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Aviation History
1994
1994 - 1430.PDF
TURBINE DIRECTORY combustion chamber and the low-pressure compressor already funded. The French engine manufacturer is one of several com peting for a possible mid-life update of the Saab JAS39 Gripen, for which proposals are due by the end of the third quarter of this year. Snecma has offered to develop an advanced low-pressure turbine section for the M88 in conjunction with Swedish industry. TRUD/SAMARA The Russian engine-design bureau has delayed the first flight of its NK-93 propfan by at least 12 months because of lack of funding. The engine is now due to be flown on an Ilyushin 11-76 testbed at the Zhukovsky research centre in 1995. TURBO-UNION Work is now well under way build over 100 RB.199 powerplants for Saudi Arabia's order of 48 additional Panavia Tornado GR.l strike aircraft. Meanwhile, the twin RB. 199-122 powered Eurofighter 2000 development aircraft numbers 1 and 2 have now been flown. WILLIAMS ROLLS-ROYCE Cessna's Williams Rolls-Royce FJ44-pow- ered Model 526 JPATS Citationjet was flown for the first time on 20 December, 1993. The Swedish air force, meanwhile, has awarded a Skr800 million ($99 mil lion) contract to Williams Rolls-Royce to re-engine 115 SK.60 (Saab 105) jet train er/light attack aircraft with the FJ44. The new powerplants will replace the SK.60's 7.3kN Turbomeca Aubisque engines. Williams Rolls-Royce was compet ing against AlliedSignal Engines for the contract. AlliedSignal had offered the F109. The new Williams Rolls-Royce contract also includes an option to re-engine a fur ther 20 SK.60s. COMMERCIAL TURB0FANS Manufacturer AlliedSignal Engines AlliedSignal Engines Allison A0 Aviadvigatel BMW Rolls-Royce BMW Rolls-Royce CFE CFM International CFM International CFM International CFM International CFM International General Electric General Electric General Electric General Electric General Electric International Aero Engines International Aero Engines International Aero Engines Pratt & Whitney Pratt & Whitney Pratt & Whitney Pratt & Whitney Pratt & Whitney Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Rolls-Royce Rolls-Royce Rolls-Royce Rolls-Royce Rolls-Royce Rolls-Royce Rolls-Royce Textron Lycoming Textron Lycoming Williams Rolls-Royce ZMKB Progress ZMKB Progress Engine TFE731-4 TFE731-5 AE3007 PS-90A BR710 BR715 CFE738-1 CFM56-3B/C CFM56-5A CFM56-5B CFM56-5C CFM56-7B CF34-3A1 CF6-80A CF6-80C2 CF6-80E1 GE90-85B V2500-A1 V2500-A5 V2500-D5 JT8D-200 PW2037/2040 PW4052-4460 PW4168 PW4084 JT15D-4 JT15D-5/5A JT15D-5D PW305A PW305B PW306A Tay 611/620 Tay 650/651 Tay 670 RB.211-535E4 RB.211-524G/H Trent 768/772 Trent 875-890 ALF502R-3 LF507-1F FJ44 D-436 D-18T Thrust kl 18.1 19.1 32 156.6 65 88.8 25.5 89-105 98-118 98-138 139-151 83-117 41 213 233-273 300-320 377 111.2 98-133 111-125 77-96.6 170/185 231-267 302 376 11.1 13.1 13.5 20.9 23.5 25.46 61.6 67.2/68.5 80.1 178-192 258-270 300-316 346-406 29.8 31.1 8.4 74 230 lb (000s) 4.08 4.3 7.2 35.2 14.75 19,9 5.72 20-23.5 22-26.5 22-31 31.2-34 18.5-26.4 9.22 48 52.5-61,5 67.5-72 84.7 25 22-30 25-28 17.4-21.7 38.25-41.7 52-60 68 84 2.5 2.9 3.04 4.678 5.23 5.7 13.850 15-15.4 18 40.1-43.1 58-60.6 67.5-71 77.9-91.3 6.7 7 1.9 16.55 51.5 sfc (Ib/h/lb) *0.79 *0.8 *0.39 0.58 -- 0.39 0.38-0.39 0.316-0.330 0.324-0.354 0.321-0.331 0.36 0.35 0.32-0.33 0.32-0.33 -- -- 0.51-0.66 0.33/0.34 0.34-0.37 0.56 0.55 0.55 0.388 0.391 0.394 *0.71 *0.69 *0.68 *0.598 *0.570 •0.557 •0.557 0.41 0.406 0.44 0.63 0.36 Dimensions (m) length fan dia 1.47 1.66 2.7 4.9 5.1** 5.2** 2.52 2.36 2.42 2.6 2.62 2.51 2.615 4 4.09 4.17 4.88 3.2 3.2 3.2 3.92 3.73 3.37 3.37 3.37 1.53 1.53 1.53 2.07 2.07 1.92 2.40 2.41 2.84 2.99 3.18 3.9 4.3 1.06 1.48 1.18 3.03 5.4 -- 1.1 1.9 1.11 1.34 1.52 1.73 1.73 1.84 1.55 1.24 2.19 2.36 2.44 3.35 1.6 1.613 1.613 1.17T 1.99 2.38 2.54 2.84 0.69 0.69 0.69 0.8 0.8 0.78 1.11 1.14 1.27 1.88 2.19 2.47 2.79 1.2 1.2 0.6 1.39 2.9 Confiquration 12 3 4 1 1 1 2 1 2 1 3 3 3 4 3 1 3 4 4 3 3 4 4 6 4 4 5 6 ... *** **** **** **"* 3 3 4 6 7 8 8 1 2 1 6 7 5 5 14 13 10 10 6 9 9 9 9 9 14 14 14 14 10 10 10 10 7 12 11 11 11 - -- 12 12 12 6 6 6 6 8 8 1 7 7 1 1 2 2 2 2 2 2 2 2 2 2 2 2 2 1 2 2 2 2 1 1 1 2 2 2 2 2 2 1+1 1+1 1+1 1+1 2 2 1 1+1 1+1 5 3 3 3 4 2 3 3 4 4 4 5 4 4 4 5 5 6 5 5 5 3 5 4 5 7 2 2 2 3 3 3 3 3 3 3 3 4 5 2 2 2 3 4 Application Cessna Citation VII BAe 125-800, CASA C-101 Embraer EMB-145, Cessna Citation X Tupolev Tu-204, Ilyushin II-96-300 Gulfstream V, Global Express McDonnell Douglas MD-95 Dassault Falcon 2000 Boeing 737-300/400/500 Airbus A319/A320 Airbus A319/A320/A321 Airbus A340 Boeing 737-700 Canadair Regional Jet Airbus A310, Boeing 767 Boeing 747-300/400, 767, Airbus A300-600, A310, McDonnell Douglas MD-11 Airbus A330 Boeing 777 Airbus A320 Airbus A319/A320/A321 McDonnell Douglas MD-90-30/50 McDonnell Douglas MD-80 series Ilyushin II-96M, Boeing 757ft Boeing 747-400, 767, Airbus A300-600, A310, McDonnell Douglas MD-11 Airbus A330 Boeing 777 Cessna Citation II Cessna Citation V/Beechjet 400A Cessna Citation V Ultra Learjet 60 Hawker 1000 Astra Galaxy Gulfstream IV, Fokker 70/100 Fokker 100, Boeing 727QF Offered for Boeing 727, 737, McDonnell Douglas DC-9 re-engineing Boeing 757, Tupolev Tu-204 Boeing 747-400, 767-300 Airbus A330 Boeing 777 BAe146 Avro International RJ Cessna Citationjet, Swearingen SJ30 Antonov An-72, An-74, Tupolev Tu-334, Yakovlev Yak-42M Antonov An-124, An-225 Thrust at take-off; sfc (specific fuel consumption^ take-off thrust unless otherwise specified (*= cruise thrust); configuration; 1 = fan; 2 = low-pressure compressor; 3 = high-pres sure compressor; 4 = high-pressure turbine (where 1 +1 is listed, the latter figure is the intermediate power turbine in a three-spool engine); 5 • low-pressure turbine: eg, an engine with a single-stage fan, two-stage LPC, 14-stage HPC, single-stage HPT and five-stage LPT= 1/2/14/1/5; application is aircraft type(s) powered;; t = JT8D-219; tt= PW2037 and 2040 both power Boeing 757, PW2037 powers II-96M; ** includes nacelle; *** single-stage titanium centrifugal LPC with axial booster stage; **** four-stage axial LPC with one centrifugal. 38 FLIGHT INTERNATIONAL 8 - 14 June, 1994
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