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Aviation History
1995
1995 - 2241.PDF
TURBINE ENGINE DIRECTORY cm JAPANESE ENGINE manufacturer IHI builds the two-shaft F3-30 turbofan for the Japan Air Self-Defence Force Kawasaki T- 4 trainer. The first production engine was delivered in 1987. MILITARY TURBOFANS/JETS Model Max thrust dry kN lb Length (m) Rotor/fan diameter (m) SFC mg/Ns Ib/h/lb fan 2 stage Total compressor stages 5 turbine hp Ip 1 2 Description Kawasaki T-4 IHI, Shin Ohtemachi Bldg 2-1, Ohtemachi 2-chome, Chiyoda-Ku, Tokyo 100, Japan. Tel: +81 (3) 3244 53 33; fax: +81 (3) 3244 53 98; telex: 22232 IHIHQT J. una INTERNATIONAL TURBINE Engine (ITEC), a joint venture between AlliedSignal and the Aero Industry' Development Center of Taiwan, is supplying its F124-100 turbofan engine to power the Czech L-l 59 combat aircraft which is being developed by Aero Vodochody. The engine, rated at 30kN, is a non-afterburning ITEC (International Turbine Engine) see AlliedSignal. version of the TFE1042-70 (F125) developed for the Taiwanese Indigenous Defence Fighter. ITEC is to ship die first engines to the Czech Republic this year, ahead of the L-159's first flight, due in April 1996, although ITEC is thought to be pressing for this to be speeded up. MILITARY TURBOFANS/JETS Model Max thrust dry Length fan Total kN lb (m| compressor stages F124-100 28.02 6.300 1.92 3 stage 4axl + lcfgl The F124 is also being offered as an alterna tive to die Rolls-Royce Turbomeca Adour, which powers die British Aerospace Hawk trainer, despite not being selected for US Navy McDonnell Douglas/British Aerospace T-45A Goshawk trainers. turbine hp Ip Application Aero L-159: F125-100 reheated powers AIDC Ching-Kuo IDF IJHI'iM'l K LIMOV MANUFACTURES the RD-33 low-bypass turbofan which powers all versions of the MiG-29 fighter aircraft, and upgraded MiG-21s. The RD-33K is the latest version and is fitted to the MiG-29K and MiG-29M. Klimov also builds TV3-117 and TV7-117 turboshafts for a range of airframe applications. MILITARY TURBOFANS/JETS Model RD-33 Max thrust dry Max thrust (reheat) Length kN 49.4 TURBOSHAFTS Model TV3-117 TV7-117V lb kN 11100 81.4 Power kw shp 1618 2170 1728 2320 lb (m) 18300 4,2 Length Rotor/fan (m) diameter (m) 2.08 0.64 2.14 0.88 Rotor/fan diameter (m) 1 SFC ug/J Ib/h/shp 96.3 0.57 0 0 compressor Ip 4 total hp 9 compressor stages lOaxI 5 axl +1 c t total turbine stages 2 2 turbine hp 1 Ip 1 power turbine 2 2 Application MiG-29. re-engined MiG-21:86kN RD-33K powers Mi&29K and -29M Application TV3-117BK powers Ka-27 and Ka-28: l,434kWTV3-117MT powers Mi-8; 1.633kW TV3-117V powers Ka-27. Ka-29 and Ka-32; 1.618kWTV3-117VK powersKa-50;TV-3-ll7VM powers Mi 17. -25. 28 and -35. Mil Mi-38 Klimov, 13 Kantemirovskaya Street, St Petersburg, 184100, Russia. Tel: +7 (245) 00 35; fax: +7 (245) 33 35; telex: 121282 JET SU. LHTEC, a joint venture between Allison Engines and AlliedSignal Engines, is sup plying its T800 turboshaft engine for the re-engineing of Bell UH-1H Huey helicopters flown by the US Border Patrol. The first re-engined aircraft was due to have been delivered in July. The T800 was originally developed for the Boeing/Sikorsky RAH-66 Comanche. Earlier this year, LHTEC signed a con tract w^ith Hindustan Aeronautics covering the supply of CTS800 engines for flight test ing of the Indian manufacturer's Advanced Light Helicopter (ALH). The 970kW CTS800 is the civil version of the T800, and may be selected to replace the Turbomeca TM333 as the ALH powerplant. AlliedSignal savs that production deliveries would begin in early 1998. Agusta's A. 129 International, an upgraded version of the Rolls-Royce Gem-powered A. 129 Mangusta attack helicopter, is also being offered with T800s. TURBOSHAFTS Model T800800 T80O801 Power kw shp 924 1,240 1.080 1.450 Length Rotor/fan (m) diameter (m) 0.84 0.55 0.85 0.55 SFC total total ug/J Ib/h/shp compressor turbine stages stages 76.7 0.453 2cfgl 2 78.4 0.463 2cfgl power Application turbine 2 Agusta A.129. reengined Bell UH-1. Huey 800; CTS800 commercial version selected for Indian ALH 2 Boeing/Sikorsky RAH-66 Comanche LHTEC, Light Helicopter Turbine Engine, The Paragon Building, Suite 400, 12400 Olive Boulevard, St Louis, Missouri 63141, USA. Tel: +1 (317) 230 6515; fax: +1 (317) 230. MILITARY TURBOFANS/JETS Model Max thrust dry Max thrust (reheat) kN lb WP6A 29.42 6.611 kN 36.78 lb 8.265 Liming Engine Manufacturing L IMING'S WP6A turbojet was developed to power the NAMC Q-5I attack aircraft. The company later developed the WP6B turbojet, although this is understood to be no longer in production. Liming, PO Box 424 (6 Dongta Street), Dadong District, Shenyang, Liaonmg 110043, China. Tel: +86 (24) 443 139; fax: +86 (24) 732 221; telex: 80025 LMMCS CN. Length (m) 5.4 Rotor/fan diameter (m) 0.66 Total compressor stages 9 Total turbine stages 2 Application WP6 powers Shenyang J-6, SAFJ>€.NAMC Q-5;WP6A powers Q-51 36 FLIGHT INTERNATIONAL 2 - 8 August 1995
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