apex cfm-56 particle emissions: concentrations and … · november 8-10, 2004 - 1 apex workshop...
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November 8-10, 2004 - 1 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
APEX CFM-56 Particle Emissions: Concentrations and Size Distributions
Bruce Anderson, Eddie Winstead, Sandy Branham, Charles Hudgins, and Lee Thornhill
NASA Langley Research Center, Hampton, VA
November 8-10, 2004 - 2 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
LaRC Project Objectives
•Characterize commercial aircraft particle physical properties (number densities, size, mass and volatility) as a function of engine power
•Examine the impact of fuel sulfur upon secondary aerosol formation
•Investigate the relationship between fuel aromatic content and EC/OC emissions
•Observe the evolution of particle concentrations and characteristics as the exhaust plume ages
November 8-10, 2004 - 3 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
LaRC Instruments
LI-COR
CO2 System
Lag Chamber
PCASP
1 LPM To PUMP
Filter Stack
0 – 50 SLPM
PUMP
Metering Valve
Sol. Valve
Sol. Valve
ORIFICE ~.8 SLPM
P
P
Pump Exhaust
0 – 10 SLPM
Dryer HEPA
0 – 10 SLPM
Bypass Flow
PSAP
FM
FM
FM
FM
TSI 3022 FM
PCV
~500 torr
Filter
Heater TSI 3760
TSI 3760
Heater
D M A
FC
FC
TSI 3025A
TSI 3025A
November 8-10, 2004 - 4 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
Derived Aerosol Parameters
Number Emission Index NEI= (∆X/∆CO2) * EI[CO2] * Mair/(ρ * Mco2)
Geometric Mean Diameter
GMD = EXP{Σ ni* ln(Dpi)/Σ ni}
Geometric Standard Deviation σ
g = EXP{[Σ n
i * (ln(Dp
i) – ln(GMD))2]/(N-1)}0.5
November 8-10, 2004 - 6 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 2000 4000 6000 80000.00E+000
1.00E+014
2.00E+014
3.00E+014
4.00E+014
5.00E+014
7% Power
4% Power
CFM-56 Emissions
Nonv
olat
ile P
artic
le E
I (m
g/kg
)
Engine Run Time (sec)
Number EI: Run-time Dependence
November 8-10, 2004 - 7 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
10 100
0.0
0.1
0.2
0.3
0.4
0.5
100%65%
30%
7%
CFM-56 Emissions: 1 m Grand Average
dN
/dLo
g(Dp
)
Diameter (nm)
Particle Size Distribution at 1 m
November 8-10, 2004 - 8 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 1005
10
15
20
25
30
35
40
45
50
Engine Power (%)
CFM-56 Emissions: 1 and 10 m Data
Nonv
olat
ile G
MD
(nm
)
Geometric Mean of Size Distribution
November 8-10, 2004 - 9 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 100
0.8
1.0
1.2
1.4
1.6
1.8
2.0
Engine Power (%)
CFM-56 Emissions: 1 and 10 m Data
Aero
sol S
igm
a
Standard Deviation of Size Distribution
November 8-10, 2004 - 10 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 100
1E14
1E151 m Grand AverageCFM-56 Emissions
1 m
Nonv
olat
ile P
artic
le E
I (#/
kg)
Engine Power (%)
Number Emission Indices
November 8-10, 2004 - 11 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 100
1E14
1E15
30 m Grand Average
CFM-56 Emissions
Nonv
olat
ile P
artic
le E
I (#/
kg)
Engine Power (%)
Number Emission Indices
SUCCESS In-flight Average
November 8-10, 2004 - 12 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 100
1E14
1E151 meter Rake
CFM-56 Emissions
High Sulfur
High Aromatic
Lo Sulfur
Parti
cle E
I (#/
kg)
Engine Power (%)
Fuel Dependence of Emission Indices
November 8-10, 2004 - 13 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 100
1E14
1E15
10 meter Rake
CFM-56 Emissions
High Sulfur
High Aromatic
Lo Sulfur
Parti
cle E
I (#/
kg)
Engine Power (%)
Fuel Dependence of Emission Indices
November 8-10, 2004 - 14 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 100
1E15
1E16
30 meter Rake
CFM-56 Emissions
High Sulfur
High Aromatic
Lo Sulfur
Parti
cle E
I (#/
kg)
Engine Power (%)
Fuel Dependence of Emission Indices
November 8-10, 2004 - 15 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 100
1E14
1E15
1E16
1 m
CFM-56 Emissions
10 m
30 m
Hi Sulfur
Parti
cle E
I (#/
kg)
Engine Power (%)
Number EI: Age Dependence
November 8-10, 2004 - 16 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 1001E13
1E14
1E15
1E16
1 m
CFM-56 Emissions
10 m
30 m
Hi Aromatic
Parti
cle E
I (#/
kg)
Engine Power (%)
Number EI: Age Dependence
November 8-10, 2004 - 17 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 100
1E14
1E15
1E16
1 m
CFM-56 Emissions
10 m
30 m
Lo Sulfur
Parti
cle E
I (#/
kg)
Engine Power (%)
Number EI: Age Dependence
November 8-10, 2004 - 18 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 1001E14
1E15
1E16
Nonvolatile CN
Total CN
Lo Sulfur @ 30 meters
CFM-56 Emissions
Parti
cle E
I (#/
kg)
Engine Power (%)
Fractional Volatility of Emissions
November 8-10, 2004 - 19 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 100
1E14
1E15
1E16
Nonvolatile CN
Total CN
Hi Sulfur @ 30 metersCFM-56 Emissions
Parti
cle E
I (#/
kg)
Engine Power (%)
Fractional Volatility of Emissions
November 8-10, 2004 - 20 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
0 20 40 60 80 100
1E14
1E15
1E16
Nonvolatile CN
Total CN
Hi Aromatic @ 30 meters
CFM-56 Emissions
Parti
cle E
I (#/
kg)
Engine Power (%)
Fractional Volatility of Emissions
November 8-10, 2004 - 21 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
10 100
0
500
1000
1500
2000
2500
3000
3500
100%
65%
40%7%
CFM-56 Emissions: 30 m High Sulfur
dN
/dLo
g(Dp
)
Diameter (nm)
Particle Size Distributions at 30 m
November 8-10, 2004 - 22 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
10 100
0.01
0.1
1
10
100
1000
High Sulfur Fuel
10 m
1 m
30 m
CFM-56 Emissions: 7% Power
dN
/dLo
g(Dp
)
Diameter (nm)
Evolution of Size Distribution
November 8-10, 2004 - 23 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
10 100
0.01
0.1
1
10
100
1000
High Sulfur Fuel
10 m
1 m
30 m
CFM-56 Emissions: 40% Power
dN
/dLo
g(Dp
)
Diameter (nm)
Evolution of Size Distribution
November 8-10, 2004 - 24 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
10 100
0.01
0.1
1
10
High Sulfur Fuel
10 m
1 m
30 m
CFM-56 Emissions: 100% Power
dN
/dLo
g(Dp
)
Diameter (nm)
Evolution of Size Distribution
November 8-10, 2004 - 25 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC
Summary of Results
• CFM-56 engine emits 1014 to 1015 nonvolatile particles per kg fuel burned
• Soot particle emissions are highest just after engine start and decrease in time for a given power setting
• Soot particle number EIs generally increase with power
• Soot particle size (and mass) increases with power
• Secondary aerosol formation is dependent on fuel sulfur content
• Secondary aerosols are typically 10 times more abundant in aged plumes than primary aerosols