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Piezoelectric Shunt Vibration Damping of F-15 Panel under High Acoustic Excitation

机译:高声激发下F-15面板的压电分流减振

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摘要

At last year's SPIE symposium, we reported results of an experiment on structural vibration damping of an F-15 underbelly panel using piezoelectric shunting with five bonded PZT transducers. The panel vibration was induced with an acoustic speaker at an overall sound pressure level (OASPL) of about 90 dB. Amplitude reductions of 13.45 and 10.72 dB were achieved for the first and second modes, respectively, using single- and multiple-mode shunting. It is the purpose of this investigation to extend the passive piezoelectric shunt-damping technique to control structural vibration induced at higher acoustic excitation levels, and to examine the controllability and survivability of the bonded PZT transducers at these high levels. The shunting experiment was performed with the Thermal Acoustic Fatigue Apparatus (TAFA) at the NASA Langley Research Center using the same F-15 underbelly panel. The TAFA is a progressive wave tube facility. The panel was mounted in one wall of the TAFA test section using a specially designed mounting fixture such that the panel was subjected to grazing-incidence acoustic excitation. Five PZT transducers were used with two shunt circuits designed to control the first and second modes of the structure between 200 and 400 Hz. We first determined the values of the shunt inductance and resistance at an OASPL of 130 dB. These values were maintained while we gradually increased the OASPL from 130 to 154 dB in 6-dB steps. During each increment, the frequency response function between accelerometers on the panel and the acoustic excitation measured by microphones, before and after shunting, were recorded. Good response reduction was observed up to the 148dB level. The experiment was stopped at 154 dB due to wire breakage from vibration at a transducer wire joint. The PZT transducers, however, were still bonded well on the panel and survived at this high dB level. We also observed shifting of the frequency peaks toward lower frequency when the OASPL was increased. Detailed experimental results will be presented.
机译:在去年的SPIE研讨会上,我们报告了使用带有五个键合PZT换能器的压电分流器对F-15腹板进行结构减振的实验结果。用声学扬声器在大约90 dB的总声压级(OASPL)引起面板振动。使用单模和多模分流,第一模和第二模的幅度分别降低了13.45 dB和10.72 dB。这项研究的目的是扩展无源压电分流阻尼技术,以控制在较高声激励水平下引起的结构振动,并检查在这些高水平下结合的PZT换能器的可控性和生存性。分流实验是在NASA兰利研究中心的热声疲劳装置(TAFA)上使用相同的F-15肋骨板进行的。 TAFA是一种渐进波管设备。使用专门设计的安装夹具将面板安装在TAFA测试部分的一堵墙中,使面板受到掠入射声激发。五个PZT传感器与两个并联电路一起使用,这些并联电路设计为将结构的第一和第二模式控制在200至400 Hz之间。我们首先确定OASPL为130 dB时的并联电感和电阻值。当我们以6 dB的步长将OASPL从130 dB逐渐增加到154 dB时,这些值得以保持。在每次增量期间,记录分流前后的面板上的加速度计之间的频率响应函数和麦克风测量的声激励。观察到高达148dB的良好响应降低。由于换能器导线接头处的振动导致导线断裂,实验在154 dB处停止。但是,PZT换能器仍牢固地贴在面板上,并能在此高dB水平下幸存下来。当OASPL增加时,我们还观察到了频率峰值向较低频率的偏移。将提供详细的实验结果。

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