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    GE90

    The GE90 engine family powers Boeing’s B777 aircraft. Even today, the GE90 is the sole engine to equip the long-range aircraft, the B777-300ER “Extended Range” and 777-200LR “Longer Range” that, in the 115B version, is certified for a thrust of 115,000 lb (c. 52,000 kg).

    To date, the GE90-115 is the largest and most powerful turbo-jet ever produced for commercial use.

    Avio is partner of GE with an 8% share for the design, development and production of the accessory drive train and some components of the low-pressure turbine. 

    Main engine characteristics

    Max Power at SL from 76.000 to 115.000 lb
    Max Fan Diameter 135 inches

    Leaflet - GE90


    Avio's module details

    Accessory Drive Train

    Avio is responsible for the design, development, production and MRO of the accessory drive train (transmission command accessories), a sector where Avio is world leader.

    The accessory drive train includes:

    • inlet gearbox: takes motion from the fan and transfers it through the radial shaft to the transfer gearbox
    • transfer gearbox: transfers motion from the radial shaft to the horizontal shaft
    • accessory gearbox: transfers motion from the horizontal shaft to the 8 accessories of the engine and aircraft

     

    Low Pressure Turbine

    Avio, under the aegis of GE, is responsible for the design and development of the sixth-stage rotor blade and production of some components of the low-pressure turbine (from second- to sixth-stage stator blades, sixth-stage disc and rotor blade).

    Main features of the low-pressure turbine

    The basic architecture of the low-pressure turbine module derives from previous versions of the GE90, preserving the flow path and existing mechanical interfaces.

    The main features include:

    Rotors:

    • Inclusion in the early stages of materials able to withstand increased operating temperatures
    • Reduced calculation of aerodynamic profiles consistent with the objective of reducing full volumes in the turbine project
    • Re-designing the sixth stage to reduce weight and increase efficiency compared to its predecessor, the GE90-92B


    Stators:

    • Inclusion in the early stages of materials able to withstand increased operating temperatures
    • Reduced calculation of aerodynamic profiles consistent with the objective of reducing full volumes

     

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