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Reliability analysis of the flap mechanism with multi-pivots

  • Huan Pang
  • , Tian Xiang Yu
  • , Hui Wang
  • , Bifeng Song
  • Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

2 引用 (Scopus)

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 important mechanisms in aircraft, the reliability of the flat is crucial for the safety and reliability of the aircraft, and it is of great significance to improve its reliability. In this paper, a highly parametric analytical model is developed using dynamic simulation software. Based on the model, the reliability of the mechanism is calculated by combining the means of Response-surface and Monte-Carlo simulation. Finally, the sensitivity analysis for driving torque provides some useful information for the flap reliability optimization.

源语言英语
主期刊名ICQR2MSE 2011 - Proceedings of 2011 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering
页258-262
页数5
DOI
出版状态已出版 - 2011
已对外发布是
活动2011 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering, ICQR2MSE 2011 - Xi'an, 中国
期限: 17 6月 2011 → 19 6月 2011

丛书

姓名ICQR2MSE 2011 - Proceedings of 2011 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering

会议

会议2011 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering, ICQR2MSE 2011
国家/地区中国
市Xi'an
时期17/06/11 → 19/06/11

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