倾转旋翼机设计特点及难点浅析  

Brief Analysis on the Design Features and Difficulties of Tiltrotor

作　　者：王伟[1] 段卓毅[1] 周林[1] 

机构地区：[1]中航工业第一飞机设计研究院,陕西西安710089

出　　处：《航空科学技术》2015年第3期1-4,共4页Aeronautical Science & Technology

摘　　要：通过对国外倾转旋翼机的发展历程及具有代表性的V-22"鱼鹰"设计特点进行分析,总结了倾转旋翼类飞机的设计特点及技术难点,并对倾转旋翼机的发展前景进行了展望,为国内此类飞机的研制提供思路和参考。Through analysis of development of foreign tiltrotor and design teatures of representative V-22 Osprey, the design features and technical difficulties of tiltrotor were analysed and the perspective of tiltrotorcraft was forecast,which can provide reference and guidance of development for such type of aircraft.

关 键 词：V-22“鱼鹰” 倾转旋翼机 垂直起降 倾转系统 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计]