Clip-on propeller mount
A propulsion unit includes a motor rotor, a clip-in base mount, a clip-in rotor cap, propeller mounts, and propeller blades. The motor rotor spins about a central rotational axis. The clip-in base mount is disposed on the motor rotor. The clip-in rotor cap is shaped to mate with and detachably clip into the clip-in base mount. The propeller mounts are attached to the clip-in rotor cap. The propeller blades each have a proximal base and a distal tip. The proximal base of each propeller blade mounts to a corresponding one of the propeller mounts.
1. A propulsion unit, comprising:
a motor rotor that spins about a central rotational axis;
a clip-in base mount disposed on the motor rotor;
a clip-in rotor cap shaped to mate with and detachably clip into the clip-in base mount;
propeller mounts attached to the clip-in rotor cap; and
propeller blades each having a proximal base and a distal tip, wherein the proximal base of each propeller blade mounts to a corresponding one of the propeller mounts.
2. The propulsion unit of claim 1 , wherein the clip-in base mount includes one or more cam grooves and the clip-in rotor cap includes holding cams that mate to the one or more cam grooves.
3. The propulsion unit of claim 2 , wherein the clip-in rotor cap is attachable to the clip-in base mount by hand without a tool.
4. The propulsion unit of claim 2 , wherein the clip-in rotor cap further includes:
a spring cavity; and
a spring disposed in the spring cavity that asserts a repelling force between the clip-in base mount and the clip-in rotor cap when the clip-in rotor cap is mated to the clip-in base mount.
5. The propulsion unit of claim 2 , wherein the clip-in base mount further comprises:
detents disposed in the one or more cam grooves to provide resistance to a rotational separation of the holding cams from the one or more cam grooves.
6. The propulsion unit of claim 5 , wherein the detents each comprise a beveled stop in the one or more cam grooves.
7. The propulsion unit of claim 6 , wherein a slope direction of the beveled stop along with a direction of the rotational separation of the holding cams from the one or more grooves enables a pop off separation of the clip-in rotor cap and the propeller blades from the motor rotor in an event that a physical object of a threshold mass impacts one or more of the propeller blades when the propeller blades are spinning.
8. The propulsion unit of claim 7 , wherein the one or more cam grooves are disposed along inside edges of the raised alignment ring.
9. The propulsion unit of claim 2 , wherein the clip-in base mount further comprises:
a raised alignment ring extending at least partially around a perimeter of the clip-in base mount.
10. An aerial vehicle, comprising:
an airframe;
propulsion units mounted to the airframe to provide propulsion to the aerial vehicle, wherein one or more of the propulsion units includes:
a motor rotor that spins about a central rotational axis;
a clip-in base mount disposed on the motor rotor;
a clip-in rotor cap shaped to mate with and detachably clip into the clip-in base mount;
propeller mounts attached to the clip-in rotor cap; and
propeller blades each having a proximal base and a distal tip, wherein the proximal base of each propeller blade mounts to a corresponding one of the propeller mounts.
11. The aerial vehicle of claim 10 , wherein the clip-in base mount includes one or more cam grooves and the clip-in rotor cap includes holding cams that mate to the one or more cam grooves.
12. The aerial vehicle of claim 11 , wherein the clip-in rotor cap is attachable to the clip-in base mount by hand without a tool.
13. The aerial vehicle of claim 11 , wherein the clip-in rotor cap further includes:
a spring cavity; and
a spring disposed in the spring cavity that asserts a repelling force between the clip-in base mount and the clip-in rotor cap when the clip-in rotor cap is mated to the clip-in base mount.
14. The aerial vehicle of claim 11 , wherein the clip-in base mount further comprises:
detents disposed in the one or more cam grooves to provide resistance to a rotational separation of the holding cams from the one or more cam grooves.
15. The aerial vehicle of claim 14 , wherein the detents each comprise a beveled stop in the one or more cam grooves.
16. The aerial vehicle of claim 15 , a slope direction of the beveled stop along with a direction of the rotational separation of the holding cams from the one or more grooves enables a pop off separation of the clip-in rotor cap and the propeller blades from the motor rotor in an event that a physical object of a threshold mass impacts one or more of the propeller blades when the propeller blades are spinning.
17. The aerial vehicle of claim 16 , wherein the one or more cam grooves are disposed along inside edges of the raised alignment ring.
18. The aerial vehicle of claim 11 , wherein the clip-in base mount further comprises:
a raised alignment ring extending at least partially around a perimeter of the clip-in base mount.
19. The aerial vehicle of claim 10 , wherein the aerial vehicle comprises a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV) and the propulsion units include horizontal propulsion units mounted to the airframe to provide horizontal propulsion and vertical propulsion units mounted to the airframe to provide vertical propulsion.