期刊文献+

高空驻留太阳能飞机主动式光伏组件面功率特性研究 被引量:14

Exploring the Characteristics of Power Density of Tracking PV Modules for High-altitude Stationary Solar-powered Airplanes
原文传递
导出
摘要 光伏组件面功率特性是影响太阳能飞机性能指标的关键因素之一。首先建立了考虑光伏组件表面温度、太阳能飞机飞行高度、纬度及一年四季等因素的光伏组件面功率模型,分析了光伏组件在一年范围内的日均直射、日均水平面功率随飞行高度、纬度和季节等关键设计指标参数的变化规律,对比研究了3种跟踪采能方式下的主动式光伏组件(TPM)的逐时、日均面功率特性。结果表明:在一天的光照时间内和全年范围内,主动式光伏组件能显著提高光伏组件的面功率特性。然后,参考了典型的太阳能飞机"Helios"和"Zephyr",综合考虑能源与气动特性,初步设计了一种采用主动式光伏组件的高空驻留太阳能飞机布局方案,通过分析其日均净面功率特性得出:合理设计主动式光伏组件,可以显著提高太阳能飞机的日均净面功率约32%~66%,甚至可达116%。这些结论均说明,从采能效率和气动特性两方面综合来说,所提出的基于主动式光伏组件的布局设计思想在高空驻留太阳能飞机总体布局设计时具有良好的应用优势。 The characteristics of power density of PV(photovoltaic) modules play a key part in the flight performance of solar-powered airplanes.Firstly,this paper establishes a model of power density for PV modules,taking into consideration the temperature of PV modules,flight altitude,flight latitude,and year-round seasons.Based on this model,this poper analyzes the variation of the day-average power density of PV modules for horizontal surfaces and surfaces perpendicular to the Sun.this paper presents a comparative study of the characteristics of power density of tracking PV modules(TPM) under three types of tracking methods,and the results show that tracking PV modules improve the power performance during both the daylight in one day and during a whole year.Then,based on two typical solar-powered airplanes,"Helios" and "Zephyr",this paper proposes a new concept of solar-powered airplane with tracking PV modules and analyzes their effects on improving the average net power density.The results show that the tracking PV modules can increase power density by 32% to 66%,and at times even up to 116% if well designed.From the point of view of both energy and aerodynamic efficiency,this paper shows that it is necessary to apply the tracking PV modules to designing stationary high-altitude solar-powered airplanes due to their superiorities.
出处 《航空学报》 EI CAS CSCD 北大核心 2013年第2期273-281,共9页 Acta Aeronautica et Astronautica Sinica
基金 国家"863"计划(2011AA7052002) 国家自然科学基金(11202162)~~
关键词 太阳能飞机 主动式光伏组件 面功率 飞行高度 飞行纬度 表面温度 跟踪方式 高空驻留飞机 solar-powered aircraft tracking PV modules power density flight altitude flight latitude surface temperature tracking method high-altitude stationary airplanes
  • 相关文献

参考文献11

  • 1Alexandru C,Pozna C. Simulation of a dual-axis solar tracker for improving the performance of a photovoltaic panel[J].Proceeding of the Institution of Mechanical Engineering Part A:Journal of Power and Energy,2010,(06):797-811.
  • 2Haws T D,Bowman W J. Thermal analysis of the pathfinder aircraft.AIAA-1999-735[R].1999.
  • 3Noth A. Design of solar powered airplanes for continuous flight[M].Suisse:Ecole Polytechnique Fédérale de Lausanne at ETH ZüRICH,2008.
  • 4Keidel B. Auslegung und simulation yon hochflie-genden dauerhaft stationierbaren solardrohnen[M].Miinchen:Fakult(a)t für Maschinenwesen at Technischen Universit(a)t Müinchen,2000.
  • 5赵争鸣;刘建政;孙晓英.太阳能光伏发电及其应用[M]北京:科学出版社,200543-72.
  • 6Durisch W,Urban J,Pmestad G. Characterisation of solar cells and modules under actual operating conditions[J].Renewable Energy,1996,(1-4):359-366.
  • 7Incropera Frank P,Dewitt D P. Fundamentals of heat and mass transfer[M].New York:John Wiley and Sons,Inc,2011.
  • 8NOAA,NASA,USAF. US standard atmosphere[S].1976.
  • 9Kata J,Plotkin A. Low-speed aerodynamics:from wing theory to panel methods[M].New York:mcgraw-hill Book Company,inc,1991.
  • 10Daniel P R. Aircraft design.a conceptual approach[M].Washington D.C.:American Institute of Aeronautics and Astronautics,Inc,1999.280-289.

二级参考文献5

  • 1刘斌,马晓平,王和平,周康生.小型电动无人机总体参数设计方法研究[J].西北工业大学学报,2005,23(3):396-400. 被引量:31
  • 2Andre NOTH. Design of Solar Powered Airplanes for Continuous Flight. Switzerland: Ingenieur en Microtechnique Ecole Polytechnique Felerale de Lausanne, 2008.
  • 3Ron Laurenzo. Soaring on a Solar Impulse. Aerospace America, 2009, 32 - 36.
  • 4Enrico Cestino. Design of Solar High Altitude Long Endurance Aircraft for Multi-Payload & Operations. Aerospace Science and Technology, 2006,10:541 - 550.
  • 5Alan Cocconi. AC Propulsion' s Solar Electric Powered SoLong UAV. San Dimas: AC Propulsion.

共引文献30

同被引文献114

引证文献14

二级引证文献51

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部