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Kinetic Modeling of Non‐Equilibrium Plasmas for Modern Applications
Igor Kaganovich for the Project TeamPrinceton Plasma Physics Laboratory
PPPLMay 3, 2019
OUTLINE
Research in Low Temperature Plasma Physics at PPPL Neutralization of positive ion beam space‐charge by electrons
Rotating spoke in a Penning discharge
Negative Hydrogen Ion Sources
GE Plasma Switch
Thermal electric converter
Secondary Electron Emission
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3
Low Temperature Plasma Projects at PPPL
Nano dusty plasma
Experiments and simulations of synthesis of nanomaterials in plasmas
New PFC materials
PPPL Low Temperature Plasma Research
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• US DOE Office of Science• Fusion Energy Science• Basic Energy Science
• Lockheed Martin• General Electric• Aerospace Corp.
• Samsung• Colgate• HiFunda (DOE STTR)
• AFOSR• ARPA‐E• Sandia National Laboratory
OUTLINE
Research in Low Temperature Plasma Physics at PPPL Neutralization of positive ion beam space‐charge by electrons
Rotating spoke in a Penning discharge
Negative Hydrogen Ion Sources
GE Plasma Switch
Thermal electric converter
Secondary Electron Emission
5
Excitation and propagation of electrostatic solitary waves (ESWs) in
ion beam neutralizationChaohui Lan1,2 I. D. Kaganovich1
1 Princeton Plasma Physics Laboratory, Princeton, New Jersey 08543, USA
2 Institute of Fluid Physics, China Academy of Engineering Physics, Mianyang, 621900, P. R. China.
Simulation modelxy Metal wall or
periodic boundary
Metal wall
Metal wall
80 cm
Metal wall or periodic boundary
Vb
Ion beam pulse
Electron injection 3 cm
• Electrostatic particle‐in‐cell algorithm, self‐magnetic field of ion beam is neglected. • 2D Cartesian coordinates, cell size Δl=0.25 mm, time step Δt=40 psIon beam pulse:• Ar+ ion beam, Eb=38 keV (Vb=37.5 cm/us), nb=1.75×1014 m‐3
• Gaussian‐like, x: flattop 250 ns (~11 cm), edges nbexp(‐t2/tb2), tb=60 ns; y: nbexp(‐y2/wb2),
wb=2 mmElectron injection:• A line source, located at x=20 cm, 2 mm length in the y direction. • The temperature of injected electrons 0.2 eV.• Injected electron current is 2/3~8/3 of ion beam current 7
Neutralization of ion beam pulse
0 10 20 30 400.00.81.62.40.00.81.62.40.00.81.62.40.00.81.62.40.00.81.62.4
0 10 20 30 40
Parti
cle
dens
ity(1
014m
-3)
x (cm)
t=635 ns
t=707 ns
t=923 ns
t=851 ns
t=779 ns
electron ion
20 30 40 50
20 30 40 50
t=995 ns
x (cm)
t=1283 ns
t=1211 ns
t=1139 ns
t=1067 ns
The appearance of peaks of electron density indicates that electrons are reflected at the edges of ion beam pulseThe zigzag distribution of electron density at initial stage indicates that the two-stream instability is developingA lot of small electron holes are generated, then they coalese and generate a large electron hole, namely ESW
• Except for location where the ESW is, others pars of ion beam pulse are close to near-neutralization. 8
Evolution of electrons in x‐vx phase space
0 10 20 30 40-14-707
14-14-707
14-14-707
14-14-707
14-14-707
140 10 20 30 40
V x/Vb
x (cm)
t=851 ns
t=779 ns
t=707 ns
t=635 ns
t=923 ns
20 30 40 50
20 30 40 50
x (cm)
t=995 ns
t=1067 ns
t=1139 ns
t=1211 ns
t=1283 ns
Electron reflection by ion beam pulse occurs when ion beam pulse gets close to the injection position. The two-stream instability isself-triggered and naturally formed.At initial stage, electron stream generates a big circle in the phase space, then it splits into many small ones.These small holes merge together and generate the ESW.
The resulting ESW is very stable, and rapidly moves inside the ion beam pulse.The ESW periodically rotates in the phase space, just like around a running track
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The influence of ion beam profile
0 2 4 6 8 100.65
0.70
0.75
0.80
Neu
traliz
atio
n de
gree
Time (s)
• ESWs can sustain longer time in a long ion beam pulse, and their lifetimes increase rapidly with the increase of the duration of ion beam pulse.• It seems that sharp boundary is conducive to the excitation and maintenance of ESWs.
0 2 4 6 8 10
0
20
40
60
80
100
120
Time (s)
Pote
ntia
l (V)
500 ns (22 cm)
0.63
0.66
0.69
0.72
0.75
Neu
traliz
atio
n de
gree
10
Collision of two solitons
0 10 20 30 40
0
40
80
120
160
3.6 s
4.2 s
4.1 s
4.0 s
3.9 s
3.8 sPote
ntia
l (V)
x (cm)
3.7 s
0 10 20 30 400
40
80
120
1606.8 s
6.6 s
6.4 s
6.2 s
6.0 s
5.8 s
Pote
ntia
l (V)
x (cm)
5.6 s
• Passing through and coalescence both can occur during collision, maybe determined by the relative velocity of two solitons
• The shape and velocity of soliton do not necessarily keep unchanged during collision of two solitons 11
Conclusions• The capture process of electrons can cause the occurrence of the
two‐stream instability inside the ion beam pulse, and this instability quickly evolves into stable moving nonlinear ESWs.
• The ESWs with longitudinal size reaching several cms can reflect back and forth between the two ends of the ion beam pulse for many times and last far longer than the duration of the ion beam pulse.
• The excitation of the ESWs reduces the neutralization degree of ion beam pulse.
• The dissipation of the ESWs causes heating of neutralizing electrons and their escape from the ion beam, leading to further reduction of neutralization degree.
• Using a longitudinally extended electron source instead of a thin emitter can effectively minimize the excitation of the ESWs.
OUTLINE
Research in Low Temperature Plasma Physics at PPPL Neutralization of positive ion beam space‐charge by electrons
Rotating spoke in a Penning discharge
Negative Hydrogen Ion Sources
GE Plasma Switch
Thermal electric converter
Secondary Electron Emission
13
14
‐ Azimuthal plasma non‐uniformity are commonly observed in Hall thrusters and many other low temperature magnetized plasma devices used in material processing.
‐ Understanding of these structures is critically important for performance of these devices and applications.
‐ Recent experiments revealed new scaling properties of these plasma structures with magnetic field and gas pressure which point to practical ways of control and suppression of these structures.
‐ 2‐D and 3‐D Particle‐in‐Cell simulations of these important experimental observations are underway.
2 kW PPPL Hall Thruster
High speed imaging of rotating plasma structures in the thruster
Hall Thruster Research
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Plasma set up with a convenient access for optical and probe diagnostics to study electron kinetic, turbulence and structure formation in plasmas relevant to soft‐plasma processing of materials, sputtering magnetrons, plasma thrusters (http://htx.pppl.gov/penning.html).
ExB Penning‐Type Plasma Discharge to Study Low Temperature Magnetized Plasma and Its ApplicationsTeam: Yevgeny Raitses, Valentin Skoutnev, Eduardo Rodrigez, Igor Kaganovich Andrey Smolyakov
Axis
RF-plasma cathode
E
CoilL
CoilR
B
Axis
CoilL
CoilR
E20 cm
40 cm
8” diameter ExB Penning Discharge Movies From spoke observation to PIC simulations
• We performed integrated experimental and modelling studies applying time‐resolved diagnostics and kinetic simulations supported by theory.
• Study more accessible E × B discharges (Penning/Magnetron)
• E x B discharges are broadly used for propulsion• Thruster exhibit coherent fluctuations that affect performance and lifetime
• Relevant to important technologies, e.g., thrusters (Hall/FRC), plasma sputtering (Magnetron), control of EM waves (plasma photonic crystal devices), fusion (Z‐pinch), electrical grid switches.
Movies have different fields of view to the same device
Structures and anomalous transport in ExB plasmas
ExperimentSimulations
A. Powis, et al., Physics of Plasmas 25, 072110 (2018) 16
OUTLINE
Research in Low Temperature Plasma Physics at PPPL Neutralization of positive ion beam space‐charge by electrons
Rotating spoke in a Penning discharge
GE Plasma Switch
Negative Hydrogen Ion Sources
Thermal electric converter
Secondary Electron Emission
17
Liang Xu, GermanyTimothy Sommerrer GE
Developing Plasma Switch for DC to AC Power Conversion
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• DC transmission lines are more efficient
than AC over distances > 600-800 km.
They can transmit power between non-
synchronized grids and also from
alternative sources wind and solar plants.
• The plasma switch would serve as a
compact, less costly alternative to the
bulky assemblies of semiconductor
switches now installed in power-
conversion systems throughout the grid.
• Today’s power converters are large,
complex, and costly, in part because high
voltages (>300 kV) must be controlled with
large numbers of low voltage devices (<10
kV) connected in series. GE HVDC transmission projects (2017), 35 GW
High Power Plasma Switch Developed by General Electric, Modeled by PPPL
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Cold emissive cathode
Operating pressure 0.1÷1 Torr
Plasma density 10¹²÷10¹³ cm‐3
Anode applied voltage ~ 300kV
Discharge gap ~ 1 cm
Paschen curve for helium gas. Kinetic simulation and analytical model vs. experimental data and textbook
Published in PoP and PSST
OUTLINE
Research in Low Temperature Plasma Physics at PPPL Neutralization of positive ion beam space‐charge by electrons
Rotating spoke in a Penning discharge
Electron Kinetics for Plasma processing Applications
Negative Hydrogen Ion Sources
Thermal electric converter
Secondary Electron Emission
20
Dmytro Sydorenko Alexander KhrabrovXifeng WangTasman PowisShali YangSarvesh Sharma
10 12 14 16 180.1
1
10
100
1000
de
nsity
(1018
m-3)
Te,hot
F CF3 CF2
CF F2 CFgas
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Controlling plasma properties by injection of electron beam into the plasma DC-RF Xenon discharge
Simulation of multi-peak electron velocity distribution function
OUTLINE
Research in Low Temperature Plasma Physics at PPPL Neutralization of positive ion beam space‐charge by electrons
Rotating spoke in a Penning discharge
GE Plasma Switch
Negative Hydrogen Ion Sources
Thermal electric converter
Secondary Electron Emission
22
23
The future fusion experiments rely on NBI systems for the heating and current drive of fusion plasmas. The systems are required to produce hydrogen or deuterium beams with particle energies in the MeV range. Volume production sources operated with pure hydrogen have the advantage of cesium-free operation. A simplified model is required to describe the vibrational kinetics and to predict the negative ion production.
Negative Hydrogen Ion Sources
2
2 2
H ( ) + e ( 2 eV) H + HH ( ) + e ( 12 eV) H ( ) + e + h
KINETICS OF VIBRATIONAL STATES• Electron impact induced processes
• Vibrational‐translational relaxation
• Wall relaxation
1 2 2 21 1
2 2 2
3 2
4 2 2
5 2
6 2
: H ( ) + e H ( ) + e (via resonant H )
: H ( ) + e H ( ) + e + (via , ): H ( ) + e 2H + e
: H ( ) + e H + 2e
: H ( ) + e H + H + 2e
: H ( ) + e H + H
u u
R
R h B CR
R
R
R
7 2 2
8 2 2 2 2
: H ( ) + H H ( 1) + H: H ( ) + H H ( 1) + H
RR
9 2 2: H ( ) + wall H ( ) ( )R
Contribution of the vibrational states of H2(v) to the production of H− ions for various pressure at 50 kW.
F. Gaboriau and J. P. Boeuf, Plasma Sources Sci. Technol. 23, 065032 (2014).
3/10
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Analytical solution (S is the excitation source):
Vibrational Distribution of Molecules Colliding with a Wall
2WR, H ( )1
1 + 1
N
kk
k n S S
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Benchmarking and Validation of GMNHIS
𝑛 𝑛 𝑛 𝜎 𝜀 , 𝜀
𝑘 𝑛 𝑘 𝑛 𝑛 𝜎 𝜀 , 𝜀 𝑘 𝑛
CONCLUSIONS
• We performed modeling of the distribution function of vibrational (VDF) states of
molecular hydrogen H2(v).
• It was found that main processes determining VDF are:
• the vibrational excitation from ground state to vibrational states H2(v=1‐14) • the relaxation of these vibrational states to ground state• the relaxation of vibrational states in collisions with walls.
• Based on these results, we derived an analytical equation for the VDF.
• We also show that the non‐Maxwellian electron energy distribution is important to
take into account, because it yields increase in the production of negative ions at low
pressure regime.
10/10
OUTLINE
Research in Low Temperature Plasma Physics at PPPL Neutralization of positive ion beam space‐charge by electrons
Rotating spoke in a Penning discharge
GE Plasma Switch
Negative Hydrogen Ion Sources
Thermal electric converter
Secondary Electron Emission
28
OUTLINE
Research in Low Temperature Plasma Physics at PPPL Neutralization of positive ion beam space‐charge by electrons
Rotating spoke in a Penning discharge
GE Plasma Switch
Negative Hydrogen Ion Sources
Thermal electric converter
Secondary Electron Emission
29
30
31
Carbon surface transforms in presence of heat and cesium flux
8
14
3
5
6
72
Secondary Electron Emission (SEE) Effects on Plasma
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PU Koel’s Lab: conductors PPPL Raitses’ Lab: dielectrics
• LEED/Auger setup
• Pulsed electron gun setup time‐resolved measurements
• First reliable SEE data for Lithium‐rich materials
A. M. Capece, M. I. Patino, Y. Raitses,B. E. Koel, Appl. Phys. Lett. 109 (2016)
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Carbon surface transforms in presence of heat and cesium flux into new material that has low work function and intense electron emission, possibly due to formation of CsOmolecules embedded into carbon graphite.
• Enhanced transport and power losses in plasma thrusters (Hall, FRC etc).
NASA JPL Mesa Antenna Measurement Facility
• Damaging and destroying high power RF device through multipactordischarge.
SEE‐induced electron cloud effect a possible limitation for particle accelerators.
Large Hadron Colliderat CERN
• Spacecraft charging
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Deleterious Effects of Secondary Electron Emission
Carbon velvet
Dendrites
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• Analytic SEE yield normalized to SEE yield at the flat surface (color bar):
Contributions to the SEE yield emitted by the tops, sides and the bottom surface (unpublished).
Magenta: Optimal packing density
• Optimum value of velvet parameters corresponding to minimum SEY:
C. Swanson et al., 2016
Optimization of velvet‐like structures to minimize the total secondary electron emission yield
Arc Synthesis of Nanomaterials
Project research objectives, scope, highlights
Project accomplishments and major scientific results:
• Simulations of arc structure and nanoparticle nucleation and growth
• Unique in situ diagnostics of plasma–based synthesis.
• Atomistic simulations of key processes of nanotube growth
• Nonstationary processes in arcs
Summary
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Plasma Science Studies of Nanomaterial Synthesis
• Goal: Uncover long standing puzzle how nanotube grow for plasma synthesis of carbon and boron nitride nanostructures, by identification of exact conditions when nanotubes grow.
• Devices: Plasma arc and DC or RF plasma torches, laser‐ablation.
• Approach: Perform detailed characterization of plasma and nanoparticles parameters using laser diagnostics; develop integrated and validated models comprised of numerical tools capable of simulating nucleation of nano‐material growth and particle transport and plasma properties.
Images of boron nitride nanotubes and boron catalyst particles.
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Fig. Predicted final composition at 1 atm. carbon pressure if only 9 first molecules are taken into account. (C1‐9 linear chains).
Fig. DFTb simulations of carbon vapor condensation at gas temperature T=3000K. Initial set up of simulations is curtesy of Longtao Han.
Prediction of chemical compositionSimulation of gas temperature and gas velocity in the arc.
From CFD simulations it follows that the temperature along the nanoparticle growth region changes from 3500 K at the beginning to about 2000 K on the distance of length L ≈ 1 cm ‐ the characteristic length of the nanoparticle growth region, width of this region is W≈ 3 mm. Therefore typical time for particle formation is about L/v where gas flow velocity is about 1m/s giving 10ms time scale for particle formation. Note that this is very long time scale as compared to time scale of atomistic processes.
Charging of SWCNTs could help in their growth• Charging of nanoparticles and nanostructures is a plasma effect on nucleation and growth processes
• DFT and Kinetic Monte‐Carlo simulations of charging effect• Armchair (5,5) SWCNT (Fig. a)• Charging of the CNT causes the higher adsorption energy Ea, increasing the migration distance, (Fig. c)
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a)
b)c)
DFT results (Fig. b)‐ additional charges distribute in the covalent bond space between adatom and CNT, increasing its covalent coupling
Encapsulation of boron particles• Simulations by Quantum‐Classical Molecular Dynamics with Density Functional Tight Binding Theory
• Bombardment by BN (left) or N (right) of boron cluster shows encapsulation of boron clusters with BN layers; the effect is observed in experiments by our and other groups
B‐pinkN‐blue
P. Krstic et al., Chem. Sci. 9, 3803 (2018)40