基于参数化模型的大型民用飞机设计航程研究
收稿日期: 2015-09-24
修回日期: 2015-10-27
网络出版日期: 2015-11-13
Design range research of large civil aircraft based on parametric model
Received date: 2015-09-24
Revised date: 2015-10-27
Online published: 2015-11-13
航程和座级直接反映民用客机的市场定位,是飞机产品能否被市场广泛接受的关键因素。目前全球大型客机市场由波音和空客两家公司垄断,又细分为窄体客机、宽体客机和超大型客机等市场。其中,宽体客机的航程跨度较大,是否发展中、短程宽体客机的争论从未终止。伴随空客公司推出A330区域型客机,中短程宽体客机是否有利可图的争论更加炙手可热。有鉴于此,基于全参数化飞机模型,研究了特定座级下设计航程与机翼、发动机、特征重量、气动特性以及燃油经济性之间的关系,分析了设计航程对民用飞机总体设计带来的影响,从技术层面阐述了设计航程变化带来的收益及代价。
马超 , 吴大卫 , 俞金海 , 陈迎春 . 基于参数化模型的大型民用飞机设计航程研究[J]. 航空学报, 2016 , 37(1) : 112 -121 . DOI: 10.7527/S1000-6893.2015.0292
Seats number and design range,as direct reflection of marketing orientation,are the key parameters of a civil aircraft.The current global large airliner market is dominated by Boeing and Airbus,including narrow body aircraft,wide body aircraft and super large aircraft,among which the wide body aircrafts have a large scope of design range,Both Airbus and Boeing have settled the new generation of wide body aircraft as the remote type.However,the controversy of the development of medium and short range wide body aircraft has never stopped.As Airbus has launched the A330Reginal project,the profit of medium and short range wide body aircraft becomes hot debate.In view of this,large airliner with certain seats level is selected in this paper to analyze the combined impact of design range on wing,engine,aerodynamic performance,characteristic weights,fuel efficiency and the operating cost,the influence of design range on civil aircraft overall design is also illuminated.Finally the benefit and losses due to design range variation are concluded in the technical prospective.
Key words： airliner; civil aircraft; design range; overall design; synthesis optimization; parametric
[1] 艾德·奥波特.运输类飞机的空气动力设计[M].顾诵芬,吴兴世,杨新军,译.上海:上海交通大学出版社,2010:7-8.OBERT E.Aerodynamic design of transport aircraft[M].GU S F,WU X S,YANG X J,translated.Shanghai:Shanghai Jiao Tong University Press,2010:7-8(in Chinese).
[2] UPTON J.Lockheed L-1011 TriStar-Airliner Tech Vol.8 [M].2001:24-27.
[3] OAG Company.Global air transport outlook[R].2014.
[4] 陈迎春,宋文斌,刘洪.民用飞机总体设计[M].上海:上海交通大学出版社,2010:33-35.CHEN Y C,SONG W B,LIU H.Civil aircraft design [M].Shanghai:Shanghai Jiao Tong University Press,2010:33-35(in Chinese).
[5] WOODSON S H,DEJARNETTE F R,CAMPBELL J F.An interactive three-dimensional boundary-layer method for transonic flow over swept wings:AIAA-1989-0112[R].Reston:AIAA,1989.
[6] HUA J,ZHANG Z Y.Transonic wing design for transport aircraft[C]//ICAS Proceedings,1990,2:1316-1322.
[7] VOLPE G,JAMESON A.Transonic potential flow calculations by two artificial density methods[C]//4th AIAA and ASME,Fluid Mechanics,Plasma Dynamics and Lasers Conference,1986:12-14.
[8] 陈俊章,刘孟诏,孙振家.飞机设计手册 第8册:重量平衡与控制[M].北京:航空工业出版社,1999:45-55.CHEN J Z,LIU M Z,SUN Z J.Aircraft design manual vol 8:weight balance and control[M].Beijing:Aviation Industry Press,1999:44-45(in Chinese).
[9] EGBERT T.Synthesis of subsonic airplane design[M].Delft:Delft University Press,1996:280-283.
[10] DANIEL P R.Aircraft design:A conceptual approach fourth edition[M].Reston:AIAA,2006:21-23.
[11] OBERT E.Aerodynamic design of transport aircraft[M].Delft:Delft University Press,2009:7-8,551-552.
[12] 中国民用航空局.AC-91-7 缩小垂直间隔(RVSM)空域的运行要求[S].北京:中国民用航空局,2007:1-3.Civil Aviation Administration of China.AC-91-7 Reduced vertical separation minimum requirement[S].Beijing:CAAC,2007:1-3(in Chinese).
[13] 黄太平.飞机性能工程[M].北京:科学出版社,2005:43-44.HUANG T P.Aircraft performance engineering[M].Beijing:Science Press,2005:43-44(in Chinese).
[14] 方宝瑞,飞机气动布局设计[M].北京:航空工业出版社,1997:1126-1130.FANG B R.Aircraft aerodynamic configuration design[M].Beijing:Aviation Industry Press,1997:1126-1130(in Chinese).
[15] 中国民用航空局.CCAR-25-R4 运输类飞机适航标准[S].北京:中国民用航空局,2009:13-14.Civil Aviation Administration of China.CCAR-25-R4 Transport category airplanes[S].Beijing:CAAC,2009:13-14(in Chinese).
[16] JACOB M.Valuation techniques for commercial aircraft program design[D].Massachusetts:Massachusetts Institute of Technology,2002:12-35.
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