The invention provides a self-adaptive deformable nose aircraft which comprises a deformable nose and a fuselage, main wings are symmetrically arranged on the two sides of the fuselage, an engine is arranged at the tail of the fuselage, side wing modules are arranged at the ends of the main wings, and a first contraction module, a second contraction module and a third contraction module are arranged in the deformable nose in the axial direction of the fuselage. The first shrinkage module, the second shrinkage module and the third shrinkage module are matched with one another to be used for adjusting the outline of the deformable machine head so as to change the airflow layout of the deformable machine head. The aircraft is compact in structure and ingenious in design, the capacity of the aircraft for coping with external medium changes can be improved, it is guaranteed that the overall flight resistance is smaller, and flight is efficient and stable.
本发明提供一种自适应可变形机头飞行器,包括可变形机头和机身,机身的两侧对称设有主翼,机身的尾部设有发动机,主翼的端部设有侧翼模块,可变形机头内沿机身的轴向设有第一收缩模块、第二收缩模块和第三收缩模块,第一收缩模块、第二收缩模块和第三收缩模块相互配合用于调整可变形机头的外形轮廓从而改变可变形机头的气流布局。本发明结构紧凑,设计巧妙,能提高飞行器应对外部介质变化的能力,保证整体的飞行阻力更小,飞行高效稳定。
Self-adaptive deformable nose aircraft
自适应可变形机头飞行器
2024-07-30
Patent
Electronic Resource
Chinese
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