The invention discloses a bionic aircraft with a folding wing mechanism. The bionic aircraft comprises a fuselage, a left folding wing, a right folding wing, a left folding driving mechanism and a right folding driving mechanism, the left folding wing is rotatably mounted on the left side of the fuselage, the right folding wing is rotatably mounted on the right side of the fuselage, the left folding driving mechanism is mounted on the fuselage and is in transmission connection with the left folding wing, and the right folding driving mechanism is in transmission connection with the right folding wing. And the right folding driving mechanism is mounted on the fuselage and is in transmission connection with the right folding wing. The unfolding degree of the left wing wing and the unfolding degree of the right wing wing are adjusted through the independent left folding driving mechanism and the independent right folding driving mechanism respectively, the wing wings on the two sides do asymmetric folding and unfolding movement, the lift force difference can be generated on the left side and the right side, and therefore left-right rolling flight operation is conducted, and rolling can be conducted in the flapping wing-fixed wing double-flight mode.
本发明公开了一种具有折叠翼翅机构的仿生飞行器。该仿生飞行器包括:机身、左折叠翼翅、右折叠翼翅、左折叠驱动机构和右折叠驱动机构,左折叠翼翅可转动地安装于机身的左侧,右折叠翼翅可转动地安装于机身的右侧,左折叠驱动机构安装于机身且与左折叠翼翅传动连接,右折叠驱动机构安装于机身且与右折叠翼翅传动连接。利用独立的左折叠驱动机构、右折叠驱动机构分别调整左右翼翅的展开程度,使两侧翼翅做非对称的折叠与展开运动,可以使左右两侧产生升力差,从而进行左右滚转飞行操作,且在扑翼‑固定翼双飞行模式均可进行滚转。
Bionic aircraft with folding wing mechanism
具有折叠翼翅机构的仿生飞行器
25.04.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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