检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:冯文正 于菲[1] 关玉明[1] 刘智光 FENG Wenzheng;YU Fei;GUAN Yuming;LIU Zhiguang(School of Mechanical Engineering,Hebei University of Technology,Tianjin 300130,China;School of Control and Mechanical Engineering,Tianjin Chengjian University,Tianjin 300384,China)
机构地区:[1]河北工业大学机械工程学院,天津300130 [2]天津城建大学控制与机械工程学院,天津300384
出 处:《航空工程进展》2023年第3期1-14,共14页Advances in Aeronautical Science and Engineering
基 金:天津市教委科研计划项目(2020KJ056)。
摘 要:变形机翼作为未来飞机设计的重要发展方向之一,其机翼面内变形的研究得到了广泛关注。本文分别从变展长、变掠角、变弦长、组合变形四个方面进行分析,阐述面内变形机翼的国内外研究现状,归纳总结变形机理及优缺点,分析其发展趋势。针对该领域的研究现状以及变形机翼的应用要求,提出变形机翼亟待解决的关键技术,包括变形蒙皮技术、变形机构、智能驱动器、传感器和控制网络,阐述各关键技术的应用要求,分析其现存问题,并对未来发展方向进行展望,为面内变形机翼的设计和应用实现提供参考。Morphing wing is one of the important development directions of future aircraft design,and the study of in-plane deformation of the morphing wing surface has received widespread attention.In this paper,four aspects in-cluding variable span length,variable sweep angle,variable chord length and combined deformation are analyzed to describe the current status of domestic and international research on in-plane morphing wings,summarize the defor-mation mechanism and its advantages and disadvantages,and analyze the future development trend of morphing wing.In view of the current research situation and the application requirements of the morphing wing,the key tech-nologies of the morphing wing are proposed,including the morphing skin technology,morphing mechanism,intelli-gent actuator,sensor and control network.The application requirements of each key technology and the existing problems are analyzed furthermore.The future development direction is summarized,which can provide some refe-rences for the design and application realization of in-plane morphing wings.
分 类 号:V224[航空宇航科学与技术—飞行器设计]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:3.148.109.137