Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (19): 30042.doi: 10.7527/S1000-6893.2024.30042
• Reviews • Previous Articles
Bin LI1, Zenan ZHANG2, Fei JIA2, Jian SUN1, Yanju LIU2(), Jinsong LENG1
Received:
2024-01-02
Revised:
2024-01-18
Accepted:
2024-03-04
Online:
2024-03-21
Published:
2024-03-19
Contact:
Yanju LIU
E-mail:yj_liu@hit.edu.cn
CLC Number:
Bin LI, Zenan ZHANG, Fei JIA, Jian SUN, Yanju LIU, Jinsong LENG. Research status and development trend of morphing wingtip technology[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(19): 30042.
Table 1
Technology-benefit analysis of morphing wingtip
研究团队 | 研究方法 | 变量参数 | 研究内容 | 效益 |
---|---|---|---|---|
Guerrero等[ | 数值仿真 | 翼尖倾角翼尖后掠角 机翼攻角 | 升力、阻力系数升阻比 | 阻力减小空气动力学效率提高 |
Friswell等[ | 风洞试验 | 翼尖倾角 | 升力特性机翼表面压力 | 升力增加调节气动载荷分布 |
Castrichini等[ | 数值仿真风洞试验 | 翼尖倾角翼尖后掠角翼尖质量铰链刚度 铰链外张角 | 静态载荷阵风载荷 颤振分析 | 静态翼根负荷减轻动态阵风载荷降低 气动弹性稳定性增强 |
Ajaj[ | 数值仿真 | 翼尖倾角翼尖跨度 铰链外张角 | 静态载荷气动稳定性 | 静态飞行载荷降低翼根弯矩降低 翼根剪切力降低 操控稳定性增强 |
Friswell等[ | 数值仿真风洞试验 | 翼尖倾角 | 滚转、升降和偏航控制 | 替代副翼、升降舵和 方向舵等传统控制面 |
Ajaj等[ | 数值仿真风洞试验 飞行试验 | 翼展长度 飞行速度 | 升阻比静态稳定性 滚转控制 | 空气动力学效率提高替代传统 滚转控制面机动性能提高 |
Mohseni等[ | 风洞试验 粒子图像测速 | 翼尖倾角机翼攻角 | 尖端涡旋升力系数 滚转控制 | 强化滚转控制横向稳定性增强 |
Vos等[ | 飞行试验 | 后缘偏转角 | 滚转控制 | 强化滚转控制 |
Table 2
Classification and research progress of morphing wingtip technology
变形类型 | 研究单位 | 驱动/机构 | 蒙皮 | 应用目的 | 研究进展 | |
---|---|---|---|---|---|---|
面内变形 | 变展长 | 阿联酋大学[ | 齿轮机构 | 刚性蒙皮 | 增升 滚转控制 | Ⅳ |
变展长 | 那不勒斯费德里二世大学[ | 气动 | 柔性蒙皮 | 减阻 | Ⅰ | |
变后掠 | 布朗大学[ | 电机 | 操控性 | Ⅳ | ||
面外变形 | 变倾角 | 波音公司[ | 铰链传动 | 刚性蒙皮 | 减阻 | Ⅴ |
变倾角 | 美国宇航局[ | 形状记忆合金 | 刚性蒙皮 | 减阻 偏航控制 | Ⅳ | |
变倾角 | 斯旺西大学[ | 波纹结构 | 柔性蒙皮 | 减阻增升 | Ⅲ | |
变倾角 | 哈尔滨工业大学[ | 气动蜂窝结构 | 形状记忆聚合物变刚度蒙皮 | 减重 减阻增升 | Ⅱ | |
变倾角 | 康奈尔大学[ | 形状记忆合金 | 柔性蒙皮 | 减阻增升 | Ⅲ | |
变倾角 | 首尔大学[ | 智能软复合材料 | 减阻增升 | Ⅲ | ||
变后缘 | 堪萨斯大学[ | 压电材料 | 柔性蒙皮 | 滚转控制 | Ⅳ | |
变后缘 | 佛罗里达州立大学[ | 压电材料 | 刚性蒙皮 | 降涡 | Ⅳ | |
变前缘 变后缘 | 德国宇航中心[ | 柔顺机构 | 柔性蒙皮 | 减阻增升 操控性 | Ⅲ | |
组合变形 | 六自由度变形 | 瑞尔森大学[ | 变形翼盒 | 刚性蒙皮 | 减阻增升 操控性 | Ⅱ |
变后掠变展长 | 中国航天空气动力技术研究院[ | 电机 | 刚性蒙皮 | 减阻增升 | Ⅲ | |
仿生式变形 | 佐治亚理工学院[ | 减阻增升 | Ⅰ |
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