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    • 1. 发明授权
    • Adaptively tuned vibration absorber for reduction of aircraft cabin noise
    • 适用于减少飞机机舱噪音的减振器
    • US5873559A
    • 1999-02-23
    • US839275
    • 1997-04-17
    • Andreas H. von FlotowMathieu MercadalKelvin B. ScribnerTimothy MixonCorydon Roeseler
    • Andreas H. von FlotowMathieu MercadalKelvin B. ScribnerTimothy MixonCorydon Roeseler
    • B64D27/26F16F7/10F16F15/02F16F15/04F16M7/00F16M13/00G01M7/00
    • F16F15/02F16F7/1005
    • An aircraft engine is attached to the fuselage by a mounting structure that has a vibration absorbing system which includes first and second sensors to produce signals indicating vibration along two orthogonal axes. A third sensor, such as an accelerometer, is coupled to the mounting structure for sensing vibration of the engine. A tachometer circuit, connected to the third sensor, produces first and second speed signals that indicate the speeds of two rotating spools in the engine. Four vibration absorbers are attached to the engine mounting structure and controllers are provided to dynamically tune the resonant frequency of each vibration absorber in response to a unique combination of one of the two vibration signals and one of the two speed signals. Thus the vibration absorbers reduce the engine spool vibrations that are transmitted through the mounting structure along the two orthogonal axes. The resonant frequency of each absorber is altered to track variation of the vibrations due to changes in engine speed.
    • 飞机发动机通过具有振动吸收系统的安装结构附接到机身,该系统包括第一和第二传感器,以产生指示沿两个正交轴线的振动的信号。 诸如加速度计的第三传感器联接到安装结构以感测发动机的振动。 连接到第三传感器的转速计电路产生指示发动机中两个旋转线轴的速度的第一和第二速度信号。 四个减振器连接到发动机安装结构,并且控制器被提供以响应于两个振动信号中的一个和两个速度信号之一的独特组合来动态地调节每个减振器的谐振频率。 因此,减振器减小沿着两个正交轴线传递通过安装结构的发动机线轴振动。 每个吸收器的谐振频率被改变以跟踪由于发动机转速变化引起的振动的变化。