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Aviation History
1995
1995 - 2240.PDF
TURBINE ENGINE DIRECTORY TURBOPROPS Model CT7-9 GLC38 T64/P4D Power kw shp 1,300 0 3.470 4,657 2.533 3,400 TURBOSHARS Model CT7-2A CT7-2D/-2D1 CT7-6/-6A CT7-6D GLC38/T407 T64-416 T64-416A T64-419 T700401 T700401C T70O-700 T700-701 T700-701A T70O701C T700/T6A T700/T6E Power kw 1.212 1,212 1,492 1,514 4.790 3.263 3.263 3.538 1.261 1,343 1,210 1.267 1.285 1.410 1,492 1,788 shp 1.625 1.625 2.000 2.030 6.429 4.380 4.380 4.750 1.690 1.800 1,622 1,698 1.723 1.890 2.000 2.400 Length (m) 2.44 1.55 2.8 Length (m) 1.19 1.19 1.19 1.19 1.55 1.97 1.97 1.97 1.18 1.15 1.15 1.18 1.18 1.18 1.19 1.19 Rotor/fan diameter (m) ug/J 0.74 0.83 0.33 Rotor/fan diameter (m) 0.64 0.64 0.64 0.64 0.83 0.5 0.5 0.5 0.635 0.64 0.64 0.635 0.635 0.635 0.64 0.64 80.6 69.2 81.7 SFC Ib/h/shp 0 0.409 0.484 SFC ug/J 80 80 77.2 76 64.2 78.7 78.7 80.1 78.4 77.7 78.5 78.4 78.5 78 76 75 Ib/h/shp 0.474 0.474 0.457 0.45 0.379 0.466 0.466 0.474 0.464 0.46 0.465 0.464 0.465 0.462 0.45 0.444 total compressor stage 6 5 axl +1 cfgl Total compressor stages 5 axl +1 cfgl hp compressor 2 14 axl hp compressor 6 axl 6 axl 6 axl 6 axl 14 axl 14 axl 14 axl 6 axl 6 axl 6 axl 6 axl 6axl 6 axl 6 axl 6 axl Total turbine stages 2 turbine hp 2 2 IP 2 2 turbines hp 2 2 2 2 2 2 2 2 2 2 2 2 2 2 2 2 IP 2 2 2 2 3 2 2 2 2 2 2 2 2 2 2 2 power Application turbine -9B powers Saab 340B. selected for Sukhio S80; 9C powers CASA/IPTN CN-235; -90 powers Let-L610G 3 under development AleniaG222.USAFC-27A Application Bell 214ST Sikorsky S-70. selected for Kamov Ka62G EH Industries EH101 (Civil) Sikorsky S-92: CT7-8 growth version for S-92 Offered for Boeing CH47 enhancement Sikorsky CH/MH-53E. S80M Sikorsky CH/MH-53E. &80M Sikorsky CH/MH-53-E Bell AH-1W. Kaman SH-2G. Sikorsky VH-60 Sikorsky HH-60H, HI+60J, SH-60B. SH-60F Sikorsky UH-60A Black Hawk MDC AH-64A Sikorsky S-70A MDC AH-64A. Sikorsky UH-60L, S-70A EH Industries EH101 (Military) NH Industries NH90 GE Aircraft Engines, One Neumann Way, Mail Drop N-109, Cincinnati, Ohio 45215-6301, USA. Tel: +1 (513) 243 6136; fax: +1 (513) 786 1568; Telex: TWX 810 461 2638. raim G TRE is developing the Kaveri turbofan as the planned powerplant for the Indian Light Combat Aircraft. The engine, an improved version of the GTX-35, but with a redesigned core, includes full-authority digital engine control and an advanced nozzle. MILITARY TURBOFANS/JETS Model Max thrust dry Max thrust (reheat) kN lb kN lb Kaveri 51.3 11.530 80.2 18.030 GTRE, Shortlands, Hammersmith, London W6 8BX, UK. Tel: +44 (181) 846 86 58; fax: +44 (181) 741 95 01; +44 (181) 741 94 60; telex: 261794 geusa-g. compressor Ip hp 3 6 turbine hp Ip 1 1 Application Indian LCA GTRE, Gas Turbine Research Establishment, Suranjan Das Road, Post Bag 9302, C V Raman Nagar, Bangalore, 560 093, India. Tel: +91 (812) 570 698; telex: 0845 2438. International Aero Engines I NTERNATIONAL AERO Engines (IAE), a joint venture between Pratt & Whitney, Rolls-Royce, MTU, FiatAvio and Japanese Aero Engines, is work ing with Calcor Aero Systems of die USA to develop a variable-area exhaust nozzle for IAE's V2500 turbofan. The nozzle will van' the exhaust-exit area by around 15%, and could yield a 4% increase in take-off thrust, says IAE. The nozzle would be controlled by the engine's full-authority digital engine control. The noz zle is scheduled to enter testing at the end of 1996, when a prototype will be fitted to a V2500-A5. IAE has also been working with Ilyushin, with a view to offering the V2500 as a candidate for re- engineing Il-86s, in competition with CFM International's CFM56. The 135kN V2500-I5, a vari ant of the -A5, would be offered for the 11-86, and may COMMERCIAL TURBOFANS Model V2500-A1 V250O-A5 V250O-D5 V2533-A5 Thrust kN 111.2 97.9 -140 111.2-124.6 146.8 lb 25.000 22,000-31,500 25.000 -28,000 33.000 Length (m) 3.2 3.2 3.2 3.2 Rotor/fan diameter (m) 1.6 1.6 1.6 1.6 fan 1 1 1 1 compressor Ip 3 4 4 4 hp 10 10 10 10 turbine hp Ip 2 5 2 5 2 5 2 5 also be considered for a stretched 11-76 freighter. IAE secured a launch customer for the V2500-A5 on the Airbus A319 (International Lease Finance), and German charter carrier Aero Lloyd became the first customer for the 145kN V2533-A5 when it ordered a fleet of extended-range A321 -200s. The V2 500-pow- ered McDonnell Douglas MD-90-30 entered service with Delta Air Lines earlier this year. Meanwhile, L\£ has had to exclude some early production V2500-A1 engines from Airbus A320 extended-range twin operations (ETOPS) while it completes a programme to retrofit redesigned com pressor blades. The redesign was carried out to strengthen high-pressure compressor blades which had failed after clearance problems between the blade tips and the compressor casing were caused by shaft flexing. Application V2500: developments on the way Airbus A320 V2527A5 powers Airbus A320: V2528-A5 powers A321, V2522-A5 powers A319:15 offered to reengine Ilyushin 11*6 V2525-D5 and V2528-D5 powers McDonnell Douglas MD-90-30: V2528 powers will MD-90-50 A321-200:140kN V2530-W5 proposed for Boeing 727 re-engineing IAE International Aero Engines, Corporate Center II, 628 Hebron Avenue, Glastonbury, Connecticut 06033-2595, USA. Tel: +1 (203) 652 1800; fax: +1 (203) 659 1410. FLIGHT INTERNATIONAL 2 - 8 August 1995 35
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