摘要
文章系统梳理了典型加油机与受油直升机平台的性能特点,概述了软式空中加油系统的核心部件结构及其协同作用机制。在此基础上,重点综述了直升机空中加油过程中的三大关键技术挑战:尾流干扰对受油机飞行稳定性的破坏机制、软管-锥套系统在复杂流场中的动态响应行为,以及自主对接引导控制技术的演进路径。研究表明:尾流扰动下的耦合难题、柔性结构的非线性建模难点及多源信息融合控制策略的实用性,仍是制约任务可靠性的核心瓶颈;未来应聚焦高精度流场建模、耦合系统的动态特性识别与优化,以及具备环境感知与自主决策能力的协同控制体系构建,为直升机复杂环境下稳定、高效的空中加油提供技术支撑。
Helicopter aerial refueling technology is essential for extending operational range and enhancing sustained combat capabilities.The performance characteristics of typical tanker and receiver platforms are reviewed and the core components and their synergistic mechanisms in soft aerial refueling systems are outlined.It highlights three major challenges:the impact of wake turbulence on flight stability,the dynamic behavior of the hose-drogue system in complex flow fields,and the evolution of autonomous coupling and guidance control.The study identifies wake turbulence coupling,nonlinear modeling of flexible structures,and multi-source information fusion as key bottlenecks,and future efforts should focus on high-precision flow field modeling,dynamic characterization of coupled systems,and the development of collaborative control systems with environmental awareness and autonomous decision-making.
作者
台环宇
聂日明
耿雷铭
付子祺
刘冠男
冯诗愚
TAI Huanyu;NIE Riming;GENG Leiming;FU Ziqi;LIU Guannan;FENG Shiyu(College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing Jiangsu 210016,China;AVIC General Huanan Aircraft Industry Co.,Ltd.,Zhuhai Guangdong 519000,China;School of Chemical Engineering and Technology,Xi’an Jiaotong University,Xi’an Shaanxi 710049,China)
出处
《海军航空大学学报》
2026年第1期136-146,共11页
Journal of Naval Aviation University
基金
南京航空航天大学2024年研究生科研与实践创新计划项目(xcxjh20240112)。
