| 飞行器螺旋桨电推进动力测试系统设计研究 |
| |
| 引用本文： | 张鑫,窦满峰,丁晓峰,何琳琳.飞行器螺旋桨电推进动力测试系统设计研究[J].微电机,2009,42(7). |
| |
| 作者姓名： | 张鑫 窦满峰 丁晓峰 何琳琳 |
| |
| 作者单位： | 1. 西北工业大学自动化学院,西安,710072
2. 郑州航空工业管理学院,郑州,450015 |
| |
| 基金项目： | 西北工业大学研究生创业种子基金，航空科学基金 |
| |
| 摘 要： | 针对飞行器螺旋桨电推进系统性能指标的空中测试问题,介绍了电推进系统的结构和动力测试原理,并设计了动力测试系统,介绍了动力测试系统的技术方案、硬件结构和软件结构.研究为空中验证电推进系统的技术指标提供了有效的途径和基础.
|
| 关 键 词： | 螺旋桨电推进系统 原理 动力测试 设计 无刷直流电动机 |
Design of Dynamic Test System for Airscrew Electric Propulsion System |
| |
| ZHANG Xin,DOU Man-feng,DING Xiao-feng,HE Lin-lin.Design of Dynamic Test System for Airscrew Electric Propulsion System[J].Micromotors,2009,42(7). |
| |
| Authors: | ZHANG Xin DOU Man-feng DING Xiao-feng HE Lin-lin |
| |
| Abstract: | For the effective function verifying problem of airscrew electric propulsion systems in the state of flight, a design of dynamic test system was proposed by analyzing the principle of testing method in this paper, which was based on the structural characteristic and operation principle of the propulsion sys-tems. Introduced the technological scheme, hardware structure and software structure of the test system,provided effective research route and foundation for propu]sion system testing. |
| |
| Keywords: | Airserew electric propulsion systems Principle Dynamic test Design BLDCM |
| 本文献已被 万方数据 等数据库收录！ |
|
