海军航空大学学报2026，Vol.41Issue(4)：625-632,8.DOI:10.7682/j.issn.2097-1427.2026.04.004
空天飞行器翼面折展驱动系统设计及仿真
Design and Simulation of Wing Surface Folding and Spreading Actuation System for Morphing Aircraft
摘要
Abstract
The escalating complexity of near-space missions imposes stringent demands for miniaturization and reusabil-ity technologies in folding wing systems of morphing aircraft.The integrated hydrostatic helical oscillating mechanism,distinguished by its high-torque capacity,exceptional reliability,and compact configuration,achieves repeated wing de-ployment/retraction through torque transmission and rotational motion,thereby offering critical insights for developing novel drive methodologies for morphing wing deformation.Investigation of morphing aircraft wing mechanisms estab-lished performance requirements for oscillating drive systems,leading to the development of an AMESim-based model for the hydrostatic repeatable oscillating hydraulic system to analyze output characteristics.The results indicate that the hydraulic swing actuator achieves an output rotation of 100° with an output torque exceeding 500 N·m,meeting the wing folding and deploying requirements for near-space morphing aircraft.This research provides technical support for the application of deformable driving mechanisms in folding wings for near-space vehicles.关键词
变体飞行器/螺旋摆动液压执行机构/AMESim/功能验证Key words
morphing aircraft/helix swing hydraulic cylinder/AMESim/functional validation分类
航空航天引用本文复制引用
慈克,付剑,李宗伦,宋洪舟,吕定翀..空天飞行器翼面折展驱动系统设计及仿真[J].海军航空大学学报,2026,41(4):625-632,8.基金项目
航天科技一院2024高校联合创新基金(CALT2024-15) （CALT2024-15）
