结构静力/疲劳试验控制模式转换技术研究 |
| |
引用本文: | 吝继锋,;陈戈,;张革命. 结构静力/疲劳试验控制模式转换技术研究[J]. 工程与试验, 2014, 0(4): 9-12 |
| |
作者姓名: | 吝继锋, 陈戈, 张革命 |
| |
作者单位: | [1]中国飞机强度研究所第八研究室,陕西西安710065; [2]全尺寸飞机结构静力/疲劳实验室,陕西西安710065 |
| |
摘 要: | 根据飞机结构静力/疲劳试验中起落架试验、试验支持、操纵系统试验、破坏试验的需求,对模式转换技术进行了研究,并利用FlexTest 200协调加载控制系统进行了模式转换验证试验。试验结果表明,模式转换技术可以应用于飞机结构静力/疲劳试验。
|
关 键 词: | 结构静力/疲劳试验 控制模式 转换 验证试验 |
Research on Technology of Control Mode Switching for Structural Static/Fatigue Test |
| |
Affiliation: | Lin Jifeng ,Chen Ge , Zhang Geming (1. The Eighth Research of China Aircraft Strength Research Institute, Xi' an 710065, Shanxi, China ; 2. Aircraft Strength Research Institute of AVIC Full Scale Aircraft Structural Static/Fatigue Lab, Xi' an 710065, Shanxi, China) |
| |
Abstract: | According to the demand of aircraft structural static/fatigue tests,such as landing gear test,test support,control system test and destruction test,this paper has a research on technology of control mode switching,and has a validation test with FlexTest 200 coordinative loading control system.Test result indicates that the technology of control mode switching can apply to aircraft structural static/fatigue tests. |
| |
Keywords: | structural static/fatigue test control mode switching validation test |
本文献已被 CNKI 维普 等数据库收录! |
|