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Environmentally-Neutral Aircraft 
Propulsion Using Low 
Temperature Plasma 
John Leylegian, Jason Tyll, and Wallace Chinitz 
GASL, Inc. 
Ronkonkoma, NY 11779 
NIAC Annual Meeting - June 6, 2000
Motivation 
• NOx 
formation is a consequence of the 
combustion of various fuels. 
• Nitric oxide (NO): 
• Quickly forms nitrogen dioxide (NO2), a 
respiratory irritant. 
• Active participant in photochemical smog 
formation.
Motivation (2) 
• Current methods of NOx reduction involve 
catalysts used either alone (e.g. Rh), or in an 
atmosphere containing hydrocarbons (e.g. 
Cu or Fe). 
• Rhodium is too expensive for widespread 
use, and extra hydrocarbons in fuel exhaust 
are undesirable.
Objective 
• To reduce NOx in turbojet emissions by an 
order of magnitude using a low-temperature 
plasma. 
• “Low-temperature plasma” implies plasma 
excitation temperatures in the range of 3000 
to 5500 K.
Previous Work 
• Luo et al. (J. Phys. Chem. A 102:7954, 
1998) decomposed NO in He using a low-temperature 
plasma at atmospheric pressure. 
• The degree of NO destruction is a function 
of initial NO concentration, residence time, 
input voltage, and additives.
Additive Effects on NO 
Reduction from Previous Work 
• CO2 
and H2O inhibited the destruction of 
NO. 
• CO, O2, C2H6, and other carbon species 
accelerated the destruction of NO.
Extending This Concept to the 
Turbojet Engine 
(Could it still work?) 
• Higher temperatures (up to 1700 K) 
• Higher pressures (up to 40 atm) 
• Shorter residence times (~0.1 s) 
• Presence of different species (O2, N2, CO2, 
H2O)
Turbojet Engine 
1. Air is compressed and heated in diffuser/compressor 
2. Fuel mixed in and burned in combustor 
3. Partially expanded in turbine to provide power for 
compressor 
4. Expansion continues through nozzle, generating thrust
Proposed Work 
• Perform experiments similar to those of Luo 
et al., using the products of hydrocarbon 
combustion, at conditions similar to those 
encountered in a turbojet engine.
Program Outline
Rig Schematic
Estimation of NO Levels 
in Jet Exhaust 
• Variation of NO in ethylene/air products with 
equivalence ratio: 
0.008 
0.006 
0.004 
0.002 
0.000 
0.3 0.4 0.5 0.6 
Equivalence Ratio 
Mole Fraction NO 
1 atm 
5 atm 
10 atm 
20 atm 
40 atm
Estimation of NO Levels 
in Jet Exhaust 
• Equilibrium temperatures of ethylene/air mixtures: 
1800 
1600 
1400 
1200 
1000 
0.3 0.4 0.5 0.6 
Equivalence Ratio 
Adiabatic Flame 
Temperature (K) 
1 atm 
5 atm 
10 atm 
20 atm 
40 atm
Estimation of NO Levels 
in Jet Exhaust 
• Variation of NO in ethylene/air products with 
temperature: 
0.004 
0.003 
0.002 
0.001 
0.000 
1000 1200 1400 1600 1800 
Flame Temperature (K) 
Mole Fraction NO 
1 atm 
5 atm 
10 atm 
20 atm 
40 atm
Determination of Power 
Requirements (1) 
Rate constant for overall reaction: 
NO → ½N2 + ½O2 
converted to Arrhenius form: k = A T 0.75 
where A is a function of the input power.
Determination of Power 
Requirements (2) 
Using the power-rate constant data of Luo et 
al. and the LSENS code, the power required 
for an order-of-magnitude reduction in NO 
mole fraction can be determined: 
P (W) = 4.868 XNO 
–1.0196 
For XNO = 0.002, P = 2.75 kW
Power Sources 
• Fuel Cells: Automotive PEM fuel cells 
available up to 20 kW (if DC is required) 
• Fuel Cell + Inverter (if AC is required) 
• Turbine
Summary 
• Oxides of nitrogen, produced by fossil fuel 
combustion, are environmental and health 
hazards. 
• Use of plasmas to reduce NO levels is a 
clean and inexpensive method. 
• A plasma generator is being designed to test 
this method on hydrocarbon-air combustion 
products at high temperature and pressure.

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Environmentally neutralpropulsion

  • 1. Environmentally-Neutral Aircraft Propulsion Using Low Temperature Plasma John Leylegian, Jason Tyll, and Wallace Chinitz GASL, Inc. Ronkonkoma, NY 11779 NIAC Annual Meeting - June 6, 2000
  • 2. Motivation • NOx formation is a consequence of the combustion of various fuels. • Nitric oxide (NO): • Quickly forms nitrogen dioxide (NO2), a respiratory irritant. • Active participant in photochemical smog formation.
  • 3. Motivation (2) • Current methods of NOx reduction involve catalysts used either alone (e.g. Rh), or in an atmosphere containing hydrocarbons (e.g. Cu or Fe). • Rhodium is too expensive for widespread use, and extra hydrocarbons in fuel exhaust are undesirable.
  • 4. Objective • To reduce NOx in turbojet emissions by an order of magnitude using a low-temperature plasma. • “Low-temperature plasma” implies plasma excitation temperatures in the range of 3000 to 5500 K.
  • 5. Previous Work • Luo et al. (J. Phys. Chem. A 102:7954, 1998) decomposed NO in He using a low-temperature plasma at atmospheric pressure. • The degree of NO destruction is a function of initial NO concentration, residence time, input voltage, and additives.
  • 6. Additive Effects on NO Reduction from Previous Work • CO2 and H2O inhibited the destruction of NO. • CO, O2, C2H6, and other carbon species accelerated the destruction of NO.
  • 7. Extending This Concept to the Turbojet Engine (Could it still work?) • Higher temperatures (up to 1700 K) • Higher pressures (up to 40 atm) • Shorter residence times (~0.1 s) • Presence of different species (O2, N2, CO2, H2O)
  • 8. Turbojet Engine 1. Air is compressed and heated in diffuser/compressor 2. Fuel mixed in and burned in combustor 3. Partially expanded in turbine to provide power for compressor 4. Expansion continues through nozzle, generating thrust
  • 9. Proposed Work • Perform experiments similar to those of Luo et al., using the products of hydrocarbon combustion, at conditions similar to those encountered in a turbojet engine.
  • 12. Estimation of NO Levels in Jet Exhaust • Variation of NO in ethylene/air products with equivalence ratio: 0.008 0.006 0.004 0.002 0.000 0.3 0.4 0.5 0.6 Equivalence Ratio Mole Fraction NO 1 atm 5 atm 10 atm 20 atm 40 atm
  • 13. Estimation of NO Levels in Jet Exhaust • Equilibrium temperatures of ethylene/air mixtures: 1800 1600 1400 1200 1000 0.3 0.4 0.5 0.6 Equivalence Ratio Adiabatic Flame Temperature (K) 1 atm 5 atm 10 atm 20 atm 40 atm
  • 14. Estimation of NO Levels in Jet Exhaust • Variation of NO in ethylene/air products with temperature: 0.004 0.003 0.002 0.001 0.000 1000 1200 1400 1600 1800 Flame Temperature (K) Mole Fraction NO 1 atm 5 atm 10 atm 20 atm 40 atm
  • 15. Determination of Power Requirements (1) Rate constant for overall reaction: NO → ½N2 + ½O2 converted to Arrhenius form: k = A T 0.75 where A is a function of the input power.
  • 16. Determination of Power Requirements (2) Using the power-rate constant data of Luo et al. and the LSENS code, the power required for an order-of-magnitude reduction in NO mole fraction can be determined: P (W) = 4.868 XNO –1.0196 For XNO = 0.002, P = 2.75 kW
  • 17. Power Sources • Fuel Cells: Automotive PEM fuel cells available up to 20 kW (if DC is required) • Fuel Cell + Inverter (if AC is required) • Turbine
  • 18. Summary • Oxides of nitrogen, produced by fossil fuel combustion, are environmental and health hazards. • Use of plasmas to reduce NO levels is a clean and inexpensive method. • A plasma generator is being designed to test this method on hydrocarbon-air combustion products at high temperature and pressure.