UHBR技术引擎的智能声学衬里:从电声超表面的设计到流动下的实验表征

K. Billon, Martin Gillet, E. Salze, M. Volery, E. De Bono, M. Ouisse, Hervé Lissek, M. Collet, J. Mardjono
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引用次数: 0

摘要

SALUTE项目旨在评估电声超表面的性能,采用受控电声致动器的表面阵列,用于UHBR技术引擎中使用的掠掠湍流下的智能声学衬里。为了在发动机模型中设计复杂气动声学特性的创新概念,进行了理论和数值研究。重点研究了在接近真实发动机实现的三维衬垫中评估超复合材料衬垫性能的原型的实现、过程的复杂性和鲁棒性。该项目为设计智能声学衬垫提供了新的工具;声学实验结果表明,该技术具有较好的鲁棒性和有效性。本文介绍了这一概念从理论到技术实现和表征的发展过程。在里昂中央学院的PHARE设施中实现了用衬垫在声流管道设施(FDF)中得到的实验结果。在与目标发动机相似的流动条件下,测试了不同配置的尾管:一个作为参考的被动尾管和一个基于电声吸收器阵列的3D主动尾管。最后的测试活动包括声学和空气动力学测量,以表征气动流动条件、膜性能、获得的合成声阻抗和由此产生的插入损失。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Smart acoustic lining for UHBR technologies engine: from the design of an electroacoustic metasurface to experimental characterization under flow
The SALUTE project aims at evaluating performance of electroacoustic metasurface, employing a surface array of controlled electroacoustic actuators, for smart acoustic lining under grazing turbulent flow to be used in UHBR Technologies Engines. Theoretical and numerical investigations have been carried out for designing innovative concepts for complex aero-acoustic characterization in an engine mock-up. A specific focus was placed in the realization of prototypes for evaluating the metacomposite liner performances in 3D liners close to real engine implementation, its process complexity and robustness. This project provides new tools for designing smart acoustic liners; while acoustical experimental tests demonstrate efficiency and robustness of such technology for controlling UHBR noise emission. This paper presents the concept development from theory to technological realization and characterization by produced numerical tools. The experimental results obtained with the liners in acoustic flow duct facilities (FDF) have been realized in the PHARE facilities of Ecole Centrale de Lyon. Different configurations of liners have been tested using similar flow conditions as in target engine: 1 passive liner used as reference and a 3D active liner based on an array of electroacoustic absorbers. The final tests campaign comprises acoustics and aerodynamics measurements to characterize the aeroacoustics flow conditions, the membrane behavior, the achieved synthetic acoustic impedance and the resulting insertion loss.
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