直升机旋翼系统构型发展综述  

Overview of Helicopter Rotor System Configuration Development

作　　者：熊宏锦 XIONG Hongjin(Naval Equipment Development,Nanchang 330024,China)

机构地区：[1]海军装备部,江西南昌330024

出　　处：《直升机技术》2025年第1期61-66,共6页Helicopter Technique

摘　　要：旋翼系统是直升机的核心动部件,不仅负责产生升力和推力,还直接影响着直升机的飞行稳定性、操控性以及整体性能,也是直升机区别于其他飞行器的最显著特点。旋翼系统构型的设计和发展直接关系到直升机的性能和安全性。直升机旋翼系统的构型发展经历了多个阶段,从传统的单旋翼构型到复合式高速直升机构型,技术不断进步。文章全面阐述了直升机旋翼系统构型的发展现状;深入剖析传统构型与新构型的原理、结构特点、优势及其适用场景;在此基础上,对旋翼系统构型的未来发展趋势进行了展望。Rotor system is the core dynamic component of helicopter,which not only generates lift and thrust,but also directly affects the flight stability,controllability and overall performance of helicopter.It is also the most remarkable characteristic that distinguishes helicopter from other aircraft.The design and development of rotor system is directly related to the performance and safety of helicopter.The configuration development of helicopter rotor systems has gone through several stages,from traditional single-rotor configurations to compound high-speed helicopter configurations with continuous technological advances.This paper comprehensively summarized the development status of helicopter rotor system configuration,deeply analyzed the principle,structural characteristics,advantages and applicable scenarios of traditional and new configurations,and on this basis,looked forward to the future development trend of rotor system configuration.

关 键 词：直升机旋翼系统 构型 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计]