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Bypass duct fairing for low bypass ratio turbofan engine and turbofan engine having the same

机译:低旁通比涡轮风扇发动机的旁通整流罩及具有该旁通整流罩的涡轮风扇发动机

摘要

A fairing installed in a bypass duct defined between an outer casing and an inner casing around an axis of a turbofan engine to make compressed air bypass a low pressure compressor is comprised of a fore section elongated aftward from the inner casing at an inlet of the bypass duct and running along an internal periphery of the outer casing; and an aft section elongated aftward in succession to the fore section and curved in a direction getting away from the internal periphery.
机译:整流罩安装在绕涡轮风扇发动机的轴线限定在外壳和内壳之间的旁通管道中,以使压缩空气绕过低压压缩机,该整流罩由在旁通入口处从内壳向后延伸的前部部分组成。导管并且沿着外壳的内周延伸;尾部与前部相继向后延伸,并向远离内周的方向弯曲。

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