Gas Turbine Engine Emissions—Part I: Volatile Organic Compounds and Nitrogen OxidesSource: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 006::page 61504Author:Michael T. Timko
,
W. Berk Knighton
,
Scott C. Herndon
,
Ezra C. Wood
,
Timothy B. Onasch
,
Megan J. Northway
,
John T. Jayne
,
Manjula R. Canagaratna
,
Richard C. Miake-Lye
DOI: 10.1115/1.4000131Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The potential human health and environmental impacts of aircraft gas turbine engine emissions during normal airport operation are issues of growing concern. During the JETS/Aircraft Particle Emissions eXperiment(APEX)-2 and APEX-3 field campaigns, we performed an extensive series of gas phase and particulate emissions measurements of on-wing gas turbine engines. In all, nine different CFM56 style engines (including both CFM56-3B1 and -7B22 models) and seven additional engines (two RB211-535E4-B engines, three AE3007 engines, one PW4158, and one CJ6108A) were studied to evaluate engine-to-engine variability. Specific gas-phase measurements include NO2, NO, and total NOx, HCHO, C2H4, CO, and a range of volatile organic compounds (e.g., benzene, styrene, toluene, naphthalene). A number of broad conclusions can be made based on the gas-phase data set: (1) field measurements of gas-phase emission indices (EIs) are generally consistent with ICAO certification values; (2) speciation of gas phase NOx between NO and NO2 is reproducible for different engine types and favors NO2 at low power (and low fuel flow rate) and NO at high power (high fuel flow rate); (3) emission indices of gas-phase organic compounds and CO decrease rapidly with increasing fuel flow rate; (4) plotting EI-CO or volatile organic compound EIs against fuel flow rate collapses much of the variability between the different engines, with one exception (AE3007); (5) HCHO, ethylene, acetaldehyde, and propene are the most abundant volatile organic compounds present in the exhaust gases that we can detect, independent of engine technology differences. Empirical correlations accurate to within 30% and based on the publicly available engine parameters are presented for estimating EI-NOx and EI-NO2. Engine-to-engine variability, unavailability of combustor input conditions, changing ambient temperatures, and complex reaction dynamics limit the accuracy of global correlations for CO or volatile organic compound EIs.
keyword(s): Engines , Organic compounds , Emissions , Electrochemical impedance spectroscopy , Fuels , Nitrogen oxides , Flow (Dynamics) , Measurement , Exhaust systems AND Gas turbines ,
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| contributor author | Michael T. Timko | |
| contributor author | W. Berk Knighton | |
| contributor author | Scott C. Herndon | |
| contributor author | Ezra C. Wood | |
| contributor author | Timothy B. Onasch | |
| contributor author | Megan J. Northway | |
| contributor author | John T. Jayne | |
| contributor author | Manjula R. Canagaratna | |
| contributor author | Richard C. Miake-Lye | |
| date accessioned | 2017-05-09T00:37:40Z | |
| date available | 2017-05-09T00:37:40Z | |
| date copyright | June, 2010 | |
| date issued | 2010 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-27116#061504_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/143175 | |
| description abstract | The potential human health and environmental impacts of aircraft gas turbine engine emissions during normal airport operation are issues of growing concern. During the JETS/Aircraft Particle Emissions eXperiment(APEX)-2 and APEX-3 field campaigns, we performed an extensive series of gas phase and particulate emissions measurements of on-wing gas turbine engines. In all, nine different CFM56 style engines (including both CFM56-3B1 and -7B22 models) and seven additional engines (two RB211-535E4-B engines, three AE3007 engines, one PW4158, and one CJ6108A) were studied to evaluate engine-to-engine variability. Specific gas-phase measurements include NO2, NO, and total NOx, HCHO, C2H4, CO, and a range of volatile organic compounds (e.g., benzene, styrene, toluene, naphthalene). A number of broad conclusions can be made based on the gas-phase data set: (1) field measurements of gas-phase emission indices (EIs) are generally consistent with ICAO certification values; (2) speciation of gas phase NOx between NO and NO2 is reproducible for different engine types and favors NO2 at low power (and low fuel flow rate) and NO at high power (high fuel flow rate); (3) emission indices of gas-phase organic compounds and CO decrease rapidly with increasing fuel flow rate; (4) plotting EI-CO or volatile organic compound EIs against fuel flow rate collapses much of the variability between the different engines, with one exception (AE3007); (5) HCHO, ethylene, acetaldehyde, and propene are the most abundant volatile organic compounds present in the exhaust gases that we can detect, independent of engine technology differences. Empirical correlations accurate to within 30% and based on the publicly available engine parameters are presented for estimating EI-NOx and EI-NO2. Engine-to-engine variability, unavailability of combustor input conditions, changing ambient temperatures, and complex reaction dynamics limit the accuracy of global correlations for CO or volatile organic compound EIs. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Gas Turbine Engine Emissions—Part I: Volatile Organic Compounds and Nitrogen Oxides | |
| type | Journal Paper | |
| journal volume | 132 | |
| journal issue | 6 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4000131 | |
| journal fristpage | 61504 | |
| identifier eissn | 0742-4795 | |
| keywords | Engines | |
| keywords | Organic compounds | |
| keywords | Emissions | |
| keywords | Electrochemical impedance spectroscopy | |
| keywords | Fuels | |
| keywords | Nitrogen oxides | |
| keywords | Flow (Dynamics) | |
| keywords | Measurement | |
| keywords | Exhaust systems AND Gas turbines | |
| tree | Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 006 | |
| contenttype | Fulltext |