| 飞翼型飞机主起落架与舱门联动收放机构设计 |
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| 引用本文： | 王小锋,张威,吴林,李田囡.飞翼型飞机主起落架与舱门联动收放机构设计[J].机电工程技术,2011,40(11):71-73. |
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| 作者姓名： | 王小锋 张威 吴林 李田囡 |
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| 作者单位： | 中航工业飞机起落架有限责任公司,湖南长沙,410200 |
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| 摘 要： | 对飞翼型飞机的起落架与舱门联动收放提出了新的设计思想.通过对空间进行分析、布局,应用CATIA进行了运动仿真分析.并对联动收放机构的强度和刚度进行了分析计算.在满足要求的基础上,实现了狭小空间内起落架与舱门的联动收放.
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| 关 键 词： | 起落架 舱门 联动收放 运动仿真 |
R&E Mechanism Design of Thin Wing Type MLG and Door |
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| WANG Xiao-feng,ZHANG Wei,WU Lin,LI Tian-nan.R&E Mechanism Design of Thin Wing Type MLG and Door[J].Mechanical & Electrical Engineering Technology,2011,40(11):71-73. |
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| Authors: | WANG Xiao-feng ZHANG Wei WU Lin LI Tian-nan |
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| Affiliation: | WANG Xiao-feng,ZHANG Wei,WU Lin,LI Tian-nan(AVIC Landing Gear Advanced Manufacturing Corp.Engineering Center,Changsha 410200,China) |
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| Abstract: | A new design idea for linkage actuated with landing gear and door is discussed in this paper.According to analyze and lay out of the R&E space,the R&E mechanism is analyzed of kinematical simulation using CATIA.Then the strength and stiffness are analyzed and calculated.In order to meet the demands,this paper solves the linkage actuated with landing gear and door among the hole-in-the-wall space. |
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| Keywords: | landing gear door linkage actuated kinematical simulation |
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