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

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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 - 5 APEX Workshop Cleveland, Ohio Bruce Anderson, NASA LaRC

Home, Sweet Home

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