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| gas turbine numerology (不含外涵道的燃气涡轮发动机的各部分分别用数字0〜9来标记。其中0指的是进气道之前的自由流动区,9则表示核心发动机尾喷口处的排气状态，1〜8分别指进气扩散道、进气道、风扇、压缩机、燃烧室、涡轮、排气道及排气喷管。如发动机具有多个压缩机或涡轮，则这个额外的部件就用4.5, 5. 5等小数来表示) | |||
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