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    • 10. 发明申请
    • DEVICE FOR REDUCING NOISE GENERATED BY AN AIRCRAFT JET ENGINE WITH CURVE DUCTS
    • 用于降低飞机喷气发动机产生的噪音的装置
    • US20110042162A1
    • 2011-02-24
    • US12935423
    • 2009-03-31
    • Jerome HuberJean-Paul BonnetJoel DelvillePeter JordanFrancois Strekowski
    • Jerome HuberJean-Paul BonnetJoel DelvillePeter JordanFrancois Strekowski
    • F01N1/14
    • F02K1/46F02K1/34F05D2240/40
    • A jet engine, including a wall surrounding a first gas flow ejected from a downstream end of the wall along a longitudinal axis, a second flow of gas running outside the wall in a direction of ejection of the first gas flow, at least one duct arranged on the periphery of the downstream end of the wall which is desired to eject a gas flow for interacting with one and/or the other gas flow, the at least one duct including a terminal section provided at the free end thereof with an outlet opening through which the fluid is ejected. The terminal section successively includes a first section of straight duct aligned along a median axis and a second duct section forming a bend relative to the straight section, the second portion having a free end provided with the outlet opening and sufficiently close to the median axis of the first section to give the terminal section a reduced restriction in a direction of formation of the bend.
    • 一种喷气发动机,包括围绕沿着纵向轴线从壁的下游端喷出的第一气流的壁,在第一气流的喷射方向上在壁外延伸的第二气体流,至少一个管道,其布置 在壁的下游端的周边上,其期望喷射与一个和/或另一个气流相互作用的气流,所述至少一个管道包括在其自由端设置有出口开口的端子部分 流体被喷射。 端子部分依次包括沿着中间轴对准的直管道的第一部分和相对于直线部分形成弯曲部的第二管道部分,第二部分具有设置有出口开口的自由端,并且足够接近中心轴 使端子部分在形成弯曲方向上的限制减小的第一部分。