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    PW2000

    Over the years, the Pratt&Whitney PW2000 engine was modified to improve performance and efficiency, and reduce CO2 and noise emissions (PW2000 Reduced Temperature Configuration - PW2043). The launch of the programme started up in 1979, and entry into service in 1984, while the last Boeing B757 that used the engine was produced in April 2005.

    Avio, partner of Pratt&Whitney, was responsible for the design and development of the accessory drive train and of the oil tank and is now responsible for the production of spare parts.

    The PW2000 is a turbofan twin-shaft engine with high-dilution ratio. It is equipped with a Full Authority Digital Electronic Control (FADEC) system. It has a twin-shaft configuration featuring:

    • high-pressure compressor with twelve axial stages 
    • two-stage high-pressure turbine
    • five-stage high-pressure turbine

    Main engine characteristics

    Max Power at SL 37.000 – 43.000 lb
    Fan diameter 78.5 inches
    Overall pressure ratio 27.6 - 31.2
    Bypass ratio 6.0

    Avio's module details

    Accessory Drive Train

    The accessory drive train includes the:

    • radial transmission that includes the inlet gearbox of motion and turret shaft
    • angular gearbox bolted to the accessories gearbox
    • accessories gearbox, mounted on the front of the engine, which drives 6 accessories of the engine and aircraft

     

     

    Other Components
    • The gearbox recovery oil pump is a pump with double-stage gears that makes the oil recovery from the accessories gearbox and angular gearbox
    • The oil tank is a separate module, supported by the engine fan case

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