空气动力驱动变体飞展翼飞机
收稿日期: 2025-02-27
修回日期: 2025-03-02
录用日期: 2025-03-05
网络出版日期: 2025-03-15
基金资助
国家自然科学基金(92052203)
Aerodynamics-driven monoplane-biplane morphing aircraft
Received date: 2025-02-27
Revised date: 2025-03-02
Accepted date: 2025-03-05
Online published: 2025-03-15
Supported by
National Natural Science Foundation of China(92052203)
陈海昕 , 冯良韬 , 段玉宇 , 郭钰坤 , 付越 , 潘晨亮 , 周奕杉 . 空气动力驱动变体飞展翼飞机[J]. 航空学报, 2025 , 46(5) : 531905 -531905 . DOI: 10.7527/S1000-6893.2025.31905
A high-aspect-ratio wing is the key to improving the lift-to-drag ratio of an aircraft. However， a high-aspect-ratio wing leads to a large wingspan， which affects the take-off and landing of the aircraft in many aspects， such as runway width， structure safety and crosswind effects. This paper introduces a monoplane-biplane morphing aircraft， which cruises as a monoplane and takes off and lands as a biplane， switching between the two modes during flight. In addition， its morphing does not rely on any active drive mechanism， but relies on ailerons to change lift to drive morphing. This design can change wingspan to a large extent， take into account the different wingspan requirements of take-off， landing and cruising， and save the structure weight， space and complexity of the morphing drive mechanism， thereby improving maintainability. However， as a new morphing mode， this design also brings challenges in many aspects， such as aerodynamic design， multi-body dynamics and control， structural reliability， and experimental verification.
Key words： monoplane-biplane; morphing; aerodynamics-driven; high aspect ratio; aircraft
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