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Aviation History
1996
1996 - 2707.PDF
ENGINE DIRECTORY TURBOSHAFTS Power Model kW shp LTS101-750B 510 LTS101-750C 510 T53-703 1,118 T55-712 2,812 T55-714/714A 3,650 T800-801 1,166 CTS800-4 1,016 684 684 1,490 3,750 4,867 1,563 1,362 ALLISON ENGINES Length m 0.79 0.79 1.21 1.18 1.18 0.845 1.047 Rotor/fan diameter (m) 0.47 0.61 0.61 0.562 0.56 ug/J 97.5 97.5 100.2 86.8 85.1 Total SFC compressor Ib/h/shp stages 0.5777 1axl + lcfgl 0.577 laxl + lcfgl 0.592 5 axl + 1 cfgl 0.514 7 axl + 1 cfgl 0.504 7 axl +1 cfgl 2cfgl 2cfgl Total turbine stages 1GP 1GP 2 - 2 - 2 2 4 4 Power turbine 1 2 2 Application -750B-1 powers Eurocopter/Kawasaki BK-117B, -750B-2 powers AS.366/HH-65A Dolphin Bell 222B, 222UT Bell AH-1F HueyCobra, Fuji/Bell UH-1J, re-engined UH-1HP Huey II; commercial versions: T5317A powers Kaman K-Max and Bell 205A; T5317B powers Fuji/Bell 205G Boeing CH-47D; 3,284kW T55-7125 5/5B also powers CH-47D Boeing MH-47E; Boeing improved corporate helicopter Comanche RAH-66* CTS800-50/51 are civil versions Potential applications: HAL ALH, Westland Super Lynx, UH-1H, Agusta A129, Eurocopter Dauphin Allison Engines, PO Box 420, Indianapolis, Indiana 46206-0420, USA. Tel: +11317) 230 2000 ALLISON ENGINES, acquired by Rolls-Royce in 1995, is studying a growth version of the AE3007 turbofan which powers the Embraer EMB-145 regional jet and CEssna Citation X business jet. Designated the AE3012, the engine would be offered as a potential powerplant for the planned Aero International (Regional) 70-seater. The AE3012 would be based on the core of the AE3 007, but use a revised low-pressure sys tem (likely to be developed in co-operation with BMW Rolls-Royce) and an enlarged, 1.1m- diameter fan. The AE3012 would cover the 45- 62kN thrust range, compared with the AE3007's upper limit of around 42kN with its existing 960mm-diameter fan. The engine is likely to face fierce competi tion in the market place, against the General Electric CF34-8C and Snecma/Pratt & Whitney Canada SPW14. Allison continues to evaluate ne.vy: applications for the A3007, including possible stretched, turbofan-powered versions of the Fairchild Dornier 328. The AE2100 turboprop, meanwhile, could be used to re-engine the Alenia G2 2 2 transport, following a joint-venture agreement between the Italian manufacturer and Lockheed Martin. This engine, which powers the latter's C-130J, Saab 2 000 and IPTN N-2 50, has also been cho sen by Dassault Aviation for its Atlantic Third Generation maritime-patrol aircraft. Among other developments, Allison'sModel 250-C47B turboshaft engine for the Bell 407 helicopter was certificated in February. • The Allison AE3001for the Embraer EMB US EEES2EKE22SI Model AE3007 | TURBOPROPS Thrust kN lb 32.03 7,200 Length m 2.7 Rotor/fan diameter (ml 9.8 SFC mg/Ns Ib/h/lb 11.05 .39 fan 1 compressors Ip HP 1 14 turbines HP Ip 2 3 Application Cessna Citation X, Embraer EMB-145, Tier 11+ UAV; AE30012 growth version under development Total Total Power Length Rotor/Fan SFC compressor turbine Power Model kW shp m diameter (ml ug/J Ib/h/shp stages stages turbine Application 250+317F 335 450 0.98 0.48 111 0.657 4 axl+ 1 cfgl 2gasturb 2 Pilatus Britten-Norman BN-2T, Agusta SF.600TP, HX-1, Beech A36 Bonanza, Redigo, Turbine P210; versions include -B17B, -B17C and -B17D. AE2100 T56 3,096 3661 TURBOSHAFTS Model 250-C20 250-C28 4,152 4,914 Power kW shp 313 373 420 500 2.74 3.71 Length m 0.98 1.2 0.67 0.99 Rotor/fan diameter (ml 0.48 0.55 69.31 84.67 0.41 0.501 SFC ug/J Ib/h/shp 109.8 102.5 0.65 0.606 14 14 Total compressor stages 6 axl +1 cfl 1 2 2 4 Total turbine Power stages turbine 2 gas turb 2 2 gas turb 2 Saab 2000 (2100A), IPTN N-250 (2100C),Lockheed C-130J (2100D3) -14 powers P-3B & C Orion; -15 powers Lockheed C-130H; -423/16 powers Grumman E-2C Hawkeye; -27 powers E-2/C-2; 501 powers Convajr 580/5800 Application -C20B powers Bell 206B Jetranger III, 206L LongRanger, 47G conversions, MD500D, Eurocopter B0.105, UH-12E, KA-226, RFB Fantrainer; -C20F powers AS355 Ecureuil 2; -C20J powers Bell 206B JetRanger III; -C20W powers Enstrom 480, Schwiezer 330; -C20R/1 powers A -C28B powers Bell 206L LongRanger 1; C-28C powers B0105LS. 250-C30 485 650 1.04 0.55 100 0.59 2 gas turb 2 -C30 powers S-76 and MD530G; -C30G powers Heli-Air Bell 222; -C30G2 powers Bell 230 and Bell 430; C-30L pdwers Bell 406CS; -C30M powers Eurocopter AS350; -C30P powers Longftanger III and IV; -C30R powers Bell AHIP 0H-58D; -C30R/1 powers 0H-58D; latest version is -C30R/2. -C- 40 powers Bell 430, -C47 powers Bell 407 T406-400 T703-700 4,586 485 6,155 650 1.52 1.04 0.59 0.55 70.9 100 0.42 0.59 14 1 2 gas turb 2 2 gas turb 2 military version of AE1107 powers Bell Boeing V-22 military version of 250-C30R powers Bell 0H-58D FLIGHT INTERNATIONAL 9 - 15 October 1996 31
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