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Process and device for reducing the spectral line noise inside an aircraft, especially a rotating-wing aircraft, in particular a helicopter

机译:用于降低飞机,特别是旋翼飞机,特别是直升机内部频谱线噪声的方法和装置

摘要

Process and device for reducing the spectral line noise inside an aircraft, especially a rotating-wing aircraft, in particular a helicopter. ;Said device (1) comprises sensors (Ca, Cb) for measuring the values of vibratory and/or acoustic parameters, controllable mechanical elements (A) forming secondary sources of noise, and a main computer (CAL) determining, on the basis of the values measured by the sensors (Ca, Cb), control commands for the mechanical elements (A), as well as at least one reference sensor (CO) for measuring a reference parameter which is correlated with the noise, and possibly an auxiliary computer (4) for calculating, on the basis of the values measured by the reference sensor (CO), a reference signal, and said main computer (CAL) determines the control commands by carrying out filtering with respect to the reference signal.
机译:用于减少飞机,特别是旋翼飞机,特别是直升机内的频谱线噪声的方法和装置。 ;所述设备( 1 )包括用于测量振动和/或声学参数值的传感器(Ca,Cb),形成次级噪声源的可控机械元件(A)和主计算机(CAL )根据传感器(Ca,Cb)测得的值,确定机械元件(A)的控制命令,以及至少一个用于测量与传感器相关的参考参数的参考传感器(CO)噪声,可能还有一台辅助计算机( 4 ),用于根据参考传感器(CO)测得的值计算参考信号,并且所述主计算机(CAL)确定控制命令通过对参考信号进行滤波。

著录项

  • 公开/公告号US2001005814A1

    专利类型

  • 公开/公告日2001-06-28

    原文格式PDF

  • 申请/专利权人 DUSSAC MARC;

    申请/专利号US20000730541

  • 发明设计人 MARC DUSSAC;

    申请日2000-12-07

  • 分类号G01L7/00;

  • 国家 US

  • 入库时间 2022-08-22 01:07:32

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