The invention relates to and provides an aircraft aerodynamic configuration with high lift-drag ratio and high storage performance, comprising: an aircraft body in the shape of a regular rectangular box; the rectification front cover is arranged at the front end of the machine body, and the front end of the rectification front cover is conical; the rectification caudal vertebra is arranged at the rear end of the machine body; a vertical stabilizer and a vertical tail rudder surface are arranged in the middle of the top surface of the rectification tail cone and are perpendicular to the top surface of the aircraft body; the vertical stabilizer is arranged along the axis of the body; the vertical fin rudder surface is rotationally arranged at the rear end of the vertical stabilizer; the two groups of lift airfoils are respectively arranged at the front part and the rear part of the top surface of the aircraft body, and the two lift airfoils in each group rotate oppositely on the top surface of the aircraft body to be in a folded state and rotate oppositely to be in an unfolded state. According to the invention, the aircraft body, the rectification front cover and the rectification tail cone adopt modular design, the lift airfoil is rotationally arranged, the lift airfoil of the aircraft can be folded and stored, and meanwhile, the aircraft body avoids a curved surface configuration, so that the processing cost is reduced.
本发明涉及本发明提供一种具有高升阻比和高收纳性的飞行器气动外形,包括:机体,机体呈规则的矩形箱体;整流前罩,设置在机体的前端,整流前罩的前端呈锥形;整流尾椎,设置在机体的后端;整流尾椎的顶面的正中间上设有垂直安定面和垂尾舵面,垂直安定面和垂尾舵面垂直于机体的顶面设置;垂直安定面沿机体轴线设置;垂尾舵面转动设置在垂直安定面的后端;两组升力翼面,分别设置在机体的顶面的前部和后部,每组的两个升力翼面在机体的顶面上相向转动至收纳状态,相背转动至展开状态。本发明,机体和整流前罩及整流尾椎采用模块化设计,升力翼面转动设置,可将飞行器升力翼面进行折叠收纳,同时机体避免了曲面构型,降低了加工成本。
Aircraft aerodynamic configuration with high lift-drag ratio and high storability
具有高升阻比和高收纳性的飞行器气动外形
24.05.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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