application of pulsed detonation engine for electric power...

23
9 9 - - Mar Mar - - 07 07 1 1 AERODYNAMIC RESEARCH CENTER MECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT Application of Pulsed Detonation Engine for Electric Power Generation Acknowledgements Acknowledgements : : This study is made possible by funding from Mechanical and Aerospace Engineering Department, UT Arlington and The National Science Council, Taiwan, ROC Philip K. Panicker Aerodynamic Research Center, University of Texas at Arlington, Arlington, Texas, 76019 Jiun-Ming (Jimmy) Li Institute of Aeronautics and Astronautics, National Cheng Kung University, Tainan, Taiwan, 701, Republic of China Frank K. Lu Donald R. Wilson ARC, MAE Department, UT Arlington, Arlington, Texas, 76019

Upload: lykhue

Post on 31-Oct-2018

215 views

Category:

Documents


0 download

TRANSCRIPT

99--MarMar--0707 11AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

Application of Pulsed Detonation Engine for Electric Power Generation

AcknowledgementsAcknowledgements: : This study is made possible by funding fromMechanical and Aerospace Engineering Department, UT Arlington

and The National Science Council, Taiwan, ROC

•Philip K. Panicker

Aerodynamic Research Center, University of Texas at Arlington, Arlington, Texas, 76019

•Jiun-Ming (Jimmy) LiInstitute of Aeronautics and Astronautics, National Cheng Kung University, Tainan, Taiwan, 701, Republic of China

•Frank K. Lu•Donald R. Wilson

ARC, MAE Department, UT Arlington, Arlington, Texas, 76019

99--MarMar--0707 22AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

AgendaAgenda

Introduction: Introduction: Why PDE for Power GenerationWhy PDE for Power GenerationHow PDE can be applied for Power GenerationHow PDE can be applied for Power Generation

Objectives of This StudyObjectives of This StudyExperimental SetupExperimental SetupVideo of Test RunVideo of Test RunResultsResultsConclusionConclusion

99--MarMar--0707 33AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

Advantages of PDEAdvantages of PDESimplicity of designDetonation wave does the work of compressing the gas, producing extremely high pressure ratios, higher temperatures.No requirement of high compression ratios and thus no compressor requiredConstant volume combustion offers better efficiencies than constant pressure combustion in Brayton cycleBetter thrust, Isp, fuel efficienciesHigher weight to thrust ratios.

. ( )=∴=+ YADAdyDY A

aaa

99--MarMar--0707 44AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

PDE Cycle vs. Brayton CyclePDE Cycle vs. Brayton Cycle

Wu, Y., Ma, F., and Yang, V., “System Performance and Thermodynamic Cycle Analysis of Air Breathing Pulse Detonation Engines”, Journal of Propulsion and Power, Vol. 19, No. 4, July-August 2003, pp. 556-567.

Ψ

is static temperature ratio for stoichiometric H2/air system

Bellini, R., and Lu, F.K., “Exergy Analysis of a Pulse Detonation Power Device”, Proceedings of the 10th BrazilianCongress of Thermal Sciences and Engineering-ENCIT 2004, Brazil. Society of Mechanical Sciences and Engineering-ABCM, Rio de Janeiro, Brazil, 2003, 2004, Paper CIT04-0734.

Second law efficiency

99--MarMar--0707 55AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

PDE ApplicationsPDE Applications

The attraction of the PDE is its simplicity and The attraction of the PDE is its simplicity and versatilityversatilityMostly military: Missiles, Mostly military: Missiles, UAVsUAVsElectric Power Generation: Hybrid PDE Electric Power Generation: Hybrid PDE with turbine and generatorwith turbine and generator

Ground based and OnboardGround based and OnboardCivilian and MilitaryCivilian and MilitaryLarge scale and small scale power plants, portable Large scale and small scale power plants, portable power generatorspower generators

99--MarMar--0707 66AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

PDE Hybrid Engines for Power GenerationPDE Hybrid Engines for Power Generation

A hybrid engine with A hybrid engine with only 1 PDE operating only 1 PDE operating at low frequency may at low frequency may affect the turbine due affect the turbine due to the slow pulsing to the slow pulsing nature of the exhaust, nature of the exhaust, which also affects the which also affects the electric power output, electric power output, creating pulsing noise.creating pulsing noise.This can be eliminated This can be eliminated by adding a flyby adding a fly--wheel, wheel, similar to those on 4 similar to those on 4 stroke 1 cylinder stroke 1 cylinder motormotor--cycle engines.cycle engines.Multiple PDE tubes Multiple PDE tubes each operating at a low each operating at a low frequency will frequency will smoothen out the smoothen out the exhaust flow.exhaust flow.

99--MarMar--0707 77AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

Many Fuel Options for PDEsMany Fuel Options for PDEsCoalCoal: US : US DoEDoE estimates that estimates that ¼¼ of world coal resources are in the of world coal resources are in the US, enough to last over 200 years. Efforts are underway to produUS, enough to last over 200 years. Efforts are underway to produce ce clean clean coal gascoal gasNatural GasNatural Gas: US : US DoEDoE claims that 900 of the next 1000 Electric claims that 900 of the next 1000 Electric Power Stations will use Natural Gas. 80% of US Natural Gas is Power Stations will use Natural Gas. 80% of US Natural Gas is produced internally. LPG, CNG used for vehicles.produced internally. LPG, CNG used for vehicles.PropanePropane: Widely used, available in many container sizes. Imagine a : Widely used, available in many container sizes. Imagine a PDE that could take propane canisters.PDE that could take propane canisters.BioBio--gasgasHydrogenHydrogen: Best and cleanest. Hydrogen economy is set to take off : Best and cleanest. Hydrogen economy is set to take off (2020??). Steps are underway to produce H(2020??). Steps are underway to produce H22 from hydrocarbon from hydrocarbon fuels, e.g., Natural Gas, coal, etc.fuels, e.g., Natural Gas, coal, etc.Coal aerosolCoal aerosol????KeroseneKeroseneJet FuelsJet FuelsOctaneOctane

PDEs can be designed to operate on virtually any fuel. It just takes a little bit more engineering.

99--MarMar--0707 88AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

PDE and Pulse Jets for the Masses

•There is a growing interest among amateurs and hobbyists and small time entrepreneurs into PDEs, Pulse jets, Turbo-charger jets

•Kits available on Ebay

and online stores

•One of the best sites:Bruce Simpson T/A FAB Jets http://www.aardvark.co.nz/pjet/links.htm

Wider interest will fuel innovation and funding driven by market forces

99--MarMar--0707 99AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

Objectives of This StudyObjectives of This StudyTo assemble a proof of concept working To assemble a proof of concept working model of a hybrid PDEmodel of a hybrid PDE--turbineturbine--generator generator systemsystemUse commonly available fuelsUse commonly available fuelsLow budgetLow budget

To identify possible problems in the To identify possible problems in the implementation of a PDEimplementation of a PDE--turbineturbine--generator systemgenerator system

99--MarMar--0707 1010AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

Experimental SetupExperimental Setup

99--MarMar--0707 1111AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

PDEPDE

99--MarMar--0707 1212AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

Electronically Controlled Gaseous InjectorsElectronically Controlled Gaseous Injectors

Solenoid ValvesSolenoid Valves••12 Vdc, 8A peak, 2A hold.12 Vdc, 8A peak, 2A hold.••Fast acting (2ms reaction time). Up to 35Hz tested Fast acting (2ms reaction time). Up to 35Hz tested successfully. 50Hz max.successfully. 50Hz max.••Easy and precise control possible using TTL Easy and precise control possible using TTL signals from a remote computer.signals from a remote computer.••Max pressure 550 kPa (90psig)Max pressure 550 kPa (90psig)

AFS-Gs60-05-5c series Fuel Valves

Alternate Fuel Systems (2004) Inc. Calgary, Canada

99--MarMar--0707 1313AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

150 mJ max energy per spark Inductive Ignition System

A transistor control circuit built in house enables the interfacing of the ignition system to the DAQ PC and allows ignition to be controlled remotely using TTL signals.

Ignition System

99--MarMar--0707 1414AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

TurboTurbo--ChargerChargerAG Kühnle, Kopp & Kausch in Frankenthal, Germany (1899)Schwitzer Company in Indianapolis, Indiana (1918)BorgWarner Automotive (Auburn Hills, Michigan) took over 3K in 1997BorgWarner Automotive took over Schwitzer Co. in 1999BorgWarner Turbo Systems is head-quartered in Kirchheimbolanden, GermanySupplies turbo-chargers to commercial and passenger engine and automobile manufacturers from Alfa Romeo to Caterpillar to Cummins to Porsche to VW

Used in Volkswagen Passat 1.8T and Audi A4/A6 1.8T model cars, which have 5 valve 4 cylinder gasoline engines.

The compressor can deliver a maximum air flow rate of 0.17 kg/sRecommended for automotive engines of up to 150 kW power rating. The turbine’s inlet is 40 mm in diameter; and the outlet is 65 mm in dia.The compressor’s inlet is 36 mm, and the outlet is 38 mm in dia. The turbine is capable of withstanding temperatures as high as 1050°C and running at up to 200,000 rpm.

99--MarMar--0707 1515AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

http://www.turbodriven.com/files/picture_passenger/bwts_picture_passenger_20_26.jpg

Oil supplied by an oil pump from an old Dodge truck, turned by an electric motor so that oil pressure is maintained at 40 to 60 psi

•Water supplied at tap pressure

Turbine over-pressure trap door was bolted shut

99--MarMar--0707 1616AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

Bicycle Dynamo GeneratorBicycle Dynamo Generator

Rated at

6VRMS , 3W @ ~2000 rpm

Powers

a bicycle headlamp (1.6 Ω, 22.5 W)

and

a red tail lamp (8.7 Ω, 4W)

www.myra-simon.com/bike/dynamos.html

Motor ↔ Generator

Motors are run at 1000 to 10,000 rpm

Small DC motors used in RC Cars run at 18,000 rpm, but they are too small and rated for lower power.

99--MarMar--0707 1717AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

bicycle bottle dynamo

ND

is the rotational speed of the dynamo rotor in rpmf is the frequency of the ac voltage in Hzp

is the number of pairs of poles.

Brushless ac generator2 pole permanent magnet rotor Wire wound stator armature dc resistance of 4.2 Ω

The magnitude of the voltage output is proportional to the strength of the magnet, the number of turns in the windings and the speed of rotation of the rotor.

Neglecting slip, speed of turbine is NT

99--MarMar--0707 1818AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

DiagnosticsDiagnostics

Generator output is connected in parallel to the bicycle headlamp (1.6 , 22.5 W) and the red tail lamp (8.7 , 4W) the DAQ through a 4:1 voltage divider The total parallel resistance R// is 1.351 Ω

The lamps are considered to be purely resistive loads for simplicity

IRMS is the RMS currentVRMS is the RMS voltageP is the power output.

•National Instruments DAQ consisting of a 1042Q chassis w/ a pair of 8 channel 2.5 MS/s S-series PXI-

6133 cards. •The DAQ is connected to a remote PC via fiber optic cable which ensures smooth, EMI free signal transmission.•4 PCB piezo-electric dynamic pressure transducers (111A24 model, 1000 psi maximum, 450 kHz resonant frequency)•1 differential pressure transducer for measuring flow rate of the compressor air output (Honeywell Micro Switch model number 164PC01D37)•Type K thermocouples•Water cooling adapters for PTs (064A01 recessed sensor and 064B02 flush sensor models).•Flow-Dyne Engineering critical flow nozzles to measure gas mass flow

99--MarMar--0707 1919AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

99--MarMar--0707 2020AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

Results of 15 Hz test PropaneResults of 15 Hz test Propane--OxygenOxygen

Time (h:m) Time (s) Peak Voltage VRMS

Freq. of Output (Hz)

Power (W)

Generator Speed (rpm)

Turbo Speed (rpm)

Compressor Flow Rate

(kg/s)

19:59 10.6562 5.7 4.03 225.124 12.02 13,507 44,575 0.0464

19:59 11.6562 8.41 5.95 621.922 26.18 37,315 123,141 0.0526

19:59 15.3906 8.42 5.95 641.491 26.24 38,489 127,015 0.0539

19:59 16.3902 8.34 5.90 600.519 25.74 36,031 118,903 0.0543

19:59 21.9219 8.11 5.73 501.458 24.34 30,087 99,289 0.0553

19:59 22.9219 8.01 5.66 484.447 23.75 29,067 95,921 0.0516

99--MarMar--0707 2121AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

ResultsResults

TOF Detonation Wave Velocity

VCJ = 2449

2000

2100

2200

2300

2400

2500

2600

2700

PT1-2 PT2-3 PT3-4

Position

Vel

ocity

(m/s

)

• Propane + Oxygen at equivalence ratio of 1.2, 0.0057 kg/s

• Exhaust of Turbine is at 800˚C

• Turbine spins at over 127,000 rpm

• Compressor outputs air flow of over 0.055kg/s

• Detonation observed in PDE

• No damage visible in turbine after over 1 minute of run time

99--MarMar--0707 2222AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

Conclusions and RecommendationsConclusions and Recommendations

A PDEA PDE--turbineturbine--generator system successfully tested.generator system successfully tested.

Generator produces about 26 W of power, while Compressor pumped Generator produces about 26 W of power, while Compressor pumped air at air at

0.055 kg/s at turbine speeds higher than 127,000 rpm.0.055 kg/s at turbine speeds higher than 127,000 rpm.

Exhaust temperature of turbine is 800Exhaust temperature of turbine is 800˚C, suggesting that there was enough C, suggesting that there was enough

enthalpy in the flow to drive another turbine stage.enthalpy in the flow to drive another turbine stage.

One PDE tube at 15 Hz drove the turbine at a significantly high One PDE tube at 15 Hz drove the turbine at a significantly high speed, as speed, as

the PDE exhaust velocity is high, as opposed to the exhaust of athe PDE exhaust velocity is high, as opposed to the exhaust of automobiles.utomobiles.

The turbineThe turbine’’s rated 200,000 rpm could be achieved by running the PDE at s rated 200,000 rpm could be achieved by running the PDE at

higher speeds.higher speeds.

99--MarMar--0707 2323AERODYNAMIC RESEARCH CENTERMECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

Conclusion and Recommendations (contd.)Conclusion and Recommendations (contd.)Radial turbines create high losses, as flow is turned 90Radial turbines create high losses, as flow is turned 90˚, suffer high

temperature and pressure effects of high speed flows.

The turbine and generator has to be matched in terms of speed, torque,

power output.

Transmission (with speed reduction for generator) has to be robust and

capable of harmonizing the speed and torque of turbine and generator.

Noise of PDE has to be dealt with.