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General Electric F118 : ウィキペディア英語版
General Electric F118

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, whilst a 2 stage LP turbine drives the 3 stage fan. The combustor is annular. In 1998, the USAF's Lockheed U-2 fleet was fitted with a modified version of the F118.〔Donald, David, ed. "U-2, The Second Generation". ''Black Jets''. AIRtime, 2003. ISBN 1-880588-67-6.〕

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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