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  2. Rolls-Royce Trent 1000 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Trent_1000

    The Rolls-Royce Trent 1000 is a high ... The updated Trent 1000 TEN with technology from the Trent XWB and the ... Dry weight: 5,936–6,120 kg (13,087–13,492 lb ...

  3. Rolls-Royce Trent XWB - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Trent_XWB

    The higher-thrust XWB-97 for the A350-1000 remains a loss-maker, and could stay that way as extending time-on-wing is more profitable. [20] In 2023 Dubai Airshow, the president of the Emirates, Tim Clark, said the A350-1000's engine, Trent XWB-97, would offer only a quarter of the time between maintenance visits compared to their needs.

  4. Rolls-Royce Trent - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Trent

    The 62,264–81,028 lbf (276.96–360.43 kN) engine has a bypass ratio over 10:1, a 2.85 m (9 ft 4 in) m fan and keeps the characteristic three-spool layout of the Trent series. The updated Trent 1000 TEN with technology from the Trent XWB and the Advance3 aims for up to 3% better fuel burn, it first ran in mid-2014, was EASA certified in July ...

  5. After an Airbus A350 U-turned due to an engine problem ... - AOL

    www.aol.com/airbus-a350-u-turned-due-110341665.html

    A Rolls Royce Trent XWB-97 engine on a Qatar Airways A350-1000 at the 2023 Paris Air Show. Pete Syme/Business Insider. Rolls Royce's Trent XWB-97 is the sole engine choice for the A350-1000, the ...

  6. Rolls-Royce Trent 7000 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Trent_7000

    Its architecture comes from the latest version of the Trent 1000, the TEN, using the A330's Trent 700 experience and technology from the Trent XWB.The 68,000–72,000 lbf (300–320 kN) engine doubles the bypass ratio and halves emitted noise compared to the Trent 700. [2]

  7. Category:High-bypass turbofan engines - Wikipedia

    en.wikipedia.org/wiki/Category:High-bypass...

    Rolls-Royce Trent 900; Rolls-Royce Trent 1000; Rolls-Royce Trent 7000; Rolls-Royce Trent XWB; S. Safran Silvercrest; Shenyang WS-20; T. Turbomeca Astafan; W. Williams ...

  8. Thrust-specific fuel consumption - Wikipedia

    en.wikipedia.org/wiki/Thrust-specific_fuel...

    TSFC or SFC for thrust engines (e.g. turbojets, turbofans, ramjets, rockets, etc.) is the mass of fuel needed to provide the net thrust for a given period e.g. lb/(h·lbf) (pounds of fuel per hour-pound of thrust) or g/(s·kN) (grams of fuel per second-kilonewton). Mass of fuel is used, rather than volume (gallons or litres) for the fuel ...

  9. Rolls-Royce RB.50 Trent - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_RB.50_Trent

    RB.50 Trent A Rolls-Royce Trent ... Dry weight: 1,000 lb turbine unit, reduction gear 250lb, propeller 250 lb, total engine/propeller weight 1,500 lb [4] Components ...