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  3. General Electric F404 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_F404

    The KAI T-50 Golden Eagle uses a single General Electric F404-GE-102 turbofan engine with Full Authority Digital Engine Control (FADEC) system; the engine is similar to the F404-402, but with additional redundancies built in for single-engine operations. The aircraft has a maximum speed of Mach 1.5.

  4. General Electric F101 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_F101

    The General Electric F101 is an afterburning turbofan jet engine. It powers the Rockwell B-1 Lancer strategic bomber fleet of the USAF. In full afterburner it produces a thrust of more than 30,000 pounds-force (130 kN). The F101 was GE's first turbofan with an afterburner. [1]

  5. General Electric F414 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_F414

    The General Electric F414 is an American afterburning turbofan engine in the 22,000-pound (98 kN) thrust class produced by GE Aerospace (formerly GE Aviation). The F414 originated from GE's widely used F404 turbofan, enlarged and improved for use in the Boeing F/A-18E/F Super Hornet.

  6. General Electric CF6 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_CF6

    This initial version of the CF6 has a single-stage fan with one core booster stage, driven by a 5-stage LP (low pressure) turbine, turbocharging a 16-stage HP (high pressure) axial compressor driven by a 2-stage HP turbine; the combustor is annular; separate exhaust nozzles are used for the fan and core airflows. The 86.4-in (2.19-m) diameter ...

  7. E-102 - Wikipedia

    en.wikipedia.org/wiki/E-102

    E-102 can refer to: E-102 Gamma, a character in the Sonic the Hedgehog video game series. E102, the E number for tartrazine This page was last edited on 11 ...

  8. Lycoming ALF 502 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_ALF_502

    LF511D: An 11,000 lbf thrust (49 kN) turbofan with a 43 in diameter (1.09 m) wide-chord fan, a three-stage power turbine, and a three-stage low-pressure booster compressor [7] LF512 / LF514: Additional turbofan engines of 12,000–14,000 lbf (53–62 kN) thrust, possibly for Avro 's proposed 120-seat RJX twin airliner or for a stretched version ...

  9. CFM International CFM56 - Wikipedia

    en.wikipedia.org/wiki/CFM_International_CFM56

    Research into the next generation of commercial jet engines, high-bypass ratio turbofans in the "10-ton" (20,000 lbf; 89 kN) thrust class, began in the late 1960s. Snecma (now Safran), who had mostly built military engines previously, was the first company to seek entrance into the market by searching for a partner with commercial experience to design and build an engine in this class.