Allison 250 B17c Parts Manual

Allison 250 B17c Parts Manual

link: https://bytlly.com/1tehq7

The Model 250 has been produced by Rolls-Royce since it acquired Allison in 1995.. As a result, nearly 30,000 Model 250 engines have been produced, making the Model 250 one of the highest-selling engines made by Rolls-Royce.. 6 :1Takeoff power: 650 WPSContinuous power: 501 WPSHeight: 638 mmWidth: 555 mmLength: 1041 mmC30PWeight: 114 kgAirflow rate: 2.. 54 kg/sPressure ratio: 8 6 :1Takeoff power: 650 WPSContinuous power: 540 WPSHeight: 638 mmWidth: 555 mmLength: 1041 mmC30SWeight: 114 kgAirflow rate: 254 kg/sPressure ratio: 8.. Some of the earlier versions have axial compressor stages mounted on the HP shaft to supercharge a relatively low pressure ratio centrifugal compressor.. 733 kg/sPressure ratio: 7 9 :1Takeoff power: 450 WPSContinuous power: 380 WPSC30MWeight: 115 kgAirflow rate: 2.. 733 kg/sPressure ratio: 7 9 :1Takeoff power: 450 WPSContinuous power: 380 WPSHeight: 589 mmWidth: 528 mmLength: 986 mmB17DWeight: 90 kgAirflow rate: 1.. 68TP variants - Spartacus & Viator Soloy Cessna 206 turbine conversionRotary-wingAgusta A109A Bell 206B/L/LT Bell 407 Bell 222SP Bell 230 Bell 430 Bell OH-58 Kiowa Bell YOH-4 Boeing AH-6 Cicaré CH-14 Enstrom 480 Eurocopter AS350 Soloy AS350RM AllStar Eurocopter AS355F Fairchild Hiller FH-1100 Hughes OH-6 Cayuse MBB Bo 105 MD Helicopters MD 500 MD Helicopters MD 600 MD Helicopters MH-6 Little Bird Northrop Grumman MQ-8 Fire Scout PZL Kania PZL SW-4 Schweizer 330/330SP Schweizer S-333 Sikorsky S-76 Kamov Ka-226OthersLoral GZ-22, non-rigid airship MTT Turbine Superbike, motorcycleSpecifications: T63-A-5Type: Turboshaft Length: 40.. 2:1, at an airflow of 6 1 lb/s (2 8 kg/s), and developing, at the shaft, 715 hp (533 kW).. Allison250-C20 / T63 / T703Rolls-Royce M250The Allison Model 250, known as the Rolls-Royce M250, (US military designations T63 and T703) is a successful turboshaft engine family, originally developed by the Allison Engine Company in the early 1960s.. One of the latest versions of the Model 250 is the -C40, which has a centrifugal compressor pulling a pressure ratio of 9.. MTU-built Allison 250-C20BVariants:250-B15250-B15A250-B15C250-B17250-B17B250-B17C250-B17D250-B17F250-B17F/1250-B17F/2250-C18250-C18A250-C20250-C20B250-C20F250-C20J250-C20R250-C20R/1250-C20R/2250-C20R/4250-C20S250-C20W250-C22B250-C28250-C28B250-C28C250-C30250-C30G250-C30G/2250-C30M250-C30P250-C30R250-C30R/3250-C30R/3M250-C30S250-C30U250-C34250-C40B250-C47B250-C47E250-C47MT63-A-5T63-A-5AT63-A-700T63-A-720T703-AD-700Applications: Fixed-wingBeechcraft Bonanza {Prop-jet conversions} Britten-Norman BN-2T Turbine Islander Extra EA-500 GAF Nomad Gippsland GA10 Partenavia AP.. 0 lb/s (1 8 kg/s), with a power output, at the shaft, of 450 hp (340 kW) The Model 250 powers a large number of helicopters, small aircraft and even a motorcycle (MTT Turbine Superbike).. 5 in (1,029 mm) Diameter: 22 5 in (572 mm) Dry weight: 136 lb (62 kg) dryCompressor: 6-stage axial + 1-stage Centrifugal compressors Combustors: Single can combustion chamber Turbine: 2-stage axial gas generator power turbine + 2-stage axial free-power output turbine Fuel type: JP-4 Aviation kerosene (alternatively JP-1 or JP-5) Oil system: pressure spray/splash, dry sumpMaximum power output: 250 hp (190 kW) for Take-off, sea level 59 °F (15 °C) Overall pressure ratio: 6.. 2:1 Turbine inlet temperature: 1,805 °F (985 °C) Specific fuel consumption: 0 77 lb/hp-hr (0.. The -C20R is typical, pulling an overall pressure ratio of 8 0:1, at an airflow of 4.. 468 kg/kW-hr) at 90% power cruise rating Power-to-weight ratio: 1 838 hp/lb (3 022 kW/kg)C20B/F/JWeight: 73 kgAirflow rate: 1.. Allison adopted a reverse airflow engine configuration for the Model 250: although air enters the intake/compression system in the conventional fashion, the compressed air leaving the centrifugal compressor diffuser is ducted rearwards around the turbine system, before being turned through 180 degrees at entry to the combustor; the combustion products expand through the two stage HP turbine, which is connected, via the HP shaft, to the compression system, before expanding through the two stage power turbine; the exhaust gases then turn through 90 degrees to exit the engine in a radial direction; a stub shaft connects the power turbine to a compact reduction gearbox, located inboard, between the centrifugal compressor and the exhaust/power turbine system.. 230 kg/sPressure ratio: 6 2 :1Takeoff power: 420 WPSContinuous power: 317 WPSHeight: 571 mmWidth: 483 mmLength: 986 mmC20RWeight: 78 kgAirflow rate: 1.. 624 kg/sPressure ratio: 7 2 :1Takeoff power: 420 WPSContinuous power: 370 WPSB17FWeight: 93 kgAirflow rate: 1. b0d43de27c
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