电动直升机概念设计与分析
收稿日期: 2016-10-19
修回日期: 2016-12-14
网络出版日期: 2017-04-05
基金资助
江苏高校优势学科建设工程（PAPD）
Conceptual design and analysis of electric helicopters
Received date: 2016-10-19
Revised date: 2016-12-14
Online published: 2017-04-05
Supported by
Priority Academic Program Development of Jiangsu Higher of Education Institutions (PAPD)
赵洪 , 李建波 , 刘铖 . 电动直升机概念设计与分析[J]. 航空学报, 2017 , 38(7) : 520866 -520866 . DOI: 10.7527/S1000-6893.2017.520866
Based on the characteristics of present batteries and electric motors, the energy and power system models adaptable to electric helicopters are established respectively. Three energy programs applicable for electric helicopters are proposed, and a methodology involving primary parameters sizing and optimization for conceptual design of electric helicopters is developed. Considering mission profile requirements, parameters sizing and sensitivity analysis for the helicopter applying the three different energy proposals are performed. Due to limitation of current development of battery technology, there still exists a wide gap between endurance of electric and of fuel-consuming helicopters. Parameter sensitivity analysis shows that the design features of electric helicopters are different from those of fuel-consuming helicopters, so that the characteristics of the power and energy systems should be specifically considered in the design of electric helicopters.
[1] ROSEN K M. A Prospective: The importance of propul sion technology to the development of helicopter systems with a vision for the future[J]. Journal of the American Helicopter Society, 2008, 53(4): 307-337.
[2] SCHNEIDER D. Helicopters go electric[J]. IEEE Spectrum, 2012, 49(1): 11-12.
[3] CHRETIEN P. The quest for the world's first electric manned helicopter flight[J]. Vertiflite, 2012, 58(2): 38-42.
[4] GUINEA D M, ROURA M, GARCIA-ALEGRA M C, et al. Specific weight: A challenge for a fuel-cell-powered electric helicopter[J]. Journal of Aircraft, 2007, 44(6): 2073-2076.
[5] 聂资, 陈铭. 电动直升机飞行性能计算和分析[J]. 北京航空航天大学学报, 2012, 38(9): 1139-1143. NIE Z, CHEN M. Calculation and analysis of electric-powered helicopter flight performance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(9): 1139-1143 (in Chinese).
[6] JOHNSON W. Propulsion system models for rotorcraft conceptual design[C]//AHS 5th Decennial Aeromechanics Specialists’ Conference. Washington, D.C.: NASA, 2014.
[7] DATTA A, JOHSON W. Requirements for a hydrogen powered all-electric manned helicopter: AIAA-2012-5405[R]. Reston: AIAA, 2012.
[8] MARTIN H. Electric flight-potential and limitations[J]. Efficient Technologies and Concepts Operation, 2012, 203(5): 371-372.
[9] Electric propulsion components with high power densities for aviation[EB/OL]. [2016-10-18]. http://nari.arc.nasa.gov/sites/default/files/attachments/Korbinian-TVFW-Aug2015.pdf.
[10] Manual_for_emrax_motor_december_2014_new.pdf. [EB/OL]. [2016-10-18]. http://www.enstroj.si/download.php?f=imagEs/stories/manal_for_emrax_motor_december_2014_new.pdf.
[11] MCDONALD R A. Electric motor modeling for conceptual aircraft design: AIAA-2013-0941[R]. Reston: AIAA, 2013.
[12] US DRIVE. Fuel cell technical team roadmap[R]. U.S. DRIVE Partnership, 2013.
[13] YU W, XU S C, NI H S. Air compressors for fuel cell vehicles: An systematic review[J]. SAE International Journal of Alternative Powertrains, 2015, 4(1): 112-115.
[14] 2016 Fuel cells section, multi-year research, development, and demonstration plan[EB/OL]. [2016-10-18] http://energy.gov/sites/prod/files/2016/06/f32/fcto_myrdd_fuel_cells_0.pdf.
[15] BRADLEY T, MOFFIT B, PAREKH D, et al. Energy management for fuel cell powered hybrid-electric aircraft: AIAA-2009-4590[R]. Reston: AIAA, 2009.
[16] 张呈林, 郭才根. 直升机总体设计[M]. 北京: 国防工业出版社, 2006: 49-57. ZHANG C L, GUO C G. Helicopter preliminary design[M]. Beijing: Defense Industry Press, 2006: 49-57 (in Chinese).
[17] 贾伟力, 陈仁良. 一种直升机总体概念设计方法[J]. 南京航空航天大学学报, 2011, 43(3): 289-295. JIA W L, CHEN R L. Conceptual design method for helicopter with main and tail rotors[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2011, 43(3): 289-295 (in Chinese).
[18] JOHNSON W. NDARC: NASA design and analysis of rotorcraft: NASATP 2009-215402[R]. Washington, D.C.: NASA, 2009.
[19] PROUTY R W. Helicopter performance, stability, and control[M]. Florida: Krieger Publishing Company, 2005: 273-332.
[20] 杨宇军, 陈建军, 马娟, 等. 基于区间因子法的可靠度与参数敏感度分析[J]. 机械强度, 2009, 31(2): 236-239. YANG Y J, CHEN J J, MA J, et al. Analysis of reliability and parametric sensitivity based on interval factor method[J]. Journal of Mechanical Strength, 2009, 31(2): 236-239 (in Chinese).
/
| 〈 |
|
〉 |
CJA