| 倾转旋翼飞机技术发展研究 |
| |
| 引用本文： | 陈恒,左晓阳,张玉琢.倾转旋翼飞机技术发展研究[J].飞行力学,2007,25(1):5-8. |
| |
| 作者姓名： | 陈恒 左晓阳 张玉琢 |
| |
| 作者单位： | 1. 空军工程大学,工程学院,陕西,西安,710038
2. 西北工业大学,无人机研究所,陕西,西安,710072 |
| |
| 摘 要： | 对倾转旋翼飞机的技术基础——推力矢量技术进行了介绍,分析了倾转旋翼飞机直升机模态和固定翼飞机模态的工作特点;针对倾转旋翼飞机的概念、方案进行了论述,并提出了倾转旋翼飞机的技术规格要求;总结了倾转旋翼飞机的技术发展历程、技术方案演变及各发展阶段的特点,并展望了其应用前景。
|
| 关 键 词： | 倾转旋翼飞机 推力矢量 垂直起降 飞行控制 |
| 文章编号： | 1002-0853(2007)01-0005-04 |
| 修稿时间： | 2005-12-14 |
Tiltrotor Aircraft Key Technology Developing Research |
| |
| CHEN Heng,ZUO Xiao-yang,ZHANG Yu-zhuo.Tiltrotor Aircraft Key Technology Developing Research[J].Flight Dynamics,2007,25(1):5-8. |
| |
| Authors: | CHEN Heng ZUO Xiao-yang ZHANG Yu-zhuo |
| |
| Abstract: | This paper introduces the VTOL technology and studies the helicopter mode and the airplane mode of the tiltrotor aircraft.We have a research on the concept and plan for the tiltrotor aircraft and put forward spec requirements for the tiltrotor aircraft.After we study the development and the key technology of the tiltrotor aircraft,we find that the tiltrotor aircraft not only posses the good concept but also become the mature technology.The application of the tiltrotor aircraft would become wide and wide. |
| |
| Keywords: | tiltrotor aircraft thrust vectoring control vertical takeoff and landing flight control |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
