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高经济性静音中航程民机设计方法讨论 被引量:9

Discussion of Design Methods for Silent and Fuel Efficient Medium Range Civil Transport
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摘要 人们已愈来愈重视工业产品对环境的影响。人们直接感受民机对环境的影响首先是机场周边的噪声。静音飞机预案的研究目标是设计一种飞机,在机场周边听不见其响声,且油耗和排污指标优于现有的和正在设计的其他飞机。通过介绍SAX(Silent Aircraft eXperiment)三代概念机的研究进程,讨论了静音飞机设计的方法和使用的关键技术,包括具有一定准确度的快速翼身融合体准三维设计方法;具有最佳中央体外形的融合体气动外形设计;可平滑下弯的外翼前缘和后缘刷;分布、埋入式多风扇可吞吸边界层的发动机组;喷口截面可变的推力矢量喷管;先进的隔音衬管;整流的起落架等。最终的概念机SAX-40实现了在机场周边的最大噪声计算值为61 dBA,接近于稠密居民区的背景噪声,且使机场周边的人们不易感觉到飞机的起飞/进场。其油耗经济性亦达到了124座-哩/加仑的优异指标。 People are more and more concerned about the influence of industrial products on environment.Aircraft noise around airports is the complained environmental impact of civil aviation.The goal of silent aircraft initiative is to design a conceptual aircraft,which is inaudible outside the airport perimeter and also in fuel efficiency and emission control superior to present and future conventional aircraft.By introducing three generations of conceptual silent aircraft experiment(SAX),this paper discussed the design method and enabling technology,including a quasi-3D design method with fast turnaround time and adequate fidelity;aerodynamic design of the blended wing body by optimally shaping its centerbody;deployed drooped leading edge and trailing edge brushes of the outer wing;distributed multi-fan embedded turbofan with boundary layer ingestion;thrust vectoring nozzle with variable exit area;advanced acoustic linears;and faired undercarriage,etc.Finally,the resulting conceptual aircraft design,SAX-40,yields a calculated noise level of 61 dBA at the airport perimeter,which is close to the background noise in a well populated area and imperceptible to the human ear on takeoff and landing.SAX-40 also has the potential for a reduced fuel burn of 124 passenger-miles per gallon.
出处 《航空学报》 EI CAS CSCD 北大核心 2008年第3期562-572,共11页 Acta Aeronautica et Astronautica Sinica
基金 国家自然科学基金(10472013) 航空科学基金(04A51044)
关键词 静音飞机 民机设计 气动设计 silent aircraft civil transport design aerodynamic design
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参考文献17

  • 1Green J E. Air travel-greener by design mitigating the environmental impact of aviation: opportunities and priorities[J]. The Aeronautical Journal, 2005,109(1099):495-510.
  • 2Green J E. Civil aviation and the environment-the next frontier for the aerodynamicist [J]. The Aeronautical Journal, 2006,109(1099) :469-486.
  • 3朱自强,王晓璐,吴宗成,陈泽民.民机设计中的多学科优化和数值模拟[J].航空学报,2007,28(1):1-13. 被引量:17
  • 4Dowling A, Greiter E D. The silent aircraft initiative-overview[R]. AIAA 2007-0452,2007.
  • 5Spakovszky Z S. Toward a "silent" aricraft[C]//22nd Syrup On aviation noise and air quality. 2007.
  • 6Diedrich A, Hileman J, Tan D, et al. Mulitidisciplinary design and optimization of the silent aircraft[R]. AIAA 2006-1323,2006.
  • 7Liebeck R H. Design of the blended wing body subsonic transport[J]. Journal of Aircraft, 2004, 41(1):10-25.
  • 8朱自强,王晓璐,吴宗成,陈泽民.民机的一种新型布局形式——翼身融合体飞机[J].航空学报,2008,29(1):49-59. 被引量:41
  • 9Hileman J I, Spakovszky Z S, Drela M. Airframe design for "silent aircraft"[R]. AIAA 2007-453,2007.
  • 10Hileman J I, Spakovszky Z S, Drela M, et al. Aerodynamic and acroacoustic three dimensional design for a silent aircraft[R]. AIAA 2006-241, 2006.

二级参考文献48

共引文献53

同被引文献120

  • 1乔渭阳.STUDY ON FLAP SIDE-EDGE NOISE BASED ON THE FLY-OVER MEASUREMENTS WITH A PLANAR MICROPHONE ARRAY[J].Chinese Journal of Aeronautics,2000,13(3):182-187. 被引量:3
  • 2宋文萍,余雷,韩忠华.飞机机体气动噪声计算方法综述[J].航空工程进展,2010,1(2):125-131. 被引量:30
  • 3于涛,范洁川,贾元胜.现代航空声学风洞技术现状与发展[J].实验流体力学,2007,21(3):86-91. 被引量:13
  • 4Van DAM C P. The aerodynamic design of multi-element high-lift systems for transport airplanes[J]. Progress in Aerospace Sciences, 2002, (38).. 101-144.
  • 5RUDOLPH P K C. High-lift systems on commercial transport airliners[R]. NASA CR-4746.
  • 6LOCKARD D P, LILLEY G M. The airframe noise reduction challenge[R]. NASA TM 2004-213013.
  • 7EWERT R. Slat noise trend predictions using CAA with sto- chastic sound sources from a random particle mesh method (RPM) [R]. 27th AIAA Aeroacoustics Conference, AIAA 2006-2667.
  • 8GILLETTE W B, MCINTOSH W M. Aircraft configuration synthesis PART II aerodynamics[M]. Edition 4. The BOE- ING Company, ACC 3007.
  • 9LILLEYS G M. The prediction of airframe noise and compari- son with experiment [J]. Journal of Sound and Vibration, 2001, 239(4): 849-859.
  • 10MITSUHIRO MURAYMA. CFD validation for high lift devices: three-element airfoil[J]. Trans. Japan Soc. Aero. Space Sci. , 2008, 49(163): 40-48.

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