飞机舱内噪声的研究现状

doi:10.7527/S1000-6893.2016.0073

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飞机舱内噪声的研究现状

左孔成, 陈鹏, 王政, 田昊, 唐道锋

中国空气动力研究与发展中心气动噪声控制重点实验室, 绵阳 621000

收稿日期:2016-01-18 修回日期:2016-03-02 出版日期:2016-08-15 发布日期:2016-05-11
通讯作者: 左孔成,Tel.:0816-2461230。E-mail:zuokongcheng@163.com E-mail:zuokongcheng@163.com
作者简介:左孔成,男,博士,助理研究员。主要研究方向:飞机舱内噪声的机理。Tel:0816-2461230。E-mail:zuokongcheng@163.com;陈鹏,男,博士,研究员。主要研究方向:气动声学机理。E-mail:pht128@163.com

Research status of aircraft interior noise

ZUO Kongcheng, CHEN Peng, WANG Zheng, TIAN Hao, TANG Daofeng

Aerodynamic Noise Control Key Laboratory, China Aerodynamics Research and Development Center, Mianyang 621000, China

Received:2016-01-18 Revised:2016-03-02 Online:2016-08-15 Published:2016-05-11

摘要/Abstract

摘要：

飞机舱内噪声是影响乘客舒适性的一项重要指标，舱内噪声的最小化是国内外共同追求的目标。在对飞机外部噪声源特性进行介绍的基础上，对噪声源/传递路径识别、舱内降噪措施以及声学试验计算等方面进行了综述。其中，噪声源以及噪声传递路径识别主要从各种识别技术手段方面展开了讨论，包括频率分析法、相关技术、修改噪声传递路径、空气传声以及结构传声的识别。而舱内降噪方法主要从被动降噪与主动降噪两方面进行全面介绍，指出被动降噪是一种修改与优化噪声传递路径的方法，而主动降噪能自动感应识别并控制噪声源，并分别给出了两者的优点及其局限性。在噪声测试与仿真模拟方面则介绍了国内外地面实验室舱内噪声的研究情况，并指出了国内的不足，对仿真计算理论进行了梳理，列出各自的适用范围。最后，指出了目前舱内噪声研究依然存在的问题与挑战，并给出了未来的研究方向。

关键词: 舱内噪声, 噪声源, 传递路径, 降噪, 飞机

Abstract:

One of the most important factors influencing passengers' comfortableness for civil aircraft is interior noise whose minimization is one of the goals for all countries in the world. This paper reviews the identification of noise sources/transmission paths, interior noise reduction measures, acoustic test and simulating calculation after introducing the characteristics of exterior noise sources. Thereinto, the discussion of identification of noise sources/transmission paths is carried out through various identification techniques, including frequency analysis, coherence techniques, source/path modification and identification of airborne/structure-born paths. The passive and active control concerning aircraft cabin noise reduction is introduced comprehensively. Active control can identify and control the noise sources with an auto-negotiation way in the event that passive control can modify and optimize the noise transmission paths, and then both their advantages and disadvantages are provided. For noise test and simulation, this paper firstly introduces current domestic and overseas research situation of ground test and points out domestic drawbacks. Whereafter, the paper presents the methods of simulating calculation and lists their range of application. At the end of this paper, the current existing problems and challenges of aircraft cabin noise are referred and possible future research direction is proposed.

Key words: interior noise, noise source, transmission path, noise reduction, aircraft

中图分类号:

V271.1

左孔成, 陈鹏, 王政, 田昊, 唐道锋. 飞机舱内噪声的研究现状[J]. 航空学报, 2016, 37(8): 2370-2384.

ZUO Kongcheng, CHEN Peng, WANG Zheng, TIAN Hao, TANG Daofeng. Research status of aircraft interior noise[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(8): 2370-2384.

参考文献

[1] LASZLO H E, MCROBIE E S, STANSFELD S A, et al. Annoyance and other reaction measures to changes in noise exposure-A review[J]. Science of the Total Environment, 2012, 435-436:551-562.
[2] LINDVALL J, VÄSTFJALL D. The effect of interior aircraft noise on pilot performance[J]. Perceptual & Motor Skills, 2013, 116(2):472-490.
[3] FIDELL S, SILVAT L. Parsimonious alternatives to regression analysis for characterizing prevalence rates of aircraft noise annoyance[J]. Noise Control Engineering, 2004, 52(2):56-68.
[4] PENNIG S, QUEHLA J, ROLNY V. Effects of aircraft cabin noise on passenger comfort[J]. Ergonomics, 2012, 55(10):1252-1265.
[5] KALTENBACH M, MASCHKE C, HE F, et al. Health impairments, annoyance and learning disorders caused by aircraft noise[J]. International Journal, 2016, 6(1):15-46.
[6] AVKA I, OKORILO O, VASOV L. Energy efficiency in aircraft cabin environment:Safety and design[J]. Energy and Buildings, 2016, 115(1):63-68.
[7] NAVANEETHAN R. General aviation aircraft interior noise problem:Some suggested solutions:NASA-CR-173784[R]. Washington, D.C.:NASA, 1984.
[8] WILBY J F. Aircraft interior noise[J]. Journal of Sound and Vibration, 1996, 190(3):545-564.
[9] NORRIS G, WAGNER M. Airbus A380:Superjumbo of the 21st century[M]. Minnesota:Zenith Imprint, 2005:7-10.
[10] BRIÈRE D, TRAVERSE P. AIRBUS A320/A330/A340 electrical flight controls-A family of fault-tolerant systems[C]//IEEE 23rd International Symposium on Fault-Tolerant Computing. Piscataway, NJ:IEEE Press, 1993:616-623.
[11] GIVONI M, RIETVELD P. The environmental implications of airlines' choice of aircraft size[J]. Journal of Air Transport Management, 2010, 16(3):159-167.
[12] TYROLER-COOPER S, PEET A. The Chinese aviation industry:Techno-hybrid patterns of development in the C919 program[J]. The Journal of Strategic Studies, 2011, 34(3):383-404.
[13] MIXSON J S, WILBY J F. Interior noise[C]//Aeroacoustics of Flight Vehicles:Theory and Practice. Volume 2:Noise Control. 1991, 2:271-355.
[14] WILBY J F. Handbook of noise and vibration control[M]. Hoboken, NJ:John Wiley & Sons, Inc., 2007:1197-1206.
[15] HARRISON K J. Quest for the quieter cabin[J]. Aviation International News, 2003, 35(1):38.
[16] 乔渭阳. 航空发动机气动声学[M]. 北京:航空工业出版社, 2010:23-58. QIAO W Y. Aero-engine aeroacoustics[M]. Beijing:Aviation Industry Press, 2010:23-58(in Chinese).
[17] WRIGHT R I, KIDNER M R F. Vibration absorbers:A review of applications in interior noise control of propeller aircraft[J]. Journal of Vibration and Control, 2004, 10(8):1221-1237.
[18] MIXSON J S, POWELL C A. Review of recent research on interior noise of propeller aircraft[J]. Journal of Aircraft, 1985, 22(11):931-949.
[19] WILBY J, WILBY E. Measurements of propeller noise in a light turboprop airplane[J]. Journal of Aircraft, 1989, 26(1):40-47.
[20] WILBY J F, GLOYNA F L. Vibration measurements of an airplane fuselage structure Ⅱ. Jet noise excitation[J]. Journal of Sound and Vibration, 1972, 23(4):467-486.
[21] LIGHTHILL M J. Jet noise[J]. AIAA Journal, 1963, 1(7):1507-1517.
[22] 李建锋, 吕俊复. 涡轮燃烧技术在涡扇航空发动机上的应用分析[J]. 空气动力学学报, 2010, 28(3):358-363. LI J F, LV J F. Application analysis of turbine combustion technology in turbofan engine[J]. Acta Aerodynamica Sinica, 2010, 28(3):358-363(in Chinese).
[23] LIU F, SIRIGNANO W A. Turbojet and turbofan engine performance increases through turbine burners[J]. Journal of Propulsion and Power, 2001, 17(3):695-705.
[24] 金奕山. 民用航空器噪声合格审定概论[M]. 上海:上海交通大学出版社, 2013:24-47. JIN Y S. Introduction to the qualification examination of civil aircraft noise[M]. Shanghai:Shanghai Jiao Tong University Press, 2013:24-47(in Chinese).
[25] TAM C K. On the spectrum of combustion noise:AIAA-2015-2969[R]. Reston:AIAA, 2015.
[26] ZAPOROZHETS O, TOKAREV V, ATTENBOROUGH K. Aircraft noise-assessment, prediction and control[M]. New York:Spon Press, 2011:75-84.
[27] CHEN Y, HE E, HU X, et al. Exploring wing-mounted engine vibration transmission for new generation airplanes with turbofan engines of high bypass ratio[J]. Journal of Northwestern Polytechnical University, 2012, 30(3):384-389.
[28] HU N, BUCHHOLZ H, HERR M, et al. Contributions of different aeroacoustic sources to aircraft cabin noise:AIAA-2013-2030[R]. Reston:AIAA, 2013.
[29] BHAT W V. Flight test measurement of exterior turbulent boundary layer pressure fluctuations on Boeing model 737 airplane[J]. Journal of Sound and Vibration, 1971, 14(4):439-457.
[30] BROOKS T F, HODGSON T. Trailing edge noise prediction from measured surface pressures[J]. Journal of Sound and Vibration, 1981, 78(1):69-117.
[31] BHAT W, WILBY J. Interior noise radiated by an airplane fuselage subjected to turbulent boundary layer excitation and evaluation of noise reduction treatments[J]. Journal of Sound and Vibration, 1971, 18(4):449-464.
[32] DOBRZYNSKI W. Almost 40 years of airframe noise research:What did we achieve[J]. Journal of Aircraft, 2010, 47(2):353-367.
[33] HARRIS C, PIERSOL A. Harris' shock and vibration handbook[M]. New York:R.R.Donelley & Sons Company, 2009:29-30.
[34] MÖSER M. Engineering acoustics:An introduction to noise control[M]. Zimmermann S, Ellis R, translated. Berlin:Springer Science & Business Media, 2009:17-63.
[35] 扈西枝, 韩峰, 何立燕, 等. 大型客机舱内声学设计方案综述(一)[J]. 民用飞机设计与研究, 2011(2):1-4. HU X Z, HAN F, HE L Y, et al. Overview of the cabin acoustic design for the large commercial aircraft (I)[J]. Civil Aircraft Design and Research, 2011(2):1-4(in Chinese).
[36] BALLESTEROS J A, SARRADJ E, FERNÁNDEZ M D, et al. Noise source identification with beamforming in the pass-by of a car[J]. Applied Acoustics, 2015, 93:106-119.
[37] KOTUS J. Multiple sound sources localization in free field using acoustic vector sensor[J]. Multimedia Tools and Applications, 2015, 74(12):4235-4251.
[38] BENEDETTI A, LEAHU G, LI VOTI R, et al. Photoacoustic detection of circular dichroism in a square array of nano-helices[C]//Fotonica AEIT Italian Conference on Photonics Technologies. 2015.
[39] ZHAO S, QIU X, BURNETT I. Acoustic contrast control in an arc-shaped area using a linear loudspeaker array[J]. The Journal of the Acoustical Society of America, 2015, 137(2):1036-1039.
[40] EMBRECHTS J J. Measurement of 3D room impulse responses with a spherical microphone array[C]//Proceedings of the Euronoise 2015 Congress. 2015:143-148.
[41] CHRISTENSON T N, FERGUSON T J. Experimental localization of noise entry points into an aircraft cabin:AIAA-1999-1835[R]. Reston:AIAA, 1999.
[42] BRUDERLIN H H. Developments in aircraft sound control[J]. The Journal of the Acoustical Society of America, 1937, 8(3):181-184.
[43] SOONG T T, COSTANTINOU M C. Passive and active structural vibration control in civil engineering[M]. New York:Springer, 2014:1-80.
[44] GRIFFIN S, WESTON A, ANDERSON J. Adaptive noise cancellation system for low frequency transmission of sound in open fan aircraft[J]. Shock and Vibration, 2013, 20(5):989-1000.
[45] KIM S M, BRENNAN M J. Active control of harmonic sound transmission into an acoustic enclosure using both structural and acoustic actuators[J]. The Journal of the Acoustical Society of America, 2000, 107(5):2523-2534.
[46] HANSEN C, SNYDER S, QIU X, et al. Active control of noise and vibration[M]. New York:CRC Press, 2012:1-7.
[47] BHATIA K G, BACKUS W E, HAGELIN J S. Vibration damping aircraft engine attachment:5065959[P]. 1991-11-19.
[48] SEELEN L, JOSEPH T P, CENCULA J E, et al. Aircraft engine mount:5275357[P]. 1994-01-04.
[49] LI Y, WANG X N, ZHANG D J. Control strategies for aircraft airframe noise reduction[J]. Chinese Journal of Aeronautics, 2013, 26(2):249-260.
[50] NEISE W, ENGHARDT L. Technology approach to aero engine noise reduction[J]. Aerospace Science and Technology, 2003, 7(5):352-363.
[51] OSWALD L J. Reduction of diesel engine noise inside passenger compartments using active, adaptive noise control[C]//Inter-noise and Noise-cn Congress and Conference Proceedings. 1984:483-488.
[52] ALUJEVIC N, FRAMPTON K D, GARDONIO P. Stability and performance of a smart double panel with decentralized active dampers[J]. AIAA Journal, 2008, 46(7):1747-1756.
[53] HIDALGO I L, NABARRETE A. Structure-borne energy transmission analysis including aircraft fuselage dampers[C]//Proceedings of ISMA 2012-USD2012. 2012:921-931.
[54] 戴德沛. 阻尼减振降噪技术[M]. 西安:西安交通大学出版社, 1986:116-122. DAI D P.Damping vibration and noise reduction technology[M]. Xi'an:Xi'an Jiaotong University Press, 1986:116-122(in Chinese).
[55] DANDAROY I, BHUIYAN M T. Aircraft with tuned vibration absorber mounted on skin:8511601[P]. 2013-08-20.
[56] RAO M D. Recent applications of viscoelastic damping for noise control in automobiles and commercial airplanes[J]. Journal of Sound and Vibration, 2003, 262(3):457-474.
[57] ROSS C R, PURVER M R J. Active cabin noise control[C]//Inter-noise and Noise-con Congress and Conference Proceedings. 1997:518-525.
[58] EMBORG U. Cabin noise control in the Saab 2000 high-speed turboprop aircraft[C]//Proceedings of the International Seminar on Modal Analysis. 1998:13-26.
[59] SUN J, JOLLY M R, NORRIS M. Passive, adaptive and active tuned vibration absorbers-A survey[J]. Journal of Mechanical Design, 1995, 117(8):234-242.
[60] GUICKING D. On the invention of active noise control by Paul Lueg[J]. Journal of the Acoustical Society of America, 1990, 87(5):2251-2254.
[61] FARHANG-BOROUJENY B. Adaptive filters:Theory and applications[M]. New York:John Wiley & Sons, 2013:1-6.
[62] ELLIOT S, NELSON P, STOTHERS I, et al. In-flight experiments on the active control of propeller-induced cabin noise[J]. Journal of Sound and Vibration, 1990, 140(2):219-238.
[63] FULLER C, ROGERS C, ROBERTSHAW H. Control of sound radiation with active/adaptive structures[J]. Journal of Sound and Vibration, 1992, 157(1):19-39.
[64] GRIFFIN S, WESTON A, ANDERSON J. Adaptive noise cancellation system for low frequency transmission of sound in open fan aircraft[J]. Shock and Vibration, 2013, 20(5):989-1000.
[65] CHEN H, SAMARASINGHE P, ABHAYAPALA T D. In-car noise field analysis and multi-zone noise cancellation quality estimation[C]//2015 Asia-Pacific Signal and Information Processing Association Annual Summit and Conference (APSIPA). Piscataway, NJ:IEEE Press, 2015:773-778.
[66] 吴亚锋, 任辉, 李江红. 螺桨飞机舱内噪声的主动控制[J]. 声学技术, 2001, 20(1):29-31. WU Y F, REN H, LI J J.Active control of propeller aircraft cabin noise[J]. Acoustic Technique, 2001, 20(1):29-31(in Chinese).
[67] 胡海岩, 郭大蕾, 翁建生. 振动半主动控制技术的进展[J]. 振动测试与诊断, 2001, 21(4):235-244. HU H Y, GUO D L, WENG J S. Advances in semi-active vibration control technology[J]. Vibration Test and Diagnosis, 2001, 21(4):235-244(in Chinese).
[68] HU Y, CHEN K, PAN K. Optimization design about plane cabin noise based on statistical energy analysis[J]. Noise and Vibration Control, 2007, 4(2):65-68.
[69] POPE L D, WILBY E G, WILBY J F. Propeller aircraft interior noise model, Part I:Analytical model[J]. Journal of Sound and Vibration, 1987, 118(3):449-467.
[70] YAN Y, LI P, LIN H. Analysis and experimental validation of the middle frequency vibro-acoustic coupling property for aircraft structural model based on the wave coupling hybrid FE-SEA method[J]. Journal of Sound and Vibration, 2016, 371(9):227-236.

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飞机舱内噪声的研究现状

Research status of aircraft interior noise

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