航空工程进展2026，Vol.17Issue(3)：60-71,12.DOI:10.16615/j.cnki.1674-8190.2026.03.06
空中加油机给油插头撞击受油机结构数值仿真研究
Numerical simulation of receiver aircraft components impacted by oil joint of tanker aircraft
陈斐颖 1余立 2陈池 3刘立豪 1张锦航 1王江阳 1刘军1
作者信息
- 1. 西北工业大学 航空学院,西安 710072
- 2. 陕西飞机工业有限责任公司 飞机设计研究院,汉中 723213
- 3. 中航(成都)无人机系统股份有限公司 研发中心,成都 611743
- 折叠
摘要
Abstract
In the process of air refueling,the oil joint of the tanker aircraft may break away from the air refueling hose and collide with the receiver aircraft,which can lead to significant damage to the receiver aircraft components and endanger the safety.In order to ensure the anti-impact ability of the receiver aircraft components,the dynamic simulation of the collision process between different parts of the receiver aircraft and the oil joint is carried out by using a transient nonlinear impact analysis,and the effects of different impact attitudes and different impact veloci-ties of the oil joint on the impact damage of the receiver aircraft components are studied.The results show that the vertical impact of the oil joint head is more destructive than that of the oil joint tail.When the oil joint head impacts the windshield or the upper wall panel vertically,the center of the leading edge is the weakest location for the verti-cal impact.It is also found that the stiffness matching between the structural components should be considered in the anti-impact design of the receiver aircraft.关键词
软管—锥管式空中加油/给油插头/受油机/撞击/损伤Key words
hose and drogue aerial refueling/oil joint/receiver aircraft/impact/damage分类
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陈斐颖,余立,陈池,刘立豪,张锦航,王江阳,刘军..空中加油机给油插头撞击受油机结构数值仿真研究[J].航空工程进展,2026,17(3):60-71,12.
