飞行器燃料再生冷却热管理系统参数设计

doi:10.11949/0438-1157.20191223

化工学报 ›› 2020, Vol. 71 ›› Issue (S1): 204-211.doi: 10.11949/0438-1157.20191223

飞行器燃料再生冷却热管理系统参数设计

陈玮玮¹(),方贤德²,鹿世化¹,林福建¹,张烨¹

^1.南京师范大学能源与机械工程学院，江苏南京 210023
^2.南京航空航天大学航空学院，江苏南京 210016

收稿日期:2019-10-23 修回日期:2019-11-27 出版日期:2020-04-25 发布日期:2020-05-22
通讯作者: 陈玮玮 E-mail:chenweiwei@njnu.edu.cn
作者简介:陈玮玮（1985—），男，博士，讲师，chenweiwei@njnu.edu.cn
基金资助:
江苏省自然科学基金项目(BK20180732);中国博士后科学基金项目(2018M632332);江苏省高等学校自然科学研究项目(18KJB470017)

Parameter design of aircraft fuel regeneration cooling thermal management system

Weiwei CHEN¹(),Xiande FANG²,Shihua LU¹,Fujian LIN¹,Ye ZHANG¹

^1.School of Energy and Mechanical Engineering, Nanjing Normal University, Nanjing 210023, Jiangsu, China
^2.College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, Jiangsu, China

Received:2019-10-23 Revised:2019-11-27 Online:2020-04-25 Published:2020-05-22
Contact: Weiwei CHEN E-mail:chenweiwei@njnu.edu.cn

摘要/Abstract

摘要：

考虑飞行器的服役环境以及热管理系统质量与几何尺寸的设计要求，探讨了以航空燃料再生冷却技术为基础的高超声速飞行器综合热管理系统的方案。根据不同的热载荷种类和换热方式，结合新提出的超临界压力碳氢燃料管内传热关联式，给出了飞行器热管理系统中两种类型换热设备的传热参数设计方法。利用MATLAB/SIMULINK平台的图形化交互界面创建并封装了飞行器热管理系统的主要功能模块，并以国内典型的RP-3型航空煤油为例，实现了以航空燃料为热沉的热管理系统参数设计过程。

关键词: 高超声速飞行器, 碳氢燃料, 对流, 传热, 超临界流体, 再生冷却

Abstract:

The scheme of hypersonic vehicle integrated thermal management system based on the aviation fuel regeneration cooling technology was discussed by considering the service environment of aircraft and the design requirements of the mass and geometric size of the thermal management system. According to different heat load types and heat transfer modes, together with the newly proposed in-tube heat transfer correlation under supercritical pressure for hydrocarbon fuels, the heat transfer parameter design methods for the two types of heat transfer equipment in aircraft thermal management system were given. The main functional modules of the aircraft thermal management system were created and encapsulated by using the graphical interactive interface of MATLAB/SIMULINK platform. Taking the typical RP-3 aviation kerosene as an example, the parameter design process of the thermal management system with aviation fuel as heat sink was realized.

Key words: hypersonic vehicle, hydrocarbon fuel, convection, heat transfer, supercritical fluid, regenerative cooling

中图分类号:

TK 124

陈玮玮, 方贤德, 鹿世化, 林福建, 张烨. 飞行器燃料再生冷却热管理系统参数设计[J]. 化工学报, 2020, 71(S1): 204-211.

Weiwei CHEN, Xiande FANG, Shihua LU, Fujian LIN, Ye ZHANG. Parameter design of aircraft fuel regeneration cooling thermal management system[J]. CIESC Journal, 2020, 71(S1): 204-211.

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参考文献 30

1	Moses P L, Rausch V L, Nguyen L T, et al. NASA hypersonic flight demonstrators — overview, status, and future plans [J]. Acta Astronautica, 2004, 55(3): 619-630.
2	沈剑, 王伟. 国外高超声速飞行器研制计划[J]. 飞航导弹, 2006, (8): 1-9.
	Shen J, Wang W. Development plan of hypersonic vehicle abroad [J]. Aerodynamic Missile Journal, 2006, (8): 1-9.
3	陈梅洁, 程珙, 田枫林, 等. 高超声速飞行器流-热-固耦合数值模拟[J]. 化工学报, 2015, 66: 89-94.
	Chen M J, Cheng G, Tian F L, et al. Hypersonic vehicle flow-heat-solid coupling simulation [J]. CIESC Journal, 2015, 66: 89-94.
4	Wang J, Ran Z. Terminal guidance for a hypersonic vehicle with impact time control [J]. Journal of Guidance Control & Dynamics, 2018, 41(8):1790-1798.
5	Hu Q, Yao M, Wang C, et al. Adaptive backstepping control for air-breathing hypersonic vehicles with input nonlinearities [J]. Aerospace Science & Technology, 2018, 73: 289-299.
6	Edwards T. Aviation fuel development – past highlights and future prospects [C]// Proceedings of AIAA International Air and Space Symposium and Exposition: The Next 100 Years. Dayton, Ohio, USA, 2003.
7	Hou Y Z, Zheng J L, Dong W. Transient test of aerodynamic heating for hypersonic vehicle [J]. Journal of Aerospace Power, 2010, 25(2): 343-347.
8	Lu H, Liu W. Numerical simulation in influence of forward-facing cavity on aerodynamic heating of hypersonic vehicle [J]. Procedia Engineering, 2012, 29(4): 4096-4100.
9	Mifsud M, Estruch-Samper D, Macmanus D, et al. A case study on the aerodynamic heating of a hypersonic vehicle [J]. Aeronautical Journal, 2012, 116(1183): 873-893.
10	Fujii K, Watanabe S, Kurotaki T, et al. Aerodynamic heating measurements on nose and elevon of hypersonic flight experiment vehicle [J]. Journal of Spacecraft & Rockets, 2015, 38(1): 8-14.
11	郭永胜, 张玲玲, 魏会, 等. 改善吸热型碳氢燃料热管理能力的研究进展[J]. 石油学报(石油加工), 2011, 27(5): 822-828.
	Guo Y S, Zhang L L, Wei H, et al. Research progress in improvement of thermal management capacities of endothermic hydrocarbon fuels [J]. Acta Petrolei Sinica (Petroleum Processing Section), 2011, 27(5): 822-828.
12	耿宸, 郭亚军, 冯松, 等. 随机温度信号互相关法测量吸热型碳氢燃料密度[J]. 化工学报, 2019, 70(1): 24-31.
	Geng C, Guo Y J, Feng S, et al. Density measurements of endothermic hydrocarbon fuel using random temperature signal cross-correlation [J]. CIESC Journal, 2019, 70(1): 24-31.
13	严俊杰, 祝银海, 芦泽龙, 等. 超临界压力碳氢燃料瞬态加热响应特性[J]. 化工学报, 2015, 66: 65-70.
	Yan J J, Zhu Y H, Lu Z L, et al. Transient response of supercritical pressure hydrocarbon fuels during heating condition [J]. CIESC Journal, 2015, 66: 65-70.
14	Leylegian J, Chinitz W. Investigation of short contact time reactors for regeneratively-cooled hypersonic vehicles [J]. Journal of Propulsion & Power, 2012, 28(2): 412-422.
15	Zhu Y, Wei P, Xu R, et al. Review on active thermal protection and its heat transfer for airbreathing hypersonic vehicles [J]. Chinese Journal of Aeronautics, 2018, 31(10): 4-28.
16	Lander H, Nixon A C. Endothermic fuels for hypersonic vehicles [J]. Journal of Aircraft, 1971, 8(4): 200-207.
17	Huang H, Sobel D R, Spadaccini L J. Endothermic heat-sink of hydrocarbon fuels for scramjet cooling [C]// Proceedings of the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Indianapolis, Indiana, USA, 2002.
18	Huang H, Spadaccini L J, Sobel D R. Fuel-cooled thermal management for advanced aeroengines [J]. Journal of Engineering for Gas Turbines and Power, 2004, 126(2): 284-293.
19	陈玮玮, 方贤德. 超临界压力下航空煤油RP-3竖直管内传热关系式评价[C]//工程热物理学会多相流学术会议暨国家自然科学基金进展交流会论文集. 南京, 2015: 156072.
	Chen W W, Fang X D. Evaluation of heat transfer correlations of aviation kerosene RP-3 under supercritical pressure in vertical tubes [C]// Proceedings of the Multiphase Flow and the Progress of the National Natural Science Foundation of Engineering Thermal Physics Society. Nanjing, 2015: 156072.
20	Chen W, Fang X. Modeling of convective heat transfer of RP-3 aviation kerosene in vertical miniature tubes under supercritical pressure [J]. International Journal of Heat and Mass Transfer, 2016, 95: 272-277.
21	孙星, 徐可可, 孟华. 超临界压力正癸烷在螺旋管中传热与裂解吸热现象的数值模拟[J]. 化工学报, 2018, 69: 20-25.
	Sun X, Xu K K, Meng H. Supercritical-pressure heat transfer of n-decane with fuel pyrolysis in helical tube [J]. CIESC Journal, 2018, 69: 20-25.
22	王彦红, 李素芬, 赵星海. 超临界压力下航空煤油传热恶化的分析与预测[J]. 化工学报, 2018, 69(12): 5056-5064.
	Wang Y H, LI S F, Zhao X H. Analysis and prediction of heat transfer deterioration of aviation kerosene under supercritical pressures [J]. CIESC Journal, 2018, 69(12): 5056-5064.
23	胡志宏, 陈听宽, 罗毓珊, 等. 高热流条件下超临界压力煤油流过小直径管的传热特性[J]. 化工学报, 2002, 53(2): 134-138.
	Hu Z H, Chen T K, Luo Y S, et al. Heat transfer to kerosene at supercritical pressure in small-diameter tube with large heat flux [J]. Journal of Chemical Industry and Engineering (China), 2002, 53(2): 134-138.
24	Tao Z, Cheng Z, Zhu J, et al. Effect of turbulence models on predicting convective heat transfer to hydrocarbon fuel at supercritical pressure [J]. Chinese Journal of Aeronautics, 2016, 29(5): 1247-1261.
25	Fu Y, Jie W, Zhi T, et al. Experimental research on convective heat transfer of supercritical hydrocarbon fuel flowing through U-turn tubes [J]. Applied Thermal Engineering, 2017, 116: 43-55.
26	王浚, 王佩广. 高超声速飞行器一体化防热与热控设计方法[J]. 北京航空航天大学学报, 2006, 32(10): 1129-1134.
	Wang J, Wang P G. Integrated thermal protection and control design methodology for hypersonic vehicles [J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(10): 1129-1134.
27	王佩广, 刘永绩, 王浚. 高超声速飞行器综合热管理系统方案探讨[J]. 中国工程科学, 2007, 9(2): 44-48.
	Wang P G, Liu Y J, Wang J. Discussion on integrated environment control/thermal management system concepts for hypersonic vehicle [J]. Engineering Science, 2007, 9(2): 44-48.
28	Jiang Q, Zhou W, Wen B, et al. Thermodynamic analysis and parametric study of a closed Brayton cycle thermal management system for scramjet [J]. International Journal of Hydrogen Energy, 2010, 35(1): 356-364.
29	Kumar S, Mahulikar S P. Design of thermal protection system for reusable hypersonic vehicle using inverse approach [J]. Journal of Spacecraft & Rockets, 2017, 54(2): 1-11.
30	Dittus F W, Boelter L M K. Heat transfer in automobile radiators of the tubular type [J]. University of California Publications in English, Berkeley, 1930, 2: 443-461.

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热管理子系统	载热介质	入口压力/ MPa	入口温度/ K	入口流量/ （kg·s^-1）	热载荷/ kW	煤油换热器	水力直径/ m	压力降/ MPa	流程数
浸液冷却	甲醇	0.1	323	0.246	10	冷边	0.03	0.01	1
浸液冷却	甲醇	0.1	323	0.246	10	热边	0.04	0.005	2
喷雾冷却	FC-72	0.1	313	0.422	8	冷边	0.03	0.01	1
喷雾冷却	FC-72	0.1	313	0.422	8	热边	0.04	0.005	2
座舱	空气	0.1	310	0.498	5	冷边	0.03	0.01	1
座舱	空气	0.1	310	0.498	5	热边	0.04	0.005	2
设备舱	无载热介质，壁温上限340 K				6	冷边	0.02	0.01	1
齿轮箱	PAO	0.1	318	0.251	8.5	冷边	0.03	0.01	1
齿轮箱	PAO	0.1	318	0.251	8.5	热边	0.02	0.005	2
液压设备	液压油	0.1	320	0.245	13	冷边	0.03	0.01	1
液压设备	液压油	0.1	320	0.245	13	热边	0.02	0.005	2
发动机	无载热介质，壁温上限850 K				200	冷边	0.1	0.01	1

热管理子系统		载热介质			冷却介质			换热面积/ m²	换热效率
热管理子系统		压力/MPa	温度/K	流量/（kg·s^-1）	压力/MPa	温度/K	流量/（kg·s^-1）	换热面积/ m²	换热效率
燃料罐	出口	无载热介质			5.0	300	0.6	无	无
浸液冷却	进口	0.1	323	0.246	5.0	300	0.1	0.4329	0.766
浸液冷却	出口	0.1	338	0.246	4.99	329.1	0.1	0.4329	0.766
喷雾冷却	进口	0.1	313	0.422	5.0	300	0.1	0.7276	0.759
喷雾冷却	出口	0.1	331	0.422	4.99	323.5	0.1	0.7276	0.759
座舱	进口	0.1	310	0.498	5.0	300	0.1	0.3319	0.747
座舱	出口	0.1	320	0.498	4.99	314.9	0.1	0.3319	0.747
设备舱	进口	无载热介质			5.0	300	0.1	0.0671	无
设备舱	出口	无载热介质			4.99	317.8	0.1	0.0671	无
齿轮箱	进口	0.1	318	0.251	5.0	300	0.1	0.5396	0.756
齿轮箱	出口	0.1	333	0.251	4.99	324.9	0.1	0.5396	0.756
液压设备	进口	0.1	320	0.245	5.0	300	0.1	0.7970	0.776
液压设备	出口	0.1	348	0.245	4.99	337.4	0.1	0.7970	0.776
发动机	进口	无载热介质			4.99	324.6	0.6	0.0945	无
发动机	出口	无载热介质			4.98	408.7	0.6	0.0945	无

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飞行器燃料再生冷却热管理系统参数设计

Parameter design of aircraft fuel regeneration cooling thermal management system

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