首页> 外国专利> NOISE ABSORPTION EQUIPMENT OF JET PROPULSION MECHANISM FOR SUPERSONIC AIRCRAFT

NOISE ABSORPTION EQUIPMENT OF JET PROPULSION MECHANISM FOR SUPERSONIC AIRCRAFT

机译:超音速飞机射流推进机理的噪声吸收设备

摘要

PURPOSE: To maintain a noise absorption function of noise absorption equipment at high temperature so as to reduce the volume of jet noise by providing a noise absorption material made of perforated plate and honeycomb positioned between a nozzle plate and a liner, and cooling the noise absorption equipment by cool air injected into the honeycomb through pores of the perforated plate along the nozzle plate. ;CONSTITUTION: This equipment comprises a nozzle plate 5, a liner 1, a perforated plate 4, a honeycomb 2 or the like. A noise absorption material is made of the honeycomb 2 and the perforated plate 4. On one surface of the honeycomb 2 positioned between the nozzle plate 5 and the liner 1, the perforated plate 4 is attached. On the other surface, a spacing side of the liner 1 is attached. A plurality of holes 11 are provided on the perforated plate 4 for introducing cool air injected from pores 10 of the perforated plate 4 into the honeycomb 2 and running against the spacing portion of the liner 1 into a fuel path through the holes 11. Thermal breakage caused by increasing temperature is prevented and a noise absorption function can be maintained.;COPYRIGHT: (C)1996,JPO
机译:目的:通过提供由多孔板和蜂窝状材料制成的吸声材料置于喷嘴板和衬套之间,并冷却吸声材料,在高温下保持吸声设备的吸声功能,从而减少喷射噪声的量。设备是通过沿喷嘴板从多孔板的孔中注入到蜂窝中的冷空气来完成的。组成:该设备包括喷嘴板5,衬板1,穿孔板4,蜂窝2等。吸音材料由蜂窝2和多孔板4制成。在蜂窝2的位于喷嘴板5和衬套1之间的一个表面上,附有多孔板4。在另一表面上,衬里1的间隔侧被附接。在多孔板4上设置有多个孔11,用于将从多孔板4的孔10注入的冷空气引入到蜂窝2中,并且与衬里1的间隔部分相通地穿过孔11进入燃料路径。防止由于温度升高引起的噪音并保持噪音吸收功能。;版权所有:(C)1996,日本特许厅

著录项

  • 公开/公告号JPH08135505A

    专利类型

  • 公开/公告日1996-05-28

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY IND LTD;

    申请/专利号JP19950225093

  • 发明设计人 KISHI KIMIHIRO;

    申请日1995-09-01

  • 分类号F02K1/82;

  • 国家 JP

  • 入库时间 2022-08-22 04:00:00

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