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    • 5. 发明申请
    • NOISE REDUCING DEVICE AND JET PROPULSION SYSTEM
    • 噪声降低装置和喷射推进系统
    • US20110000181A1
    • 2011-01-06
    • US12918899
    • 2009-02-25
    • Tsutomu OishiYoshinori Oba
    • Tsutomu OishiYoshinori Oba
    • F02G1/00F01N1/14
    • F02K3/06B64C7/02B64D27/18F02K1/34F02K1/44F02K1/46F05D2260/96
    • A noise reducing device in a jet engine that has a cylindrical casing, a cylindrical partition wall that is inserted in the casing while protruding partially from a trailing edge of the casing, and a compressor that compresses air that is taken into the cylindrical partition wall, with the inside of the cylindrical partition wall serving as a duct in which a core stream of high-speed air flows, and the space between the cylindrical partition wall and the casing serving as a duct in which a bypass stream of low-speed air flows, and being connected with a wing of an airplane by a pylon that has a projection portion that extends beyond the casing to the downstream of the core stream and the bypass stream, the noise reducing device includes a nozzle, disposed at the pylon on the downstream of the core stream, that injects a fluid toward a noise generation source that is produced from the mutual approach of an ambient air stream that is produced outside of the bypass stream and the core stream.
    • 一种喷气式发动机中的降噪装置,具有圆筒形壳体,一部分从壳体的后缘突出地插入壳体中的圆筒形分隔壁,以及压缩器,该压缩机压缩进入圆筒形分隔壁的空气, 其中圆筒形分隔壁的内部用作高速空气的核心流动的管道,以及圆柱形分隔壁和用作低压空气流动的旁路流的管道的壳体之间的空间 并且通过具有延伸超过壳体的突出部分到芯流和下游流的下游的塔架与飞机的翼连接,降噪装置包括设置在下游的塔架处的喷嘴 的核心流,其将流体朝向由旁路流外部产生的环境空气流的相互接近产生的噪声产生源和核心层 电子邮件