Locking mechanism of propeller, propeller, motor, power unit and unmanned aerial vehicle
A technology of locking mechanism and locking parts, which is applied in the field of aircraft, can solve the problems such as the propeller is separated from the motor, reduces the portability of the aircraft, and the disassembly and assembly of the propeller and the motor are difficult, achieving the effect of quick disassembly, ensuring practicability, and improving portability
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Embodiment 1
[0057] figure 1 A structural schematic diagram of a locking mechanism of a propeller 1 provided for an embodiment of the present invention Figure 1 ; figure 2 It is a schematic diagram of an exploded structure of a locking mechanism of a propeller provided by an embodiment of the present invention; image 3 A structural schematic diagram of a locking mechanism of a propeller 1 provided for an embodiment of the present invention Figure II ; Figure 4 A schematic cross-sectional view of a locking mechanism of a propeller 1 provided for an embodiment of the present invention Figure 1 ; refer to attached Figure 1-4 It can be seen that this embodiment provides a locking mechanism for the propeller 1 , which is used for detachably locking the propeller 1 on the motor 2 . The propeller 1 includes a first body, and the motor 2 includes a second body. The locking mechanism includes a pressing piece 3 , a first elastic piece 5 , a locking piece 4 , and a second elastic piece ...
Embodiment 2
[0067] On the basis of the first embodiment above, continue to refer to the appended Figure 1-4 It can be seen that the specific structure of the pressing part 3 is not limited in this embodiment, and those skilled in the art can set it according to specific design requirements. More preferably, the pressing part 3 is configured to include: the execution end 301 and the transmission end 302 . The actuating end 301 is used for abutting against the first elastic member 5 , and the driving end 302 is used for directly or indirectly connecting with the locking member 4 .
[0068] When the execution end 301 is pressed, the execution end 301 moves in a direction close to the locking member 4, so that the locking member 4 is in an unlocked state; when the first elastic member 5 provides an elastic restoring force to the pressing member 3, the execution end 301 Move in a direction away from the locking member 4, so that the locking member 4 is in a locked state.
[0069] Wherein, th...
Embodiment 3
[0071] Figure 5 A schematic cross-sectional view of a locking mechanism of a propeller 1 provided for an embodiment of the present invention Figure II ; Figure 6 for image 3 A-A to the sectional schematic diagram; On the basis of the above-mentioned embodiment two, continue to refer to the appended Figure 1-6 It can be seen that, further, an accommodation space 8 for the locking member 4 to slide along the second direction is formed between the transmission end 302 and the first body or between the transmission end 302 and the second body.
[0072] Since the locking member 4 can slide along the second direction, in order to realize the sliding operation of the locking member 4, an accommodating space 8 is provided between the transmission end 302 and the first body or between the transmission end 302 and the second body. The accommodating space 8 is used to realize the sliding operation of the locking member 4 in the second direction, and limit the extent of the slidin...
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