[1]张智,闻子侠,朱齐丹,等.舰载机阻拦过程动力学仿真[J].哈尔滨工程大学学报,2014,(05):571-579.[doi:10.3969/j.issn.10067043.201305035]
 ZHANG Zhi,WEN Zixia,ZHU Qidan,et al.Kinetic simulation of shipboard arresting system[J].hebgcdxxb,2014,(05):571-579.[doi:10.3969/j.issn.10067043.201305035]
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舰载机阻拦过程动力学仿真(/HTML)
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《哈尔滨工程大学学报》[ISSN:1006-6977/CN:61-1281/TN]

卷:
期数:
2014年05期
页码:
571-579
栏目:
出版日期:
2014-05-25

文章信息/Info

Title:
Kinetic simulation of shipboard arresting system
文章编号:
10067043(2014)05057109
作者:
张智 闻子侠 朱齐丹 张雯 喻勇涛
哈尔滨工程大学 自动化学院,黑龙江 哈尔滨 150001
Author(s):
ZHANG Zhi WEN Zixia ZHU Qidan ZHANG Wen YU Yongtao
College of Automation, Harbin Engineering University, Harbin 150001, China
关键词:
系统仿真动力学仿真舰载机阻拦系统有限元动力学
分类号:
V244.4
DOI:
10.3969/j.issn.10067043.201305035
文献标志码:
A
摘要:
为研究舰载机阻拦过程受力规律,提出了一种动力学与有限元相结合的阻拦过程仿真建模方法,采用动力学方法建立飞机机体六自由运动模型、尾钩运动模型及阻拦液缸运动模型,并采用有限元方法建立阻拦索波动模型、阻拦索与滑轮组及尾钩的作用力模型,仿真模型真实地反映了阻拦过程各项规律及影响因素,包括阻拦过程索的弯折波动、应力传递、尾构挂索后摆动及钩索滑移等过程,以及飞机偏心、偏航阻拦的影响规律,仿真结果验证了模型的有效性和优越性。

参考文献/References:

[1]BLACK R. A study in terminal bending of uniform and encapsulated eire rope with linear and nonlinear constitutive equations[R]. Philadelphia,USA,1971. [2]THOMLINSON J. A study of the aircraft arresting hook bounce problem[R]. American: R&M 2980, 1957. [3]GIBSON P T, GRESSH A. Analytical study of aircraft arresting gear cable design[R]. American: AD617788, 1965. [4]GIBSON P T, ALEXANDER G H, CRESS H A. Validation of design theory for aircraft arresting gear cable[R]. American: AD665328. 1968.  [5]柳刚,聂宏.飞机阻拦钩碰撞动力学和拦阻钩纵向阻尼器性能[J].航空学报,2009, 30(11): 20932099.LIU Gang, NIE Hong. Dynamics of bounce of aircraft arresting hook impacting with deck and performance of arresting hook longitudinal damper[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(11): 20932099. [6]柳刚.舰载飞机着舰阻拦钩碰撞及拦阻动力学研究[D].南京:南京航空航天大学,2010: 1121. LIU Gang. Investigation on arresting dynamics for carrierBased aircraft with consideration of arresting hook bounce[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2010:1121. [7]张萍,金栋平.计及弯折波的舰载机拦阻过程控制[J].南京航空航天大学, 2010,32(11):20082015.ZHANG Ping, JIN Dongping. Control of arresting process for carrier aircraft considering kinkwave[J]. 2010, 32(11): 20082015. [8]ZHANG Wen, ZHANG Zhi, ZHU Qidan, et al. Research on the dynamics model of carrierbased aircraft landing gears on the dynamic deck[J]. Chinese Journal of aeronautics, 2009,22(4):371379.  [9]MATTHEWS F L, RAWLINGS R D. Landing signal officer reference manual[M]. Virginia Beach: Landing Signal Officers School Naval Air Station Oceana, 1999: I11. [10]KRAUT W K, SWIENCINSKI H J. Reliability of the mark 7 mod 3 arresting gear[R]. American: AD845390, 1968. [11]张澍森,金栋平.飞机阻拦过程的非线性最优控制[J]. 航空学报, 2009, 30(5): 849854.ZHANG Shusen, JIN Dongping. Nonlinear optimal control of aircraft arresting pross[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(5): 849854. [12]MIKHALUK D, VOINOV I, BOROVKOV A. Finite element modeling of the arresting gear and simulation of the aircraft deck landing dynamics[C]// European LS DYNA Conference.Petersburg, Russia, 2008.3135. [13]朱齐丹,闻子侠,张智.阻拦系统动力学建模与仿真[J]. 航空学报,2012,33(3):520529.ZHU Qidan, WEN Zixia, ZHANG Zhi. Kinetic modeling and simulation of shipboard arresting system[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(3):520529.

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备注/Memo

备注/Memo:
收稿日期:2013-05-14. 网络出版时间:2013-04-16. 基金项目:国家自然科学基金资助项目(61104037;61304060); 国家 科技合作专项项目(2013DFR10030);中央高校基本科研 业务费立项基金资助项目(HEUCFX41304). 作者简介:张智(1981-), 男, 讲师, 博士. 通信作者:张智,E-mail: neverbadzz@ 163.com.
更新日期/Last Update: 2014-07-10