[1]朱齐丹,李新飞,喻勇涛.考虑载荷突卸的舰载机弹射起飞动力学分析[J].哈尔滨工程大学学报,2012,(09):1150-1157.[doi:10.3969/j.issn.1006-7043. 201111078]
 ZHU Qidan,LI Xinfei,YU Yongtao.Analysis of dynamic characteristics of catapult launch for a carrier-based aircraft with sudden load discharge[J].hebgcdxxb,2012,(09):1150-1157.[doi:10.3969/j.issn.1006-7043. 201111078]
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考虑载荷突卸的舰载机弹射起飞动力学分析(/HTML)
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《哈尔滨工程大学学报》[ISSN:1006-6977/CN:61-1281/TN]

卷:
期数:
2012年09期
页码:
1150-1157
栏目:
出版日期:
2012-09-25

文章信息/Info

Title:
Analysis of dynamic characteristics of catapult launch for a carrier-based aircraft with sudden load discharge
文章编号:
1006-7043(2012)09-1150-08
作者:
朱齐丹 李新飞 喻勇涛
1.哈尔滨工程大学 自动化学院,黑龙江 哈尔滨 150001; 2.哈尔滨工程大学 船舶工程学院,黑龙江 哈尔滨 150001
Author(s):
ZHU Qidan LI Xinfei YU Yongtao
1. College of Automation, Harbin Engineering University, Harbin 150001, China; 2.College of Shipbuilding Engineering, Harbin Engineering University, Harbin 150001, China
关键词:
弹射起飞舰载机前起落架载荷突卸突伸
分类号:
V226
DOI:
10.3969/j.issn.1006-7043. 201111078
文献标志码:
A
摘要:
为了分析舰载机弹射起飞过程中的动力学特点,建立了一种考虑前起落架载荷突卸的弹射起飞动力学模型.研究了在弹射开始时由于牵制载荷突卸而引起的前起落架沿着垂直方向的快速振动现象,并分析了该现象的动力学成因;研究了在弹射末端由于弹射杆载荷突卸而引起的前起落架的快速突伸规律,分析了各种参数对前起落架突伸的影响.结果分析表明:为了减小前起落架支柱受力的波动峰值,应适当增加弹射杆长度和牵制杆长度,及牵制杆最大破坏力值;但为了降低弹射起飞难度,应适当减小弹射杆长度.

参考文献/References:

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备注/Memo

备注/Memo:
国家自然科学基金资助项目(61104037)
更新日期/Last Update: 2012-10-17