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前緣延伸(英語:leading-edge extension,簡稱LEX)是飛行器機翼前緣向前延伸的部件,主要用於改善大迎角與低空速時的氣流,以控制、延緩失速現象。

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各類機翼前緣延伸

前緣延伸包括前緣縫翼、前緣鋸齒(dogtooth)、前緣翻邊(leading edge cuff)、前緣根部延伸(leading-edge root extension)等種類。[1][2]

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