valve Design
Belt drive arrangement between engine and ORC expander -
pump.
Next StepsInternal Combustion Engine
• Continue engine testing.
• Validate simulation models using the test results.
• Modify and test engine as per the proposed SACI concept.
• Implement SACI Model.
Waste Heat Recovery System/ORC
• ORC system will be fabricated and tested.
• Validate simulation models and make improvements.
Expander – Pump for ORC
• Alpha expander and pump assembly will be designed and fabricated.
• Performance testing will be carried out.
System
• Prepare system integration plan.
• Improve system CAD model.
Expander-Pump Assembly
ORC Test Setup CAD Model
Scope of Low Cost Natural Gas Pump
Several GENSET projects require pressurized natural gas (35 PSIG) at the inlet of their system. While natural gas pumps currently exist, ARPA-E has recognized the need for an smaller, inexpensive solution.
• Scope: Design, fabricate and test a Gen 1, Gen 2 and Gen 3 prototype with the following specifications.• Performance: 5 LPM at 35 PSIG (Inlet at 0.25 PSIG)
• Power: < 60W
• Cost Target: < $100 per unit
• Life: Same as GENSET (10 yrs)
• Proven Life: 3000 hrs
Thank You
Low cost motor Deep drawn aluminum outer housing