The modularized reconfigurable wide-working-condition aircraft comprises a fuselage, wings, detachable canards, detachable connecting rods, a detachable horizontal tail wing, a detachable undercarriage, an optical pod and a tail rotor, the wings are arranged on the two sides of the fuselage correspondingly, and detachable power rods are arranged on the upper sides of the wings on one side of the fuselage; a detachable power rod is arranged on the upper side of a wing on the other side of the fuselage, three rotor wing modules are arranged below the power rod, a detachable power rod is arranged on the upper side of the wing on the other side of the fuselage, and three rotor wing modules are arranged below the power rod, so that the fuselage layout of a six-rotor-wing structure is formed. The power rod arranged on the upper side of the wing is replaced with an arc-shaped connecting rod after being detached, the detachable horizontal tail is arranged on the topmost portion, and after the undercarriage arranged on the lower side of the fuselage is detached and folded, the aircraft structure is changed, and modular reconstruction is achieved. Mounting and dismounting are carried out through the detachable modules on the upper sides of the wings, and tool-free switching of two aircraft configurations, namely the horizontal vertical aircraft and the catapult-assisted take-off aircraft, is achieved.
本发明公开一种模块化可重构宽工况飞行器,包括机身、机翼、可拆卸鸭翼、可拆卸连杆、可拆卸水平尾翼、可拆卸起落架、光学吊舱和尾桨,机身的两侧分别设置有一个机翼,在机身一侧机翼的上侧设置可拆卸动力杆,动力杆下方分别设置3件旋翼模组,在机身另一侧机翼的上侧设置可拆卸动力杆,动力杆下方分别设置3件旋翼模组,以此形成6旋翼构型的机身布局。设置在机翼上侧的动力杆拆卸后替换成一个弧形连杆,最顶部设置可拆卸水平尾翼,设置在机身下侧的起落架拆卸收起后,飞机构型发生改变,实现了模块化重构。本发明通过机翼上侧的可拆卸模组进行安装拆卸,实现了无工具切换两种飞行器构型,分别为水平垂起飞行器与弹射起飞飞行器。
Modularized reconfigurable wide-working-condition aircraft
模块化可重构宽工况飞行器
07.01.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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