Parameter design of aircraft fuel regeneration cooling thermal management system

doi:10.11949/0438-1157.20191223

Abstract

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

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

CLC Number:

TK 124

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.

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.

Figures/Tables 5

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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	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

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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