1、 ICAO 964b-AN/943 * m 4843436 0063925 27T m Doc =-ANI943 ICAO ENGINE .EXHAUST EMISSIONS DATA BANK FIRST EDITION - 1995 Approved by the Secretary Genera and published under his authority INTERNATIONAL CIVIL AVIATION ORGANIZATION Copyright International Civil Aviation Organization Provided by IHS unde
2、r license with ICAONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ICAO 9646-AN/943 * 484L4Lb ClOb3926 Lob = Published in separate English, French, Russian and Spanish editions by the Intemational Civil Aviation Organization. All correspondence, except orders and s
3、ubscriptions, should be addressed to the Secretary General. Orders for this publication should be sent to one of the following addresses, together with the appropriate remittance (by bank draft, cheque or money order) in U.S. dollars or the currency of the country in which the order is placed. Docum
4、ent Sales Unit International Civil Aviation Organization 1000 Sherbrooke Street West, Suite 400 Montreal, Quebec Canada H3A 2R2 Tel.: (514) 285-8022 Telex: 05-2451 3 Sitatex: YULCAYA Fa: (514) 285-6769 Credit card orders (Visa or American Express only) are accepted at the above address. Egypr. ICAO
5、Representative, Middle East Office, 9 Shagaret El Dorr Street, Zamalek 1121 1, Cairo. France. Reprsentant de IOACI, Bureau Europe et Atlantique Nord, 3 bis, villa mile-Bergerat, India. Oxford Book and Stationery Co., Scindia House, New Delhi 1 loo01 92522 Neuilly-sur-Seine (Cedex). or 17 Park Street
6、, Calcutta 700016. The English Book Store, 17-L Connaught Circus, New Delhi 1 1 0001. Japan. Japan Civil Aviation Promotion Foundation, 15-1 2, 1-chome, Toranomon, MinateKu, Tokyo. Kenya. ICAO Representative, Eastern and Southern African Office, United Nations Accommodation, Mexico. Representante de
7、 la OACI, Oficina Norteamrica, Centroamrica y Caribe, Peru. Representante de la OACI, Oficina Sudamrica, Apartado 4127, Lima 100. Senegal. Reprsentant de IOACI, Bureau Afrique occidentale et centrale, Bote postale 2356, Dakar. Spain. A.E.N.A. - Aeropuertos Espaoles y Navegacin Area, Calle Juan Ignac
8、io Luca de Tena, 14, Thailand. ICAO Representative, Asia and Pacific Office, P.O. Box 1 1, Samyaek Ladprao, Bangkok 10901. United Kingdom. Civil Aviation Authority, Printing and Publications Services, Greville House, P.O. Box 46294, Nairobi. Apartado postal 5-377, C.P. 06500, Mxico, D.F. Planta Terc
9、era, Despacho 3. 11, 28027 Madrid. 37 Gratton Road, Cheltenham, Clos., GL50 2BN. 11/84 The Catalogue of ICAO Publications and Audio Visual Training Aids Issued annually, the Catalogue lists all publications and audio visual training aids currently available. Morlthly supplements announce new pu blic
10、ations and audio visual training aids, amendments, supplements, reprints, etc. Available free from the Document Sales Unit, ICAO Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for ResaleNo reproduction or networking permitted without license from IHS-,
11、-,-ICAO 9b4b-AN/943 * m 44343b 0063927 042 ICAO Engine Exhaust Emissions Data Bank Doc % i.e.: a) The DJFm values are based on an idealized LTO cycle in ISA conditions. In assessing, for example, total aircraft emissions at a specific airport, consideration must be given to the appropriateness of th
12、e prescribed thrusts, the times in mode and the reference conditions. b) The LTO cycle only assesses the emissions below 915 m (3 o00 ft) and therefore may not be a good guide for comparing the emissions of different engines in other ight modes, e.g. cruise. REVISION OF DATA The data bank will be re
13、vised and reissued on a regular basis. New data will be included for: a) engines certificated since the last issue of the data bank; b) engines already certificated for which data were not previously available; or c) engines already certificated and listed in the data bank for which: 1) emissions da
14、ta have been recalculated as a result of a better definition of engine performance characteristics with continuing production of an engine type; . 2) component design changes have been introduced which affect the emissions levels, e.g. new combustor design; or 3) improvements in emissions measuremen
15、t techniques have resulted in changes to their emissions data. New data and comments should be submitted to: International Civil Aviation Organization OperationdAirworthiness Section loo0 Sherbrooke Street West Montreal, Quebec Canada H3A 2R2 Copyright International Civil Aviation Organization Provi
16、ded by IHS under license with ICAONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ICA0 9b4b-AN/943 * 484L4Lb 0063734 282 Combustor type Data type INDEX OF ENGINES KEY The combustor type is only shown where there is an option on a particular engine. P C Indicates ce
17、rtification data. R Indicates data generated prior to the introduction of regulations. Indicates data revised by the manufacturer since the original data were supplied. 5 Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for ResaleNo reproduction or netwo
18、rking permitted without license from IHS-,-,-ICAO 9b4b-AN/943 * m 484141b 00b3935 119 m Engine Combustor Identification 6 ICAO Engine Exhaust Emissions Data Bank UD Data Page TYP CF6-80C2A2 CF6-80C2A2 CF6-80C2A1 I lGE015 C c033 lGE016 R c034 I 1GE014 I C I CO32 CF6- 80C2A3 I I 1GE017 C I CO35 CF6-80
19、C2A3 CF6-80C2A5 1GEOl8 R c036 1GE019 C c037 I CF6-80C2A5 CF6-80C2A8 1GE020 R c038 1GE02 1 C c039 CF6-80C2B4F I 1GE028 l C CF6-80C2B 1 CF6-80C2B 1F CF6-80C2B 1F CF6-80C2B2 CF6-80C2B2F CF6-80C2B4 1GE022 C c040 lGE023 C c041 1GE024 R c042 1GE025 C c043 1GE026 C c044 1GE027 C c045 11 CF6-80C2B6 CF6- 80C
20、2B 6F CF6-80C2DlF CF6-80E 1Al CF6-80ElA2 c046 1GE029 C 1GE030 C 1GE03 1 C 1GE032 C 1GE033 C c047 CF34-3A CF34-3A1 c048 c049 LEC II 1GE034 C LEC II 1GE035 C c050 CO5 1 c052 c053 II CFM56-2A series I IlCM001 1 C IC008 Copyright International Civil Aviation Organization Provided by IHS under license wi
21、th ICAONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ICA0 964b-AN/9Y3 * 484L4Lb 00b393b O55 = 1AA003 1AAo04 1ZMOO1 1PWoo1 Index of engines 7 R c005 R c006 C C 148 P c064 Engine Identification 1PW002 1PW003 1PW004 1PW005 Combustor P c065 P c066 P c067 C c068 CFM56
22、-2B- 1 I CFM56-2-C5 CFM56-3B-2 CFM56-5A- 1 CFM56-5A3 I CFM56-5C2 D-30 (I1 series) D-30KP-2 D-30KU D-30KU- 154 D-36 JT3D-3B I JT3D-7 series JT8D-7 series Smoke fix JT8D-7 series I Red emiss JT8D-9 series Smoke fix JT8D- 11 UD I Data Page 1CM002 I C ICOOS 1CM003 C 1CMo04 R 1CM005 R 1CM006 R c010 c012
23、c013 1CM007 1CM008 1CM009 1CMO10 C 1CMO11 C 1AA001 R 1AA002 R c014 c015 c016 c017 c018 c003 c004 1PW006 1PW007 1PW008 Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ICAO 9b4
24、b-AN/43 *Y m 484L4Lb 0063937 T9L W Engine Identification 8 ICAO Engine Exhaust Emissions Data Bank Combustor UD Data Page TvPe JT8D- 15 JT8D- 15 Smoke fix 1PWoo9 P CO7 2 Red emiss 1PW010 C c073 JT8D- 15A JT8D- 17 JT8D- 17 I Redemiss I lPW013 I C I CO76 1PW011 C c074 Smoke fix 1PW012 P c075 JT8D- 17A
25、 JT8D- 17AR JT8D- 17R I I 1PW017 I C I CO80 JT8D-209 1PW014 C c077 1PW015 C c078 1PW016 C c079 JT8D-217 series JT8D-219 JT9D-7 JT9D-7A lPW018 C CO8 1 1PW019 C c082 1PW020 P c083 1PW021 P c084 JT9D-7F JT9D-7F JT9D-7 J JT9D-7Q JT9D-7R4D JT9D-7R4Dl JT9D-7R4E JT9D-7R4E 1 Mod V 1PW022 P c085 Mod VI 1PW02
26、3 P c086 1PW024 P c087 lPW025 P c088 1PW026 C c089 1PW026 C c089 1PW027 C c090 1 PW027 C c090 JT9D-7R4E 1 (H) JT9D-7R4E4 1PW028 C c091 1PW028 C CO9 1 Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for ResaleNo reproduction or networking permitted witho
27、ut license from IHS-,-,- ICA0 9646-AN/943 * = 4843436 0063938 928 JT9D-7R4G2 JT9D-7R4H 1 JT9D-20 JT9D-20J JT9D-59A JT9D-70A Index of engines 9 1PW029 C c092 1PW030 C c093 1PW03 1 P c094 1PW032 P c095 1PW033 P c096 1PW034 P c097 Il I I I i JT15D-1 series JT15D-4 series JT15D-5 II JT15D-5A (1 Engine 1
28、PW035 P c098 1PW036 P c099 1PW037 C Cloo 1PW037 C Cloo Identification I JT15D-5C LF507 series 1PW038 C c 101 1TL004 C c 147 M54H-01 NK-8-2U NK-8-2U NK-86 NK-86A II JT15D-5B I 1RR001 P C 123 1KK001 R c059 1KK002 R c060 1KK003 R CO6 1 1KK004 R c062 IlPW037 I C I Cl00 NK-86MA Olympus 593 MK 610 PS-9OA
29、PW2037 PW2040 1KK005 C c063 1 RR022 P d001 1AA005 C c007 1PW039 C c 102 lPW040 C C 103 I Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ICAO 964b-AN/943 * 484l14Lb ClOb3939
30、8b4 Engine Combustor UD Data Identification TYP PW4056 1PW041 C PW4056 Red smoke 1PW042 C PW4060 Red smoke 1PW043 C PW4152 1PWW C 10 ICAO Engine Exhaust Emissions Data Bank Page C 104 C 105 C 106 C 107 PW4152 PW4156 Red smoke 1PW045 C c 108 1PW046 C c109 PW4156 PW4158 1 I I I Red smoke 1PW047 C c110
31、 Red smoke 1PW048 C c111 PW4164 PW4168 PW4256 Floatwall 1PW049 C c112 Floatwall 1PW050 C C113 1PW051 C c114 PW4460 PW4x50 PW4x52 PW4x56 Red smoke 1PW052 C C115 Phase 3 1PW053 C C116 Phase 3 lPW054 C C117 Phase 3 1PW055 C C118 PW4x58 PW4x60 PW4x62 Phase 3 1PW056 C c119 Phase 3 1PW057 C c120 Red smoke
32、 1PW058 C c121 PW4x62 RB211-22B RB211-22B RB211-524B series RB211-524B series Phase 3 1PW059 C c122 1RR002 P C124 1RR003 P C125 Package 1 1RR004 P C126 Phase 2 1RR005 C C127 Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for ResaleNo reproduction or ne
33、tworking permitted without license from IHS-,-,-ICA0 9b4b-AN/943 XX 48414Lb 0063940 586 = Engine Identification Index of ennines 11 Combustor UD Data Type Page RB2 11 -524C2 RB2 11-524D4 RB211-524D4 RB211-524G RB2 11-5246 RB2 11-5248 1RR006 P C128 Package 1 1RR007 P C129 Phase 2 1RR008 C C130 1RR009
34、 C C131 1RRO10 R C132 1RRO11 R C133 RB211-535C IRR012 C C134 SPEY Mk555 I I 1RR017 I P I C139 I I RB211-535E4 RB211-535E4 1RR013 C C135 1RR014 R C136 SPEY Mk511 SPEY Mk511 1RR015 P C137 Transply IM 1RR016 C C138 SPEY MW55 TAY Mk611-8 TAY Mk620- 15 TAY Mk650-15 TFE73 1-2-2B Transply IIF 1RR018 C c140
35、 1RR019 C C141 1RR020 C C142 1RR021 C C 143 1AS001 P Cool TFE731-3 V2500-A1 V2525-D5 V2527-A5 1AS002 P c002 1IAoo1 C c054 1IA002 C c055 1IA003 C c056 V2528-D5 V2530-A5 1IA004 C c057 1IA005 C CO58 Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for Resal
36、eNo reproduction or networking permitted without license from IHS-,-,-ICA0 964b-AN/943 tt 4841416 0063941 412 Appendix A REGULATORY LEVELS These applicability requirements and regulatory levels are those found in Annex 16, Volume II, Part III, Chapter 2 (subsonic engines) and Chapter 3 (supersonic e
37、ngines) and are included for reference purposes only. 1. SUBSONIC ENGINES 1.1 Smoke 1.1.1 Applicability The regulatory levels are applicable to engines whose date of manufacture is on or after 1 January 1983. 1.1.2 Regulatory smoke number The characteristic level of the smoke number at any thrust se
38、tting, measured in accordance with Annex 16, Volume II, must not exceed 83.6 (Fm)-00.274 or a value of 50, whichever is lower. 1.2 Gaseous emissions 1.2.1 Applicability The regulatory levels apply to engines whose rated output is greater than 26.7 kN and whose date of manufacture is on or after 1 Ja
39、nuary 1986 and as further specified for oxides of nitrogen. 1.2.2 Regulatory levels The characteristic levels of the gaseous emissions measured over the LTO cycle in accordance with Annex 16, Volume II, must not exceed the following regulatory levels: Hydrocarbons (HC): DJFw = 19.6 Carbon monoxide (
40、CO): DPw = 11 8 Oxides of nitrogen (NOx) A-I Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ICAO 964b-AN/943 * 4843436 0063942 359 W A-2 ICAO Engine Exhaust Emissions Data B
41、ank for engines of a type or model of which the date of manufacture of the rst individual production model was on or before 31 December 1995 and for which the date of manufacture of the individual engine was on or before 31 December 1999: Dpm = 40 + II, for engines of a type or model of which the da
42、te of manufacture of the first individual production model was after 31 December 1995 or for which the date of manufacture of the individual engine was after 31 December 1999: DJFm = 32 + 1.6% 2. SUPERSONIC ENGINES 2.1 Applicability The regulatory levels are applicable to engines intended for propul
43、sion at supersonic speeds whose date of manufacture is on or after 18 February 1982. 2.2 Smoke The characteristic level of the regulatory smoke number at any bust setting, measured in accordance with Annex 16, Volume II, must not exceed 83.6 (F*m)-00.274 or a value of 50, whichever is lower. 2.3 Gas
44、eous emissions The characteristic levels of the gaseous emissions measured over the LTO cycle in accordance with Annex 16, Volume II, must not exceed the following regulatory levels: Hydrocarbons (HC): DP*, = 140(0.92)xoo Carbon monoxide (CO): DFm = 4 550(7tm)-.03 Oxides of nitrogen (NO 222.4 231.3
45、28.4 249.1 30.7 I 266.9 33.4 I 275.8 31.9 I 275.8 DJFm and SN (Characteristic) 4.9 42.7 52.2 9.0 C C108 1.8 17.4 59.9 18.4 C C109 I Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for ResaleNo reproduction or networking permitted without license from IH
46、S-,-,-ICA0 9b4b-AN/943 tt 44L4lib 00b395L 3bli Appendix B B- 9 Rolls Royce Ltd Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ICAO 7bYb-AN/743 * = 48414Lb 0063752 2T8 Engine
47、 Combustor Press Rated DJFm and SN Identification Type UID Ratio output (Charactenstic) oN) HC CO NO, SN D-36 1ZMOO1 19.9 63.8 14.0 52.8 59.6 17.4 B-IO ICAO Engine Exhaust Emissions Data Bank Textron Lycoming Data Type Page C C148 Engine Combustar Identification ALF 502L-2 1TLoo1 ALF 502R-3 1m2 ALF
48、502R-5 LF507 series Press Rated DdF, and SN Ratio output (Characteristic) 13.0 31.0 16.7 110.6 40.4 13.6 C C147 Zaporozhye Machine-Building Design Bureau Progress (ZMKB Progress) Copyright International Civil Aviation Organization Provided by IHS under license with ICAONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ICAO 764b-AN/743 * = 4843436 0063753 334 PRESSURE kPa TEMPERATURE OC I 96.7-98.1 12 to 15 Appendix C SUBSONIC ENGINES ICAO ENGINE EXHAUST EMISSIONS DATA BANK ISSUE 1 - OCTOBER 1993 Note : DJF, a
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