常规旋翼构型复合式高速直升机发展概况及关键技术  

Development overview and key technologies of high speed hybrid helicopter with single main rotor

作　　者：黄明其[1] 徐栋霞 何龙[1] 朱清华[2] 王亮权 HUANG Mingqi;XU Dongxia;HE Long;ZHU Qinghua;WANG Liangquan(Rotor Aerodynamics Key Laboratory,Low Speed Aerodynamics Institute,China Aerodynamics Research and Development Center,Mianyang Sichuan 621000,China;National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics,College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)

机构地区：[1]中国空气动力研究与发展中心低速空气动力研究所旋翼空气动力学重点实验室,四川绵阳621000 [2]南京航空航天大学航空学院直升机旋翼动力学国家级重点实验室,南京210016

出　　处：《航空动力学报》2021年第6期1156-1168,共13页Journal of Aerospace Power

基　　金：中国空气动力研究与发展中心基础和前沿技术研究基金资助项目(PJD20170165);某装备科研资助项目(JK20191A040327)。

摘　　要：对常规旋翼构型复合式高速直升机的发展概况及关键技术进行了综述。首先,结合常规旋翼构型复合式高速直升机的布局型式及操纵方式,介绍了该构型复合式直升机的一般概念。然后,根据常规旋翼构型复合式高速直升机的前飞动力结构特点,将其分为三种类型,并分别对不同类型复合式直升机的布局型式及其发展概况进行了梳理。在此基础上,针对目前该构型高速直升机所面临的问题,总结了该构型直升机的总体布局设计与优化、过渡模态操纵分配设计等关键技术。最后,结合国内外高速直升机的发展趋势,以及该构型高速直升机的特点,分析了常规旋翼构型复合式高速直升机的发展前景,并对其在我国的发展提出了初步建议。The development and key technologies of high speed hybrid helicopter with single main rotor were reviewed. Firstly, the general concept about the layout type and control mode of high speed hybrid helicopter with single main rotor was briefly introduced. Then, the high speed hybrid helicopters with single main rotor were divided into three configurations based on their own forward flight power structure features. At the same time, the layout of different configurations and their development situations were described respectively. And on this basis, according to the present problems faced by high speed hybrid helicopter with single main rotor, the key technologies such as the overall layout design and optimization, transition mode control and distribution design were summarized and sorted out. Lastly, combined with the development trend of high speed helicopter at home and abroad and the characteristics of helicopter with this configuration, the development prospect of high speed hybrid helicopter with single main rotor was analyzed and some preliminary suggestions on its development in our country were put forward.

关 键 词：复合式高速直升机 常规旋翼 辅助推进 布局优化 操纵策略 气动干扰 

分 类 号：V211.52[航空宇航科学与技术—航空宇航推进理论与工程]