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Noise shield for stationary jet aircraft - uses shroud of triangular panels covers rear end of aircraft to reduce ambient noise

机译:固定式喷气飞机的隔音罩-使用三角形面板罩覆盖飞机的后端以减少环境噪声

摘要

A noise shielding system is for use with stationary jet engine aircraft that is capable of use with a wide range of aircraft types. For aircraft with wing mounted engines, two triangular panel sections are inclined symmetrically to each other and are joined along one edge. Additional panel sections join the leading edge of each main panel section. The complete assembly may be free standing on the ground or else fixed to a base section. An aperture at the rear end provides a passage for exhaust gases. Providing that the aircraft is located at a specified distance into the shroud the ambient noise level is considerably attenuated.
机译:噪声屏蔽系统用于固定式喷气发动机飞机,该飞机能够与多种飞机类型一起使用。对于装有机翼发动机的飞机,两个三角形面板部分彼此对称倾斜,并沿一个边缘连接。其他面板部分连接每个主面板部分的前端。整个组件可以在地面上自由站立,也可以固定在基座上。后端的孔提供了排气通道。假设飞机位于距护罩一定距离处,则环境噪声水平会大大降低。

著录项

  • 公开/公告号FR2261180B3

    专利类型

  • 公开/公告日1977-10-28

    原文格式PDF

  • 申请/专利权人 MEYER THOMAS;

    申请/专利号FR19750004654

  • 发明设计人

    申请日1975-02-14

  • 分类号B64F1/26;

  • 国家 FR

  • 入库时间 2022-08-22 23:52:04

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