太阳能飞机的发展现状及设计特点分析

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• 英文论文题名：Overview of Solar Powered Aircraft and Analysis of Designing Characteristics
• 论文作者：王伟 ; 耿健中 ; 段卓毅 ; 杜欢
• 英文论文作者：Wang Wei ; Geng Jianzhong ; Duan Zhuoyi ; Du Huan ; AVIC The First Aircraft Institute
• 年：2016
• 作者机构：中航工业第一飞机设计研究院;
• 论文关键词：太阳能飞机 ; 设计特点 ; 发展现状 ; 轻质结构
• 英文论文关键词：solar powered aircraft ; designing characteristics ; present developing situation ; light Structure
• 会议召开时间：2016-10-31
• 会议录名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛文集（上册）
• 英文会议录名称：Discovery,Innovation and Communication——Proceedings of 7th CSAA Science and Technology Youth Forum
• 语种：中文
• 分类号：V272
• 学会代码：ZGHU
• 会议名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛
• 会议地点：中国广东中山
• 主办单位：中国航空学会
• 学会名称：中国航空学会
• 页数：8
• 文件大小：2791k
• 原文格式：O
• 会议级别：全国

摘要

高空超长航时太阳能飞机可用于执行侦察、监测、预警和通信中继等任务,具有广阔的发展潜力及应用前景,是临近空间飞行器重要的研究对象之一。受其独特的能源形式限制,太阳能飞机一般具有展弦比大、翼载荷低、结构面密度低、结构柔性大等特点。本文对太阳能飞机的发展现状进行一定的总结,并对该类飞机总体、气动、结构等独特的设计特点进行分析。研究工作对该类飞机的设计,具有一定的参考意义。
High altitude ultra long endurance solar powered aircraft which may provide a unique cost-effective platform for a large number of tasks,from continuous reconnaissance and surveillance to early warning and telecommunication relay,is one of the most important research objects among the near space vehicles that may has a wide development potential and application prospect.Restricted by its unique form of energy,high aspect ratio wings and low structural surface density and low wing loading are the specific characteristics of this type of high-altitude long endurance solar powered aircraft.The present development situations are summaried in this work,and the aerodynamically and structural designing characteristics of solar powered aircraft are also analyzed.The research work have some reference values to die design of solar powered aircraft.

引文

[1]Cestino E.Design of Very Long-Endurance Solar Powered UAV[D].PHD Thesis,Department of Aerospace Engineering,Politecnico di Torino,2006.
    [2]高广林,李占科,宋笔锋.太阳能无人机关键技术分析[J].飞行力学,2010,28(1):1-4.
    [3]Terry D Haws and W Jerry Bowman.Thermal Analysis of the Pathfinder Aircraft.AIAA,1999-0735,1999.
    [4]邓海强,余雄庆.太阳能飞机的现状和发展趋势[J].航空科学技术,2006(1):28-30.
    [5]Romeo G.Frulla G,Cestino E,et al.HELIPLAT;Design,Aerodynamic,Structural Analysis of Long-Endurance SolarPowered Stratospheric Platform[J].Aircr,2004,41(6),1505-1520.
    [6]王彦广,李健全,李勇,等.近空间飞行器的特点及其应用前景[J].航天器工程,2007,16(1):50-57.
    [7]Kirk Flittie,Bob Curtin.Pathfinder Solar-Powered Aircraft Flight Performance[J].AIAA,1998-4446,1998.
    [8]Edward H Teets Jr,Casey J Donohue,Patrick T Wright.Meteorological Support of the Helios World Record High Altitude Flight to 96863 Feet[R].NASA/TM-2002-210727,2002.
    [9]Garbe G and E E Montgomery.An Overview of NASA's Solar Sail Propulsion Project[C].39th AIAA PAPER/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,July,2003.
    [10]Noll TE,Brown JM,Perez-Davis ME,et al.Investigation of the Helios Prototype Aircraft Mishap[R],Tech.rep,NASA,2004.
    [11]Gerald D Miller.Solar Powered Aerial Vehicle[P].2010.
    [12]Andre Noth.Design of solar powered airplanes for continuous flight[D].Switzerland:Ing6nieuren Microtechnique Ecole Polytechnique F6derale de Lausanne,2008.
    [13]Romeo G,Frulla G.HELIPLAT;Aerodynamic and Structural Analysis of HALE Solar Powered Platform[C].AIAA,2002-3504,2002.
    [14]Romeo G,Frulla G and Cestino E.A High-Altitude LongEndurance Solar-powered Unmanned Air Vehicle for Multi-Payload and Operations[J].Aerospace engineering,2006,221(part G):199-216.
    [15]Hannes Ross.Fly around the World with a Solar Powered Airplane[R].AIAA.2008-8954,2008.
    [16]Ron Laurenzo.Soaring on a Solar Impulse[J].Aerospace America,2009:32-36.
    [17]昌敏,周洲,郑志成.太阳能飞机原理及总体参数敏度分析[J].西北工业大学学报,2010,28(5):792-796.
    [18]马东立,包文卓,乔宇航.基于重力储能的太阳能飞机飞行轨迹研究[J].航空学报,2014,35(2):408-416.
    [19]昌敏,周洲,李盈盈.基于能量平衡的太阳能飞机可持续高度分析[J].西北工业大学学报,2012,30(4):541-546.
    [20]吴安民.太阳能飞机设计计算与TRANSYS程序模拟[D].硕士学位论文,西安:西北工业大学.2003.
    [21]邓海强.小型太阳能飞机气动/结构/推进一体化设计研究[D].硕士学位论文,南京:南京航空航天大学.2006.
    [22]Youngblood JW.Design of Long Endurance Unmanned Airplanes Incorporating Solar and Fuel Cells Propulsion[R].AIAA,1984-1430,1984.