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Amirhossein (Amir) Alikhanzadeh
Supervisor: Murray J. Thomson
Combustion Research Laboratory, Department of Mechanical
and Industrial Engineering
University of Toronto, Toronto, Ontario, Canada
Investigation of the effects of beam scattering and
beam wandering on laser beams passing thorough the
off-gas duct of an Electric Arc Furnace (EAF)
Master of Applied Science Thesis Defense
University of Toronto, Ontario
December 10th , 2014
Project Overview
2
TDL unable to
penetrate EAF
off –gas duct
Beam scattering
due to collision
with dust particles
Literature review -
Model
Rayleigh
scattering
Mie scattering
Geometric
scattering
Experiment In lab
Beam wandering
due to turbulence
and temperature
gradient
Experiment
In lab
Vertical Flow reactor
(VFR)
3
Motivation : Steel industry
- Uses primarily scrap steel
- Lower energy consumption
- Regulations on the emissions
- 12 to 14 Billion $ sale in Canada (2012)
- High production
- Recycling rate of 40 % to 60 % in
Canada (7 million tonnes recycled in
2012)
- 7.5 % of industrial energy use
BENCHMARKING ENERGY INTENSITY IN THE CANADIAN STEEL INDUSTRY
(Prepared by Natural resources Canada)
EAF 2002 Energy intensity indicator
(MJ/tonnes of Hot Rolled Product)
4
Electric Arc Furnace – Process control
- Heats charged material by means of electric arc
- Consists of three holes plus a “fourth hole”  off-gas extraction
- Off-gas temperature of around 1400 degrees Celsius
Courtesy of Yuhui Sun [University of Toronto]
5
Objective: How important is this
study? Zolo - SCAN
- Zolo-SCAN
- System developed for in-situ measurement
- Difficulty getting the beam over the path
length of the exhaust duct
- Critical Path Length; two reasons
6
Objective: How important is this
study? LINDARC
- Based on TDLAS
- Water cooled rod
- Making readings at the centre
- Reasons similar to Zolo-SCAN
7
Problems with the systems such as
LINDARC and Zolo-SCAN
Most of the issues come from having the rods:
- Dust accumulation
- Rod corrosion
- Damage to the equipment because of molten steel
- Bridging the gap (LINDARC) by means of molten steel
High maintenance expenditure
8
Background: Light interaction with
medium
Light – medium
interaction
Attenuation
(Loss)
Absorption Scattering
Rayleigh
scattering
Mie scattering
Direction and
shape
Scintillation
Beam
wandering
9
Background: What is beam
scattering?
Light interaction
with particles
Reflection (Light
deviated from its
original path
Refraction
Diffraction
Absorption
(Absorbed and
converted to heat)
Reflection
Refraction
Diffraction
Heat dissipation
10
Scattering model: Mie theory
0
0.05
0.1
0.15
0.2
0.25
0.3
0.35
0.4
0 0.5 1 1.5 2 2.5 3 3.5
Volumefraction
Particle diameter (microns)
Particle size distribution (Evans Group)
S-A sample Dust sample
-
Mie Scattering
• Particle size is comparable to the
wavelength
• Not heavily dependant on the
wavelength change
• Particle size parameter: 𝑥 =
𝜋𝑑
λ
Scattering model: Literature
validation
Scattering coefficient in
literature
Scattering coefficient
calculated with the model
11
Scattering model: Model implications – Changing
particle sizes and their distribution
Constant scattering area
- Total scattering area is kept the same while constituent particles are varied in size and
subsequently concentration
- The assumed particle sizes are 0.5,1,1.5,2,2.5 µm in diameter
Concentration of 1.5 micron = 0
Concentration of 1.5 micron = 25
Concentration of 1.5 micons = 50
Concentration of 1.5 micons = 75
Concentration of 1.5 micons = 100
0
5E+09
1E+10
1.5E+10
2E+10
2.5E+10
0.5 1
1.5
2
2.5
0.00E+00
2.50E+09
5.00E+09
7.50E+09
1.00E+10
Numberofparticles/cubicmeter
Particle size in microns 12
Scattering model: Model implications – Effects of
changing particle sizes and their distribution on light
transmission
13
- How NIR transmission is affected when the wavelength is close to the dominant particle sizes
0.5
0.6
0.7
0.8
0.9
1
0 25 50 75 100
I/I0
Percentage of 1.5 micron particles
Light transmission with change in particle size and concentration
VIS - Transmission
NIR- Transmission
MIR- Transmission
Scattering model: Model implications –
Effect of refractive index
0.8
0.9
1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9
LIGHTTRANSMISSION
REFRACTIVE INDEX
Light Transmission (VIS)
Light Transmission (NIR)
Light Transmission (MIR)
14
15
Scattering Experiment:
Description/Purpose
Vibration motors
Different size sieve
VIS source
MIR source
NIR sourceNIR detector
VIS detector
MIR detector
Collecting foil
Particles
Vibration motor
Sieve
Particles
15 cm
25cm25cm25cm25cm
16
Scattering Experiment: Result
- Model could not be
fully verified with
experiments
- The experiment
showed that model
implications of less
scattering at long
wavelength is held
- Although only
qualitative
measurements for
mass, it can be seen
that more particles
means more
attenuation of light
0
25
50
75
100
Talc - 4.4 g Talc - 7.8 g Al2O3 - 6.6 g Al2O3 - 5.6 g
Attenuation
Test ( Particles used - mass dropped in one minute)
Light attenuation from particle scattering
VIS - %Attenuation
NIR - %Attenuation
MIR - %Attenuation
17
Scattering model: Real particle sizes
- Malvern Spraytec
- Agglomeration of the particles is
evident by comparison to Evans’
result
Talc
Aluminum oxide
Jamie Loh [University of Toronto]
18
Scattering : Conclusions
Particle size
distribution
Particle weight %
distribution
Particle refractive
index
Incident
wavelength
Predict how much beam
is lost due to scattering
19
Beam wandering due to
turbulence?
Turbulence
Time Steps
- Varying Temperature, Density and
Index of refraction through
turbulence
- Amplitude fluctuations  Signal
fades
- Beam Wandering (Steering) –
Location movement
- or Scintillation  Distorted beam
shape
https://www.youtube.com/watch?v=VEFEQUY-KNA&list=LLSmktf7Lsrml6zbh078Zing&index=2
20
Turbulence: Theory
- Kolmogorov theory of turbulence
- Energy flow starts from the outer scale and cascades
to smaller scale
- Act as small lenses
- Light beam of diameter bigger than the eddy would
refract and smaller than the eddy broadens the
beam; the net effect is a combination of the two
Energy injection
Energy transfer
Energy dissipation
Lo
lo
21
Beam wandering: Effects of
refractive index change
https://www.youtube.com/watch?v=bW6EcCcjFW0&index=4&list=PLKvrYlykYnYvXdpiffFtD2-jUrv7_2NJE
Laser Detector
Laser
Detector
LASER
LASER
DetectorDetector
a)
b)
Time
Lightbeampower
Lightbeampower
Time
Light beam Detector
(a)
Time
Lightbeampower
Lightbeampower
Time
Light beam Detector
(b)
Time
Lightbeampower
Lightbeampower
Time
Light beam
Detector
(a)
22
Beam wander: Small-scale
experiment
- To see how temperature gradient changes the beam
NIR
laserVIS
laser
Photo detectors
Time
Temperature
Beam wander: Small-scale
experiment implication
Amplitude = 0.0352* T
R² = 0.9825
0
5
10
15
20
0 100 200 300 400 500
Amplitude(cm)
Temp (oC)
DEVIATION FROM CENTRE OF THE DETECTOR VS HOT
PLATE SURFACE TEMPERATURE
23
- Linear relationship between temperature (gradient) and deviation from the detector
24
Beam wandering: Experiment goal
- The experiment was designed to test if adding a large collecting lens
would improve the signal
Light beam Detector
Light beam Detector
(a)
(b)
Light beam Detector
Light beam Detector
(a)
(b)
25
Beam wander: Experiment at the
Vertical Flow Reactor
Light beam
(VIS – NIR)
Detector movement
Front view
Collecting lens
Detector
(a)(b)
Plano convex lenses
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
- Mapping the intensity of laser received
at the detector
Light beam
Detector movement
Front view
Collecting lens
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
Light beam
(VIS – NIR)
Detector movement
Front view
Collec
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
Light beam
(VIS – NIR)
Detector movement
Front view
Co
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
Light beam
(VIS – NIR)
Detector movement
Front view
Collec
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
Light beam
(VIS – NIR)
Detector movement
Front view
Collec
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
Light beam
(VIS – NIR)
Detector movement
Front view
Collec
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
Light beam
Detector movement
Front view
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)
Light beam
(VIS – NIR)
Detector movement
Front view
Co
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
Light beam
(VIS – NIR)
Detector movement
Front view
Co
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
Light beam
(VIS – NIR)
Detector movement
Front view
Co
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
Light beam
(VIS – NIR)
Detector movement
Front view
(b)
Detector movement
Front view
2.5 cm
2.5 cm 2.5 cm
- 2.5 cm
(a)
Light beam
Detector movement
Front view
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (b)
Light beam
Detector movement
Front view
((b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a) (
Light beam
(VIS – NIR)
Detector movement
Front view
(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a)
Light beam
Detector movement
Front view
(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a)
Light beam
(VIS – NIR)
Detector movement
Front view
(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a)
Light beam
Detector movement
Front view
(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
- 2.5 cm
(a)
Detector movement
Front view
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)Detector movement
Front view
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)
Detector movement
Front view
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)Detector movement
Front view
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)
Detector movement
Front view
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)Detector movement
Front view
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)
Detector movement
Front view
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)Detector movement
Front view
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)
Detector movement
Front view
Collecting
(a)(b)
Detector movement
Front view
2.5 cm
5 cm 2.5 cm
(a) (b)Detector movement
Front view
Collect
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)Detector movement
Front view
Collecting lens
(a)(b)
Detector movement
Front view
2.5 cm
m 2.5 cm
(a) (b)Detector movement
Front view
Collecting l
(a)(b)
Detector movement
Front view
2.5 cm
- 2.5 cm 2.5 cm
(a) (b)Detector movement
Front view
Collecting lens
(a)(b)
Detector movement
Front view
2.5 cm
2.5 cm
(a) (b)Detector movement
Front view
Collecting lens
(a)(b)
Detector movement
Front view
2.5 cm
2.5 cm 2.5 cm
(a) (b)Detector movement
Front view
Collecting lens
(a)(b)
Detector movement
Front view
2.5 cm
2.5 cm
) (b)Detector movement
Front view
Collecting lens
(a)(b)
Detector movement
Front view
2.5 cm
cm 2.5 cm
(a) (b)
26
Beam wander: Near Infrared Laser
signal strength map on Vertical axes
0
0.2
0.4
0.6
0.8
1
1.2
1.4
1.6
-15 -10 -5 0 5 10 15
INTENSITY(V)
POSITION (MM)
NO HEAT - NO LENS HEATED - NO LENS
0
2
4
6
8
10
12
-6 -4 -2 0 2 4 6
INTENSITY(V)
POSITION (MM)
NO HEAT- WITH LENS HEATED - WITH LENS
Vertical axis – No lens Vertical axis – With lens
41 % drop
9 % drop
16 mm
6 mm
27
Beam wander: Near Infrared Laser
signal strength map on Horizontal
0
2
4
6
8
10
12
-12 -7 -2 3 8
Intensity(V)
Horizontal Position (mm)
NO HEAT - NO
LENS
NO HEAT- WITH
LENS
HEATED - NO
LENS
HEATED - WITH
LENS
Beam wander: Visible Laser signal
strength map on Horizontal axis
0
0.15
0.3
0.45
0.6
0.75
0.9
1.05
1.2
1.35
-8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8
Intensity(V)
Horizontal Position (mm)
NO HEAT - NO LENS
HEATED - NO LENS
HEATED - WITH LENS
28
Beam wander: Visible Laser signal
strength map on Vertical axis
0
0.15
0.3
0.45
0.6
0.75
0.9
1.05
1.2
1.35
-8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8
Intensity(V)
Vertical Position (mm)
NO HEAT - NO LENS
HEATED - NO LENS
HEATED - WITH LENS
29
30
Beam wander: Frequency of
occurrence - Method
- The “aperture” is fixed in position and the intensity of light inside the aperture is received
by the detector
http://www.pnas.org/content/111/34/12320.full
Beam wander: Frequency of
occurrence - Result
0000
25
75
0 0.00.00.00.0
34.2
60.7
4.7
0
25
50
75
100
1.4-1.51.3-1.41.2-1.31.1-1.21.0-1.10.9-10.8-0.9
PercentageofdatapointsinIntensitybin
Intensity (V)
VIS Source:Frequency of occurance
No Heat No Lens
Heated No Lens
Heated with Lens
31
- Adding the lens  Higher power and peak, narrower profile
Beam wander: Frequency of
occurrence - Result
- Adding the lens  Higher power and peak, narrower profile
0.000.000.000.000.000.000.000.000.000.000.00
37.25
59.80
2.94
0.00
0
20
40
60
80
100
NIR Source:Frequency of occurance
Mean centre data (NHNL)
Mean centre data (NHL)
Mean centre data (HNL)
Mean centre data (HL)
32
33
Conclusion
Large collecting lens, continuous
monitoring of the temperature in
the medium for modeling
(Reduce fluctuation and improve signal strength)
Current wavelengths are mainly
Infra red; limitation in terms of
the dust particles that exist in the
off-gas duct
Zolo-SCAN, LINDARC: Define a
Critical Path Length, need robust
system, high maintenance
Moving to a longer wavelengths;
THz is a possible solution
(Minimize the effects of scattering)
Stronger signal
at the detector
34
Suggestions for future work
Improvements
on this study
Model Experiment
35
Future work: Model
Adding Rayleigh
and Geometric
scattering to
improve dynamic
range for particle
sizes
Find an
experimental
relationship
between the
concentration and
light transmission
36
Future work: Experiment
Model the
conditions of
the turbulent
medium
Real –time
continuous
measurements of
the temperatures
inside the medium
Need improvement
in characterizing the
particle sizes and
distributions for the
scattering
predictions
37
Acknowledgments
- Dr.Zhenyou Wang (University of Toronto)
- Dr. Arathi Padmanabhan (University of Toronto)
- Prof.Murray Thomson (University of Toronto)
38
Questions
39
Background: Rayleigh scattering
- Responsible for blue sky
- Responsible for red sunset
- Preferential scattering
Rayleigh Scattering
• Particulate much smaller than wavelength
• RS ∝ 𝑑6
• RS ∝ λ−4
Scattering coefficient
- Responsible for blue sky
- Responsible for red sunset
- Preferential scattering
D-MIR D-NIR D-VIS
3.237212 1.480141 0.603516
0
2
4
6
1 1.2 1.4 1.6 1.8 2
SCATTERINGCOEFFICIENT
REFRACTIVE INDEX CHANGE FOR X=3
Scattering coefficient - x=2.5
Scattering coefficient - x=3
AVG
40

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Thesis Defense Amir

  • 1. Amirhossein (Amir) Alikhanzadeh Supervisor: Murray J. Thomson Combustion Research Laboratory, Department of Mechanical and Industrial Engineering University of Toronto, Toronto, Ontario, Canada Investigation of the effects of beam scattering and beam wandering on laser beams passing thorough the off-gas duct of an Electric Arc Furnace (EAF) Master of Applied Science Thesis Defense University of Toronto, Ontario December 10th , 2014
  • 2. Project Overview 2 TDL unable to penetrate EAF off –gas duct Beam scattering due to collision with dust particles Literature review - Model Rayleigh scattering Mie scattering Geometric scattering Experiment In lab Beam wandering due to turbulence and temperature gradient Experiment In lab Vertical Flow reactor (VFR)
  • 3. 3 Motivation : Steel industry - Uses primarily scrap steel - Lower energy consumption - Regulations on the emissions - 12 to 14 Billion $ sale in Canada (2012) - High production - Recycling rate of 40 % to 60 % in Canada (7 million tonnes recycled in 2012) - 7.5 % of industrial energy use BENCHMARKING ENERGY INTENSITY IN THE CANADIAN STEEL INDUSTRY (Prepared by Natural resources Canada) EAF 2002 Energy intensity indicator (MJ/tonnes of Hot Rolled Product)
  • 4. 4 Electric Arc Furnace – Process control - Heats charged material by means of electric arc - Consists of three holes plus a “fourth hole”  off-gas extraction - Off-gas temperature of around 1400 degrees Celsius Courtesy of Yuhui Sun [University of Toronto]
  • 5. 5 Objective: How important is this study? Zolo - SCAN - Zolo-SCAN - System developed for in-situ measurement - Difficulty getting the beam over the path length of the exhaust duct - Critical Path Length; two reasons
  • 6. 6 Objective: How important is this study? LINDARC - Based on TDLAS - Water cooled rod - Making readings at the centre - Reasons similar to Zolo-SCAN
  • 7. 7 Problems with the systems such as LINDARC and Zolo-SCAN Most of the issues come from having the rods: - Dust accumulation - Rod corrosion - Damage to the equipment because of molten steel - Bridging the gap (LINDARC) by means of molten steel High maintenance expenditure
  • 8. 8 Background: Light interaction with medium Light – medium interaction Attenuation (Loss) Absorption Scattering Rayleigh scattering Mie scattering Direction and shape Scintillation Beam wandering
  • 9. 9 Background: What is beam scattering? Light interaction with particles Reflection (Light deviated from its original path Refraction Diffraction Absorption (Absorbed and converted to heat) Reflection Refraction Diffraction Heat dissipation
  • 10. 10 Scattering model: Mie theory 0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0 0.5 1 1.5 2 2.5 3 3.5 Volumefraction Particle diameter (microns) Particle size distribution (Evans Group) S-A sample Dust sample - Mie Scattering • Particle size is comparable to the wavelength • Not heavily dependant on the wavelength change • Particle size parameter: 𝑥 = 𝜋𝑑 λ
  • 11. Scattering model: Literature validation Scattering coefficient in literature Scattering coefficient calculated with the model 11
  • 12. Scattering model: Model implications – Changing particle sizes and their distribution Constant scattering area - Total scattering area is kept the same while constituent particles are varied in size and subsequently concentration - The assumed particle sizes are 0.5,1,1.5,2,2.5 µm in diameter Concentration of 1.5 micron = 0 Concentration of 1.5 micron = 25 Concentration of 1.5 micons = 50 Concentration of 1.5 micons = 75 Concentration of 1.5 micons = 100 0 5E+09 1E+10 1.5E+10 2E+10 2.5E+10 0.5 1 1.5 2 2.5 0.00E+00 2.50E+09 5.00E+09 7.50E+09 1.00E+10 Numberofparticles/cubicmeter Particle size in microns 12
  • 13. Scattering model: Model implications – Effects of changing particle sizes and their distribution on light transmission 13 - How NIR transmission is affected when the wavelength is close to the dominant particle sizes 0.5 0.6 0.7 0.8 0.9 1 0 25 50 75 100 I/I0 Percentage of 1.5 micron particles Light transmission with change in particle size and concentration VIS - Transmission NIR- Transmission MIR- Transmission
  • 14. Scattering model: Model implications – Effect of refractive index 0.8 0.9 1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 LIGHTTRANSMISSION REFRACTIVE INDEX Light Transmission (VIS) Light Transmission (NIR) Light Transmission (MIR) 14
  • 15. 15 Scattering Experiment: Description/Purpose Vibration motors Different size sieve VIS source MIR source NIR sourceNIR detector VIS detector MIR detector Collecting foil Particles Vibration motor Sieve Particles 15 cm 25cm25cm25cm25cm
  • 16. 16 Scattering Experiment: Result - Model could not be fully verified with experiments - The experiment showed that model implications of less scattering at long wavelength is held - Although only qualitative measurements for mass, it can be seen that more particles means more attenuation of light 0 25 50 75 100 Talc - 4.4 g Talc - 7.8 g Al2O3 - 6.6 g Al2O3 - 5.6 g Attenuation Test ( Particles used - mass dropped in one minute) Light attenuation from particle scattering VIS - %Attenuation NIR - %Attenuation MIR - %Attenuation
  • 17. 17 Scattering model: Real particle sizes - Malvern Spraytec - Agglomeration of the particles is evident by comparison to Evans’ result Talc Aluminum oxide Jamie Loh [University of Toronto]
  • 18. 18 Scattering : Conclusions Particle size distribution Particle weight % distribution Particle refractive index Incident wavelength Predict how much beam is lost due to scattering
  • 19. 19 Beam wandering due to turbulence? Turbulence Time Steps - Varying Temperature, Density and Index of refraction through turbulence - Amplitude fluctuations  Signal fades - Beam Wandering (Steering) – Location movement - or Scintillation  Distorted beam shape https://www.youtube.com/watch?v=VEFEQUY-KNA&list=LLSmktf7Lsrml6zbh078Zing&index=2
  • 20. 20 Turbulence: Theory - Kolmogorov theory of turbulence - Energy flow starts from the outer scale and cascades to smaller scale - Act as small lenses - Light beam of diameter bigger than the eddy would refract and smaller than the eddy broadens the beam; the net effect is a combination of the two Energy injection Energy transfer Energy dissipation Lo lo
  • 21. 21 Beam wandering: Effects of refractive index change https://www.youtube.com/watch?v=bW6EcCcjFW0&index=4&list=PLKvrYlykYnYvXdpiffFtD2-jUrv7_2NJE Laser Detector Laser Detector LASER LASER DetectorDetector a) b) Time Lightbeampower Lightbeampower Time Light beam Detector (a) Time Lightbeampower Lightbeampower Time Light beam Detector (b) Time Lightbeampower Lightbeampower Time Light beam Detector (a)
  • 22. 22 Beam wander: Small-scale experiment - To see how temperature gradient changes the beam NIR laserVIS laser Photo detectors Time Temperature
  • 23. Beam wander: Small-scale experiment implication Amplitude = 0.0352* T R² = 0.9825 0 5 10 15 20 0 100 200 300 400 500 Amplitude(cm) Temp (oC) DEVIATION FROM CENTRE OF THE DETECTOR VS HOT PLATE SURFACE TEMPERATURE 23 - Linear relationship between temperature (gradient) and deviation from the detector
  • 24. 24 Beam wandering: Experiment goal - The experiment was designed to test if adding a large collecting lens would improve the signal Light beam Detector Light beam Detector (a) (b) Light beam Detector Light beam Detector (a) (b)
  • 25. 25 Beam wander: Experiment at the Vertical Flow Reactor Light beam (VIS – NIR) Detector movement Front view Collecting lens Detector (a)(b) Plano convex lenses Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) - Mapping the intensity of laser received at the detector Light beam Detector movement Front view Collecting lens (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) Light beam (VIS – NIR) Detector movement Front view Collec (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) Light beam (VIS – NIR) Detector movement Front view Co (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) Light beam (VIS – NIR) Detector movement Front view Collec (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) Light beam (VIS – NIR) Detector movement Front view Collec (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) Light beam (VIS – NIR) Detector movement Front view Collec (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) Light beam Detector movement Front view (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b) Light beam (VIS – NIR) Detector movement Front view Co (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) Light beam (VIS – NIR) Detector movement Front view Co (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) Light beam (VIS – NIR) Detector movement Front view Co (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) Light beam (VIS – NIR) Detector movement Front view (b) Detector movement Front view 2.5 cm 2.5 cm 2.5 cm - 2.5 cm (a) Light beam Detector movement Front view (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) (b) Light beam Detector movement Front view ((b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) ( Light beam (VIS – NIR) Detector movement Front view (b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) Light beam Detector movement Front view (b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) Light beam (VIS – NIR) Detector movement Front view (b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) Light beam Detector movement Front view (b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm - 2.5 cm (a) Detector movement Front view (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b)Detector movement Front view (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b) Detector movement Front view (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b)Detector movement Front view (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b) Detector movement Front view (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b)Detector movement Front view (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b) Detector movement Front view (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b)Detector movement Front view (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b) Detector movement Front view Collecting (a)(b) Detector movement Front view 2.5 cm 5 cm 2.5 cm (a) (b)Detector movement Front view Collect (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b)Detector movement Front view Collecting lens (a)(b) Detector movement Front view 2.5 cm m 2.5 cm (a) (b)Detector movement Front view Collecting l (a)(b) Detector movement Front view 2.5 cm - 2.5 cm 2.5 cm (a) (b)Detector movement Front view Collecting lens (a)(b) Detector movement Front view 2.5 cm 2.5 cm (a) (b)Detector movement Front view Collecting lens (a)(b) Detector movement Front view 2.5 cm 2.5 cm 2.5 cm (a) (b)Detector movement Front view Collecting lens (a)(b) Detector movement Front view 2.5 cm 2.5 cm ) (b)Detector movement Front view Collecting lens (a)(b) Detector movement Front view 2.5 cm cm 2.5 cm (a) (b)
  • 26. 26 Beam wander: Near Infrared Laser signal strength map on Vertical axes 0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 -15 -10 -5 0 5 10 15 INTENSITY(V) POSITION (MM) NO HEAT - NO LENS HEATED - NO LENS 0 2 4 6 8 10 12 -6 -4 -2 0 2 4 6 INTENSITY(V) POSITION (MM) NO HEAT- WITH LENS HEATED - WITH LENS Vertical axis – No lens Vertical axis – With lens 41 % drop 9 % drop 16 mm 6 mm
  • 27. 27 Beam wander: Near Infrared Laser signal strength map on Horizontal 0 2 4 6 8 10 12 -12 -7 -2 3 8 Intensity(V) Horizontal Position (mm) NO HEAT - NO LENS NO HEAT- WITH LENS HEATED - NO LENS HEATED - WITH LENS
  • 28. Beam wander: Visible Laser signal strength map on Horizontal axis 0 0.15 0.3 0.45 0.6 0.75 0.9 1.05 1.2 1.35 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 Intensity(V) Horizontal Position (mm) NO HEAT - NO LENS HEATED - NO LENS HEATED - WITH LENS 28
  • 29. Beam wander: Visible Laser signal strength map on Vertical axis 0 0.15 0.3 0.45 0.6 0.75 0.9 1.05 1.2 1.35 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 Intensity(V) Vertical Position (mm) NO HEAT - NO LENS HEATED - NO LENS HEATED - WITH LENS 29
  • 30. 30 Beam wander: Frequency of occurrence - Method - The “aperture” is fixed in position and the intensity of light inside the aperture is received by the detector http://www.pnas.org/content/111/34/12320.full
  • 31. Beam wander: Frequency of occurrence - Result 0000 25 75 0 0.00.00.00.0 34.2 60.7 4.7 0 25 50 75 100 1.4-1.51.3-1.41.2-1.31.1-1.21.0-1.10.9-10.8-0.9 PercentageofdatapointsinIntensitybin Intensity (V) VIS Source:Frequency of occurance No Heat No Lens Heated No Lens Heated with Lens 31 - Adding the lens  Higher power and peak, narrower profile
  • 32. Beam wander: Frequency of occurrence - Result - Adding the lens  Higher power and peak, narrower profile 0.000.000.000.000.000.000.000.000.000.000.00 37.25 59.80 2.94 0.00 0 20 40 60 80 100 NIR Source:Frequency of occurance Mean centre data (NHNL) Mean centre data (NHL) Mean centre data (HNL) Mean centre data (HL) 32
  • 33. 33 Conclusion Large collecting lens, continuous monitoring of the temperature in the medium for modeling (Reduce fluctuation and improve signal strength) Current wavelengths are mainly Infra red; limitation in terms of the dust particles that exist in the off-gas duct Zolo-SCAN, LINDARC: Define a Critical Path Length, need robust system, high maintenance Moving to a longer wavelengths; THz is a possible solution (Minimize the effects of scattering) Stronger signal at the detector
  • 34. 34 Suggestions for future work Improvements on this study Model Experiment
  • 35. 35 Future work: Model Adding Rayleigh and Geometric scattering to improve dynamic range for particle sizes Find an experimental relationship between the concentration and light transmission
  • 36. 36 Future work: Experiment Model the conditions of the turbulent medium Real –time continuous measurements of the temperatures inside the medium Need improvement in characterizing the particle sizes and distributions for the scattering predictions
  • 37. 37 Acknowledgments - Dr.Zhenyou Wang (University of Toronto) - Dr. Arathi Padmanabhan (University of Toronto) - Prof.Murray Thomson (University of Toronto)
  • 39. 39 Background: Rayleigh scattering - Responsible for blue sky - Responsible for red sunset - Preferential scattering Rayleigh Scattering • Particulate much smaller than wavelength • RS ∝ 𝑑6 • RS ∝ λ−4
  • 40. Scattering coefficient - Responsible for blue sky - Responsible for red sunset - Preferential scattering D-MIR D-NIR D-VIS 3.237212 1.480141 0.603516 0 2 4 6 1 1.2 1.4 1.6 1.8 2 SCATTERINGCOEFFICIENT REFRACTIVE INDEX CHANGE FOR X=3 Scattering coefficient - x=2.5 Scattering coefficient - x=3 AVG 40

Hinweis der Redaktion

  1. Reyleigh sigmas=f*e4*lambda0^4/6/pi/epsilon0^2/c^4*(1/lambda4) Moolecular =Absorption Aerosoles  scattering (has orders of magnitude less in numbers) but Mie is applied and the effect is bigger (coefficient) compared to rayleigh
  2. Attenuation coefficients depend on the dimension, chemical composition and the concentration of particles dispersed in the gasous medium. Assumed spherical and homogenous
  3. - Smoother if more orders of the Bessel function are used to generate the draph
  4. BY looking at the plot of Mie attenuation factor it can be said that for larger particles the scattering becomes less dependant on the wavelength and approaches 2 which means that for large enough particles, the attenuation cross section is equal to twice its geometrical cross section.
  5. BY looking at the plot of Mie attenuation factor it can be said that for larger particles the scattering becomes less dependant on the wavelength and approaches 2 which means that for large enough particles, the attenuation cross section is equal to twice its geometrical cross section.
  6. BY looking at the plot of Mie attenuation factor it can be said that for larger particles the scattering becomes less dependant on the wavelength and approaches 2 which means that for large enough particles, the attenuation cross section is equal to twice its geometrical cross section. Displays the importance of change in refractive index of the particles Aluminum oxide was chosen with refractive index of 1.7682 Dust particles from Dofasco have 2.01
  7. Beam spreading and wandering due to propagation through air pockets of varying Temperature, Density and Index of refraction Results in random phase and amplitude variations  Fading of the signal Lens like air pockets result in randomized interference in the warfront of the beam Is seen through beam Wandering (Steering) or Scintillation  Distorted beam shape Video: Experimental movie of laser beam changes due to atmospheric turbulence. The turbulence was "played" on a spatial light modulator and the resulting beam changes measured on a CCD. As the movie plays, so the strength of the turbulence is increasing. When the turbulence is very strong, one cannot see the original Gaussian beam any longer. Reference : https://www.youtube.com/watch?v=VEFEQUY-KNA&index=2&list=LLSmktf7Lsrml6zbh078Zing
  8. A well defined wave front will be distorted moving through a turbulent medium; scintillation, beam wander and broadening. (n-1)=79e-6 p/T (p in mili bars and T in Kelvin) , small pressure variations and their quick dispersion delta(n)=79e-6/(omega-1)*p/T^2*delta (T) and omega= cp/cv=1.4 for air. Given the temperature structure parameter, refractive index structure can be found: Cn=[79*10^-6p/T^2]CT and CT=Root(<(T1-T2)^2>)r^(-1/3). Typical values STRONG-INTERMEDIATE-WEAK (5e-7 == 4e-8 ==8e-9) If the beam diameter is larger than the all the turbuklence scale sizes, the turbules act like weak lenses that deflect the beam ina random way without changing its diameter. If not, diffraction and refraction happens and the beam profile is smeared out. A constantly changing pattern at the end of the turbulent path is formed. If a small detector is placed at the beam, the result is scintillation which is fluctuations in the light intensity. Video: https://www.youtube.com/watch?v=bW6EcCcjFW0&list=PLKvrYlykYnYvXdpiffFtD2-jUrv7_2NJE&index=4
  9. From : Single-shot stand-off chemical identification of powders using random Raman lasing He-Ne after propagating the full 400-m path length
  10. From : Single-shot stand-off chemical identification of powders using random Raman lasing He-Ne after propagating the full 400-m path length
  11. The model has limitations in terms of the particle sizes that can be input to the model Due to the same limitations in particles size parameter, the results of the model are only valid through far infrared region and cannot be used for longer wavelengths By adding Rayleigh theory and geometric theory to the model, the dynamic range is vastly improved The model assumes a linear relationship between the concentration of particles and the amount of light transmission; a more accurate relationship can be developed thorough experiments which improves the accuracy of the model; the assumption of linear relationship is valid for x~1 but for much higher concentrations may not be valid
  12. Needs improvement on the particle size and concentration measurement; Scattering Needs continuous measurements of temperature gradient of the medium to predict the laser beam behaviour; Beam Wandering
  13. Reyleigh sigmas=f*e4*lambda0^4/6/pi/epsilon0^2/c^4*(1/lambda4) Moolecular =Absorption Aerosoles  scattering (has orders of magnitude less in numbers) but Mie is applied and the effect is bigger (coefficient) compared to rayleigh
  14. Reyleigh sigmas=f*e4*lambda0^4/6/pi/epsilon0^2/c^4*(1/lambda4) Moolecular =Absorption Aerosoles  scattering (has orders of magnitude less in numbers) but Mie is applied and the effect is bigger (coefficient) compared to rayleigh