首页 | 本学科首页   官方微博 | 高级检索  
     检索      

民用飞机气动布局发展演变及其技术影响因素
引用本文:张帅,夏明,钟伯文.民用飞机气动布局发展演变及其技术影响因素[J].航空学报,2016,37(1):30-44.
作者姓名:张帅  夏明  钟伯文
作者单位:1. 中国商飞北京民用飞机技术研究中心总体论证研究部, 北京 102211; 2. 南京航空航天大学航空宇航学院, 南京 210016
摘    要:在民用飞机气动布局发展演变的历程中,技术因素是根本推动力。为了研究未来民机的发展方向、技术需求以及应对策略,在回顾民机气动布局发展历程的基础上,梳理了在现代民机气动布局形成与演变过程中有着重要影响的4大类技术因素:航空发动机、气动设计、结构设计、飞行控制,并且揭示了这些技术因素在民机发展及其气动布局演变中所发挥的作用。结合未来航空运输市场出现的新需求,分析了未来民机的主要发展方向,重点分析了未来非常规布局民机可能采用的翼身融合、双气泡机身、支撑翼以及联结翼等气动布局形式。最后探讨了新技术条件下民用飞机发展在技术方面的需求和挑战,以及未来民用飞机总体设计的技术策略,明确了多学科设计优化是满足未来民机总体设计需求的有效技术途径。

关 键 词:航空运输  民用飞机  气动布局  总体设计  技术因素  
收稿时间:2015-10-20
修稿时间:2015-11-17

Evolution and technical factors influencing civil aircraft aerodynamic configuration
ZHANG Shuai,XIA Ming,ZHONG Bowen.Evolution and technical factors influencing civil aircraft aerodynamic configuration[J].Acta Aeronautica et Astronautica Sinica,2016,37(1):30-44.
Authors:ZHANG Shuai  XIA Ming  ZHONG Bowen
Institution:1. Department of Aircraft Configuration Studies, Beijing Aeronautical Science & Technology Research Institute of COMAC, Beijing 102211, China; 2. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:Technology is a basic impetus on the development and evolution of the civil aircraft aerodynamic configuration.In order to study the development directions,technical requirements and strategies for the future civil aircraft,this paper reviews the development of civil aircraft aerodynamic configuration and then summarizes four technical factors,i.e.,aeroengine,aerodynamic design,structural design and flight control,which have important influence on the formation and evolution of the modern civil aircraft aerodynamic configuration.The role of these technical factors in the development of the civil aircraft aerodynamic configuration has also been revealed.Considering the new requirements for the future air transportation,this paper points out the main developing directions of the future civil aircraft,and emphatically analyzes the aerodynamic configurations such as blended wing-body,double bubble body,braced-wing and joined-wing,which might be used in the future unconventional civil aircraft.Furthermore,the challenge in technology development,as well as the technology strategies for the future civil aircraft conceptual design,has been discussed.Finally,the paper clarifies that the multidisciplinary design optimization is an effective method for the future civil aircraft conceptual design.
Keywords:air transportation  civil aircraft  aerodynamic configuration  conceptual design  technical factors
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号