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General Electric TF34

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This page is a soft redirect.A TF34 mounted on the starboard pylon of an S-3B Viking aboard USS Kitty Hawk (CV-63). #REDIRECTmw:Help:Magic words#Other
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TF34
Type

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This page is a soft redirect. Turbofan #REDIRECTmw:Help:Magic words#Other
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National origin

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Manufacturer

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This page is a soft redirect. General Electric #REDIRECTmw:Help:Magic words#Other
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First run

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This page is a soft redirect. 1971 #REDIRECTmw:Help:Magic words#Other
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Major applications

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This page is a soft redirect. A-10 Thunderbolt II
S-3 Viking #REDIRECTmw:Help:Magic words#Other
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Variants

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This page is a soft redirect. General Electric CF34 #REDIRECTmw:Help:Magic words#Other
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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.

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

Applications

Specifications (TF34)

General characteristics

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

Components

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

Performance

See also

Related development

Comparable engines
Related lists

References

  1. ^ "Fact Sheet: A-10 THUNDERBOLT II". USAF. 2012-05-21. Retrieved 27 May 2012. 
  2. ^ Fulghum, David A.; Bill Sweetman (14 December 2009). "Stealth over Afghanistan". Aviation Week (McGraw-Hill): 26–27. 

External links

Template:USAF gas turbine engines

pl:General Electric CF34