Assembly and method for aircraft engine noise reduction
    1.
    发明授权
    Assembly and method for aircraft engine noise reduction 有权
    飞机发动机降噪装配和方法

    公开(公告)号:US07047725B2

    公开(公告)日:2006-05-23

    申请号:US10446896

    申请日:2003-05-28

    IPC分类号: B64F1/26

    摘要: An assembly useful in reducing aircraft engine noise such as turbofan engine noise comprises: (a) a core portion comprising at least one entrance end and at least one exit end for the passage of acoustic energy therethrough; (b) a first member having an exterior face and an interior face, wherein the first member is adjacent to at least a part of the core portion, and the first member has a plurality of openings therein to permit the passage of acoustic energy therethrough; and (c) a second member having an exterior face and an interior face, wherein the interior face of the second member is adjacent to the core portion. The core portion may be a honeycomb acoustic structure, and the first member may be perforated to permit the passage of acoustic energy into and out of the conduit portion.

    摘要翻译: 用于减少飞机发动机噪声(诸如涡扇发动机噪声)的组件包括:(a)芯部,包括至少一个入口端和至少一个出口端,用于使声能通过其中; (b)具有外表面和内表面的第一构件,其中所述第一构件与所述芯部的至少一部分相邻,并且所述第一构件在其中具有多个开口以允许声能通过其中; 和(c)具有外表面和内表面的第二构件,其中第二构件的内表面与芯部分相邻。 核心部分可以是蜂窝声学结构,并且第一构件可以被穿孔以允许声能进入和离开导管部分。

    Fan noise reduction from turbofan engines using adaptive
Herschel-Quincke tubes
    3.
    发明授权
    Fan noise reduction from turbofan engines using adaptive Herschel-Quincke tubes 失效
    使用自适应Herschel-Quincke管的涡扇发动机的风扇降噪

    公开(公告)号:US6112514A

    公开(公告)日:2000-09-05

    申请号:US159634

    申请日:1998-09-24

    摘要: An array of adaptive or fixed Herschel-Quincke tubes aligned in a circumferential or helical array about an inlet of a turbofan engine. The array of tubes effectively divide the acoustic energy generated by the engine. One of the energy components propagates within the tubes while the other propagates within the engine compartment. At some time certain, the acoustic energy in the tubes is reintroduced into the engine compartment to cancel the acoustic energy remaining in the engine as it propagates from the fan towards the inlet and outlet openings.

    摘要翻译: 一组自适应或固定的赫歇尔 - 奎因(Herschel-Quincke)管围绕涡轮风扇发动机的入口以圆周或螺旋阵列排列。 管阵列有效地分割发动机产生的声能。 其中一个能量部件在管内传播,而另一个在发动机舱内传播。 在某些时候确定的是,管中的声能被重新引入发动机舱,以消除当发动机从风扇向入口和出口开口传播时剩余的声能。

    Active dual reaction mass absorber for vibration control
    4.
    发明授权
    Active dual reaction mass absorber for vibration control 失效
    用于振动控制的主动双重反作用吸收体

    公开(公告)号:US5884736A

    公开(公告)日:1999-03-23

    申请号:US825614

    申请日:1997-03-31

    IPC分类号: F16F7/10

    CPC分类号: F16F7/1011

    摘要: An active vibration absorber including a frame connected to a structure to be controlled and at least two reaction mass elements operatively connected to the frame. Each of the reaction mass elements is independently movable with respect to said frame. The absorber includes a force generating member for controlling relative movement between the reaction mass elements for damping vibration of the structure. The inventive dual reactive mass absorber requires less control force to produce the same vibration attenuation as conventional single reactive mass absorbers.

    摘要翻译: 一种主动减震器,包括连接到待控制的结构的框架和至少两个可操作地连接到框架的反作用质量元件。 每个反应质量元件可相对于所述框架独立地移动。 吸收器包括用于控制用于阻尼结构的振动的反作用质量元件之间的相对运动的力产生构件。 本发明的双反电池吸收器需要较少的控制力以产生与常规单个反作用质量吸收器相同的振动衰减。