Coupling assembly for a removable propeller
Disclosed is an aerial vehicle. The aerial vehicle may include a removable battery. Various embodiments of removable battery assemblies include a pull-bar battery assembly, a latch battery assembly, and a lever battery assembly. The aerial vehicle may also include a propeller locking mechanism to which propellers may be removably coupled. The propeller locking mechanism may obviate the need for tools for coupling or decoupling propellers to the aerial vehicle. Vents in the arm of the aerial vehicle may provide an air pathway, providing convective cooling for the electronics aerial vehicle.
1. A propeller locking mechanism comprising:
a shaft coupled to a rotor;
a plate including an opening to receive the shaft;
a spring coupled to the shaft at a first end and coupled to the plate at a second end; and
pins extending from the shaft, each pin being structured to fit into a corresponding slot formed on a propeller hub.
2. The propeller locking mechanism of claim 1 , wherein the plate has a toothed surface.
3. The propeller locking mechanism of claim 2 , wherein the toothed surface and a plurality of teeth of the propeller hub interface with each other.
4. The propeller locking mechanism of claim 1 , wherein a plurality of propeller blades are coupled to the propeller hub.
5. The propeller locking mechanism of claim 1 , wherein the propeller hub comprises:
an aperture formed by a first opening at a first end of the propeller hub, a second opening at a second end of the propeller hub, and an internal surface of the propeller hub connecting the first opening to the second opening; and
grooves, each groove formed on the internal surface of the propeller hub, each groove including a first opening at the first end of the propeller hub and a second opening at the second end of the propeller hub.
6. The propeller locking mechanism of claim 5 , wherein the plate is reciprocally coupled to a plurality of teeth extending from the second end of the propeller hub.
7. The propeller locking mechanism of claim 5 , wherein each groove is of sufficient size for the pins to pass through.
8. The propeller locking mechanism of claim 5 , wherein each groove rotates around an axis concentric with the aperture.
9. The propeller locking mechanism of claim 5 , wherein:
the shaft is structured to fit in the aperture; and
the plate is structured to mesh with the second end of the propeller hub.
10. The propeller locking mechanism of claim 1 , wherein the spring is compressed beyond its equilibrium when the propeller locking mechanism and the propeller hub are coupled together.
11. The propeller locking mechanism of claim 1 , wherein the propeller hub is a cylindrical shell.
12. A propeller coupling assembly comprising:
a propeller locking mechanism comprising:
a shaft coupled to a rotor,
a plate including an opening to receive the shaft,
a spring encircling the shaft, the spring being coupled to the shaft at a first end and being coupled to the plate at a second end, and
one or more pins each extending from the shaft; and
a propeller hub structured to couple to the propeller locking mechanism.
13. The propeller coupling assembly of claim 12 , wherein the propeller hub includes:
an aperture formed by a first opening at a first end of the propeller hub, a second opening at a second end of the propeller hub, and an internal surface of the propeller hub connecting the first opening to the second opening;
one or more grooves, each groove formed on the internal surface of the propeller hub, each groove including a first opening at the first end of the propeller hub and a second opening at the second end of the propeller hub; and
one or more slots, each slot formed on the first end of the propeller hub.
14. The propeller coupling assembly of claim 13 , wherein:
each of the one or more pins are structured to fit into a corresponding slot of the one or more slots;
the shaft is structured to fit in the aperture; and
the plate is structured to mesh with the second end of the propeller hub.
15. A propeller comprising:
a plurality of propeller blades; and
a propeller hub coupled to each of the propeller blades, the propeller hub having:
an aperture formed by a first opening at a first end of the propeller hub, a second opening at a second end of the propeller hub, and an internal surface of the propeller hub connecting the first opening to the second opening,
one or more grooves, each groove formed on the internal surface of the propeller hub, each groove including a first opening at the first end of the propeller hub and a second opening at the second end of the propeller hub,
one or more slots, each slot formed on the first end of the propeller hub, each of the one or more slots structured to receive a respective pin, and
a plurality of teeth extending from the second end of the propeller hub, the plurality of teeth structured to couple to a reciprocal toothed plate.
16. The propeller of claim 15 , wherein the internal surface of the propeller hub is formed as an open cylinder surface that includes the one or more grooves.
17. The propeller of claim 15 , wherein respective widths of the one or more grooves are the same of respective widths of the one or more slots.
18. The propeller of claim 15 , wherein the internal surface of the propeller hub is structured to receive a shaft coupled to a rotor.
19. The propeller of claim 15 , wherein each of the one or more grooves rotate around an axis concentric with the aperture.
20. The propeller of claim 15 , wherein the second opening of each of the one or more grooves is directly opposite a respective one of the one or more slots.