The invention relates to a propeller and flight equipment. The propeller comprises a center shaft, a propeller hub, blades, a folding mechanism and a clutch mechanism, the center shaft is suitable for being connected to an output shaft of the rotor motor, the propeller hub is connected to the center shaft and can be driven by the center shaft to rotate, the blades are rotatably connected to the propeller hub, and the folding mechanism is connected between the propeller hub and the blades to control the blades to be unfolded or folded relative to the propeller hub. The clutch mechanism is connected between the propeller hub and the propeller blades, the clutch mechanism comprises a driving part, a first clutch part and a second clutch part, the first clutch part is connected to the driving part, the second clutch part is connected to the folding mechanism, and the first clutch part can be clamped with or separated from the second clutch part under the driving of the driving part. According to the propeller, through the special design of the clutch mechanism, the power of the rotor wing motor is introduced into the folding mechanism, so that the folding mechanism does not need an independent motor, the structure of the propeller is simplified, and the manufacturing cost of the propeller is reduced.
本申请涉及一种螺旋桨以及飞行设备。螺旋桨包括中心轴、桨毂、桨叶、折叠机构以及离合机构,中心轴适于连接于旋翼电机的输出轴,桨毂连接于中心轴,并能够由中心轴驱动而转动,桨叶可转动地连接于桨毂,折叠机构连接于桨毂与桨叶之间,以控制桨叶相对于桨毂展开或收拢,离合机构连接于桨毂与桨叶之间,离合机构包括驱动件、第一离合件以及第二离合件,第一离合件连接于驱动件,第二离合件连接于折叠机构,第一离合件在驱动件的驱动下能够与第二离合件相卡持或脱离。上述螺旋桨通过特殊的离合机构的设计,将旋翼电机的动力引入折叠机构,使折叠机构不需要单独的电机,简化了螺旋桨的结构,降低螺旋桨的制造成本。
Propeller and flight equipment
螺旋桨以及飞行设备
2024-02-13
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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