介绍美国宇航局的宽带吸声器,类似于天然芦苇

IF 1.2 4区 工程技术 Q3 ACOUSTICS
L. Koch, Michael G. Jones, P. Bonacuse, C. Miller, J. Johnston, M. Kuczmarski
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引用次数: 0

摘要

薄、轻、耐用的宽带吸声器能够吸收宽频率范围内的声音,特别是低于1000 Hz的声音,同时也能在恶劣的操作条件下生存,例如暴露于液体和固体碎片的喷雾和高温下,这是许多噪声控制应用所需要的。虽然目前商用的宽带声学衬垫令人印象深刻,如三聚氰胺泡沫和蜂窝穿孔结构,但每种风格都有其局限性。为了减少飞机发动机的噪音污染,美国宇航局最近申请了一项宽带吸声器的专利,该吸声器声称比现有的声学衬垫有一些好处。灵感来自大自然,这些结构类似于天然芦苇束的几何形状和吸声能力,芦苇是生长在世界各地湿地的细长草。NASA已经开始了概念验证实验。本报告总结了天然芦苇组件的设计、制造和正常入射阻抗管测试,以及类似天然芦苇束不规则几何形状的增材制造塑料原型。一些合成原型进行了带和不带穿孔面罩的测试。结果表明,与相似厚度和重量的基线吸声器相比,有许多合成设计在500 Hz至3000 Hz的频率范围内表现出大量的吸声,特别是在1000 Hz以下。其中许多原型的平均吸声系数大于0.6。此外,设计和打印了一个环形原型,但尚未进行测试。这个多功能结构的环形原型设计用于传递热量和吸收声音,是为了适应美国宇航局格伦研究中心的DGEN航空推进研究涡扇发动机试验台而开发的。本发明可用于各种航空航天、汽车、工业和建筑噪声控制应用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
An introduction to NASA’s broadband acoustic absorbers that resemble natural reeds
Thin, lightweight, and durable broadband acoustic absorbers capable of absorbing sounds over a wide frequency range, especially below 1000 Hz, while also surviving harsh operational conditions such as exposure to sprays of liquid and solid debris and high temperatures are desired for many noise control applications. While today’s commercially available broadband acoustic liners are impressive, such as melamine foam and perforate-over-honeycomb structures, each style has its limitations. Motivated by the need to reduce aircraft engine noise pollution NASA has recently patented a broadband acoustic absorber that claims some benefit over existing acoustic liners. Inspired by nature, these structures resemble the geometry and acoustic absorption of bundles of natural reeds, slender grasses that grow in wetlands across the world. Proof-of-concept experiments have begun at NASA. This report summarizes the design, fabrication, and normal incidence impedance tube tests performed for assemblies of natural reeds and additively-manufactured plastic prototypes that resemble the irregular geometry of bundles of natural reeds. Some synthetic prototypes were tested with and without perforated face sheets. Results indicate that there are a number of synthetic designs that exhibit substantial acoustic absorption in the frequency range of 500 Hz to 3000 Hz, and especially below 1000 Hz, as compared to baseline acoustic absorbers of similar thicknesses and weights. Many of these prototypes have an average acoustic absorption coefficient greater than 0.6. Additionally, an annular prototype was designed and printed but not yet subjected to tests. This annular prototype of a multifunctional structure designed to transfer heat and absorb sound was developed to fit inside the NASA Glenn Research Center’s DGEN Aeropropulsion Research Turbofan engine testbed. This invention can be considered and developed for a variety of aerospace, automotive, industrial, and architectural noise control applications.
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来源期刊
International Journal of Aeroacoustics
International Journal of Aeroacoustics ACOUSTICS-ENGINEERING, AEROSPACE
CiteScore
2.10
自引率
10.00%
发文量
38
审稿时长
>12 weeks
期刊介绍: International Journal of Aeroacoustics is a peer-reviewed journal publishing developments in all areas of fundamental and applied aeroacoustics. Fundamental topics include advances in understanding aeroacoustics phenomena; applied topics include all aspects of civil and military aircraft, automobile and high speed train aeroacoustics, and the impact of acoustics on structures. As well as original contributions, state of the art reviews and surveys will be published. Subtopics include, among others, jet mixing noise; screech tones; broadband shock associated noise and methods for suppression; the near-ground acoustic environment of Short Take-Off and Vertical Landing (STOVL) aircraft; weapons bay aeroacoustics, cavity acoustics, closed-loop feedback control of aeroacoustic phenomena; computational aeroacoustics including high fidelity numerical simulations, and analytical acoustics.
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