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Reliability Analysis of the Flap Mechanism with Multi-Pivots
文献类型:会议
作者:Pang, Huan[1]  Yu, Tian-Xiang[2]  Wang, Hui[3]  Song, Bifeng[4]  
机构:[1]Department of Aeronautical Engineering Design, School of Aeronautics, Northwestern Polytechnical University, Xi'an, China
[2]Department of Aeronautical Engineering Design, School of Aeronautics, Northwestern Polytechnical University, Xi'an, China
[3]Department of Aeronautical Engineering Design, School of Aeronautics, Northwestern Polytechnical University, Xi'an, China
[4]Department of Aeronautical Engineering Design, School of Aeronautics, Northwestern Polytechnical University, Xi'an, China
年:2011
通讯作者:Pang, H (reprint author), NW Polytech Univ, Sch Aeronaut, Dept Aeronaut Engn Design, Xian 710072, Peoples R China.
会议名称:2011 INTERNATIONAL CONFERENCE ON QUALITY, RELIABILITY, RISK, MAINTENANCE, AND SAFETY ENGINEERING (ICQR2MSE)
页码范围:258-262
会议开始日期:2011-06-17
收录情况:EI(20113614309142)  CPCI-S(WOS:000306959700050)  
所属部门:航空学院
人气指数:707
浏览次数:689
语言:外文
关键词:multi-pivots; coaxiality; response-surface; Monte-Carlo; reliability; sensitivity
摘要:
The flap is an over constrained mechanism with multiple pivots, which assembled along a common axis on the wing. Practically, due to various errors and structure deformation caused by aerodynamic load, it's hard to make sure that the pivots are coaxial. Some pivots which deviate from the axis will have undesirable impacts on the dynamic performance of the mechanism when the flap runs up and down. Severely, the mechanism will be seizure and the entire system will be failure. As one of the most im ...More
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