Nonintrusive optical measurements of aircraft engine exhaust emissions and comparison with standard intrusive techniques

被引:67
作者
Schäfer, K
Heland, J
Lister, DH
Wilson, CW
Howes, RJ
Falk, RS
Lindermeir, E
Birk, M
Wagner, G
Haschberger, P
Bernard, M
Legras, O
Wiesen, P
Kurtenbach, R
Brockmann, KJ
Kriesche, V
Hilton, M
Bishop, G
Clarke, R
Workman, J
Caola, M
Geatches, R
Burrows, R
Black, JD
Hervé, P
Vally, J
机构
[1] Fraunhofer Inst Atmosphar Umweltforsch, D-82467 Garmisch Partenkirchen, Germany
[2] Def Evaluat & Res Agcy, Propuls Dept, Pyestock GU14 0LS, Hants, England
[3] German Aerosp Ctr, Inst Optoelect, D-82230 Wesseling, Germany
[4] Auxitrol SA, Aerosp Equipment Div, F-18941 Bourges 9, France
[5] Berg Univ Wuppertal, Inst Phys Chem, D-42097 Wuppertal, Germany
[6] Univ Reading, JJ Thomson Phys Lab, Reading RG6 6AF, Berks, England
[7] British Aerosp PLC, Sowerby Res Ctr, Operat, Bristol BS12 7QW, Avon, England
[8] Rolls Royce PLC, Strateg Res Ctr, Derby DE24 8BJ, England
[9] Univ Paris 10, Lab Energy & Energy Econ, F-92410 Ville Davray, France
关键词
D O I
10.1364/AO.39.000441
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
Nonintrusive systems for the measurement on test rigs of aeroengine exhaust emissions required for engine certification (CO, NOx, total unburned hydrocarbon, and smoke), together with CO, and temperature have been developed. These results have been compared with current certified intrusive measurements on an engine test. A spectroscopic database and data-analysis software has been developed to enable Fourier-transform Infrared measurement of concentrations of molecular species. CO2, CO, and NO data showed agreement with intrusive techniques of approximately +/-30%. A narrow-band spectroscopic device was used to measure CO2 (with deviations of less than +/-10% from the intrusive measurement), whereas laser-induced incandescence was used to measure particles. Future improvements to allow for the commercial use of the nonintrusive systems have been identified and the methods are applicable to any measurement of combustion emissions. (C) 2000 Optical Society of America. OCIS codes: 010.0010, 280.0280, 300.0300.
引用
收藏
页码:441 / 455
页数:15
相关论文
共 37 条
[1]   Diode laser absorption sensors for gas-dynamic and combustion flows [J].
Allen, MG .
MEASUREMENT SCIENCE AND TECHNOLOGY, 1998, 9 (04) :545-562
[2]  
Andreev EP, 1998, J OPT TECHNOL+, V65, P895
[3]  
[Anonymous], 1986, FOURIER TRANSFORM IN, DOI DOI 10.1016/BS.AFNR.2016.12.008
[4]   SOOT-VISUALIZATION STRATEGIES USING LASER TECHNIQUES - LASER-INDUCED FLUORESCENCE IN C2 FROM LASER-VAPORIZED SOOT AND LASER-INDUCED SOOT INCANDESCENCE [J].
BENGTSSON, PE ;
ALDEN, M .
APPLIED PHYSICS B-LASERS AND OPTICS, 1995, 60 (01) :51-59
[5]  
BISHOP G, 1996, SIRUS POWERFUL INFRA
[6]  
BLACK JD, 1998, C P CP598 AGARD
[7]   European scientific assessment of the atmospheric effects of aircraft emissions [J].
Brasseur, GP ;
Cox, RA ;
Hauglustaine, D ;
Isaksen, I ;
Lelieveld, J ;
Lister, DH ;
Sausen, R ;
Schumann, U ;
Wahner, A ;
Wiesen, P .
ATMOSPHERIC ENVIRONMENT, 1998, 32 (13) :2329-2418
[8]   Soot mass concentration measurements in diesel engine exhaust using laser-induced incandescence [J].
Case, ME ;
Hofeldt, DL .
AEROSOL SCIENCE AND TECHNOLOGY, 1996, 25 (01) :46-60
[9]  
DASH SM, 1978, 3075 NASA AER RES AS
[10]  
Finlayson-Pitts B.J., 1986, Atmospheric Chemistry: Fundamentals and Experimental Techniques