机动行为下飞机油箱晃动流固耦合动力学分析

doi:10.7527/S1000-6893.2018.22471

固体力学与飞行器总体设计

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机动行为下飞机油箱晃动流固耦合动力学分析

杨尚霖¹, 陈晓峰², 杜发喜², 雷忠琦¹, 姚小虎¹

1. 华南理工大学土木与交通学院, 广州 510640;
2. 成都飞机工业(集团)有限责任公司技术中心, 成都 610092

收稿日期:2018-06-25 修回日期:2018-08-09 出版日期:2019-03-15 发布日期:2018-11-14
通讯作者: 姚小虎 E-mail:yaoxh@scut.edu.cn
基金资助:
国家自然科学基金（11372113，11472110，11672110）

Dynamic analysis of fluid-structure interaction on aircraft fuel tank sloshing during maneuver

YANG Shanglin¹, CHEN Xiaofeng², DU Faxi², LEI Zhongqi¹, YAO Xiaohu¹

1. School of Civil Engineering and Transportation, South China University of Technology, Guangzhou 510640, China;
2. Technology Center, Chengdu Aircraft Industrial (Group) Co., Ltd., Chengdu 610092, China

Received:2018-06-25 Revised:2018-08-09 Online:2019-03-15 Published:2018-11-14
Supported by:
National Natural Science Foundation of China (11372113,11472110,11672110)

摘要/Abstract

摘要： 飞机执行机动飞行时整体处于大过载状态，此时的油箱晃动流固耦合问题较为复杂。针对这一问题，以某型飞机整体油箱为研究对象，建立ABAQUS与Star-CCM+联合仿真流固耦合方法，对飞机半滚倒转机动行为下的油箱晃动流固耦合效应进行分析，得到了半滚倒转过程中燃油的形态变化，流体域压力以及油箱部件的应力时程曲线等结果，并探究了油箱充液率变化对流固耦合效应的影响。结果表明：机动过载对油箱部件应力应变的影响大于燃油晃动冲击，除上蒙皮外部件应力均随着充液率增加而增加。

关键词: 机动行为, 油箱晃动, 流固耦合, 半滚倒转, 过载

Abstract: When the aircraft performs the maneuver flight, the whole structure is in a large overload condition, and the problem of the fluid-structure interaction of the fuel tank sloshing is complicated. Based on a certain type of aircraft fuel tank, a fluid-structure interaction simulation method is proposed with ABAQUS and Star-CCM+ software. By investigating the fluid-structure interaction effect of the fuel tank sloshing during the Split-S maneuver, the morphological change of fuel, the pressure of the fluid filed and the time-history curves of the stress of tank components are obtained. The influence of the filling rate changes on tank sloshing is analyzed. The results indicate that the influence of the overload on the stress and strain of tank components is greater than that of the liquid sloshing, and the stress of all components increase with the increase of filling rate except the upper skin.

Key words: maneuver, fuel tank sloshing, fluid-structure interaction, Split-S, overload

中图分类号:

V222

杨尚霖, 陈晓峰, 杜发喜, 雷忠琦, 姚小虎. 机动行为下飞机油箱晃动流固耦合动力学分析[J]. 航空学报, 2019, 40(3): 222471-222471.

YANG Shanglin, CHEN Xiaofeng, DU Faxi, LEI Zhongqi, YAO Xiaohu. Dynamic analysis of fluid-structure interaction on aircraft fuel tank sloshing during maneuver[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(3): 222471-222471.

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E-mail：hkxb@buaa.edu.cn

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机动行为下飞机油箱晃动流固耦合动力学分析

Dynamic analysis of fluid-structure interaction on aircraft fuel tank sloshing during maneuver

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