Transcript Document
PHILIPS
TU/e
Experiments on CFL Ignition
Ignition Studies of
Low-Pressure Discharge Lamps
M. Gendre - M. Haverlag - H. van den Nieuwenhuizen - J. Gielen - G. Kroesen
Friday, March 31st 2006
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Outlines
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Goals of the study
Set-up
DC breakdown
AC resonant ignition
Summary
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Goals of the Study
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Understanding Plasma Ignition
Motivations
Physics:
better comprehension of dielectric-plasma
phase transitions in general
Technology: understand how compact fluorescent
lamps ignite under various conditions
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Goals of the Study
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Interest of a better understanding
1900s
Courtesy of R. Richter, private communication
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Goals of the Study
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Interest of a better understanding
2000s
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Goals of the Study
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Understanding Lamp Ignition
Q: How does low-pressure breakdown work ?
Townsend model: electron avalanche between electrodes
- homogeneous E field
E
- infinite electrode extension
Neglected by Townsend
- inhomogeneous field
anode
cathode
ion
atom
electron
- diffusion losses of charges
toward the walls
- wall surface charges
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Goals of the Study
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Goals and Approach
A: Thorough study of ignition in a ‘standard’ linear lamp
studies:
- different experiments on same lamp design
- different lamp configurations (gas, pressures…)
- control of experiments (repeatability, accuracy…)
- cross-comparisons between results
Global Overview of the Phenomenon
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Outlines
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Goals of the study
Set-up
DC breakdown
Back to AC resonant ignition
Summary
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Set-Up
Global Circuitry
power
amplifier
function
generator
HV probe
RL
HV probe
321electrode
pulse
Faraday
current
potential
time
optical
generation
reference
recording
imaging
heating
cage
probing
low-voltage
current
active
same
fast
custom-built
critical
iCCD
time
electrode
for
measured
camera
the
base
waveform
floating
accuracy
at
forat
for
all
ch
digital
1
oscilloscope
-200-1200V
amplified
three
1000K
instruments
50-500ns
capacitive
of
the critical
experiments
forto
time
eprobe
points
emission
resolution
IA
2
ch 4
3
double
subelectrode
one
lamp
full
ms
voltage
potential
pulse
lamp
and
impedance
mA
scheme
ignition
taken
mapping
timeas
for
and
constant
the
in
time
charge
each
main
current
and
image
over
reference
clean-up
space
resolutions
time
taken
Faraday cage
IF
load
current
electrode
simultaneous
20
7mm
toresistor
and
60waveforms
images
voltage
1ms
for
triggering
space
lamp
are
kept
lamp
current
recorded
at
of
added
and
constant
scope
time
for
regulation
and
by
resolutions
each
value
oscilloscope
camera
time step
IG
TTL trigger
lens
computer
camera
controller
ICCD
camera
capacitive
probe
driver
voltage
regulator
data
no drift
processed
of electrode
to give
performances
space-time
diagrams
during
the experiments
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Set-Up
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Experimental Frame of Reference
electrostatic
probe
lamp
ITO
Faraday’s
window
rackcage
probe
- transparent
- senses
- stable
housethe
145mm
and
electrostatic
and
long,
lamp
electrically
locate
10mm
surface
the
environment
diameter
conducting
probe
potential
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Outlines
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Goals of the study
Set-up
DC Breakdown
AC resonant ignition
Summary
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DC Breakdown
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time
Ignition Mechanism Overview
light
K
A
K
potential
A
Argon 3 torr global
–600Vevolution identical
in both cases
Pre-breakdown wave:
apparent lag of light
- starts at the cathode
emission (max 1ms)
- propagates toward the anode
smooth evolution of
- speed and intensity decreases
lamp potential
Return strike:
potential gradient in the
ofwave
first wave
- starts at endwake
of first
propagation
- propagates toward the cathode
x (cm)
14
-500
- speed and intensity decreases
0
+5000
-400
-300
-200
-100
0V
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DC Breakdown
Cathode-Initiated Breakdown
3torr Ar-Hg lamp : -500V dt=100ns
K
A (0)
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DC Breakdown
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Argon
Argon
3torr
3torr
–400V
–200V
–300V
: Successful
: Failed Ignition
Ignition
resolution potential: 10ns
optical: 500ns
100ns
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DC Breakdown
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Pre-Breakdown Wave Position vs. Voltage
51- 44 km/s
10 - 3 km/s
- wave speed directly proportional to voltage
- ignition condition: first wave has to reach the anode
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DC Breakdown
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Lamp Net Charges vs. Voltage
- first wave charging effect increases with voltage
- decrease of net charge only for successful breakdown
- Ignition condition: charging threshold to be reached
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DC Breakdown
Global Overview of the Phenomenon
_
Qualitative model
e
+
Wall
and
field
displacement
High charging
Local
radial/axial
Townsend-like
E-field
breakdown
component
Further
Current
ionization
stabilized
in
by
front
ballast
of cathode
Wave
Field
rotation
propagation
and
toward
anode
Electrodes
Exponential
current
circuit
increase
closed
- ionization
wave
drivenbridged,
by
front enhancement
field,
rate ofthe
wallcathode
charge
- wave speed dependent on E/p value
Global
lampelectron
charge
decrease
Decreasing
current flux
Steep
current
increase
- gradual decrease of field and wave speed during propagation
- ignition condition : E/p high enough for 1st wave to reach anode
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Outlines
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Goals of the study
Set-up
DC breakdown
AC resonant ignition
Summary
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AC Resonant Ignition
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Optical Recording
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AC Resonant Ignition
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Electrostatic Recordings
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AC Resonant Ignition
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Correlation with DC Breakdown
- synchronous propagation of K and A waves
- importance of surface charge memory effect
- easier ignition in alternating potentials as a result
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Outlines
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Goals of the study
Set-up
DC breakdown
AC resonant ignition
Summary
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Summary
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Global Overview
- multiple diagnostic tools running simultaneously
- cross comparisons between optical/electrical data
- various experimental conditions investigated
- correlation between wave propagation and lamp charging
- minimum lamp charging required for successful ignition
- new information inferred from data analysis
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ANY QUESTIONS?
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Set-Up
Global RC-Probe Circuit
Z
-
Faraday’s cage
+
R
r
x
Provides lamp surface potential vs. time/space
- limited field disturbance around the lamp
- Z chosen so total system transfer function = pure real
- little need for post-experiment data treatment
U
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Set-Up
Calculated Data from RC-Probe Output
Measured: F=f(t,x)
F
Calculated: axial E field: EX (t , x)
x
F
radial E field: ER (t , x)
a ln(b / a) ( g / a ) ln(c / b)
|E| field: E (t , x) E X2 ER2
1
EX
<E field: E tan
ER
disp. current: I D CL
F
total disp. current
t
linear charge: QL F CL total charge