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Aviation History
1994
1994 - 1432.PDF
TURBOPROPS continued Manufacturer General Electric General Electric General Electric/Lycoming Motorlet Motorlet Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Rolls-Royce/Snecma/MTU SMPMC Lextron Lycoming Turbomeca Zhuzhou ZMKB Progress Engine CT7-9 T64/P4D GLC38 M601Z M602 PT6A-25C PT6A-67 PW120A PW118 PW121 PW119B PW123 PW124B PW125B PW126A PW127 Tyne Mk21/22 WJ6A LTP101-600 Arrius WJ9 AT-20D Power (kW) 1,300 2,540 3,470 TURBINE DIRECTORY sfc ug/J) 80.6 81.7 69.2 380 132 1,360 95.8 410 106.4 895 1,080 1,700 1,862 1,990 2,200 2,200 2,200 2,310 2,460 4,550 3,39 462 315 507 3,800 92.4 79 80.2 79.7 79.5 76.7 76.7 76.7 77 75.8 - 92.9 -- - Power is at take-off; sfc (specific fuel consumption) is at take-off power Dimensions length diameter 1 2.44 2.79 1.55 1.67 2.56 1.57 1.88 2.06 2.06 2.06 2.06 2.06 2.06 2.06 2.06 2.06 2.76 3.1 0.91 0.82 -3.1 configuration: 1 = 0.74 1.03 0.83 0.59 0.75 0.48 0.48 0.63 0.63 0.63 0.63 0.84 0.84 0.84 0.84 0.84 1.1 0.84 0.53 0.47 - 0.84 1 -- -- - (6) (14) (6) (3) (4) (5) (2) (2) (2) (2) (2) (2) (2) (2) (2) (2) Confiquration 2 3 2 (2 (2 1 1 -- 1 1 2 2 10 4 2 2 3 -- 1 1 3 Application 5 Saab 340, CASA/IPTN CN-235, Let-L610G 2 Alenia G-222 3 Zlin 37T Agro Turbo 2 Let L-610M Embraer Tucano BeechC-12 2 de Havilland Dash 8 2 Embraer EMB-120 2 de Havilland Dash 8, ATR 42 2 Dornier 328 2 de Havilland Dash 8 2 BAe Jetstream 61 2 Fokker 50 2 BAe ATP 2 ATR 72 Dassault ATL.2, Transall C.160 SAC Y-8 Various Various HAMCY-12 Various ow-pressure compressor; 2 = high-pressure compressor; 3 = high-pressure turbine; 4 = low pressure turbine; 5 = power turbine; where figure is given in brackets, this indicates the total number TURBOSHAFTS Manufacturer Allison Allison Allison Allison Changzhou General Electric General Electric General Electric General Electric Klimov Klimov LHTEC LHTEC MTU/Turbomeca/R-R Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada Pratt & Whitney Canada WSK-PZL Rzeszow WSK-PZL Rzeszow RKBM/Rybinsk Rolls-Royce Rolls-Royce Rolls-Royce Rolls-Royce Rolls-Royce Turbomeca Textron Lycoming Textron Lycoming Textron Lycoming Turbomeca Turbomeca Turbomeca ZMKB Progress Engine 250-C20 250-C28 250-C30/T703 T406-400 WZ6 T700-401/701C CT7-6 T64-419 GLC38/T407 TV3-117V TV7-117 T800-800 T800-801 MTR390 PW206A PW206B PT6B-35H PT6B-36B PT6T-3 PT6T-3BE PT6T-3B PT6T-3D PT6T-6/6B GTD-350 PZL-10W TVD-1500 Gem 42 Gem 60 Gem2Mk1004 Gnome 1400 RTM322 LTS101-750C T53-703/T5317A T55-712 Arriel 1C1 TM333-2B Makilia 1A1 D-136 Power is at take-off; sfc (specific fuel consumpt turbine; 5 = power turbine. Power sfc (kW) (ug/J) 313 109.8 375 102.4 485 100 4,590 70.9 1,150 1,410 78 1,490 82.8 3,540 80 4,790 64.2 1,660 96.3 1,870 924 76.7 1,080 78.4 960 76 477 91.7 422 94.4 670 94.4 730 98.1 1,340 100.5 1,340 101.4 1,340 101.4 1,428 100.5 1,470 99.8 300 136 660 97.1 970 63.2 835 109 1.000 103 705 1,240 102 1,720 76 510 97.5 1,110 101.4 2,800 89.5 520 96.8 89.4 1,400 8,490 110.8 on) is at take-off power; Dimensions (m) length diameter 0.98 1.02 1.04 1.52 - 1.17 1.17 2 1.55 2.08 2.14 0.85 0.85 1.08 0.91 1.04 1.52 1.5 1.67 1.67 1.67 1.67 1.67 1.39 1.88 1.25 1.1 1.1 1.1 1.39 1.17 0.79 1.21 1.18 1.09 0.53 1.4 2.72 1 = low 0.48 0.55 0.55 0.59 - 0.64 0.74 0.5 0.83 0.64 0.88 0.55 0.55 0.44 0.5 0.5 0.62 0.49 0.52 0.74 0.76 0.57 0.57 0.57 0.56 0.64 0.57 0.47 0.61 0.42 1.05 0.51 - of compressor and/or turbine stages. Configuration 1 6 -- (14) 1 5 (6) (14) 5 (10) 5 (2) (2) (2) (1) (1) 3 3 3 2xPT 3 3 2xPT -- -4 4 4 (10) 3 -- -- 0.45 -- -pressure compressor; 2 2 1 1 1 1 1 1 1 1 1 1 -1 1 -8 7 -1 1 1 1 2 6 8 2 3 -7 3 4 (2) (2) (2) 2 2 2 1 (2) (2) (2) (2) (2) (2) (2) (2) 1 2 (1) (1) 1 1 1 1 1 1 - 1 1 1 1 - 1 2 2 1 4 2 1 1 1 1 1 1 (2) (2) 1 1 2 2 2 2 2 1 1 1 4 2 1. 1 5 2 1- 2 -- 2 2 2 3 2 2 2 2 -1 1 -- -- -- -- -2 2 2 2 2 2 - • -2 - Application Various Eurocopter BO.105, Bell 206L Various Bell Boeing V-22 CAF Z-8 Various Bell 214ST, Sikorsky S-70, EH Industries EH101 Sikorsky CH/MH-53-E Offered for Boeing CH-47 Enhanced Various Mil Mi-38 Offered for Bell UH-1 re-engining Boeing/Sikorsky RAH-66 Comanche Eurocopter Tiger MDC Explorer and Eurocopter EC.135 Eurocopter EC.135 Aerospatiale Lama, Alouette III re-engining Sikorsky S-76B Bell 212, Agusta-Bell Sikorsky S-58T Bell 212, 412 Bell 212, 412SP, Agusta-Bell 212, 412SP Bell 412HP Bell 412, Sikorsky S-58T PZL Mi-2 Hoplite PZL W-3 Sokol Kamov Ka-62 Westland W30 Westland Lynx Agusta A.129 Westland Sea King EH Industries EH101 Bell 222 Bell AH-1S Boeing CH-47D, MH-47E Eurocopter AS.365N, Agusta AO.109K, Sikorsky S-76 Hindustan Aeronautics ALH Eurocopte: AS.332 Mil Mi-26 = high-pressure compressor; 3 = high-pressure turbine; 4 • low-pressure Figures in brackets are total number of low-pressure/high-pressure compressor or turbine stages. 40 FLIGHT INTERNATIONAL 8-14 June, 1994
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