Affiliation of Author(s):航空学院
Journal:Hangkong Xuebao
Abstract:The design of the adaptive rotor is different from that of the conventional passive rotor. By actively changing the rotor parameters, the rotor lift-to-drag ratio can be optimized to get adaptive to the flight environment and flight condition, so as to reduce the power consumption of the rotor and improve the flight performance of the helicopter. This paper summarizes national and international research progress in using adaptive rotors to improve the performance of the rotor, including the variable speed rotor, variable diameter rotor, individual blade pitch control rotor, active twist rotor, morphing blade airfoil, etc. The research progress and prospects in performance improvement by adaptive rotors are also summarized. © 2018, Press of Chinese Journal of Aeronautics. All right reserved.
ISSN No.:1000-6893
Translation or Not:no
Date of Publication:2018-04-25
Co-author:Chen Weidong,Wei, Wulei,Sang, Yuwei
Correspondence Author:韩东
Professor
Supervisor of Doctorate Candidates
Gender:Male
Alma Mater:南京航空航天大学
Education Level:南京航空航天大学
Degree:Doctoral Degree in Engineering
School/Department:College of Aerospace Engineering
Discipline:Flight Vehicle Design
Business Address:A5-311
Contact Information:025-84896444 donghan@nuaa.edu.cn
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