直升机悬停回转时尾桨载荷计算研究 |
| |
引用本文: | 蔡慧莲,晏峰.直升机悬停回转时尾桨载荷计算研究[J].直升机技术,2002(3):1-5. |
| |
作者姓名: | 蔡慧莲 晏峰 |
| |
作者单位: | 中国直升机设计研究所,景德镇,333001 |
| |
摘 要: | 本文推导了直升机尾桨线性和非线性的静、动力分析方法,从理论上推导出直升机尾桨叶在悬停回转时的运动学及动力学之间的关系,并对Z11型机悬停回转状态下尾桨叶载荷进行了计算。
|
关 键 词: | 直升机 尾桨 载荷 |
RESEARCH ON TAIL ROTOR SPOT TURN LOAD CALCULATING OF HELICOPTER |
| |
Authors: | CAI Hui-lian YAN Feng |
| |
Abstract: | This article search the analysis method of helicopter tail rotor in dynamics, considering the linearity and non-linearity deduce the equations of kinematics and dynamics of tail rotor on case of spot turn,and then give a sample that Zll load calculation on spot turn case. |
| |
Keywords: | helicopter tail rotor load |
本文献已被 CNKI 维普 万方数据 等数据库收录! |
|