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  2. Rolls-Royce Trent 1000 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Trent_1000

    Trent 1000 Engine on British Airways Boeing 787-10. The Trent 1000 is a high bypass turbofan with three independent, coaxial shafts and a single annular combustor with 18 spray nozzles. The Low Pressure shaft with a swept-bladed, 2.85 m (9 ft 4 in) fan is powered by six axial turbines.

  3. 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 ...

  4. Rolls-Royce Trent XWB - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Trent_XWB

    The Rolls-Royce Trent XWB is a high-bypass turbofan produced by Rolls-Royce Holdings.In July 2006, the Trent XWB was selected to exclusively power the Airbus A350. [2] The first engine was run on 14 June 2010, [3] it first flew on an A380 testbed on 18 February 2012, [4] was certified in early 2013, [5] and first flew on an A350 on 14 June 2013. [6]

  5. 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 ...

  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. Thrust-specific fuel consumption - Wikipedia

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

    Thrust-specific fuel consumption (TSFC) is the fuel efficiency of an engine design with respect to thrust output. TSFC may also be thought of as fuel consumption (grams/second) per unit of thrust (newtons, or N), hence thrust-specific.

  8. Category:Rolls-Royce aircraft gas turbine engines - Wikipedia

    en.wikipedia.org/wiki/Category:Rolls-Royce...

    Rolls-Royce Trent 900; Rolls-Royce Trent 1000; Rolls-Royce Trent 7000; Rolls-Royce Trent XWB; Rolls-Royce Tyne; V. Armstrong Siddeley Viper; W. Rolls-Royce Welland

  9. General Electric GEnx - Wikipedia

    en.wikipedia.org/wiki/General_Electric_GEnx

    GEnx on 747-8I prototype. As of 2016, the GEnx and the Rolls-Royce Trent 1000 were selected by Boeing following a run-off between the three big engine manufacturers. The GEnx uses some technology from the GE90 turbofan, [1] including swept composite fan blades and the 10-stage high-pressure compressor (HPC) featured in earlier variants of the engine.