弹性杆端在某型机主桨毂中的设计与应用  

The Design and Application of Main Rotor Head Elastomeric Rod End

作　　者：金坤健[1] 彭利乐[1] 谢留 章华[1] 

机构地区：[1]中国直升机设计研究所,江西景德镇333001 [2]中国人民解放军驻一二二厂军事代表室,黑龙江哈尔滨150000

出　　处：《直升机技术》2010年第3期44-48,共5页Helicopter Technique

摘　　要：以某型机主桨毂弹性杆端设计分析为例,介绍了弹性杆端的结构特点,阐述了主桨毂运动学分析模型及骨架驱动模型在弹性杆端设计分析中的应用,同时阐述了弹性杆端对主桨毂周边结构的影响分析。为弹性杆端在主桨毂及其它系统中的应用提供参考。The article gave a example with the design of the Elastomeric Rod End on one helicopter Main Rotor Head.Introduced the configuration of the Elastomeric Rod End,expatiated the application of the Main Rotor Head kinematics model and framework drive model on the Elastomeric Rod End design.And expatiated the influence of the Elastomeric Rod End for Main Rotor Head.The example provides the means for MRH Elastomeric Rod End and other application.

关 键 词：弹性杆端 主桨毂 设计与应用 

分 类 号：V22[航空宇航科学与技术—飞行器设计]