UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT
In order to study the parameters of a folding wing‘s spreading performance which is used on the guided missile’s actuator,the unfolding performance was researched. First,a kinetic equation based on Lagrange’ s Equation was established,which provided a theoretic base for the simulation. Then,related...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Journal of Mechanical Strength
2017-01-01
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| Series: | Jixie qiangdu |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.01.040 |
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| _version_ | 1841535094283567104 |
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| author | LIU DuanChen HAN XueFeng ZHANG Yue ZHANG MingYue LIU XiaoDong |
| author_facet | LIU DuanChen HAN XueFeng ZHANG Yue ZHANG MingYue LIU XiaoDong |
| author_sort | LIU DuanChen |
| collection | DOAJ |
| description | In order to study the parameters of a folding wing‘s spreading performance which is used on the guided missile’s actuator,the unfolding performance was researched. First,a kinetic equation based on Lagrange’ s Equation was established,which provided a theoretic base for the simulation. Then,related dates such as deployable time,impact and stress of the rudder slice were obtained by rigid-flexible coupling dynamics imitating analysis of the spreading process through MSC. ADAMS.Finally,characters of the spreading performance and weak points affected by the impact were tested by experiments. The results show that the unfolding time is 175 ms,impulse strength is 42. 9N,which is less than the strength of the material,and meets the requirements of design. The performance can be described accurately by the simulation mode. Results of both simulations and experiments can provide theoretical basis for structural design and optimizing. |
| format | Article |
| id | doaj-art-a6f8c83cfa3543d08a03c1abc1ba408f |
| institution | Kabale University |
| issn | 1001-9669 |
| language | zho |
| publishDate | 2017-01-01 |
| publisher | Editorial Office of Journal of Mechanical Strength |
| record_format | Article |
| series | Jixie qiangdu |
| spelling | doaj-art-a6f8c83cfa3543d08a03c1abc1ba408f2025-01-15T02:35:05ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692017-01-013923023430597661UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENTLIU DuanChenHAN XueFengZHANG YueZHANG MingYueLIU XiaoDongIn order to study the parameters of a folding wing‘s spreading performance which is used on the guided missile’s actuator,the unfolding performance was researched. First,a kinetic equation based on Lagrange’ s Equation was established,which provided a theoretic base for the simulation. Then,related dates such as deployable time,impact and stress of the rudder slice were obtained by rigid-flexible coupling dynamics imitating analysis of the spreading process through MSC. ADAMS.Finally,characters of the spreading performance and weak points affected by the impact were tested by experiments. The results show that the unfolding time is 175 ms,impulse strength is 42. 9N,which is less than the strength of the material,and meets the requirements of design. The performance can be described accurately by the simulation mode. Results of both simulations and experiments can provide theoretical basis for structural design and optimizing.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.01.040 |
| spellingShingle | LIU DuanChen HAN XueFeng ZHANG Yue ZHANG MingYue LIU XiaoDong UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT Jixie qiangdu |
| title | UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT |
| title_full | UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT |
| title_fullStr | UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT |
| title_full_unstemmed | UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT |
| title_short | UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT |
| title_sort | unfolding performance of folding wing for actuator and experiment |
| url | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.01.040 |
| work_keys_str_mv | AT liuduanchen unfoldingperformanceoffoldingwingforactuatorandexperiment AT hanxuefeng unfoldingperformanceoffoldingwingforactuatorandexperiment AT zhangyue unfoldingperformanceoffoldingwingforactuatorandexperiment AT zhangmingyue unfoldingperformanceoffoldingwingforactuatorandexperiment AT liuxiaodong unfoldingperformanceoffoldingwingforactuatorandexperiment |