扇翼飞行器的研究进展与应用前景
收稿日期: 2014-10-24
修回日期: 2015-02-15
网络出版日期: 2015-03-25
基金资助
国家级项目
Research progress and application prospects of fan-wing aircraft
Received date: 2014-10-24
Revised date: 2015-02-15
Online published: 2015-03-25
Supported by
National Level Project
随着科学技术的迅猛发展,飞机无论在构型还是性能方面都获得了飞速发展,但是新原理飞机的研制却进展不大。扇翼飞行器是近期发展起来的低速大载荷新型飞行器,它是不同于现有固定翼、旋翼飞行器的新构型、新原理飞行器。而国内对于该飞行器的研究才刚刚起步,可参考的文献资料很少。因此,本文通过国内外扇翼飞行器发展状况的研究,对扇翼飞行器研究进展进行总结分析。首先介绍了扇翼飞行器的飞行原理;其次系统地回顾了扇翼飞行器的提出,并总结了其在国内外研究的进展情况;接着根据扇翼飞行器近期的发展动态,对该飞行器的应用前景作出分析;最后总结了扇翼飞行器发展中亟待解决的关键技术,以及其未来发展的难点和趋势。
孟琳 , 叶永强 , 李楠 . 扇翼飞行器的研究进展与应用前景[J]. 航空学报, 2015 , 36(8) : 2651 -2661 . DOI: 10.7527/S1000-6893.2015.0058
With the rapid development of science and technology, airplane is developing by leaps and bounds both in configuration and performance. However, few truly new aircraft has been developed except the fan-wing aircraft, a new low-speed, large-load aerial vehicle that has been developed in recent years, which is different from fixed-wing aircraft and rotorcraft. But the domestic research on this aircraft has just started and little literature is available for reference. Therefore, based on the domestic and foreign research on the fan-wing aircraft, the research progress of the fan-wing aircraft is summarized and analyzed. Firstly the flying principle of the fan-wing aircraft is reviewed. Next, the raise of the fan-wing aircraft in detail is reviewed too. And the past of the research and development in the fan-wing aircraft history is summarized. Then, according to its recent trend and development, analysis of its application in future is conducted. Finally, key technology of the fan-wing aircraft is summarized. In addition, the problems and trends in its future development are presented.
[1] Dang T Q, Bushnell P R. Aerodynamics of cross-flow fans and their application to aircraft propulsion and flow control[J]. Progress in Aerospace Sciences, 2009, 45(1): 1-29.
[2] Dang T Q, Kummer J D. Cross-flow fan propulsion system: U.S. Patent 7641144[P]. 2010-1-5.
[3] Toffolo A, Lazzaretto A, Dario Martegani A. An experimental investigation of the flow field pattern within the impeller of a cross-flow fan[J]. Experimental Thermal and Fluid Science, 2004, 29(1): 53-64.
[4] Mortier P. Fan or blowing apparatus: US Patent 507445[P].1893.
[5] Ackeret J. Present and future problems of airplane propulsion[J]. Schweizer Bauzeitung, 1938: 112(1): 1-13.
[6] Dornier P. Multiple drive for aircraft having wings provided with transverse flow blowers: US Patent 3065928[P]. 1962-11-27.
[7] Dornier P. Aircraft with ground effect landing gear: US Patent 3082976[P]. 1963-03-26.
[8] Harloff G J. Cross-flow fan experimental development and finite-element modeling[D]. Arlington, TX: University of Texas, 1979.
[9] Harloff G J, Wilson D R. Cross-flow propulsion fan experimental development and finite-element modeling[J]. Journal of Aircraft, 1981, 18(4): 310-317.
[10] Hancock J P. Test of a high efficiency transverse fan[C]//AIAA/SAE/ASME 16th Joint Propulsion Conference. Reston: AIAA, 1980.
[11] Mazur J S. A study of the cross flow fan[D]. Detroit, MI: Wayne State University, 1984.
[12] Gossett D H. Investigation of cross flow fan propulsion for light weight VTOL aircraft[D]. Monterey, CA: Naval Postgraduate School, 2000: 29-37.
[13] Peebles P. Aerodynamic lift generating device: US6527229B1[P]. 2003-03-04.
[14] Foreshaw S. Wind tunnel investigation of the new 'Fanwing' design[D]. London: Imperial College, 1999.
[15] Kogler K. FanWing: experimental evaluation of a novel lift and propulsion device[D]. London: Imperial College, 2002.
[16] Ahad O, Graham J M R. Flight simulation and testing of the FanWing experimental aircraft[J]. Aircraft Engineering and Aerospace Technology, 2007, 79(2): 131-136.
[17] Kummer J D, Dang T Q. Hight-lift propulsive airfoil with integrated cross flow fan[J]. Journal of Aircraft, 2006, 43(4): 1059-1068.
[18] Duddempudi D, Yao Y, Edmondson D, et al. Computational study of flow over generic fan-wing airfoil[J]. Aircraft Engineering and Aerospace Technology, 2007, 79(3): 238-244.
[19] Askari S, Shojaeefard M H. Numerical simulation of flow over an airfoil with a cross flow fan as a lift generating member in a new aircraft model[J]. Aircraft Engineering and Aerospace Technology, 2009, 81(1): 59-64.
[20] Askari S, Shojaeefard M H. Shape optimization of the airfoil comprising a cross flow fan[J]. Aircraft Engineering and Aerospace Technology, 2009, 81(5): 407-415.
[21] Askari S, Shojaeefard M H, Goudarzi K. Experimental study of stall in an airfoil with forced airflow provided by an integrated cross-flow fan[J]. Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering, 2011, 225(G1): 97-104.
[22] Seyfang G R. Fanwing-developments and applications[C]//28th Congress of the International Council of the Aeronautical Sciences. Brisbane: ICAS, 2012: 1-9.
[23] Seyfang G R. Recent developments of the fan-wing aircraft[C]//The International Conference of the European Aerospace Societies. Brussels: CEAS, 2011: 1-7.
[24] Niu Z G, Jiang J L, Li Z F. Study on numerical simulation of two-dimensional airfoil fan-wing aircraft[C]//Forum on Key Technologies of Large Aircraft and Aeronautical Society of China Proceedings of the 2007 Annual Meeting. Beijing: CSAA, 2007: 1-5 (in Chinese). 牛中国, 蒋甲利, 李周复. 扇翼飞机二维机翼数值模拟分析研究[C]//大型飞机关键技术高层论坛暨中国航空学会2007年学术年会论文集. 北京:中国航空学会, 2007: 1-5.
[25] Niu Z G, Jiang J L, Li Z F. Numerical analysis of fan-wing fan blades angle[J]. Aerodynamic Research & Experiment, 2008, 26(2): 6-10 (in Chinese). 牛中国, 蒋甲利, 李周复. 扇翼飞行器风扇叶片偏角影响数值分析[J]. 气动研究与实验, 2008, 26(2): 6-10.
[26] Niu Z G, Jiang J L, Liu J, et al. Design and research of fan-wing airfoil[J]. Aerodynamic Research & Experiment, 2009, 27(3): 6-11 (in Chinese). 牛中国, 蒋甲利, 刘杰, 等. 扇翼飞行器机翼设计与研究[J]. 气动研究与实验, 2009, 27(3): 6-11.
[27] Jiang J L, Niu Z G, Liu J, et al. Research on the wing composition of fan-wing flight[J]. Aeronautical Science and Technology, 2009(3): 30-35 (in Chinese). 蒋甲利, 牛中国, 刘捷, 等. 扇翼飞行器机翼布局研究[J]. 航空科学技术, 2009(3): 30-35.
[28] Wang R H, Zhang H L, Huang T G, et al. Numerical study of flow over fan-wing airfoil[J]. Applied Science and Technology, 2012, 38(12): 5-8 (in Chinese). 王仁华, 张海黎, 黄同高, 等. 扇翼飞行器绕翼型流动数值研究[J]. 应用科技, 2012, 38(12): 5-8.
[29] Huang T G, Yang Z, Wang R H, et al. Longitudinal mathematical modeling and flight control of the fan-wing aircraft[J]. Applied Science and Technology, 2011, 38(11): 5-8 (in Chinese). 黄同高, 杨忠, 王仁华, 等. 扇翼飞行器纵向运动建模与控制方法[J]. 应用科技, 2011, 38(11): 5-8.
[30] Chen T. Research on flight control system of fan-wing aircraft[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2014 (in Chinese). 陈滔. 扇翼飞行器飞行控制系统研究[D]. 南京: 南京航空航天大学, 2014.
[31] Di N S. Computational simulation and experimental research on fan wing for flying robot[D]. Shanghai: East China University of Science and Technology, 2014 (in Chinese). 邸南思. 面向飞行机器人的扇翼翼型数值分析与实验研究[D]. 上海: 华东理工大学, 2014.
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