直升机总体设计思路和方法发展分析

doi:10.7527/S1000-6893.2015.0271

发展综述与需求论证

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直升机总体设计思路和方法发展分析

倪先平^1,2, 朱清华²

1. 中国航空工业集团公司, 北京 100028;
2. 南京航空航天大学直升机旋翼动力学国家级重点实验室, 南京 210016

收稿日期:2015-08-06 修回日期:2015-10-12 出版日期:2016-01-25 发布日期:2015-10-26
通讯作者: 倪先平,Tel.:010-58355861,E-mail:nixianp@sohu.com E-mail:nixianp@sohu.com
作者简介:倪先平男,博士,研究员,博士生导师。主要研究方向:直升机总体设计。Tel:010-58355861,E-mail:nixianp@sohu.com;朱清华男,博士,副教授。主要研究方向:直升机总体设计,新构型旋翼飞行器设计。Tel:025-84892196,E-mail:Zhuqinghua@nuaa.edu.cn

Development of ideas and methods of helicopter general design

NI Xianping^1,2, ZHU Qinghua²

1. Aviation Industry Corporation of China, Beijing 100028, China;
2. National Laboratory of Science and Technology on Rotorcraft Aeromechanics, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China

Received:2015-08-06 Revised:2015-10-12 Online:2016-01-25 Published:2015-10-26

摘要/Abstract

摘要：

直升机总体设计对于型号研制成功与否有着极为重要的影响。随着直升机相关学科以及信息化技术的发展,直升机总体设计亦从传统的原准机设计法、参数统计法等发展到现代的多学科设计优化法。特别是系统工程和并行工程思想以及现代项目管理理念在航空产品研制中的应用,对直升机的总体设计思想产生了重大影响,推动着直升机总体设计向智能化、综合化和系统化方向发展。首先,简要回顾了直升机总体设计技术的发展历程,介绍了传统设计方法和现代设计方法在型号中的应用及其相互之间的差异;然后,重点分析了系统工程和并行工程思想、现代项目管理理念、直升机新构型以及数字化技术对直升机总体设计思想和方法的影响;最后,展望了直升机总体设计方法的未来发展趋势。

关键词: 直升机, 总体设计, 设计综合, 原准机法, 多学科设计优化

Abstract:

The general design has a key influence on the successful development of a helicopter.With the development of the relevant disciplines of helicopter and IT technique,the helicopter general design has developed from traditional prototype design method,parameter statistics method to modern "multidisciplinary design optimization method".Especially the application of the ideas of system engineering,concurrent engineering and modern program management in the development of aviation products produces great influence on the helicopter general design idea,pushing helicopter general design to develop towards intelligence,synthesis and systematization.Firstly,the development of helicopter general design methods is reviewed briefly,and the application of the traditional and modern design methods in the helicopter development and the differences between those methods are introduced.Then,the influences on the ideas and methods of helicopter general design produced by such aspects as the ideas of system engineering,concurrent engineering and modern program management,the helicopter new configuration and new digital technology are analyzed.Finally the development trends of helicopter general design methods are prospected.

Key words: helicopter, general design, design synthesis, prototype method, multidisciplinary design optimization

中图分类号:

倪先平, 朱清华. 直升机总体设计思路和方法发展分析[J]. 航空学报, 2016, 37(1): 17-29.

NI Xianping, ZHU Qinghua. Development of ideas and methods of helicopter general design[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(1): 17-29.

参考文献

[1] STEPHEN G K.Guide for conceptual helicopter design[D].Monterey:Naval Postgraduate School,1983.
[2] ALLEN C H.An analysis of three approaches to the helicopter preliminary design problem[D].Monterey:NAVAL Postgraduate School,1984.
[3] RUTHERFORD C J W,STROZIER C J K.Formulation of a helicopter preliminary design course[C]//Proceedings of AIAA Aircraft Design,Systems and Technology Meeting.Reston:AIAA,1983.
[4] PROUTY R W.Helicopter design technology[M].2nd ed.Malabar:Kieger Publishing Company,1998.
[5] MARAT N T,VENGALATTORE T N,INDERJIT C.Preliminary design of transport helicopters[J].Journal of the American Helicopter Society,2003,48(2):71-79.
[6] JOHN R B,DONALD J M,BRENDA J,et al.Integrated helicopter design tools[C]//Proceedings of the 52nd AHS Annual Forum.Fairfax,VA:AHS Press,1996.
[7] 张呈林,郭才根.直升机总体设计[M].北京:国防科技出版社,2006:1-7,22,136-150.ZHAND C L,GUO C G.Helicopter general design[M].Beijing:National Defense Industry Press,2006:1-7,22,136-150(in Chinese).
[8] 刘虎,罗明强,田永亮,等.飞机总体设计支持技术探索与实践[M].北京:北京航空航天大学出版社,2013:3-12.LIU H,LUO M Q,TIAN Y L,et al.Exploration and practice of supporting technology for aircraft conceptual design[M].Beijing:Beihang University Press,2013:3-12(in Chinese).
[9] 顾诵芬.飞机总体设计[M].北京:北京航空航天大学出版社,2001.GU S F.Aircraft general design[M].Beijing:Beihang University Press,2001(in Chinese).
[10] 倪先平,蔡汝鸿,曹喜金,等.直升机技术发展现状与展望[J].航空学报,2003,24(1):15-20.NI X P,CAI R H,CAO X J,et al.Present situation and prospects of helicopter technology[J].Acta Aeronautica et Astronautica Sinica,2003,24(1):15-20(in Chinese).
[11] LEISHMAN J G.A chronicle of early British rotorcraft[C]//Proceedings of the 60th Annual Forum and Technology Display of the AHS.Fairfax,VA:AHS Press,2004.
[12] 倪先平.直升机参数选择方法浅析[C]//第三届全国直升机年会论文集.北京:中国航空学会,1987:146-159.NI X P.Analysis for the selection methods of a helicopter parameters[C]//Proceedings of the 3rd Annual Forum of China Helicopter Society.Beijing:CSAA,1987:146-159(in Chinese).
[13] 倪先平.直升机总体参数优化选择[C]//第一届全国飞机总体设计学术交流会论文集.北京:中国航空学会,1991.NI X P.The optimization selection for the general parameters of a helicopter[C]//Proceedings of the 1st Annual Forum of Aircraft General Design.Beijing:CSAA,1991(in Chinese).
[14] LIOR M.Statistical methods for helicopter preliminary design and sizing[C]//Proceedings of the 31st European Rotorcraft Forum.Bonn,Germany:ERF Press,2005.
[15] 普劳蒂 R W.直升机性能及稳定性和操纵性[M].高正,陈文轩,施永立,译.北京:航空工业出版社,1990.PROUTY R W.Helicopter performance,stability and control[M].GAO Z,CHEN W X,SHI Y L,translated.Beijing:Aviation Industry Press,1990(in Chinese).
[16] JAEHOON L,SANG J S.Development of an advanced rotorcraft preliminary design framework[J].International Journal of Aeronautical & Space Sciences,2009,10(2):134-139.
[17] ROCCHETTO A,POLONI C.A hybrid numerical optimization technique based on genetic and feasible direction algorithms for multipoint helicopter rotor blade design[C]//Proceedings of the 1st European Rotorcraft Forum.Bonn,Germany:ERF Press,1995.
[18] PALASIS D,WAGNER S.Development of a conceptual design method for rotor-wing aircraft using digital computers[C]//Proceedings of the 17th European Rotorcraft Forum.Bonn,Germany:ERF Press,1991.
[19] 张呈林,彭名华.直升机总体设计技术的新进展[J].航空制造技术,2010(13):57-60.ZHANG C L,PENG M H.New progress of general design technology for helicopter[J].Aeronautical Manufacturing Technology,2010(13):57-60(in Chinese).
[20] ROSENSTEIN HAROLD J,STANZIONE KAYDON A.Computer aided helicopter design[C]//Proceedings of the 37th AHS Annual Forum.Fairfax,VA:AHS Press,1981:112-127.
[21] SCHRAGE D P,MAVRIS D N,WASIKOWSKI M.GTPDP:A rotor wing aircraft preliminary design and performance estimation program including optimization and cost[C]//Proceedings of AHS Vertical Lift Aircraft Design Conference.Fairfax,VA:AHS Press,1986.
[22] BANERJEE D,SHANTHAKUMARAN P.Application of numerical optimization methods in helicopter industry[C]//Proceedings of the 13th European Rotorcraft Forum.Bonn,Germany:ERF Press,1987:1-37.
[23] MAVRIS D N,de LAURENTIS D A,BANDTE O,et al.A stochastic approach to multi-disciplinary aircraft analysis and design[C]//Proceedings of AIAA 36th Aerospace Sciences Meeting and Exhibit.Reston:AIAA,1998.
[24] STEVENS J M G F,BOER J F,LAMME W F,et al.Helicopter pre-design strategy:Design-to-mass or design-to-cost? NLR-TP-2009-306[R].Amsterdam:NLR,2010.
[25] 彭名华,张呈林.直升机总体多学科优化设计[J].直升机,2010(3):11-16.PENG M H,ZHANG C L.Helicopter conceptual/preliminary multidisciplinary design optimization[J].Helicopter,2010(3):11-16(in Chinese).
[26] 彭名华.直升机总体多学科设计优化研究[D].南京:南京航空航天大学,2009.PENG M H.Research on helicopter conceptual/prelimi-nary multidisciplinary design optimization[D].Nanjing:Nanjing University of Aeronautics & Astronautics,2009(in Chinese).
[27] DANIEL P S.Technology for rotorcraft affordability through integrated product/process development(IPPD)[C]//Proceedings of the 55th AHS Annual Forum.Fairfax,VA:AHS Press,1999.
[28] HIRSH J E,WILKERSON J B,NARDUCCI R P.An integrated approach to rotorcraft conceptual design[C]//Proceedings of AIAA 45th Aerospace Sciences Meeting and Exhibit.Reston:AIAA,2007.
[29] DANIEL P S,WILLIAM M C.Integrated product/process development approach for balancing technology push and pull between the user and developer[C]//Proceedings of the 68th AHS Annual Forum.Fairfax,VA:AHS Press,2012.
[30] WAYNE J.NDARC-NASA design and analysis of rotorcraft validation and demonstration[C]//Proceedings of the American Helicopter Society Aeromechanics Specialists' Conference.Fairfax,VA:AHS Press,2010.
[31] MICHAEL A,RAJNEESH S.OpenMDAO/NDARC framework for assessing performance impact of rotor technology integration[C]//Proceedings of the 70th AHS Annual Forum.Fairfax,VA:AHS Press,2014.
[32] BASSET P M,TREMOLET A,CUZIEUX F,et al.The CREATION project for rotorcraft concepts evaluation:The first steps[C]//Proceedings of the 37th European Rotorcraft Forum.Bonn,Germany:ERF Press,2011.
[33] WILLIAM A C,DAVID H L.The genetic algorithm as an automated methodology for helicopter conceptual design[J].Journal of Engineering Design,1997,8(3):231-250.
[34] EMRE G M,ADEEL K,DANIEL P S.Weight estimation using CAD in the preliminary rotorcraft design[C]//Proceedings of the 33rd European Rotorcraft Forum.Bonn,Germany:ERF Press,2007.

E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

直升机总体设计思路和方法发展分析

Development of ideas and methods of helicopter general design

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