Flame initiation by nanosecond plasma discharges: Putting some new spark into ignition Paul D. Ronne - PowerPoint PPT Presentation

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Flame initiation by nanosecond plasma discharges: Putting some new spark into ignition Paul D. Ronne

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Travel supported by the Combustion Institute. Faculty collaborator: ... Brad Tallon, Matthew Beck ... Postdocs: NASA Glenn, Cleveland; US Naval ... – PowerPoint PPT presentation

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Title: Flame initiation by nanosecond plasma discharges: Putting some new spark into ignition Paul D. Ronne


1
Flame initiation by nanosecond plasma
dischargesPutting some new spark into
ignitionPaul D. RonneyUniversity of Southern
California, USANational Central
UniversityJhong-Li, Taiwan, October 3,
2005Research supported by U.S. AFOSR, ONR
DOETravel supported by the Combustion Institute
  • Faculty collaborator Martin Gundersen (USC-EE)
  • Research Associates Nathan Theiss, Jian-Bang
    Liu
  • Graduate students Jason Levin, Fei Wang,
  • Jun Zhao, Tsutomu Shimizu
  • Undergraduate students Brad Tallon, Matthew
    Beck
  • Jennifer Colgrove, Merritt Johnson, Gary Norris

2
University of Southern California
  • Established 125 years ago this week!
  • jointly by a Catholic, a Protestant and a Jew -
    USC has always been a multi-ethnic,
    multi-cultural, coeducational university
  • Today 32,000 students, 3000 faculty
  • 2 main campuses University Park and Health
    Sciences
  • USC Trojans football team ranked 1 in USA last 2
    years

3
USC Viterbi School of Engineering
  • Naming gift by Andrew Erma Viterbi
  • Andrew Viterbi co-founder of Qualcomm,
    co-inventor of CDMA
  • 1900 undergraduates, 3300 graduate students, 165
    faculty, 30 degree options
  • 135 million external research funding
  • Distance Education Network (DEN) 900 students in
    28 M.S. degree programs 171 MS degrees awarded
    in 2005
  • More info http//viterbi.usc.edu

4
Paul Ronney
  • B.S. Mechanical Engineering, UC Berkeley
  • M.S. Aeronautics, Caltech
  • Ph.D. in Aeronautics Astronautics, MIT
  • Postdocs NASA Glenn, Cleveland US Naval
    Research Lab, Washington DC
  • Assistant Professor, Princeton University
  • Associate/Full Professor, USC
  • Research interests
  • Microscale combustion and power generation
  • (10/4, INER 10/5 NCKU)
  • Microgravity combustion and fluid mechanics
    (10/4, NCU)
  • Turbulent combustion (10/7, NTHU)
  • Internal combustion engines
  • Ignition, flammability, extinction limits of
    flames (10/3, NCU)
  • Flame spread over solid fuel beds
  • Biophysics and biofilms (10/6, NCKU)

5
Paul Ronney
6
Transient plasma ignition - motivation
  • Multi-point ignition of flames has potential to
    increase burning rates in many types of
    combustion engines, e.g.
  • Pulse Detonation Engines
  • Reciprocating Internal Combustion Engines
  • (Simplest approach) Leaner mixtures (lower NOx)
  • (More difficult) Redesign intake port and
    combustion chamber for lower turbulence since the
    same burn rate is possible with lower turbulence
    (reduced heat loss to walls, higher efficiency)
  • High altitude restart of gas turbines
  • Lasers, multi-point sparks challenging
  • Lasers energy efficiency, windows, fiber optics
  • Multi-point sparks multiple intrusive electrodes
  • How to obtain multi-point, energy efficient
    ignition?

7
Transient plasma (pulsed corona) discharges
  • Not to be confused with plasma torch
  • Initial phase of spark discharge (highly conductive (arc) channel not yet formed
  • Characteristics
  • Multiple streamers of electrons
  • High energy (10s of eV) electrons compared to
    sparks (1 eV)
  • Electrons not at thermal equilibrium with
    ions/neutrals
  • Ions stationary - no hydrodynamics
  • Low anode cathode drops, little radiation
    shock formation - more efficient use of energy
    deposited into gas

8
Corona vs. arc discharge
Corona phase (0 - 100 ns) Arc phase (
100 ns)
9
Images of corona discharge flame
  • Axial (left) and radial (right) views of
    discharge
  • with rod electrode
  • Axial view of discharge flame
  • (6.5 CH4-air, 33 ms between images)

10
Characteristics of corona discharges
  • For short durations (1s to 100s of ns depending
    on pressure, geometry, gas, etc.) DC breakdown
    threshold of gas can be exceeded without
    breakdown if high voltage pulse can be created
    and stopped quickly enough

 
11
Characteristics of corona discharges
Corona arc
Corona only
  • If arc forms, current increases some but voltage
    drops more, thus higher consumption of capacitor
    energy with little increase in energy deposited
    in gas (still have corona, but followed by
    (relatively ineffective) arc)

 
12
Corona discharges are energy-efficient
  • Discharge efficiency ?d 10x higher for corona
    than conventional sparks

13
Objectives
  • Compare combustion duration and ignition energy
    requirements of spark-ignited and corona-ignited
    flames in constant-volume vessel
  • Determine effect of corona electrode geometry and
    ignition energy on combustion duration
  • Determine if reduced combustion duration observed
    for corona ignition in quiescent, constant-volume
    experiments also applies to turbulent flames
  • Integrate pulsed corona discharge ignition system
    into premixed-charge IC engines
  • Compare performance of corona-ignited and
    spark-ignited engines
  • Efficiency
  • Emissions

14
Experimental apparatus (constant volume)
  • Pulsed corona discharges generated using
    thyratron or pseudospark gas switch Blumlein
    transmission line
  • 2.5 (63.5 mm) diameter chamber, 6 (152 mm) long
  • Rod electrode (shown below) or single-needle
  • Energy release (stoich. CH4-air, 1 atm) 1650 J
    energy release
  • Discharge energy input for ignition is trivial
    fraction of heat release!

15
Definitions
  • Delay time 0 - 10 of peak pressure
  • Rise time 10 - 90 of peak pressure

16
Electrode configurations
17
Pulsed corona discharges in IC engine-like
geometry
  • Top view Side view

18
Minimum ignition energy vs. mixture
  • 1 pin corona discharge vs. spark - same
    geometry
  • MIE significantly higher ( 100x) for corona -
    more distributed energy deposition in streamers?
  • Minimum spark kernel diameter 0.2 mm for
    stoich. CH4-air

19
Pressure effects on MIE
  • MIE for pulsed corona does NOT follow Emin P-2
    as spark ignition does more like P-1 at low P,
    P0 at higher P
  • Smaller chamber diameter enables ignition at
    higher P - higher voltage gradient

20
Effect of geometry on delay time
21
Effect of geometry on delay time
  • Delay time of spark larger ( 1.5 - 2x) than
    1-pin corona ( same geometry)
  • Consistent with computations by Dixon-Lewis,
    Sloane that suggest point radical sources improve
    ignition delay 2x compared to thermal sources
  • More streamer locations (more pins, rod) yield
    lower delay time ( 3.5x lower for rod than
    spark)
  • Suggests benefit of corona is both chemical (1.5
    - 2x) and geometrical ( 2x)

22
Effect of geometry on rise time
23
Effect of geometry on rise time
  • Rise time of spark larger same as 1-pin corona
    ( same flame propagation geometry)
  • More streamer locations (more pins, rod) yield
    lower rise time ( 3 - 4x lower for rod than
    spark), but multi-pin almost as good with less
    energy

24
Peak pressures
25
Peak pressures
  • Peak pressures significantly higher for
    multi-point corona that one-pin corona or spark
  • Improvement (for rod) nearly independent of
    mixture
  • Probably due to change in flame propagation
    geometry, not heat losses
  • Radial propagation (corona) vs. axial propagation
    (arc)
  • Corona more combustion occurs at higher
    pressure (smaller quenching distance)
  • Corona lower fraction of unburned fuel
  • Consistent with preliminary measurements of
    residual fuel

26
Energy geometry effects on delay time
  • What is optimal electrode configuration to
    minimize delay/rise time for a given energy?
  • Delay time 2-ring, 4-ring plain rod similar
    (all are much better than spark)

27
Energy geometry effects on rise time
  • Rise time 2-ring or 4-ring best
  • Note step behavior for multi-point ignition at
    low energies - not all sites ignite
  • Delay time doesnt show step behavior

28
Energy geometry effects (lean mixture)
  • Delay time same conclusion as stoichiometric
    mixture

29
Energy geometry effects (lean mixture)
  • Rise time 4-ring stands out

30
Rod diameter effects
  • Plain rod optimal diameter exists ( 0.15),
    drod/dcyl 0.06
  • Large d low field concentration, few streamers?
  • Small d Too many streamers, too much energy
    deposition?

31
Effect of number of pins on 1 ring
32
Effect of number of pins on 1 ring
  • MIE lower (!!) with more pins, optimal 4
  • More pins Slightly beneficial effect on delay
    time, slightly adverse effect (!) on rise time
  • More is not necessarily better!

33
Thyratron vs. pseudospark generator
  • Little effect of discharge generator type
    (pseudospark 1/2 discharge duration compared
    to thyratron)

34
Turbulent test chamber
35
Turbulence effects
  • Simple turbulence generator (fan grid)
    integrated into coaxial combustion chamber, rod
    electrode
  • Turbulence intensity 1 m/s, u/SL 3
    (stoichiometric)
  • Benefit of corona ignition same in turbulent
    flames - shorter rise delay times, higher peak
    P
  • Note quiescent corona faster than turbulent
    spark! (Faster burn with less heat loss)

36
Turbulence effects
  • Similar results for lean mixture but benefit of
    turbulence more dramatic - higher u/SL ( 8)

37
Engine experiments
  • 2000 Ford Ranger I-4 engine with dual-plug head
    to test corona spark at same time, same
    operating conditions
  • National Instruments / Labview data acquisition
    control
  • Horiba emissions bench, samples extracted from
    corona - equipped cylinder
  • Pressure / volume measurements
  • Optical Encoder mounted to crankshaft
  • Spark plug mounted Kistler piezoelectric pressure
    transducer

38
Electrode configuration
  • Macor machinable ceramic used for insulator
  • Coaxial shielded cable used to reduce EMI
  • Simple single-point electrode tip, replaceable
  • Point to plane geometry first step - by no
    means optimal

39
On-engine corona ignition system
  • Corona electrode and spark plug with pressure
    transducer in 1 cylinder
  • Wired for quick change between spark and corona
    ignition under identical operating conditions
  • 500 mJ/pulse (equivalent wall plug energy
    requirement of 50 mJ spark)
  • Range of ignition timings for both spark corona
  • 3 modes tested
  • Corona only
  • Single conventional plug
  • Two conventional plugs (results very similar to
    single plug)

40
On-engine corona ignition system
41
On-engine results
  • Corona ignition shows increase in peak pressure
    under all conditions tested

42
On-engine results
  • Corona ignition shows increase in IMEP under all
    conditions tested

43
IMEP at various air / fuel ratios
  • Indicated mean effective pressure (IMEP) higher
    for corona than spark, especially for lean
    mixtures (nearly 30)
  • Coefficient of variance (COV) comparable

44
IMEP at various loads
  • Corona showed an average increase in IMEP of 16
    over a range of engine loads

45
Burn rate
  • Integrated heat release shows faster burning with
    corona leads to greater effective heat release

2900 RPM, ? 0.7
46
Burn rates
  • Corona ignition shows substantially faster burn
    rates at same conditions compared to 2-plug
    conventional ignition

2900 RPM, ? 0.7
47
Emissions data - NOx
  • Improved NOx performance vs. indicated efficiency
    tradeoff compared to spark ignition by using
    leaner mixtures with sufficiently rapid burning

48
Emissions data - hydrocarbons
  • Hydrocarbons emissions similar, corona vs. spark

49
Emissions data - CO
  • CO emissions similar, corona vs. spark

50
Conclusions
  • Flame ignition by transient plasma or pulsed
    corona discharges is a promising technology for
    ignition delay rise time reduction
  • More energy-efficient than spark discharges
  • Shorter ignition delay and rise times
  • Rise time more significant issue
  • Longer than delay time
  • Unlike delay time, cant be compensated by spark
    advance
  • Higher peak pressures
  • Benefits apply to turbulent flames also
  • Demonstrated in engines too
  • Higher IMEP for same conditions with same or
    better BSNOx
  • Shorter burn times and faster heat release
  • Improvements due to
  • Chemical effects (delay time) - radicals vs.
    thermal energy
  • Geometrical effects - (delay rise time) - more
    distributed ignition sites

51
Future work
  • Improved electrode designs
  • Solid-state discharge generators
  • Multi-cylinder corona ignition
  • Corona-ignited, low turbulence (thus low heat
    loss) engines???
  • Transient plasma discharges for fuel electrospray
    dispersion?

52
Thanks to
  • National Central University
  • Prof. Shenqyang Shy
  • Combustion Institute (Bernard Lewis Lectureship)
  • AFOSR, ONR, DOE (research support)
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