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Noise in the main cabin of active damping system and aircraft and/or the reduced method of vibration

机译:主动阻尼系统和飞机主舱内的噪音和/或减少的振动方法

摘要

Active Vibration Control System( 110 )Including multiple actuators( 150-155 )It is corresponding,And close to each engine( 102 )Aircraft( 100 ),At least one sensor( 650 )In the main cabin for being located at aircraft( 100C ) ( 100 ),And be configured to the vibration of detection amplitude and frequency and sound generate it is one or more by respective engine( 102 ),And generate one or more vibrations and acoustic feedback signal,Controller( 500 )It is connected to multiple actuators( 110 )0 and at least one each described sensor( 110 )1,Controller( 110 )2 are configured to realize multiple actuators that control is no more than two( 110 )3 ( 110 )4 each engines are based on the feedback signal and are being no more than two actuators( 110 )5 effects inhibit one or more vibrations and the respective engine of sound due to the respective engine of rotary shaft( 110 )6.
机译:主动振动控制系统(110)包括多个执行器(150-155)相对应,并靠近每个发动机(102)飞机(100),至少一个传感器(650)在主舱内,用于飞机(100C) )(100),并被配置为检测振幅,频率和声音的振动,由相应的引擎(102)产生一个或多个,并产生一个或多个振动和声音反馈信号,控制器(500)连接到多个致动器(110)0和至少一个各自描述的传感器(110)1,控制器(110)2被配置为实现多个致动器,其控制不超过两个(110)3(110)4,每个发动机基于反馈信号并且是不超过两个致动器(110)5的效果会抑制一个或多个振动,并且由于旋转轴(110)6的各个引擎会抑制声音的各个引擎。

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