Dynamic modeling and simulation of sheave damper based on AMESim software
<b>[Objectives]</b> Considering the shortcomings of the traditional sheave damper in buffer performance and the peak value of the greatest cable tension,<b>[Methods]</b> this paper presents a sheave damper with variable damping according to piston displacement as a replacemen...
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Editorial Office of Chinese Journal of Ship Research
2017-10-01
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doaj-8001994541e64c64a6c72f49ce3479652020-11-24T23:29:16ZengEditorial Office of Chinese Journal of Ship ResearchZhongguo Jianchuan Yanjiu1673-31851673-31852017-10-0112510410810.3969/j.issn.1673-3185.2017.05.013201705013Dynamic modeling and simulation of sheave damper based on AMESim softwareBI Ke0LI Xiang1TANG Zhiyin2OUYANG Bin3HE Haitao4WANG Qi5WU Gang6College of Power Engineering, Naval University of Engineering, Wuhan 430033, ChinaCollege of Power Engineering, Naval University of Engineering, Wuhan 430033, ChinaCollege of Power Engineering, Naval University of Engineering, Wuhan 430033, ChinaNational Key Laboratory of Science and Technology on Vessel Integrated Power System, Naval University of Engineering, Wuhan 430033, ChinaCollege of Power Engineering, Naval University of Engineering, Wuhan 430033, ChinaCollege of Power Engineering, Naval University of Engineering, Wuhan 430033, ChinaCollege of Power Engineering, Naval University of Engineering, Wuhan 430033, China<b>[Objectives]</b> Considering the shortcomings of the traditional sheave damper in buffer performance and the peak value of the greatest cable tension,<b>[Methods]</b> this paper presents a sheave damper with variable damping according to piston displacement as a replacement for the traditional sheave damper, and AMESim software is used for the modeling and simulation.<b>[Results]</b> The results show that the new sheave damper can significantly improve the arresting gear performance indicators, and has better adaptability for aircraft impact load. Compared with the traditional sheave damper, the new method can reduce cable tension by 25% and reduce the maximum deceleration of aircraft by 23%.<b>[Conclusions]</b> As such, the research in this paper can provide a theoretical reference for improving the performance of aircraft arresting gear.http://www.ship-research.com/EN/Y2017/V12/I5/104arresting gearsheave dampervarious dampingAMESim |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
BI Ke LI Xiang TANG Zhiyin OUYANG Bin HE Haitao WANG Qi WU Gang |
spellingShingle |
BI Ke LI Xiang TANG Zhiyin OUYANG Bin HE Haitao WANG Qi WU Gang Dynamic modeling and simulation of sheave damper based on AMESim software Zhongguo Jianchuan Yanjiu arresting gear sheave damper various damping AMESim |
author_facet |
BI Ke LI Xiang TANG Zhiyin OUYANG Bin HE Haitao WANG Qi WU Gang |
author_sort |
BI Ke |
title |
Dynamic modeling and simulation of sheave damper based on AMESim software |
title_short |
Dynamic modeling and simulation of sheave damper based on AMESim software |
title_full |
Dynamic modeling and simulation of sheave damper based on AMESim software |
title_fullStr |
Dynamic modeling and simulation of sheave damper based on AMESim software |
title_full_unstemmed |
Dynamic modeling and simulation of sheave damper based on AMESim software |
title_sort |
dynamic modeling and simulation of sheave damper based on amesim software |
publisher |
Editorial Office of Chinese Journal of Ship Research |
series |
Zhongguo Jianchuan Yanjiu |
issn |
1673-3185 1673-3185 |
publishDate |
2017-10-01 |
description |
<b>[Objectives]</b> Considering the shortcomings of the traditional sheave damper in buffer performance and the peak value of the greatest cable tension,<b>[Methods]</b> this paper presents a sheave damper with variable damping according to piston displacement as a replacement for the traditional sheave damper, and AMESim software is used for the modeling and simulation.<b>[Results]</b> The results show that the new sheave damper can significantly improve the arresting gear performance indicators, and has better adaptability for aircraft impact load. Compared with the traditional sheave damper, the new method can reduce cable tension by 25% and reduce the maximum deceleration of aircraft by 23%.<b>[Conclusions]</b> As such, the research in this paper can provide a theoretical reference for improving the performance of aircraft arresting gear. |
topic |
arresting gear sheave damper various damping AMESim |
url |
http://www.ship-research.com/EN/Y2017/V12/I5/104 |
work_keys_str_mv |
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1725546506616832000 |