舰载飞机着舰时拦阻钩碰撞反弹动力学分析

doi:10.7527/S1000-6893.2017.221233

固体力学与飞行器总体设计

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舰载飞机着舰时拦阻钩碰撞反弹动力学分析

彭一明, 聂宏

南京航空航天大学机械结构力学及控制国家重点实验室, 南京 210016

收稿日期:2017-03-13 修回日期:2017-05-22 出版日期:2017-11-15 发布日期:2017-05-21
通讯作者: 聂宏 E-mail:hnie@nuaa.edu.cn
基金资助:
国家自然科学基金（11372129）；江苏高校优势学科建设工程资助项目

Dynamics analysis of arresting hook bounce after touchdown and impacting with deck

PENG Yiming, NIE Hong

State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received:2017-03-13 Revised:2017-05-22 Online:2017-11-15 Published:2017-05-21
Supported by:
National Natural Science Foundation of China (11372129); Project Funded by the Priority Academic Program Development of Jiangsu Higher Education Institutions

摘要/Abstract

摘要：

为了解舰载飞机着舰时拦阻钩碰撞甲板后被反弹的动力学性能，以某舰载飞机为研究对象，建立了全机着舰动力学模型和拦阻钩碰撞甲板的碰撞模型，进行了全机着舰动力学仿真，通过拦阻钩碰撞反弹试验对碰撞模型进行修正，得到了更加准确的碰撞模型。将仿真结果与试验结果进行对比，验证了模型的准确性。研究了甲板涂层、俯仰角、航向速度、下沉速度和拦阻钩阻尼器参数对拦阻钩反弹动力学性能的影响。结果表明：航向速度对反弹高度和碰撞力几乎没有影响；随着下沉速度和俯仰角的增加，反弹高度和碰撞力也增加；拦阻钩阻尼器参数的变化不会影响碰撞力，但是对反弹动力学性能会产生明显的影响。

关键词: 舰载飞机, 拦阻钩, 碰撞, 动力学, 阻尼器

Abstract:

In order to research the dynamic performance of the arresting hook after touchdown and impacting with the deck when the aircraft is arrested, a full-aircraft assembly model of a certain type of aircraft is developed to conduct dynamics simulation of the landing of the aircraft carrier. The model is updated with the data of arresting hook bounce test, and a more accurate model is obtained. The simulation results are compared with the test results, and the accuracy of the dynamics model is verified. The impact of the deck coating, pitch angle, engaging velocity, sinking velocity and parameters of the arresting hook damper on the dynamics performance of arresting hook bounce is studied. The results show that the engaging velocity has little effect on bounce height and impact force. The bounce height and impact force get larger with the increase of the sinking velocity and pitch angle. The parameters of hook damper almost have no effect on the impact force, but obvious effect on the bounce height.

Key words: carrier aircraft, arresting hook, impact, dynamics, damper

中图分类号:

V226

彭一明, 聂宏. 舰载飞机着舰时拦阻钩碰撞反弹动力学分析[J]. 航空学报, 2017, 38(11): 221233-221233.

PENG Yiming, NIE Hong. Dynamics analysis of arresting hook bounce after touchdown and impacting with deck[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(11): 221233-221233.

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E-mail：hkxb@buaa.edu.cn

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舰载飞机着舰时拦阻钩碰撞反弹动力学分析

Dynamics analysis of arresting hook bounce after touchdown and impacting with deck

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