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Localization of noise sources around aircraft in flight based on time-domain beamforming technique

机译:基于时域波束成形技术的飞行器周围噪声源定位

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Acoustic models of aircraft can be used to predict aircraft noise around airports. When constructing such models, detailed aircraft sound source properties, including the positions and frequency characteristics of individual noise sources, are necessary to achieve high fidelity. We have developed a phased array microphone system to accurately locate noise sources on and around an aircraft in flight. This paper describes the measurement technique and its results, while the companion paper will discuss how to construct a prediction model from those measurements. Acoustic signals from an aircraft flying overhead are measured by a microphone array on the ground and transformed into an aircraft-fixed coordinate system to correct frequency and amplitude distortions due to Doppler effect. Then, a time-domain delay-and-sum beamforming algorithm is applied with additional methods such as weight factors for each microphone and diagonal removal from Cross-Spectral Matrix to improve resolution and quality of acoustic images. In experiments, a 30m-diameter array of 195 microphones was deployed on a temporary platform beside the runway of a regional airport. Noise measurement flights were conducted using JAXA's 'Hisho' experiment aircraft, and acoustic maps were calculated at different emission angles. The aircraft's flaps and landing gear were confirmed to be the dominant noise sources when the engines were at idle. The flaps are characterized as dipole sound sources with directivity in the direction perpendicular to the flap panel, so sound from the extended flap panels is radiated in the forward direction.
机译:飞机的声学模型可用于预测机场周围的飞机噪声。在构建这样的模型时,为获得高保真度,需要详细的飞机声源特性,包括各个噪声源的位置和频率特性。我们已经开发出相控阵麦克风系统,可以精确定位飞行中的飞机上和飞机周围的噪声源。本文介绍了测量技术及其结果,而随附的论文将讨论如何根据这些测量结果构建预测模型。来自地面上空飞行的飞机的声音信号通过地面上的麦克风阵列进行测量,并转换为飞机固定的坐标系,以纠正由于多普勒效应而引起的频率和幅度失真。然后,将时域延迟和求和波束成形算法与其他方法一起应用,例如,每个麦克风的权重因子和从“互谱矩阵”中去除对角线,以提高声学图像的分辨率和质量。在实验中,直径为30m的195个麦克风阵列被部署在区域机场跑道旁边的临时平台上。使用JAXA的“ Hisho”实验飞机进行了噪声测量飞行,并在不同的发射角度计算了声学图。确认发动机怠速时飞机的襟翼和起落架是主要的噪声源。襟翼的特征是在垂直于襟翼板的方向上具有方向性的偶极声源,因此来自扩展襟翼板的声音沿向前方向辐射。

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