The Motion Reliability Simulation and Analysis of Main Rotor Head of Helicopter Rotor System

摘要：

The motion of main rotor head of helicopter rotor system is complex.Its reliability influences flying qualities and safety of helicopter directly.But, traditional experiments and deterministic simulation have been difficult to measure movement (flapping,lead-laging and pitching angles) and analyze motion reliability of main rotor head quantitatively.The virtual prototype model was built in the integrating simulation environment,which integrated Catia,MSC.Simdesigner and Adams.On the platform of Adams,we used the deformation of torsional spring to fit the moving angles.The kinematic and dynamic properties were simulated and analyzed deterministically.According to the compared result with the test data,it is shown that the virtual prototype is true and the result is feasible.Finally,we implemented reliability software-ARES which has been developed independently to call Adams and computed the flapping reliability quantitatively.The reliability and the sensitive parameters were obtained.Combined with the results and practical engineering,we presented an effective way to improve the flapping reliability from 0.9904 to 0.9993.

关键词： Helicopter Main Rotor Head Flapping Motion Virtual Prototype Reliability

作者: Chen Fang Zhang JianGuo Gong Qi Song yonglei Suduo

作者单位: Dept.of Project Systems Engineering Beijing,PR .China Chinese Helicopter Research and Development Institute Jingdezhen P.R.China Center of Aviation Safely Technology,CAAC Beijing,P.R.China

会议类型: 国际会议

会议名称: 2009 8th International Conference on Reliability,Maintainability and Safety(第八届中国国际可靠性、维修性、安全性会议)

会议地点: 成都

会议语种:英文

页码: 1008-1011

在线出版日期: 2009-08-24（万方平台首次上网日期，不代表论文的发表时间）