南京航空航天大学学报2024，Vol.56Issue(2)：197-207,11.DOI:10.16356/j.1005-2615.2024.02.001
直升机尾传动轴抗弹击损伤研究综述
Research on Ballistic Damage and Anti-ballistic Design of Helicopter Tail Drive Shaft:An Overview
摘要
Abstract
Helicopter tail drive shaft is susceptible to ballistic damage in military applications,significantly compromising the safety of helicopter flight.Consequently,extensive research on ballistic damage and anti-ballistic design of helicopter tail drive shaft has been conducted both domestically and internationally.Firstly,the military significance of researching the ballistic damage and anti-ballistic design of helicopter tail drive shaft is elaborated.Secondly,the current research status and development trends of ballistic damage and anti-ballistic design of helicopter tail drive shaft at home and abroad are detailed from four aspects:evaluation criteria,research methods,influencing factors,and methods for improving anti-ballistic performance of the tail drive shaft.Finally,the shortcomings of domestic research in this area are discussed,and the research directions that urgently need to be carried out in the future are prospected from the views of material property testing,new numerical simulation methods,research on damage by fragment penetration and numerical simulation of ballistic damage of composite tail drive shaft.关键词
直升机尾传动轴/弹击损伤/数值模拟/抗弹击设计/复合材料尾传动轴Key words
helicopter tail drive shaft/ballistic damage/numerical simulation/anti-ballistic design/composite tail drive shaft分类
航空航天引用本文复制引用
王旦,未雷,李鹏,徐鹏行,王希,李坚,朱如鹏..直升机尾传动轴抗弹击损伤研究综述[J].南京航空航天大学学报,2024,56(2):197-207,11.基金项目
国家自然科学基金(52005253) （52005253）
直升机传动技术国家级重点实验室开放基金(HTL-A-21G07,HTL-A-22K01). （HTL-A-21G07,HTL-A-22K01）
