Effects of engine aging on aircraft no emissions

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1997, Pages

  Lukachko, Stephen P ^a   Waltz, Ian A ^a  

^a MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; COMBUSTORS; ENGINES; FIGHTER AIRCRAFT; MARINE ENGINES; SUPERSONIC AIRCRAFT;

ADVANCED TECHNOLOGY; AGING EFFECTS; AIRCRAFT EMISSIONS; COMPONENT EFFICIENCIES; EMPIRICAL CORRELATIONS; FLOW CAPACITY; FLOW PARAMETERS; SPECIFIC FUEL CONSUMPTION;

GAS TURBINES;

EID: 84973616529     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-386     Document Type: Conference Paper

References (38)

1. 43 FR 58, EPA, "Control of Air Pollution From Aircraft and Aircraft Engines: Proposed Amendments to Standards, " Federal Register, pp. 12615-12634, 1978.
2. 47 FR 251, EPA, "Emissions Standards and Test Procedures, " Federal Register, pp. 58461-58474, 1982.
3. 55 FR 155, DOT, "Fuel Venting and Exhaust Emission Requirements for Turbine Engine Powered Airplanes: Final Rule, " Federal Register, pp. 32856-32866, 1990.
4. Aker, G.F. and H.I.H. Saravanamuttoo, "Predicting Gas Turbine Performance Degradation Due to Compressor Fouling Using Computer Simulation Techniques, " Transactions of the ASME: Journal of Engineering for Gas Turbines and Power, Vol. 111, pp. 343-350, 1989.
5. Arnold, B.R. and J.R. Gast, "A Cooperative Airline Program to Evaluate Engine Parts Aging Effects on a Current Turbofan Engine Model, " SAE Paper 700329, pp. 1032-1041, 1970.
6. Becker, RE., G. Frings, and WC. Cavage, "Exhaust Emissions Characteristics and Variability for Pratt and Whitney JT8D- 7A Gas Turbine Engines Subjected to Major Overhaul and Repair: Final Report, " FAA-CT-79-53, 1980.
7. The Boeing Company, Martin, R.L., "Appendix D. Boeing Method 2 Fuel Flow Methodology Description, " presented to the CAM) Working Group HI Certification Subgroup, 1995.
8. Dupis, RJ., H.I.H. Saravanamuttoo, and D.M. Rudnitski, "Modelling of Component Faults in Application to On-Condition Health Monitoring, " ASME 86-GT-153, presented at the International Gas Turbine Conference and Exhibit, Dusseldorf, W. Germany, 1986.
9. Frings, G., "Exhaust Emission Characteristics and Variability for Maintained General Electric CF6-50 Turbofan Engines, " FAA Report No. FAA-CT-80-36, Final Report, 1980.
10. Frith, P.C., 'Diagnosis of Compressor Degradation in Helicopter Engines, " 5th Australian Aeronautical Conference, Melbourne, Australia, 1993.
11. General Electric, GE: The Leading Edge, manufacturer's literature, 1992.
12. Gleason, C.C., and Bahr, D.W., "NASA Experimental Clean Combustor Program (ECCP), " NASA CR-135-384, 1979.
13. Harbrard, A., "The Variable-Cycle Engine to Meet the Economic and Environmental Challenge of the Future Supersonic Transport Aircraft, " Revue Scientifique SNECMA, No. 1, 1990.
14. ICAO, International Civil Aviation Organization, ICAO Engine Exhaust Emissions Data Bank, ICAO Doc 9646-AN/943, 1st ed., 1995.
15. ICAO, International Civil Aviation Organization, International Standards and Recommended Practices: Environmental Protection, Annex 16 to the Convention on International Civil Aviation, Volume II: Aircraft Emissions, 2nd ed., 1993.
16. Kurzke, J., "GASTURB Version 6.0: A Program to Calculate Design and Off-Design Performance of Gas Turbines, " 1995.
17. Lakshminarasimha, A.N., and HJ.H. Saravanamuttoo, "Prediction of Fouled Compressor Performance Using Stage Stacking Techniques, " ASME Symposium on Turbornachinery Performance Deterioration, FED-Vol. 37, 1986.
18. Liebeck, R.H. et al., "Advanced Subsonic Design and Economic Studies, " NASA CR- 195443, 1995.
19. Lulcachlco, S.P., I.A. Waltz, R.C. Mialce-Lye, R.C. Brown, and M.R. Anderson, "Chemical Processes in the Turbine and Exhaust Nozzle, " presented at Comite Avion Ozone Impact of Aircraft upon the Atmosphere International Colloquium, Paris, 1996.
20. Lyon, T.F. and D.W. Bahr, "CF6-50 Engine Emissions Testing with Traverse Probe, " FAA Report No. FAA-CT-81-18, conducted by General Electric Company, Aircraft Engine Business Group, Final Report, 1981.
21. Lyon, T.F., W.J. Dodds, and D.W. Bahr, "Determination of Pollutant Emissions Characteristics of General Electric CF6-6 and CF6-50 Model Engines, Final Report, " FAA-EE-80-27, 1980.
22. Maclssac, B.D., "Engine Performance and Heaxth Monitoring Models using Steady State and Transient Prediction Methods." in Steady and Transient Performance Prediction of Gas Turbine Engines, NATO, AGARD-LS-183, 1992.
23. Mattingly, J.D., Elements of Gas Turbine Propulsion, McGraw-Hill, 1996.
24. NASA/ICAO, NASA/ICAO Database - Research on Atmospheric Effects of Aviation, maintained by H. Wesoky, 1996.
25. Platt, M. and ER. Norster, 'Time Degradation Factors for Turbine Engine Exhaust Emissions: Volume I, Program Description and Results, Interim Report, " FAA-RD-78-56 or N79-17860, 1978.
26. Platt, M. and ER. Norster, "Time Degradation Factors for Turbine Engine Exhaust Emissions: Volume 1, Program Description and Results, Final Report, " FAA-RD-79-8, 1979.
27. Prather, Mi. et al., The Atmospheric Effects of Strwospheric Aircraft: A First Program Report, NASA Reference Publication 1272, NASA Office of Space Science and Applications, Washington, DC, 1992.
28. Richardson, J.H., G.P. Sallee, and F.K Smalcula, "Causes of High Pressure Compressor Deterioration in Service, " AIAA/SAE, ASME 15th Joint Propulsion Conference, AIAA 79-1234, Las Vegas, Nevada, 1979.
29. Roffe, G., and KS. Venkataramani, "Emission Measurements for a Lean Premixed Propane/Air System at Pressures up to 30 Atmospheres", NASA CR- 159421, 1978.
30. Saravanamuttoo, H.I.H., and A.N. Lalcsluninarasimha, "A Preliminary Assessment of Compressor Fouling, " ASME 85-GT- 153, Gas Turbine Conference and Exhibit, Houston, Texas, 1985.
31. Saravanamuttoo, H.I.H., and B.D. MacIsaac, "Thermodynamic Models for Pipeline Gas Turbine Diagnostics, " Transactions of the ASME: Journal of Engineering for Power, Vol. 105, pp. 875-884, 1983.
32. Schumann, U., ed., AERONOX: The Impact of NOx Emissions from Aircraft Upon the Atmosphere at Flight Altitudes 8-15 km: Final Report to the Commission of European Communities, Brussels, Belgium, EC-DLR, 1995.
33. Singh, D., A. flamed, and W. Tabakoff, "Simulation of Performance Deterioration in Eroded Compressors, " ASME 96-GT- 422, 1996.
34. Stevenson, J.D. and H.I.H. Saravanamuttoo, "Effect of Cycle Choice and Deterioration on Thrust Indicators for Civil Engines, " ISABE 95-7077, in Twelfth International Symposium on Air Breathing Engines, ed. F.S. Billig, Vol. 2, Melbourne, Australia, 1995.
35. Stolarsld, KS., and H.L. Wesoky (eds.), The Atmospheric Effects of Stratospheric Aircraft A Third Program Report, NASA Reference Publication 1313, NASA Office of Space Science and Applications, Washington, DC, 1993.
36. Treager, I.E., Aircraft Gas Turbine Engine Technology, 2nd Ed., McGraw-Hill, 1979.
37. Urban, L.A., 'Parameter Selection for Multiple Fault Diagnostics of Gas Turbine Engines, " AGARD-CP-165, 1974.
38. Wulf, Ray H., "Engine Diagnostics Program: CF6-50 Engine Performance Deterioration, " NASA CR-159867, conducted by the General Electric Company, Aircraft Engine Business Group, 1980.