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  2. CFE CFE738 - Wikipedia

    en.wikipedia.org/wiki/CFE_CFE738

    The CFE CFE738 is a small turbofan engine aimed at the business/commuter jet market manufactured by the CFE Company, and is used on the Dassault Falcon 2000. Design and development [ edit ]

  3. General Electric Passport - Wikipedia

    en.wikipedia.org/wiki/General_Electric_Passport

    The GE Passport is a high bypass ratio turbofan. The engine is a twin-spool, axial-flow turbofan with a high bypass ratio of 5.6:1 and an overall pressure ratio of 45:1. The front fan is attached to the three-stage low-pressure compressor; the 23:1 pressure ratio 10-stage high-pressure compressor includes five blisk stages for weight reduction.

  4. 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. Its architecture could be extended for a range of 8,000 to 10,000 lbf (36 to 44 ...

  5. Honeywell/ITEC F124 - Wikipedia

    en.wikipedia.org/wiki/Honeywell/ITEC_F124

    The F124 engine is a low-bypass, two-spool engine (meaning that there are two rotating shafts, a high-pressure shaft and a low-pressure shaft). The fan/low-pressure compressor has three stages with titanium blades. The first stage has 30 blades, [19] and the overall pressure ratio for the three-stage fan is 2.5:1. Some of the air is bypassed ...

  6. Garrett TFE731 - Wikipedia

    en.wikipedia.org/wiki/Garrett_TFE731

    The -5 model was certified in 1982, and a decade later, an engine utilizing the TFE731-5 power section and a TFE731-3 fan was built and designated the TFE731-4, intended to power the Cessna Citation VII aircraft. [4] The most recent version is the TFE731-50, based on the -60 used on the Falcon 900DX, which underwent its flight test program in ...

  7. Rolls-Royce BR700 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_BR700

    The engine has a maximum thrust of 16,900 lbf (75.2 kN). [9] The 50 in (130 cm) fan with 24 swept blades is 2 in (5.1 cm) larger than the BR710. The HP axial compressor benefits from three-dimensional aerodynamics for greater efficiency and has 10 stages including five blisks to reduce weight.

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    mail.aol.com

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  9. GE Honda HF120 - Wikipedia

    en.wikipedia.org/wiki/GE_Honda_HF120

    The engine has a wide-chord swept fan, two-stage low-pressure compressor and counter rotating high-pressure compressor based on a titanium impeller, for a 2,050 lbf (9.1 kN) takeoff thrust. [5] The HF120 engine's components interact with greater efficiency by incorporating 3D aerodynamic design, and its effusion-cooled combustor design emits ...