Dynamic response analysis of the transmission of tilt-rotor in different modes

MIAO Jun; WANG San-min; NING Song

Chinese

您当前的位置：

首页 >

文章列表页 >

Dynamic response analysis of the transmission of tilt-rotor in different modes

更新时间：2026-07-07

- Dynamic response analysis of the transmission of tilt-rotor in different modes
- Vol. 23, Issue 8, (2008)
- 作者机构：
  
  西北工业大学机电学院,西安,710072
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2008
- 稿件说明：
移动端阅览
MIAO Jun, WANG San-min, NING Song. Dynamic response analysis of the transmission of tilt-rotor in different modes[J]. 2008, 23(8).
DOI：

MIAO Jun, WANG San-min, NING Song. Dynamic response analysis of the transmission of tilt-rotor in different modes[J]. 2008, 23(8). DOI：

摘要

以倾转旋翼机发动机短舱内的传动系统为研究对象

根据设计的传动结构建立了它的动力学模型和动态响应方程

分析了倾转旋翼机旋翼在起降、巡航和过渡三种状态下的激励特性

并针对三种状态下旋翼激励的特点对传动系统动态响应进行了数值求解

最后研究了传动系统中齿轮啮合的动载系数的变化特点

并对系统的共振频率进行了探讨.研究工作对倾转旋翼机的传动系统的可靠性分析和动态优化设计等均有参考意义.

Abstract

Based the transmission structure in the nacelle of tilt-rotor

the complex gears and shafts coupling dynamic modeling and dynamic response equations were built.And

three types of the force characteristics on the blades: cruise

hover and transition were analyzed.The dynamic response was computed using Runge-Kutta method to obtain the dynamic gearmesh coefficient.Finally

the natural frequency was discussed.The results provide some useful information to analyze the reliability and the dynamics optimization of the transmission.

关键词

Keywords

references

Views

455

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Dynamic efficiency investigation of the transmission of tilt-rotor

Modeling study on tilt-rotor's aeroelastic stability in cruise flight

考虑多源不确定性的复合材料风扇叶片高周疲劳失效概率评估

与发动机匹配的旁路式双喉道气动矢量喷管数值模拟研究

组合式弹性金属密封泄漏特性实验研究与结构优化

Related Author

GUO Jia-shun

WANG San-min

YUAN Ru

XUE Li-peng

ZHANG Cheng-lin

Related Institution

School of Mechanical Engineering,Northwestern Polytechnical University

National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰