舰载飞机起降装置动力学试验研究进展  

Research Progress on Dynamic Test of Carrier Aircraft Take-off and Landing Device

作　　者：胡锐 刘小川[1] 白春玉[1] 杨正权[1] 陈熠 Hu Rui;Liu Xiaochuan;Bai Chunyu;Yang Zhengquan;Chen Yi(Aviation Key Laboratory of Science and Technology on Structure Impact Dynamics,Aircraft Strength Research Institute of China,Xi’an 710065,China)

机构地区：[1]中国飞机强度研究所结构冲击动力学航空科技重点实验室,陕西西安710065

出　　处：《航空科学技术》2022年第1期10-19,共10页Aeronautical Science & Technology

摘　　要：舰载飞机起降阶段通常被认为是事故率最高的阶段,其特殊的起降环境导致舰载机起飞和拦阻着舰的过程相较于陆基飞机更加复杂,所涉及的动力学问题一直是国内外相关研究人员的研究热点。从舰载机起落架和拦阻钩等起降装置着手,重点对舰载机起落架动力学试验、拦阻钩动力学试验以及全机落震试验进行了综述,详细地论述了舰载飞机起降过程涉及到的关键动力学试验问题及其研究现状。最后,对舰载飞机起降装置动力学试验研究的发展进行了总结和展望。The take-off and landing stage of carrier-based aircraft is generally considered to be the stage with the highest accident rate.Its special take-off and landing environment leads to more complex than land-based aircraft,and the dynamic issues involved have always been the research hotspots of domestic and foreign researchers.This paper starts with landing gear and arresting hooks of carrier aircraft,then summarizes dynamic test of landing gear,dynamic test of arresting hook and full-scale aircraft drop tests,discusses in more detail the key dynamic test problems involved in the take-off and landing progress of carrier aircraft and their research status.Finally,the development of dynamic test research of carrier aircraft take-off and landing device is summarized and prospected.

关 键 词：起降装置 起落架 拦阻钩 舰载飞机 动力学试验 

分 类 号：V226[航空宇航科学与技术—飞行器设计]