基于MATLAB/Simulink的飞机燃油箱内燃油温度仿真计算

推进技术 ›› 2014, Vol. 35 ›› Issue (1): 62-69.

基于MATLAB/Simulink的飞机燃油箱内燃油温度仿真计算

康振烨,刘振侠,任国哲,吕亚国

西北工业大学动力与能源学院,陕西西安 710072;西北工业大学动力与能源学院,陕西西安 710072;西北工业大学动力与能源学院,陕西西安 710072;西北工业大学动力与能源学院,陕西西安 710072

发布日期:2021-08-15
作者简介:康振烨(1988—),男,硕士生,研究领域为航空燃油系统,航空发动机滑油系统。 E-mail:kangzhenye@foxmail.com

Simulation and Calculation of Fuel Temperature in Aircraft Fuel Tank Based on MATLAB/Simulink

College of Power and Energy, Northwestern Polytechnical University, Xi’an 710072, China;College of Power and Energy, Northwestern Polytechnical University, Xi’an 710072, China;College of Power and Energy, Northwestern Polytechnical University, Xi’an 710072, China;College of Power and Energy, Northwestern Polytechnical University, Xi’an 710072, China

Published:2021-08-15

摘要/Abstract

摘要： 燃油温度是飞机燃油箱可燃性评估的关键参数之一。为了研究飞机燃油箱内温度的分布规律及传热模型的正确性,采用MATLAB/Simulink软件平台搭建出了客机的燃油箱热仿真模型。在输入飞行实验所对应的的边界条件后,通过数值模拟获得燃油箱内部各计算节点处的燃油温度。结果表明,在三种不同的航行条件下,燃油箱热模型仿真结果均能较好地与飞行实验结果吻合,能够将计算误差控制在一定范围内。采用该燃油箱热模型进行热仿真数值模拟可以获得较为准确的飞机燃油箱热特性,能够在飞机设计阶段,用于对燃油箱结构以及内热源部件布置的优化。 

关键词: 飞机;燃油箱;热模型;数值模拟;燃油温度 

Abstract: The fuel temperature is one of the key parameters of the aircraft fuel tank flammability assessment. In order to study the temperature distribution of the aircraft fuel tank and the correctness of the heat transfer model, the MATLAB/Simulink software platform was used to build an aircraft fuel tank thermal simulation model. Entering boundary conditions corresponding to flight experiments, the fuel temperature inside the fuel tank at the compute nodes can be obtained through numerical simulation. The results show that under three different sailing conditions, the simulation results of fuel tank thermal model could preferably coincide with the flight test results and calculation error can be controlled within a certain range.Using this fuel tank thermal model in thermal numerical simulation, aircraft fuel tank thermal characteristics can be obtained accurately, and it can be used for optimization of the fuel tank structure and internal heat source component arrangement in the stage of aircraft design. 

Key words: Aircraft; Fuel tank; Thermal model; Numerical simulation; Fuel temperature

康振烨,刘振侠,任国哲,吕亚国. 基于MATLAB/Simulink的飞机燃油箱内燃油温度仿真计算[J]. 推进技术, 2014, 35(1): 62-69.

KANG Zhen-ye, LIU Zhen-xia, REN Guo-zhe, LV Ya-guo. Simulation and Calculation of Fuel Temperature in Aircraft Fuel Tank Based on MATLAB/Simulink[J]. Journal of Propulsion Technology, 2014, 35(1): 62-69.

参考文献

[1] CCAR-25-R4-2001,运输类飞机适航标准[S].
[2] AC-25.981-2A-2008,Federal Aviation Administration.Fuel Tank Flammability Reduction Means [S].
[3] Cavage William M, Bowman Timothy.Modeling in Flight Inert Gas Distribution in a 747Center Wing Fuel Tank[R].AIAA 2005-4906.
[4] Jensen D L.Analysis of a Boeing 747Aircraft Fuel Tank Vent System[J].Journal of Aircraft 2001,8(5):828-834.
[5] 李彦江,冯震宙,刘永寿.飞机燃油系统仿真分析研究[J].西安工业大学学报,2008,8(04):401-405.
[6] 李彦江,刘永寿,姜志峰,等.飞机燃油系统功能仿真分析 [J].航空计算技术,2009,9(4).
[7] 刘小芳,刘卫华.飞机供氧和燃油箱惰化技术概况[J].华北航天工业学院学报,2008,8(3):4-7.
[8] 徐志英,庄达民.飞机燃油系统热管理研究[J].航空动力学报,2007,2(11):1833-1837.
[9] 张兴娟,张作琪,高峰.先进战斗机超声速巡航过程中的燃油温度变化特性分析[J].航空动力学报,2010,25(2):258-263.
[10] 肖再华.飞机燃油箱惰化[J].航空科学技术,2005(1):31-32.
[11] (美)Langton R.飞机燃油系统[M].颜万亿译,上海:上海交通大学出版社,2010.
[12] 韩捷初.某型号燃油调节系统[J].推进技术,1998,9(2):23-26.(HAN Jie-chu.Fuel Regulation System of a Ramjet Engine[J].Journal of Propulsion Technology, 1998,9(02):23-26.)
[13] 吕亚国.飞机燃油系统计算研究[D].西安:西北工业大学,2006.
[14] 吕亚国,刘振侠,黄生勤,等.加油控制失效时飞机通气系统性能计算[J].航空计算技术,2008,8(1):26-28.
[15] 杨华保.旅客机燃油质量分布特性计算方法研究[J].航空计算技术,1999,29(2):19-22.
[16] 袁梅,林柯,崔德刚.飞机燃油油量测量及姿态误差修正方法[J].航空计测技术,2001,1(1):24-26.
[17] 康芹,李世武,郭建利.热网络法概论[J].工业加热,2006,5(5):15-18.
[18] (美)卡里卡B V,(美)戴斯蒙德R M.工程传热学[M].刘吉萱主译,北京:人民教育出版社,1981.
[19] 杨世铭,陶文铨.传热学[M].北京:高等教育出版社,1998.