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Williams FJ33 : ウィキペディア英語版 | Williams FJ33
The Williams FJ33 is a family of turbofan jet engines intended for use in very light jet aircraft. The FJ33 is a scaled-down version of the FJ44 engine. ==Design== Engine configuration is believed to be a single stage fan, with booster stage/s, driven by a 2 stage LP turbine, supercharging a centrifugal HP compressor, driven by a single stage HP turbine. An annular combustor is featured. The FJ33 has a dry weight of less than , overall diameter of , overall length, and produces between and static thrust. Specific fuel consumption at thrust (SLS, ISA) is understood to be .
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Williams FJ33」の詳細全文を読む
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