陈树生1(), 贾苜梁1, 刘衍旭1, 高正红1, 向星皓2
收稿日期:
2023-09-18
修回日期:
2023-09-28
接受日期:
2023-11-03
出版日期:
2024-03-25
发布日期:
2023-11-16
通讯作者:
陈树生
E-mail:sshengchen@nwpu.edu.cn
基金资助:
Shusheng CHEN1(), Muliang JIA1, Yanxu LIU1, Zhenghong GAO1, Xinghao XIANG2
Received:
2023-09-18
Revised:
2023-09-28
Accepted:
2023-11-03
Online:
2024-03-25
Published:
2023-11-16
Contact:
Shusheng CHEN
E-mail:sshengchen@nwpu.edu.cn
Supported by:
摘要:
能够根据任务需求、飞行环境自适应改变外形来达到最佳飞行性能的变体飞行器已成为未来飞行器发展的重要方向之一。综述了变体飞行器变形方式及气动布局设计关键技术研究现状。首先,按照时间发展历程,将变体技术的发展分为简单机械变形、多维度柔性变形2个阶段。其次,按照变体部位和变形方式详细介绍了头部变体、机翼变体、动力装置变体和组合变体方案的发展历程和现状,重点阐述了可变后掠机翼、可变前掠机翼、折叠机翼、伸缩机翼、斜置机翼、连续变弯度机翼等机翼变体方案的研究进展,总结其在不同布局构型上的应用,并分析了各自的气动、操稳特性。之后,归纳了飞行器变体的实现目的,将其分为单域最优变构型、多域融合变构型、一器多能变构型3种。接着,与固定外形飞行器进行对比,梳理了变体飞行器因为变构型的实现而衍生的气动布局与总体协调设计、时变空气动力学效应评估、气动布局方案优化、多学科耦合设计等方面的关键技术难点,重点对变体飞行器动态气动力计算方法和气动优化设计技术的研究进展和现状进行了综述和分析。最后,展望了变体技术未来研究方向和发展前景,面向宽速域和大空域飞行需求,探索可以提高多飞行任务性能的新概念变形方式,建立智能变体设计模型及多学科强耦合一体化设计体系将成为重要发展趋势。
中图分类号:
陈树生, 贾苜梁, 刘衍旭, 高正红, 向星皓. 变体飞行器变形方式及气动布局设计关键技术研究进展[J]. 航空学报, 2024, 45(6): 629595-629595.
Shusheng CHEN, Muliang JIA, Yanxu LIU, Zhenghong GAO, Xinghao XIANG. Deformation modes and key technologies of aerodynamic layout design for morphing aircraft: Review[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 629595-629595.
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