Английская Википедия:General Electric F118

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Шаблон:Short description

The General Electric F118 is a non-afterburning turbofan engine produced by GE Aviation, and is derived from the General Electric F110 afterburning turbofan.

Design and development

The F118 is a non-afterburning derivative of the F110 specially developed for the B-2 Spirit stealth bomber. A single stage HP turbine drives the 9 stage HP compressor, while a 2-stage LP turbine drives the 3 stage fan. The combustor is annular. In 1998, the USAF's Lockheed U-2S fleet was fitted with a modified version of the F118.[1]

Variants

F118-GE-100
Variant for the B-2[2]
F118-GE-101
Variant for the U-2S[2]

Applications

Specifications (F118-100)

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See also

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References

Notes

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Bibliography

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External links

Шаблон:Commons category

Шаблон:GE aeroengines Шаблон:USAF gas turbine engines

  1. Donald, David, ed. "U-2, The Second Generation". Black Jets. AIRtime, 2003. Шаблон:ISBN.
  2. 2,0 2,1 Taylor 1996, p 594