Engine Performance and Certification Emissions Dan Bulzan, Changlie - - PowerPoint PPT Presentation

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Engine Performance and Certification Emissions Dan Bulzan, Changlie - - PowerPoint PPT Presentation

National Aeronautics and Space Administration Engine Performance and Certification Emissions Dan Bulzan, Changlie Wey, and Robert Howard NASA Glenn Research Center, ASRC Corporation, AEDC/ATA AAFEX II Workshop Jan 13, 2012 Nashville, TN


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SLIDE 1

National Aeronautics and Space Administration

www.nasa.gov

Engine Performance and Certification Emissions

Dan Bulzan, Changlie Wey, and Robert Howard NASA Glenn Research Center, ASRC Corporation, AEDC/ATA AAFEX II Workshop Jan 13, 2012 Nashville, TN

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SLIDE 2

National Aeronautics and Space Administration

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Engine Performance

  • CFM56-2C1 engines

– 22,000 lbs thrust – Bypass Ratio 6.0 – Overall PR 31

  • # 2(port) engine operated on JP-8 for

reference and E-31 testing

  • #3(starboard) engine operated on test fuels
  • N1, N2, Fuel flow rate, and exhaust

temperature recorded manually

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SLIDE 3

National Aeronautics and Space Administration

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Fuel Properties (Post-Test)

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Test JP-8 Tallow HRJ FT HRJ/JP-8 FT+THT Sulfur (ppm mass) 188 6 4 276 1083 Aromatics (% vol) 21.8 0.4 1.4 10.2 2.1 Initial Boiling Point (°C) 149 158 146 150 151 50% Recovered (°C) 201 209 177 204 177 End Point (°C) 268 254 226 263 224 Flash Point (°C) 46 52 43 46 43 Density @ 15°C (kg/L) 0.811 0.758 0.761 0.783 0.761 Freezing Point (°C) -47

  • 53
  • 49
  • 76
  • 54
  • 77

Viscosity @ -20°C (mm²/s) 4.1 4.9 3.7 4.3 3.2 Hydrogen Content (% mass) 13.5 15.3 15 14.4 15 Smoke Point 22 34 34 31 30 Net Heat of Combustion (MJ/kg) 42.8 43.6 43.8 43.3 43.8 Olefins (% vol) 0.7 0.2 1.6 0.6 1.5

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SLIDE 4

National Aeronautics and Space Administration

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AAFEX 1 & 2 Comparison, JP-8

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SLIDE 5

National Aeronautics and Space Administration

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Engine Performance

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SLIDE 6

National Aeronautics and Space Administration

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Engine Performance

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SLIDE 7

National Aeronautics and Space Administration

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Engine Performance

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SLIDE 8

National Aeronautics and Space Administration

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Engine Performance

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SLIDE 9

National Aeronautics and Space Administration

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Exhaust Gas Temperature

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SLIDE 10

National Aeronautics and Space Administration

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Left (#2) Engine Rake Right (#3) Engine Rake Gaseous Certification Emissions Sampling Rakes at 1 m Downstream

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SLIDE 11

National Aeronautics and Space Administration

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Right (#3) Rake showing mounted probes

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SLIDE 12

National Aeronautics and Space Administration

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NOx Emissions

12 1/3/2012

Fuel Flow Rate, lbm/hr

2000 4000 6000 8000 10000

EINOx (g/kg-fuel)

5 10 15 20 25 C C C C

FT2+THT HRJ Blend FT2 HRJ JP8 ICAO

C

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SLIDE 13

National Aeronautics and Space Administration

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NOx Emissions – HV Corrected

13 1/3/2012

Corrected Fuel Flow Rate, lbm/hr

2000 4000 6000 8000 10000

EINOx (g/kg-fuel)

5 10 15 20 25 C C C C

FT2+THT HRJ Blend FT2 HRJ JP8 ICAO

C

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SLIDE 14

National Aeronautics and Space Administration

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CO Emissions

14 1/3/2012

Fuel Flow Rate, lbm/hr

2000 4000 6000 8000 10000

EICO (g/kg-fuel)

20 40 60 80 100 120 C C C C

ICAO

C

JP8 HRJ FT2 HRJ Blend FT2+THT

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SLIDE 15

National Aeronautics and Space Administration

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CO Emissions – HV Corrected

15 1/3/2012

Corrected Fuel Flow Rate, lbm/hr

2000 4000 6000 8000 10000

EICO (g/kg-fuel)

20 40 60 80 100 120 C C C C

ICAO

C

JP8 HRJ FT2 HRJ Blend FT2+THT

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SLIDE 16

National Aeronautics and Space Administration

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Unburned Hydrocarbons

16 1/3/2012

Fuel Flow Rate, lbm/hr

2000 4000 6000 8000 10000

EIHC (g/kg-fuel)

5 10 15 20 25 C C C C

ICAO

C

JP8 HRJ FT2 HRJ Blend FT2+THT

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SLIDE 17

National Aeronautics and Space Administration

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Unburned Hydrocarbons – HV Corrected

17 1/3/2012

Corrected Fuel Flow Rate, lbm/hr

2000 4000 6000 8000 10000

EIHC (g/kg-fuel)

5 10 15 20 25 C C C C

ICAO

C

JP8 HRJ FT2 HRJ Blend FT2+THT

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SLIDE 18

National Aeronautics and Space Administration

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NOx Emissions

18 1/3/2012

N1, Corrected to Standard Day Condition

20 40 60 80 100

EINOx (g/kg-fuel)

5 10 15 20 25 C C C C

ICAO

C

JP8 HRJ FT2 HRJ Blend FT2+THT

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SLIDE 19

National Aeronautics and Space Administration

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CO Emissions

19 1/3/2012

N1, Corrected to Standard Day Condition

20 40 60 80 100

EICO (g/kg-fuel)

20 40 60 80 100 120 C C C C

ICAO

C

JP8 HRJ FT2 HRJ Blend FT2+THT

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SLIDE 20

National Aeronautics and Space Administration

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Unburned Hycrocarbon Emissions

20 1/3/2012

N1, Corrected to Standard Day Condition

20 40 60 80 100

EIHC (g/kg-fuel)

5 10 15 20 25 C C C C

ICAO

C

JP8 HRJ FT2 HRJ Blend FT2+THT

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SLIDE 21

National Aeronautics and Space Administration

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Combustion Efficiency

21 1/3/2012

N1, Corrected to Standard Day Condition

20 40 60 80 100

Combustion Efficiency, %

95 96 97 98 99 100

JP8 HRJ FT2 HRJ Blend FT2+THT

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SLIDE 22

National Aeronautics and Space Administration

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SO2 Emissions

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Fuel Flow, pph

1000 2000 3000 4000 5000 6000 7000 8000

EISO2 (g/kg-fuel)

1 2 3 4 5 HRJ FT 2 (Sasol) JP-8 HRJ Blend FT 2 + THT ICAO C

1/3/2012

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SLIDE 23

National Aeronautics and Space Administration

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CO Emissions – Low Power Conditions

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Ambient Temperature, F

40 50 60 70 80 90

EICO (g/kg-fuel)

20 40 60 80 100 120

Solid Symbol: 4% Open symbol: 7% JP8 HRJ FT2 HRJ Blend FT2+THT

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SLIDE 24

National Aeronautics and Space Administration

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Unburned Hydrocarbons – Low Power Conditions

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Ambient Temperature, F

40 50 60 70 80 90

EIHC (g/kg-fuel)

5 10 15 20 25

Solid Symbol: 4% Open symbol: 7% JP8 HRJ FT2 HRJ Blend FT2+THT

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SLIDE 25

National Aeronautics and Space Administration

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Conclusions

  • Negligible effect of fuel type on engine performance

when compared on mass measurement basis and corrected for heating value within the accuracy of the measurements

  • Slight reduction in NOx emissions at higher power

conditions for FT fuel

  • Scatter in CO and HC emissions at idle and sub idle

due more to temperature effects than fuel type

  • SO2 emissions correlated directly with Sulfur in the

fuel as expected

  • Some slight leakage under engine with neat HRJ and

F-T fuels

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SLIDE 26

National Aeronautics and Space Administration

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Acknowledgments

  • Jeffrey Braun (Air Force Certification Division) and

Tim Edwards (Air Force Research Laboratory) for providing the Alternative fuels for the experiments

  • NASA Dryden Aircraft Operations Facility Personnel

for their assistance in performing the testing.

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SLIDE 27

National Aeronautics and Space Administration

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Fuel Flow, pph

1000 2000 3000 4000 5000 6000 7000 8000

EINOx (g/kg-fuel)

5 10 15 20

C C C C

Engine #3 RG4 RG5 RP5 RG6 Rake =

  • 8
  • 4
  • 2
  • 10

ICAO

C

LG5 LG4 LG3 Engine #2

EINOx of JP8 Fuels (AAFEX vs. AAFEX-2)

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AAFEX-2 AAFEX

1/3/2012

Fuel flow, pph

2000 4000 6000 8000

EINOx (g/kg-fuel)

5 10 15 20 C C C C Rake -6 4 6 8

JP8, RG10 JP8, RG7 ICAO

C

JP8, LG6 JP8, GRC

Rake -6 -4

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SLIDE 28

National Aeronautics and Space Administration

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Fuel Flow, pph

1000 2000 3000 4000 5000 6000 7000 8000

EICO (g/kg-fuel)

20 40 60 80 100 120

C C C C Engine #3 RG4 RG5 RP5 RG6 Rake =

  • 8
  • 4
  • 2
  • 10

ICAO C LG5 LG4 LG3 Engine #2

EICO of JP8 Fuels (AAFEX vs. AAFEX-2)

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AAFEX-2 AAFEX

1/3/2012

Fuel flow, pph

2000 4000 6000 8000 10000

EICO (g/kg-fuel)

20 40 60 80 100 120 C C C C Rake -6 4 6 8

JP8, RG10 JP8, RG7 ICAO

C

JP8, LG6 JP8, GRC

Rake -6 -4

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SLIDE 29

National Aeronautics and Space Administration

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Fuel Flow, pph

1000 2000 3000 4000 5000 6000 7000 8000

EIHC (g/kg-fuel)

5 10 15 20 25

C C C C

Engine #3 RG4 RG5 RP5 RG6 Rake =

  • 8
  • 4
  • 2
  • 10

ICAO

C

LG5 LG4 LG3 Engine #2

EIHC of JP8 Fuels (AAFEX vs. AAFEX-2)

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AAFEX-2 AAFEX

1/3/2012

Fuel flow, pph

2000 4000 6000 8000 10000

EIHC (g/kg-fuel)

5 10 15 20 25 C C C C Rake -6 4 6 8

JP8, RG10 JP8, RG7 ICAO

C

JP8, LG6 JP8, GRC

Rake -6 -4