一种一体化热防护系统综合效能量化评价方法
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摘要
一体化热防护系统(ITPS)已经成为高超速飞行器关注的主要发展方向,承力和防热的双重作用使得ITPS能够显著降低飞行器的整体重量。在对ITPS进行综合效能分析时,需要考虑结构效率、材料性能、结构的可设计性和工艺的复杂性等因素。本文从ITPS设计的合理性、ITPS减重的可行性、设计的难易度、工艺的复杂度4个方面进行了讨论,为设计人员提供指导。
Integrated Thermal Protection System(ITPS) has become the main development direction of high-speed aircraft. The combined effect of load bearing and heat protection allows ITPS to significantly reduce the overall weight of the aircraft. In the comprehensive performance analysis of ITPS, factors such as structural efficiency, material properties, structural designability, and process complexity need to be considered. This paper discusses the rationality of ITPS design, the feasibility of ITPS weight reduction, the difficulty of design, and the complexity of the process,which can provide guidance to designers.
Integrated Thermal Protection System(ITPS) has become the main development direction of high-speed aircraft. The combined effect of load bearing and heat protection allows ITPS to significantly reduce the overall weight of the aircraft. In the comprehensive performance analysis of ITPS, factors such as structural efficiency, material properties, structural designability, and process complexity need to be considered. This paper discusses the rationality of ITPS design, the feasibility of ITPS weight reduction, the difficulty of design, and the complexity of the process,which can provide guidance to designers.
引文
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[10]梦松鹤,杨强,霍施宇,等.一体化热防护技术现状和发展局势[J].宇航学报,2013,34(10):1295-1302.Meng Songhe,Yang Qiang,Huo Shiyu,et al.State-of-arts and trend of integrated thermal protection systems[J].Journal of Astronautic,3013,34(10):1295-1302.(in Chinese)
[11]Materials Research&Design,Inc.Thermal protection for reentry&hypersonic systems[EB//OL].[2013-04-26].http://www.m-r-d.com/experience/thermal-protection.php.
[12]杨强.一体化热防护系统设计与综合效能多级优化方法研究[D].哈尔滨:哈尔滨工业大学,2013.Yang Qiang.Design and performance evaluation method of integrated thermal production systems[D].Harbin:Harbin Institute of Technology,2013.(in Chinese)
[13]杨志斌,成竹,李丽霞,等.一种一体化热防护系统承力结构的设计研究[J].应用力学学报,2018,35(4):883-889.Yang Zhibin,Cheng Zhu,Li Lixia,et al.Research on a loadcarrying capacity structure design of integrated thermal protection systems[J].Chinese Journal of Applyed Mechanics2018,35(4):883-889.(in Chinese)(责任编辑王为)
[2]程克明,吕英伟.飞行器持续气动加热的耦合性分析[J].南京航空航天大学学报,2000,32(2):150-155.Cheng Keming,Lv Yingwei.Coupling analysis of continuous aerodynamic heating of aircraft[J].Journal of Nanjing University of Aeronautics and Astronautics,2000,32(2):150-155.(in Chinese)
[3]Bapanapalli S K,Martinez O M,Gogu C,et al.Analysis and design of corrugated-core sandwich panels for Thermal Protection Systems of space vehicles[C]//47th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference,Newport,RhodeIsland,USA,2006.
[4]Kumar S,Diane Villanueva D,Sankar B V,et al.Optimization of integrated thermal protection system[R].AIAA 2008-59282008.
[5]Sharma A,Sankar B V,Raphael T,et al.Multi-fidelity analysis of corrugated-core sandwich panels for integrated thermal protection systems[R].AIAA 2009-2201,2009.
[6]Ravishankar B,Sankar B V,Haftka R T.Homogenization of integrated thermal protection system with rigid insulation bars[R].AIAA 2010-2687,2010.
[7]Villanueva d,Haftka R T,Sankar B V.Accounting for future redesign in the optimization of an integrated thermal protection system[R].AIAA 2012-1933,2012.
[8]胡秋野.波纹夹层板一体化热防护系统多级优化方法研究[D].南京:南京航空航天大学,2017.Hu Qiuye.Multilevel optimization of corrugated-core integrate thermal protection system[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2017.(in Chinese)
[9]解维华,霍施宇,杨强,等.新型一体化热防护系统热力分析与试验研究[J].航空学报,2013,34(9):2169-2175.Xie Weihua,Huo Shiyu,Yang Qiang,et al.Thermal mechanical analysis and test study of a new integrated thermal protection system[J].Acta Aeronautica et Astronautica Sinica,2013,34(9):2169-2175.(in Chinese)
[10]梦松鹤,杨强,霍施宇,等.一体化热防护技术现状和发展局势[J].宇航学报,2013,34(10):1295-1302.Meng Songhe,Yang Qiang,Huo Shiyu,et al.State-of-arts and trend of integrated thermal protection systems[J].Journal of Astronautic,3013,34(10):1295-1302.(in Chinese)
[11]Materials Research&Design,Inc.Thermal protection for reentry&hypersonic systems[EB//OL].[2013-04-26].http://www.m-r-d.com/experience/thermal-protection.php.
[12]杨强.一体化热防护系统设计与综合效能多级优化方法研究[D].哈尔滨:哈尔滨工业大学,2013.Yang Qiang.Design and performance evaluation method of integrated thermal production systems[D].Harbin:Harbin Institute of Technology,2013.(in Chinese)
[13]杨志斌,成竹,李丽霞,等.一种一体化热防护系统承力结构的设计研究[J].应用力学学报,2018,35(4):883-889.Yang Zhibin,Cheng Zhu,Li Lixia,et al.Research on a loadcarrying capacity structure design of integrated thermal protection systems[J].Chinese Journal of Applyed Mechanics2018,35(4):883-889.(in Chinese)(责任编辑王为)