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    • 5. 发明授权
    • Actively controlled acoustic treatment panel
    • 主动控制声学处理面板
    • US5702230A
    • 1997-12-30
    • US603850
    • 1996-01-29
    • Robert E. KraftAsif A. Syed
    • Robert E. KraftAsif A. Syed
    • F01D25/04F02C7/045F02K1/82G10K11/178
    • G10K11/1788F01D25/04F02C7/045F02K1/827B64D2033/0206B64D2033/0286F05D2260/96G10K2210/107G10K2210/109G10K2210/1281G10K2210/3046G10K2210/3224G10K2210/3227
    • An actively controlled acoustic treatment panel for suppressing noise in a gas turbine engine nacelle including a backsheet formed by a planar matrix of adjacent individually controllable elements, where each of the controllable elements has a transducer and a honeycomb cell enclosing the transducer. A facesheet is also bonded to the controllable elements. A plurality of sensors are positioned within the acoustic treatment panel for sensing acoustic pressure of the noise propagated against the facesheet. A driver is provided for electrically driving each of the transducers to effect displacement thereof in a direction substantially perpendicular to the facesheet. Circuitry is also operatively connected to the pressure sensors and the driver for controlling velocity magnitude and phase of the transducers during displacement, wherein a resulting acoustic impedance at the facesheet achieves a desired acoustic impedance boundary condition at the nacelle. The transducer is further made up of an inner lamination layer, an outer lamination layer, and a piezoelectric membrane positioned between the inner and outer lamination layers, wherein a plurality of aligned openings are provided in the inner and outer lamination layers so that the piezoelectric membrane can be displaced either toward or away from the facesheet.
    • 一种用于抑制燃气涡轮发动机舱中噪声的主动控制的声处理板,包括由相邻独立可控元件的平面矩阵形成的底片,其中每个可控元件具有换能器和包围换能器的蜂窝电池。 面板也结合到可控元件上。 多个传感器位于声处理面板内,用于感测抵靠面板传播的噪声的声压。 提供驱动器,用于电驱动每个换能器以在基本上垂直于面板的方向上实现其位移。 电路还可操作地连接到压力传感器和驱动器,用于在位移期间控制换能器的速度幅度和相位,其中在面板处产生的声阻抗在机舱处获得期望的声阻抗边界条件。 换能器还由内层叠层,外层叠层和定位在内层和外层之间的压电膜构成,其中在内和外层叠层中设置多个对准的开口,使得压电膜 可以朝向或远离面板移位。
    • 7. 发明授权
    • Method and apparatus for nonintrusively determining mach number
    • 非侵入式确定马赫数的方法和装置
    • US4829813A
    • 1989-05-16
    • US075482
    • 1987-07-20
    • Asif A. Syed
    • Asif A. Syed
    • G01P5/00G01F1/66G01P5/175
    • G01P5/175
    • The Mach number M.sub.o of flow in the intake nozzle or bypass duct of a gas turbine aircraft engine is determined from the acoustic impedance of a Helmholtz resonator to an engine fan-stator sound source. Pressure measurements P.sub.1 (t) and P.sub.2 (t), made nonintrusively at the duct wall surface and resonator cavity bottom are subjected to Fourier analysis to give P.sub.1 (f) and P.sub.2 (f), and acoustic impedance for the flow is determined from a complex transfer function H.sub.12. Flow Mach number is then established using known acoustic impedance/Mach number correlation relationships or a stored look-up table. An alternative embodiment, utilizes a sound source mounted in the Helmholtz resonator bottom and determines Mach number by pressure measurements made at spaced locations on the resonator chamber wall.
    • 燃气轮机飞机发动机的进气喷嘴或旁通管道中的流量的马赫数Mo从亥姆霍兹共振器到发动机风扇定子声源的声阻抗确定。 对压力测量P1(t)和P2(t)进行傅立叶分析,得到P1(f)和P2(f),流体的声阻抗由 复合传递函数H12。 然后使用已知的声阻抗/马赫数相关关系或存储的查找表建立流量马赫数。 一个替代实施例,利用安装在亥姆霍兹共振器底部的声源,并通过在谐振器腔室壁上的间隔位置处进行的压力测量来确定马赫数。