| 飞机飞行试验用振动／应变测量系统设计 |
| |
| 引用本文： | 宋娜,胡春燕.飞机飞行试验用振动／应变测量系统设计[J].航空计测技术,2010,30(1):35-38. |
| |
| 作者姓名： | 宋娜 胡春燕 |
| |
| 作者单位： | 中航工业北京长城计量测试技术研究所,北京100095 |
| |
| 摘 要： | 为了对飞机飞行试验中零部件的振动和应变进行测量，本文对机载振动／应变实时测量系统进行了设计。该系统包括振动／应变测量系统、数据采集存储系统和数据处理系统，为飞机飞行试验中振动、应变的测量提供了轻便、可靠的测试设备。
|
| 关 键 词： | 机载 振动 应变 实时 数据采集 |
Design of Vibration & Strain Measurement System for Aeroplane Aviation Test |
| |
| SONG Na,HU Chunyan.Design of Vibration & Strain Measurement System for Aeroplane Aviation Test[J].Aviation Metrology & Measurement Technology,2010,30(1):35-38. |
| |
| Authors: | SONG Na HU Chunyan |
| |
| Institution: | (Changcheng Institute of Metrology ＆ Measurement, Beijing 100095, China) |
| |
| Abstract: | In order to measure the vibration and strain of the aircraft accessories and parts among the aeroplane aviation test, airborne vibra- tion and strain real-time measurement system is designed, which include vibration ＆ strain measurement system, data acquisition ＆ storage system and data processing system. It provide lightweight, reliable test equipment for measurement of vibration and strain during aeroplane aviation test. |
| |
| Keywords: | aeroplane vibration strain real-time data acquisition |
| 本文献已被 维普 万方数据 等数据库收录！ |
