基于流-固热耦合的受热航空发动机管路安全性分析

苏杨; 杨岳朋; 王方; 金捷; 文放

doi:10.13224/j.cnki.jasp.20240552

基于流-固热耦合的受热航空发动机管路安全性分析

doi: 10.13224/j.cnki.jasp.20240552

苏杨^1,,
杨岳朋¹,
王方^{1, 2, 3},
金捷^{1, 2, 3,*, ,},
文放^{1, 4}

1.
北京航空航天大学能源与动力工程学院，北京 100191
2.
北京航空航天大学江西研究院，南昌 330096
3.
北京航空航天大学成都航空动力创新研究院，成都 611930
4.
中国航空工业集团有限公司中国航空综合技术研究所，北京 100028

基金项目: 国家自然科学基金（20232ACB204026，12172345，92041001）

详细信息

作者简介:
苏杨（2001-），男，硕士生，主要研究方向为航空发动机通油管路流热耦合

通讯作者:
金捷（1968-），男，研究员、硕士生导师，博士，研究方向为两相湍流燃烧理论及其应用。E-mail：jinjie@buaa.edu.cn

中图分类号: V232
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- 被引次数: 0
出版历程
- 收稿日期: 2024-08-07
- 网络出版日期: 2026-07-29

Research on safety of aero-engine oil tube under heating condition based on fluid-solid-thermal coupling

Su Yang^1
,,
Yang Yuepeng¹,
Wang Fang^{1, 2, 3},
Jin Jie^{1, 2, 3,*
, ,},
Wen Fang^{1, 4}

1.
School of Energy and Power Enginering，Beihang University，Beijing 100191，China
2.
Jiangxi Research Institute，Beihang University，Nanchang 330096，China
3.
Chengdu Innovation Research Institute on Aircraft Power，Beihang University，Chengdu 611930，China
4.
China Aero-Polytechnology Establishment，Aviation Industry Corporation of China，Limited，Beijing 100028，China

摘要

摘要:
基于标准文件和流-固热耦合方法，对航空发动机通油管路处于防火试验标准规定的加热条件下的安全性进行了分析。通油管采用28 MPa挤压式无扩口组合导管，管内工质为RP-3航空煤油，选择高温标准烟气模拟加热导管的燃气。为模拟管路在不同操作条件或油泵故障的情况，设置了不同煤油进口流量进行计算。结果表明：在承受标准加热条件时，管壁温度分布不均，而随着煤油流量的降低，管壁的温度上升，出现传热恶化现象。温度升高会降低材料的强度，而温度不均匀分布则会产生热应力，增加导管工作的安全隐患。当煤油流量减小到一定大小时，管壁的等效应力将超过材料的屈服强度，管路存在较高的破裂的风险。
- 航空发动机通油管路 /
- 标准文件 /
- 航空煤油 /
- 流-固热耦合 /
- 管路安全性
Abstract:
The safety of the aviation engine oil tube under the heating conditions specified in fire test standards was analyzed based on standard documents and fluid-solid-thermal coupling method. Tube assembles for flareless connection, swaged type, 28 MPa, were used, the working fluid in the pipe was RP-3 aviation kerosene, and the high temperature standard flue gas was selected to simulate the gas for heating the tube. In order to simulate the situation of tube under different working conditions or pump failure, different kerosene inlet flow rates were set up for calculation. The results showed that the temperature distribution of the tube wall was uneven under standard heating conditions. With the decrease of kerosene flow rate, the temperature of the tube wall increased and the heat transfer deterioration occurred. The increase of tube wall temperature could reduce the strength of the material, and the uneven distribution of tube wall temperature could produce thermal stress, which may increase the safety hazard of the tube. When the kerosene flow rate was reduced to a certain amount, the equivalent stress of the tube wall could exceed the yield strength of the material, and the tube was prone to fracture.
- aero-engine oil tube /
- standard document /
- aviation kerosene /
- fluid-solid-thermal coupling /
- tube safety

HTML

图 1 28 MPa下RP-3航空煤油热物性参数

Figure 1. Thermophysical properties of RP-3 kerosene at 28 MPa

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图 2 计算域几何模型

Figure 2. Geometric model of computational domain

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图 3 数值方法检验

Figure 3. Validation of the computational method

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图 4 4种网格方案下外壁面最高壁温

Figure 4. Maximum wall temperature of the outer wall under four grids

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图 5 5.07 L/min流量下导管周向平均外壁温轴向分布

Figure 5. Axial distribution of circumferentially averaged outer wall temperature of the tube at a flow rate of 5.07 L/min

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图 6 5.07 L/min流量下导管轴向平均外壁温周向分布（X=330～400 mm）

Figure 6. Circumferential distribution of axially averaged outer wall temperature of the tube at a flow rate of 5.07 L/min （X=330—400 mm）

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图 7 不同煤油流量下导管外壁最高温度与煤油出口温度

Figure 7. Maximum temperature of the outer wall of the tube and the outlet temperature of kerosene under different kerosene flow rates

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图 8 不同煤油进口体积流量下管内沿程表面传热系数

Figure 8. Convective heat transfer coefficient along the pipe under different kerosene inlet volume flow

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图 9 5.07 L/min工况下管壁等效应力分布

Figure 9. Equivalent stress distribution of the tube wall under the working condition of 5.07 L/min

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图 10 3.80 L/min工况下管壁等效应力分布

Figure 10. Equivalent stress distribution of the tube wall under the working condition of 3.80 L/min

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图 11 0.5 L/min工况下管壁等效应力分布

Figure 11. Equivalent stress distribution of the tube wall under the working condition of 0.5 L/min

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图 12 5.07 L/min工况下管壁等效应力、温度及对应温度下屈服强度分布

Figure 12. Equivalent stress, temperature and yield strength distribution of the pipe wall at the corresponding temperature under the condition of 5.07 L/min

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图 13 3.80 L/min工况下管壁等效应力、温度及对应温度下屈服强度分布

Figure 13. Equivalent stress, temperature and yield strength distribution of the pipe wall at the corresponding temperature under the condition of 3.80 L/min

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图 14 0.5 L/min工况下管壁等效应力、温度及对应温度下屈服强度分布

Figure 14. Equivalent stress, temperature and yield strength distribution of the pipe wall at the corresponding temperature under the condition of 0.5 L/min

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表 1 煤油进口工况

Table 1. Kerosene inlet conditions

工况编号	进口煤油压力/MPa	进口煤油温度/K	进口煤油体积流量/（L/min）
1	28	366.15	5.07
2	28	366.15	3.80
3	28	366.15	2.54
4	28	366.15	1.27
5	28	366.15	0.50
6	28	366.15	0.25

下载: 导出CSV

参考文献(26)

[1]	何江, 孙有朝, 王丰产. 运输类飞机动力装置防火适航要求分析[C]//2010年航空器适航与空中交通管理学术年会论文集. 北京: 南京航空航天大学民航学院, 2010: 186-190. He Jiang, Sun Youchao, Wang Fengchan. Analysis of fire protection airworthiness requirements for powerplant on transport category aircraft [C]//Proceedings of the 2010 Annual Conference on Aircraft Airworthiness and Air Traffic Management. Beijing: College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, 2010: 186-190. (in Chinese He Jiang, Sun Youchao, Wang Fengchan. Analysis of fire protection airworthiness requirements for powerplant on transport category aircraft [C]//Proceedings of the 2010 Annual Conference on Aircraft Airworthiness and Air Traffic Management. Beijing: College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, 2010: 186-190. (in Chinese)
[2]	CCAR-33-R2 航空发动机适航规定[S].
[3]	王向辉. 某航空发动机滑油管路适航防火试验故障原因分析[J]. 航空维修与工程, 2022(9): 92-96. Wang Xianghui. Cause analysis on airworthiness fireproof test failure of an aero-engine lubricating oil pipeline[J]. Aviation Maintenance & Engineering, 2022(9): 92-96. (in Chinese doi: 10.3969/j.issn.1672-0989.2022.09.027 Wang Xianghui. Cause analysis on airworthiness fireproof test failure of an aero-engine lubricating oil pipeline[J]. Aviation Maintenance & Engineering, 2022(9): 92-96. (in Chinese) doi: 10.3969/j.issn.1672-0989.2022.09.027
[4]	王伟, 吕凯, 叶子多. 航空发动机防火试验的对流和辐射传热计算[C] //中国航空学会飞机防火系统专业委员会第二届飞机防火系统学术研讨会论文集. 合肥: 中国科学技术大学出版社, 2015: 75-78. Wang Wei, Lv Kai, Ye Ziduo. Convective and radiative heat transfer calculation for aeroengine fire test[C]//Proceedings of the 2nd Symposium on Aircraft Fire Protection System, Aircraft Fire Protection System Committee of Chinese Society of Aeronautics and Astronautics. Hefei: University of Science and Technology of China Press, 2015: 75-78. (in Chinese Wang Wei, Lv Kai, Ye Ziduo. Convective and radiative heat transfer calculation for aeroengine fire test[C]//Proceedings of the 2nd Symposium on Aircraft Fire Protection System, Aircraft Fire Protection System Committee of Chinese Society of Aeronautics and Astronautics. Hefei: University of Science and Technology of China Press, 2015: 75-78. (in Chinese)
[5]	Robert I O. Development of a Nex-Generation burner for use in testing thermal acoistic insulation burn through resistance[R]. DOT/FAA/AR-TN09/23, 2009.
[6]	Kao Yihuan. Experimental investigation of NexGen and gas burner for FAA fire test[D]. Cincinnati, US: University of Cincinnati, 2012.
[7]	刘帅. 航空发动机防火试验的热流分布仿真研究[D]. 天津: 中国民航大学, 2016. Liu Shuai. Simulation research on heat flux distribution of aero-engine fire protection test[D]. Tianjin: Civil Aviation University of China, 2016. (in Chinese Liu Shuai. Simulation research on heat flux distribution of aero-engine fire protection test[D]. Tianjin: Civil Aviation University of China, 2016. (in Chinese)
[8]	夏越美. 飞机软管、硬管组件防火试验方法标准[J]. 航空标准化与质量, 1995(2): 6-10. Xia Yuemei. Standard for fire test method of aircraft hose and rigid pipe components[J]. Aeronautic Standardization & Quality, 1995(2): 6-10. (in Chinese Xia Yuemei. Standard for fire test method of aircraft hose and rigid pipe components[J]. Aeronautic Standardization & Quality, 1995(2): 6-10. (in Chinese)
[9]	丁芳, 李松阳, 崔振涛, 等. 燃油管路的防火仿真分析方法: CN 114528722 A[P]. 2022-05-24.
[10]	HB 7044-2014 民用飞机软管和管组件防火试验要求[S].
[11]	HB 7842-2008 28 MPa挤压式无扩口组合导管[S].
[12]	HB 6058-2008 挤压式无扩口管套[S].
[13]	HB 7872-2008 28 MPa无扩口外套螺母[S].
[14]	HB 5970-2008 24°无扩口外螺纹接头端头尺寸[S].
[15]	王世伦, 王峙南, 朱之琹. 中国航空材料手册[M]. 北京: 中国标准出版社, 1988.
[16]	Zhong Fengquan, Fan Xuejun, Yu Gong, et al. Heat transfer of aviation kerosene at supercritiacl conditions[R]. AIAA-4615, 2009.
[17]	孙青梅, 米镇涛, 张香文. 吸热型碳氢燃料RP-3仿JP-7临界性质(t_e, p_e)的测定[J]. 燃料化学学报, 2006(4): 466-470. Sun Qingmei, Mi Zhentao, Zhang Xiangwen. Determination of critical properties (t_e, p_e) of endothermic hydrocarbon fuels: RP-3 and simulated JP-7[J]. Journal of Fuel Chemistry and Technology, 2006(4): 466-470. (in Chinese Sun Qingmei, Mi Zhentao, Zhang Xiangwen. Determination of critical properties (t_e, p_e) of endothermic hydrocarbon fuels: RP-3 and simulated JP-7[J]. Journal of Fuel Chemistry and Technology, 2006(4): 466-470. (in Chinese)
[18]	Pu Hang, Chang Haotian, Wang Jinzhao, et al. Experimental investigation and analysis of convective heat transfer to supercritical pressure aviation kerosene RP-3 in vertical miniature tubes based on the pseudo-boiling theory[J]. Applied Thermal Engineering, 2023, 219: 119651. doi: 10.1016/j.applthermaleng.2022.119651
[19]	Fu Yanchen, Huang Haoran, Wen Jie, et al. Experimental investigation on convective heat transfer of supercritical RP-3 in vertical miniature tubes with various diameters[J]. International Journal of Heat and Mass Transfer, 2017, 112: 814-824. doi: 10.1016/j.ijheatmasstransfer.2017.05.008
[20]	Dang Guoxin, Zhong Fengquan, Zhang Yongjiang, et al. Numerical study of heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube[J]. International Journal of Heat and Mass Transfer, 2015, 85: 1003-1011. doi: 10.1016/j.ijheatmasstransfer.2015.02.052
[21]	张永江. 超临界压力下航空煤油流动与传热特性研究[D]. 北京: 中国科学院大学, 2017. Zhang Yongjiang. Study on flow and heat transfer characteristics of aviation kerosene under supercritical pressure[D]. Beijing: University of Chinese Academy of Sciences, 2017. (in Chinese Zhang Yongjiang. Study on flow and heat transfer characteristics of aviation kerosene under supercritical pressure[D]. Beijing: University of Chinese Academy of Sciences, 2017. (in Chinese)
[22]	Yu Jiajia, Huang Li, Sun Shouli, et al. Flow and heat transfer of RP-3 aviation kerosene in horizontal tube at supercritical pressure under altered gravity levels[J]. Applied Thermal Engineering, 2022, 207: 118162. doi: 10.1016/j.applthermaleng.2022.118162
[23]	浦航. 细通道内超临界压力RP-3对流传热特性与机理研究[D]. 大连: 大连理工大学, 2020. Pu Hang. Characteristics and mechanism of convective heat transfer to supercritical pressure RP-3 in mini-channels[D]. Dalian: Dalian University of Technology, 2020. (in Chinese Pu Hang. Characteristics and mechanism of convective heat transfer to supercritical pressure RP-3 in mini-channels[D]. Dalian: Dalian University of Technology, 2020. (in Chinese)
[24]	李勋锋, 仲峰泉, 范学军, 等. 超临界压力下航空煤油水平管内对流换热特性数值研究[J]. 航空动力学报, 2010, 25(8): 1690-1697. Li Xunfeng, Zhong Fengquan, Fan Xuejun, et al. Numerical study of convective heat transfer characteristics of kerosene flowing in a horizontal pipe at supercritical pressure[J]. Journal of Aerospace Power, 2010, 25(8): 1690-1697. (in Chinese doi: 10.13224/j.cnki.jasp.2010.08.028 Li Xunfeng, Zhong Fengquan, Fan Xuejun, et al. Numerical study of convective heat transfer characteristics of kerosene flowing in a horizontal pipe at supercritical pressure[J]. Journal of Aerospace Power, 2010, 25(8): 1690-1697. (in Chinese) doi: 10.13224/j.cnki.jasp.2010.08.028
[25]	赵国柱, 宋文艳, 张若凌. 超临界压力下RP-3航空煤油吸热裂解反应的数值研究[J]. 航空学报, 2014, 35(6): 1513-1521. Zhao Guozhu, Song Wenyan, Zhang Ruoling. Numerical study on thermal cracking of RP-3 aviation kerosene under supercritical pressure[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(6): 1513-1521. (in Chinese doi: 10.7527/S1000-6893.2013.0547 Zhao Guozhu, Song Wenyan, Zhang Ruoling. Numerical study on thermal cracking of RP-3 aviation kerosene under supercritical pressure[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(6): 1513-1521. (in Chinese) doi: 10.7527/S1000-6893.2013.0547
[26]	Fan Xuejun, Yu Gong, Li Jianguo, et al. Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance[J]. Combustion Science and Technology, 2007, 179(10): 2199-2217. doi: 10.1080/00102200701386198