| 直升机整流罩锁紧机构方案设计与研究 |
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| 引用本文： | 张巍,吕长生,姜大成,陈申. 直升机整流罩锁紧机构方案设计与研究[J]. 机械设计与制造, 2010, 0(4) |
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| 作者姓名： | 张巍 吕长生 姜大成 陈申 |
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| 作者单位： | 陆航驻哈尔滨地区代表室,哈尔滨,150066 |
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| 摘 要： | 提出了直升机整流罩锁紧机构设计方案,利用Pro/E软件进行各零部件的三维建模、虚拟装配。通过锁紧触点运动轨迹方程的建立进行了Pro/E环境下锁紧机构运动仿真,并应用有限元分析软件MSC.Patran校核了锁紧梁的强度。通过理论设计、运动仿真和强度校核结果表明了该锁紧机构设计方案的可行性。
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| 关 键 词： | 直升机 整流罩锁紧机构 轨迹方程 有限元分析 强度校核 |
Program design and research on helicopter dome locking machine |
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| ZHANG Wei,LV Chang-sheng,JIANG Da-cheng,CHEN Shen. Program design and research on helicopter dome locking machine[J]. Machinery Design & Manufacture, 2010, 0(4) |
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| Authors: | ZHANG Wei LV Chang-sheng JIANG Da-cheng CHEN Shen |
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| Affiliation: | Customer Representative of General Staff Department in Harbin District/a>;Harbin 150066/a>;China |
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| Abstract: | Design scheme about helicopter dome locking machine is put forward,the use of Pro/E parts and components for the three-dimensional modeling,virtual assembly. Trajectory through the locking contact equation,a Pro/E environment body motion simulation. Application of finite element analysis software MSC. Patran check the strength of the locking beam. Through theoretical design,motion simulation and Checking the results of strength show that the feasibility of the design. |
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| Keywords: | Helicopter Dome locking machine Trajectory equation Finite element analysis Strength Check |
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