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

HUANG Mingqi; XU Dongxia; HE Long; ZHU Qinghua; WANG Liangquan

doi:10.13224/j.cnki.jasp.2021.06.004

Chinese

您当前的位置：

首页 >

文章列表页 >

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

更新时间：2026-07-07

- Development overview and key technologies of high speed hybrid helicopter with single main rotor
- Vol. 36, Issue 6, Pages: 1156-1168(2021)
- 作者机构：
  
  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
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.2021.06.004
  CLC：
- Published：2021
- 稿件说明：
移动端阅览
黄明其, 徐栋霞, 何龙, 朱清华, 王亮权. 常规旋翼构型复合式高速直升机发展概况及关键技术[J]. 航空动力学报, 2021, 36(6): 1156-1168.

doi: 10.13224/j.cnki.jasp.2021.06.004
黄明其, 徐栋霞, 何龙, 朱清华, 王亮权. 常规旋翼构型复合式高速直升机发展概况及关键技术[J]. 航空动力学报, 2021, 36(6): 1156-1168. DOI： 10.13224/j.cnki.jasp.2021.06.004.

doi: 10.13224/j.cnki.jasp.2021.06.004 DOI：

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。

Abstract

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

Keywords

references

Views

328

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Numerical simulation on aerodynamic interference of UAVs like X⁃47B in rhombus formation

Channel layout and shape optimization of active cooling thin⁃walled structures

Investigation of control strategy for quad⁃tilt⁃rotor aircraft in helicopter mode

Aerodynamic characteristics of quad tilt rotor aircraft in vertical flight

Control strategy for compound coaxial helicopter under conversion mode

Related Author

Yonggang YU

Zhongyun XIAO

Xingda CUI

Lu ZHANG

Fan LIU

Shuai MA

Shiping SUN

Dehui XU

Related Institution

Computation Aerodynamics Institute，China Aerodynamics Research and Development Center

State Key Laboratory of Aerodynamics，China Aerodynamics Research and Development Center

School of Aeronautical Manufacturing Engineering， Nanchang Hangkong University

Faculty of Rocket and Space Technology， National Aerospace University “KhAI”

National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics，College of Aerospace Engineering，Nanjing University of Aeronautics and Astronautics

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰