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General Electric TF34

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General Electric TF34

The General Electric TF34 is a military turbofan engine used on the A-10 Thunderbolt II and S-3 Viking. Developed by GE Aircraft Engines during the late 1960s, the original engine comprises a single stage fan, driven by a 4-stage low pressure (LP) turbine, supercharging a 14-stage high pressure (HP) compressor, driven by a 2-stage HP turbine. An annular combustor is featured. The TF34-GE-400A is rated at 9,275 lbf (41.26 kN) static thrust.

Contents

The civilian variant, the CF34, is used on a number of business and regional jets.

Applications

  • A-10 Thunderbolt
  • S-3 Viking
  • Sikorsky S-72
  • Lockheed Martin RQ-170 Sentinel - possible, not confirmed.

    • General characteristics

  • Type: twin-shaft, bypass turbofan engine
  • Length: 103 in (2.62 m)
  • Diameter: 49 in (1.24 m)
  • Dry weight: 1670 lb (757 kg)

    • Components

  • Compressor: single-stage fan, 14 stage HP axial flow compressor
  • Combustors: annular
  • Turbine: 4 stage LP, 2 stage HP

    • Performance

  • Maximum thrust: 9,250 lbf (41.2 kN)
  • Thrust-to-weight ratio: 5.6:1

    • References

    General Electric TF34 Wikipedia
    (Text) CC BY-SA


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