In this paper, thermal management technologies for hypersonic flight vehicles are reviewed from the point view of heat dissipation and reuse. For heat dissipation, concepts concerning such as passive/semi-active/active thermal protection, structure/thermal integrated protection, and other multi-functions are reviewed. For heat reuse, some regenerative cooling and thermoelectric conversion technologies are also reviewed. Finally, based on the characteristics and research progress of aforementioned technologies, some potential research fields of thermal management for hypersonic flight vehicles are proposed.
GOU Jianjun
,
HU Jiaxin
,
CHANG Yue
,
CHEN Bing
,
GONG Chunlin
. Research progress of thermal management technologies for hypersonic flight vehicles[J]. Science & Technology Review, 2020
, 38(12)
: 103
-108
.
DOI: 10.3981/j.issn.1000-7857.2020.12.009
[1] Gori F, Corasaniti S, Worek W M, et al. Theoretical prediction of thermal conductivity for thermal protection systems[J]. Applied Thermal Engineering, 2012, 49:124-130.
[2] Rong Y, Wei Y, Zhan R. Research on thermal protection by opposing jet and transpiration for high speed vehicle[J]. Aerospace Science and Technology, 2016, 48(Supplement C):322-327.
[3] 王一凡. 面向高速飞行器的波纹夹芯型一体化热防护设计及热力耦合分析方法研究[D]. 西安:西北工业大学航天学院, 2017.
[4] Gong C L, Gou J J, Hu J X, et al. A novel TE-material based thermal protection structure and its performance evaluation for hypersonic flight vehicles[J]. Aerospace Science and Technology, 2018, 77:458-470.
[5] Ochoa O O. Functionally graded multifunctional hybrid composites for extreme environments[R]. Texas:Texas A & M University, 2010.
[6] Bouchez M, Beyer S, Schmidt S. PTAH-SOCAR fuelcooled composite materials structure:2011 status[C]//17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. California:American Institute of Aeronautics and Astronautics, 2011.
[7] Bouchez M, Swiergiel N, Pradat F, et al. Challenge in robust design of composite architectured structures[C]//21st AIAA International Space Planes and Hypersonics Technologies Conference. Xiamen:American Institute of Aeronautics and Astronautics, 2017.
[8] Zhang C, Qin J, Yang Q, et al. Design and heat transfer characteristics analysis of combined active and passive thermal protection system for hydrogen fueled scramjet[J]. International Journal of Hydrogen Energy, 2015, 40(1):675-682.
[9] Li X, Wang Z. Exergy analysis of integrated TEG and regenerative cooling system for power generation from the scramjet cooling heat[J]. Aerospace Science and Technology, 2017, 66(Supplement C):12-19.
[10] Ulas A, Boysan E. Numerical analysis of regenerative cooling in liquid propellant rocket engines[J]. Aerospace Science and Technology, 2013, 24(1):187-197.
[11] 杨成骁, 王长辉. 液体火箭发动机推力室复合冷却流动与传热研究[J/OL].[2019-11-20]. https://doi.org/10.13675/j.cnki.tjjs.190375.
[12] Hou Z Y, He G Q, Li W Q, et al. Numerical investigation on thermal behaviors of active-cooled strut in RBCC engine[J]. Applied Thermal Engineering, 2017, 113:822-830.
[13] Jing T T, He G Q, Li W Q, et al. Flow and thermal analyses of regenerative cooling in non-uniform channels for combustion chamber[J]. Applied Thermal Engineering, 2017, 119:89-97.
[14] Yan D, He G Q, Li W Q, et al. Thermal analysis of regenerative-cooled pylon in multi-mode rocket based combined cycle engine[J]. Acta Astronautica, 2018, 148:121-131.
[15] Gou J J, Chang Y, Yan Z W, et al. The design of thermal management system for hypersonic launch vehicles based on active cooling networks[J]. Applied Thermal Engineering, 2019, 159:113938.
[16] 胡嘉欣. 可重复使用RBCC运载器主要部位热防护方案研究[D]. 西安:西北工业大学航天学院, 2019.
[17] Li F, Zhai R, Wu Y, et al. Enhanced thermoelectric performance of n-type bismuth-telluride-based alloys via In alloying and hot deformation for mid-temperature power generation[J]. Journal of Materiomics, 2018, 4(3):208-214.
[18] Lv S, He W, Jiang Q, et al. Study of different heat exchange technologies influence on the performance of thermoelectric generators[J]. Energy Conversion and Management, 2018, 156(Supplement C):167-177.
[19] Lan S, Yang Z, Chen R, et al. A dynamic model for thermoelectric generator applied to vehicle waste heat recovery[J]. Applied Energy, 2018, 210(Supplement C):327-338.
[20] Cheng K, Qin J, Jiang Y, et al. Performance assessment of multi-stage thermoelectric generators on hypersonic vehicles at a large temperature difference[J]. Applied Thermal Engineering, 2018, 130:1598-1609.
