多电飞机混合作动系统工作模式优化分析  

作　　者：范凯[1] 

机构地区：[1]海军装备部,陕西西安710021

出　　处：《科技创新与应用》2020年第20期44-45,共2页Technology Innovation and Application

摘　　要：文章基于现阶段,多电飞机飞行控制系统结构设计中,所实践的非相似余度混合作动系统,对传统液压作动器、电动静液作动器所构建的作动系统工作模式优化展开研究。同时通过工况条件、系统功率特点、仿真参数分析等方式,对多电飞机混合作动系统新型工作模式的可行性做出简单阐述,希望给予相关从业者建议与参考。This paper is based on the optimization of the working mode of actuation system constructed by traditional hydraulic actuators and electro-hydrostatic actuators in the non-similar redundancy mixed-action phase practiced in the structural design of the multi-electric aircraft flight control system at this stage.At the sametime,through working conditions,system power characteristics,simulation parameters analysis and other methods,the feasibility of the new working mode of the hybrid electric aircraft cooperative system is briefly described,in the hope of providing suggestions and references for relevant practitioners.

关 键 词：多电飞机 混合 作动系统 工作模式 

分 类 号：V227[航空宇航科学与技术—飞行器设计]