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Aviation History
1997
1997 - 2473.PDF
ENGINE DIRECTORY iimK'Khimi PO Box 420, Indianapolis, Indiana 46206-0420, USA, tel:+l (317) 230 2000; fax:+l (317] 230 3562; INTERNET: www.allison.com Allison has revised plans for the 45-63kN growth version of its AE3007 turbofan, pro posed for the Embraer EMB-170 and Aero International (Regional) Airjet 70, to minimise costs. The new engine, designated the AE3OXX, will use a Rolls-Royce Tay fan, while BMW Rolls-Royce will supply the turbine section, using technology from its BR710 turbofan. A42kNAE3007-Al is being developed for a "hot-and-high" EMB-145, increasing thrust 15% by upgrading the hot section with high- temperature, single-crystal blades. A derated variant, the 28.5kN AE3007-A3, has been selected for die EMB-135. Allison is offering a version of the AE2100 turboprop for the upgraded ShinMaywa US- 1A Kai amphibian. The AE2100J has a modi fied gearbox and propeller. The all-composite Bell Boeing V-22 tilt-rotor is powered by two Allison T406-400 turboprops •H.XhiWti'ijj?^ Model AE3007 Thrust kN lb 32.03 7,198 Length m 2.7 Rotor/fan diameter (ml 9.8 SFC mg/Ns Ib/h/hp 11.05 0.39 Fan 1 Compressors LP HP 1 14 Turbines HP LP 2 3 Application Citation X, EMB-145. Teledyne Global Hawk UAV; AE30XX growth version under development Power Total Total SFC compressor turbine Model AE2100 T56 kW 3.095 3,661 shp 4.154 4,914 m diameter (m) 2.74 0.67 3.71 0.99 ug/J 69.31 84.67 Ib/h/shp 0.41 0.501 stages stages Application 14 2 Saab 2000, IPTN N-250, C-130J 14 4 -14 powers P-3B/C: -15 powers C-130H: -423/16 powers E-2C; -27 powers E-2/C-2; 501 powers Convair 580/5800 HllilMHWiH Model 250-C20-B 250-C28 Total Total Power Length Rotor/fan SFC compressor turbine kW shp m diameter (ml ug/J Ib/h/shp stages stages Application 313 420 0.98 0.48 109.8 0.65 - -C20B powers Bell 206B, 206L, Bell 47G conversions, MD 500D. B0105. Hiller UH-12E. Kamov Ka-226. Fantrainer; -C20F powers AS355; -C20J powers 206B: -C20W powers Enstrom 480, Schwiezer 330 432 580 1.2 0.55 102.5 0.607 -C28B powers Bell 206L; -C28C powers B0105LS. 250-C30P 485 651 1.04 0.55 100 0.592 T406-400 4,586 6,156 1.52 0.59 70.9 0.42 14 Bell Boeing V-22 T703-700 485 651 1.04 0.55 100 0.592 military 250-C30R. powers Bell 0H-58D •iWMiWMAtdl 93 Komsomolsky Prospect,GSP-624, Perm 614600, Russia, tel:+7 3422 45 25 52, fax: +7 3422 45 67 44, telex: 134802 UVA SU The 157kNAviadvigatel/Perm Motors PS-90A entered service on the Ilyushin 11-96 in 1993, with Aeroflot Russian International Airlines. Poor reliability-the airline had to perform per form 31 engine changes on its five II-96-300s during 1995 - persuaded Ilvushin to re-engine the 11-96 with Pratt & Whitney PW2000 turbo- fans. The I1-96T is now due to be certificated in October 1997. In March 1997, the Russian Government authorised guarantees of Si 50 million tor the manufacture of 20 Tupolev Tu-204s with PS- 90As engines for Moscow Aviation Inter national Leasing. German company BGT is working with Tupolev and Aviadvigatel to develop a full- authority digital engine-control system for the PS-90AontheTu-204. The first re-engined Ilvushin I1-76MF, with PS-90As replacing Aviadvigatel D-30KP lis, is being flight-tested. wmm Model D-30KU PS-90A Thrust kN lb 104 23.371 156.9 35,258 Max thrust dry Model kN lb D-30-F6 93.2 20.944 Length m 5.7 4.9 Max thrust (reheat) kN lb 152.1 34,180 Rotor/fan SFC diameter (m) mg/Ns 1.45 1.9 Length m 7.09 13.83 16.85 Ib/h/hp 0.489 0.595 Rotor/fan SFC diameter |m) mg/Ns Ib/h/lb 1.02 20.4 0.721 Fan 1 1 Compressors Turbines LP HP HP LP Application 3 11 2 13 2 Compressors Fan LP HP 5 10 4 II-62M. Tu-154M; D-30KP powers II-76T; D- 30KPV powers Beriev A-40 4 11-96-30, Tu-204, II-76MP * cruise Turbines Application LP HP 2 2 MiG-31 FLIGHT INTERNATIONAL 24 - 30 September 1997 33
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