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  2. Turbofan - Wikipedia

    en.wikipedia.org/wiki/Turbofan

    The core (or gas generator) of the engine must generate enough power to drive the fan at its rated mass flow and pressure ratio. Improvements in turbine cooling/material technology allow for a higher (HP) turbine rotor inlet temperature, which allows a smaller (and lighter) core, potentially improving the core thermal efficiency.

  3. Rolls-Royce AE 3007 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_AE_3007

    The AE 3007 is a direct drive turbofan engine with a single stage fan, ... Gas generator rpm 15,196–15,452: 15,452–16,245 Length 115.08 in (292.3 cm) Width

  4. CFE CFE738 - Wikipedia

    en.wikipedia.org/wiki/CFE_CFE738

    Chosen to power the Falcon 2000 in 1990, the engine was also first run in May 1990, [1] and it was first flown on a Boeing 727 testbed on 31 August 1992. [2] The CFE738-1 made its inaugural flight on a Falcon 2000 prototype on March 4, 1993.

  5. CFM International CFM56 - Wikipedia

    en.wikipedia.org/wiki/CFM_International_CFM56

    The CFM56 is a high-bypass turbofan engine (most of the air accelerated by the fan bypasses the core of the engine and is exhausted out of the fan case) with several variants having bypass ratios ranging from 5:1 to 6:1, generating 18,500 to 34,000 lbf (80 kN to 150 kN) of thrust. The variants share a common design, and differ only in details.

  6. Honeywell HTF7000 - Wikipedia

    en.wikipedia.org/wiki/Honeywell_HTF7000

    The Honeywell HTF7000 is a turbofan engine produced by Honeywell Aerospace.Rated in the 6,540–7,624 lbf (29.09–33.91 kN) range, the HTF7000 is used on the Bombardier Challenger 300/350, Gulfstream G280, Embraer Legacy 500/450 and the Cessna Citation Longitude.

  7. General Electric GE9X - Wikipedia

    en.wikipedia.org/wiki/General_Electric_GE9X

    The engine, with a fan diameter of 134 in (340 cm), is installed in a 174 in (440 cm) diameter nacelle, with 1.5 ft (0.46 m) of ground clearance. [17] The engine and nacelle weighed 40,000 lb (18 t) with its new pylon and wing strengthening, compared to 17,000 lb (7.7 t) for the CF6-80C2s and its pylon.

  8. General Electric TF39 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_TF39

    This tip-turbine driven lift-fan concept was turned 90 degrees and developed as an 80-inch-diameter "cruise fan" demonstrator, driven by a J79 gas generator. [4] For the CX-X program GE demonstrated a half-scale engine, the GE1/6, with 15,830 lb thrust and an sfc of 0.336. [8] This was developed into the TF39 with a 97 in diameter fan.

  9. Williams FJ33 - Wikipedia

    en.wikipedia.org/wiki/Williams_FJ33

    Engine configuration is a single stage fan, with booster stage, driven by a two-stage LP turbine, supercharging a centrifugal HP compressor, driven by a single stage HP turbine. [3] An annular combustor is featured.