The electromagnetic foldable wing mechanism comprises a wing frame, the wing frame comprises a main supporting rod, an auxiliary supporting rod and a wing bone, one end of the main supporting rod is rotationally connected with one end of the auxiliary supporting rod, and the wing bone is connected to the main supporting rod; the wing film covers the wing frame and is respectively connected with the main supporting rod, the auxiliary supporting rod and the wing bone; and the driving assembly comprises a first coil and a second coil, the first coil is connected to the main supporting rod, and the second coil is connected to the auxiliary supporting rod. According to the foldable wing mechanism, the wings can be automatically folded after the aircraft is used, so that the space occupied by the whole aircraft is smaller, the portability of the whole aircraft is improved, and the folded wings are not easy to damage in the transfer process of the aircraft; meanwhile, the whole foldable wing mechanism is simple in structure, low in failure rate, convenient to install and maintain, light in overall weight and capable of meeting the requirement for light weight of the miniature aircraft.
本发明涉及一种用于扑翼微飞行器的电磁式可折叠翼机构及微飞行器,包括机翼架,其包括主支撑杆、副支撑杆和翼骨,主支撑杆的一端与副支撑杆的一端转动连接,翼骨连接于主支撑杆上;翅膜,其覆盖于机翼架上并分别与主支撑杆、副支撑杆及翼骨相连;驱动组件,其包括第一线圈和第二线圈,第一线圈连接于主支撑杆上,第二线圈连接于副支撑杆上。本可折叠翼机构可在飞行器使用完毕后进行机翼的自动折叠收拢,使整个飞行器占用的空间变的更小,提高了整机的便携性,且在飞行器转运的过程中,折叠起来的机翼也更不易发生损坏;同时,整个可折叠翼机构的构造简单,故障率低,安装及维护都较为方便,整体重量轻,能够满足微型飞行器轻量化的要求。
Electromagnetic foldable wing mechanism for flapping-wing micro-aircraft and micro-aircraft
一种用于扑翼微飞行器的电磁式可折叠翼机构及微飞行器
02.07.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
FLAPPING WING DRIVE MECHANISM OF FLAPPING WING-TYPE AIRCRAFT
Europäisches Patentamt | 2022
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