临近空间飞艇具有大范围不间断的高效信息获取与传输能力,是近期国际上竞相发展的未来信息平台。蒙皮材料是临近空间飞艇的主要材料,其质量和性能决定了飞艇的大小、寿命和成本,是发展临近空间飞艇的基础。本文中针对临近空间飞艇蒙皮材料选取和应用存在的若干困难,从蒙皮材料工程需求出发,对蒙皮材料的强度、耐候性、阻隔性和试验评价方法等方面的研究现状进行总结和分析,讨论未来高性能临近空间飞艇蒙皮材料的研究发展方向。
The near space airship has widespread and uninterrupted ability of efficient information capturing and transmitting, which is the future information platform recently developed warmly in the world. The envelope materials are the chief materials of the near space airship, and regarded as the foundation of developing the near space airship, whose mass and performance determine the size, service life and cost of the airship. Aiming at several difficulties existing in the selection and application of the envelope materials for the near space airship, and based on the project requirements of the envelope materials, several aspects of the research progress in the envelope materials were reviewed in this paper, including the strength, weatherability, barrier property and test evaluation method, and the direction of future research on the high performance envelope materials for the near space airship were discussed.
参考文献
[1] | Yung G L, Dong M K,Chan H Y. Development of Koreanhigh altitude platform systems [J]. International Journal ofWireless Information Networks> 2006. 13(1) ; 31-42. |
[2] | Yu D R,Lv X W. Configurations analysis for high - altitude/long - endurance airships [ J ]. Aircraft Engineering andAerospace Technology, 2010,82(1) : 48-59. |
[3] | Alexey P,Zhan Q L,David P,et al. Stratospheric satellitesfor earth observations [J]. American Meteorological Society,2009, 90(8); 1109-1119. |
[4] | Miura R,Suzuki M. Preliminary flight test program ontelecom and broadcasting using high altitude platform stations[J]. Wireless Personal Communications, 2003,24(2) : 341 -361. |
[5] | Floriano D R, Mauro T,Salvatore M. Integrated services onhigh altitude platform . Receiver driven smart selection ofHAP-geo satellite wireless access segment and performanceevaluation [J]. International Journal of Wireless InformationNetworks, 2006,13(1): 77-94. |
[6] | 李利良,郭伟民,何家芳.国外近空间飞艇的现状和发展[J].武器装备自动化,2008,27(2): 32-34. |
[7] | Keiji K. Masa - aki S,Yoshiaki K. Development of high -specific-strength envelope materials [Cl//AIAAs 3rd AnnualAviation Technology, Integration, and Operations Tech. Denver, Colorado: American Institute of Aeronautics andAstronautics, Inc,2003: 1-7. |
[8] | Kimito T, Yasumasa H, Shoji M. The studies andapplications for LTA [C] // 7th AIAA Aviation Technology,Integration and Operations Conference. Belfast, NorthernIreland: American Institute of Aeronautics and Astronautics,Inc, 2007: 1-30. |
[9] | 谭惠丰,王超,王长国.实现结构轻量化的新型平流层飞艇研究进展[J].航空学报,2010,31(2): 257-264. |
[10] | Shoji M, Atsushi T. On the structures of the low altitudestationary flight test vehicle [C] // AIAA 5th Aviation,Technology, Integration, and Operations Conference.Arlington, Virginia: American Institute of Aeronautics andAstronautics, Inc, 2005: 1-9. |
[11] | Sasa S, Yoshida H,Ohashi K, et al. Flight test overview ofground to stratosphere flight test vehicle [C] // The FifthStratospheric Platform Systems Workshop Proceedings.Tokyo, Japan: SPSW2005 Program Committee, 2005: 123-128. |
[12] | Daniels K M, Downs R J, Meldner H, et al. High strength-to- weight ratio non - woven technical fabrics for aerospaceapplications [ C ] // AIAA Balloon Systems Conference.Seattle, Washington: American Institute of Aeronautics andAstronautics, Inc, 2009: 1-9. |
[13] | Masaaki N,Shoji M, Toyotoshi K, et al. Investigation of longterm weathering characteristics on high strength and lightweight envelope material Zylon [C] // 11th AIAA AviationTechnology, Integration, and Operations ( ATIO )Conference. Virginia Beach, VA: American Institute ofAeronautics and Astronautics, Inc* 2011 : 1-6. |
[14] | 刘卓峰,肖加余,王宇,等.芳纶基质飞艇气囊囊体材料的制备研究[J]-髙科技纤维与应用,2006,31(3): 26-28. |
[15] | 曹旭,高诚贤.PBO基质平流层飞艇蒙皮材料的制备研究[J].髙科技纤维与应用,2009,34(4): 37-42. |
[16] | 王兆希,窦宝峰,逄型召.平流层浮空器用柔性复合材料的断裂性能[J].复合材料学报,2011, 28(2): 211-216. |
[17] | 屈卫东,范启富.平流层演示飞艇自主飞行试验[J].装备指挥技术学院学报,2007,18(1): 96-98. |
[18] | Lewis J, Geoffrey S S,Isaac R P. High - altitude airships forthe future force army,DASW01 - 01 - C - 0003 [R]. USA:RAND Corporation, 2005. |
[19] | Wanggu K, Youngwook S,Kyeongsik W,et al. Mechanicalproperty characterization of film - fabric laminate forstratospheric airship envelope [J]. Composite Structures. 2006,75: 151-155. |
[20] | 冯艳丽,赵海泉,胡淑芳,等.国产化髙性能F-12芳纶纤维研究进展[C]//杜善义.复合材料:创新与可持续发展(下册):第十六届全国复合材料学术会议.长沙:中国复合材料学会,2010: 1179-1187. |
[21] | 冯艳丽.自主研发的F-12高强有机纤维[J].浮空器研究2009, 3(3): 32-35. |
[22] | 郁文娟.近期国外塑料包装材料发展的最新动向[J].包装工程,1997, 18(2/3): 3-6. |
[23] | 樊岩,胡绍华,章悦庭.EVOH树脂[J].化工新型材料,2000(2): 23-26. |
[24] | Shoji M, Kouichi S, Toyotoshi K. Tear propagation of a high-performance airship envelope material [ J ], Journal ofAircraft, 2008, 45(5): 1546-1553. |
[25] | Said M A, Dingwall B,Gupta A,et al. Investigation of ultraviolet (UV) resistance for high strength fibers [J]. Advancesin Space Research, 2006,37: 2052-2058. |
[26] | Liu Y Y, Zhang C H,Liu Y T, et al. Accelerated ultravioletaging study of the Vectran fiber [J]. Journal of AppliedPolymer Science, 2012,124(4) : 3286-3292. |
[27] | 刘宇婷.Vectran纤维光老化性能的研究及防护处理[D].哈尔滨:哈尔滨工业大学,2009. |
[28] | 白向红.飞艇蒙皮材料力学性能演化规律研究[D].哈尔滨:哈尔滨工业大学,2009. |
[29] | Airships are back in fashion[EB/OL]. (2011 -08 -05)[2011 -12-12]. http://www. uasvision. com/2011/08/05/the -blimps-of-war/. |
[30] | Maekawa S,Maeda T,Sasaki Y,et al. Development ofadvanced lightweight envelope materials for stratosphericplatform airship [C]//43rd Aircraft Symposium, Aeronauticaland Space Sciences. Japan: Japan Society for Aeronautical andSpace Sciences, 2005: 120-124. |
[31] | 任一鹏,田中伟,吴子牛.飞艇空气动力学及其相关问题[J].航空学报,2010, 31(3): 431-443. |
- 下载量()
- 访问量()
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%