Hovering aerial vehicle with removable rotor arm assemblies
The invention provides a hovering aerial vehicle with removable rotor arms and protective shrouds. Removing the shrouds reduces the weight of the vehicle and increases flight time. Removing the rotor arms makes the vehicle easier to transport. Removable rotor arms also simplify field repair or replacement of damaged parts.
1. A hovering unmanned aerial vehicle comprising:
a central pod having an externally exposed frame and enclosing a main processor;
a plurality of independent electrically driven rotors, each rotor rigidly mounted at a fixed distance from the center of the vehicle;
a plurality of rotor arm assemblies removably secured to and extending from the frame, each rotor arm assembly including:
an extending rotor arm;
one of the independent electrically driven rotors; and
electrical power and control infrastructure for the rotor; and
conduits for passing electrical power, control signals and information from the pod to each of the rotor arm assemblies.
2. An aerial vehicle comprising:
a central pod;
a set of independent rotor arm assemblies, each rotor arm assembly having a first end connected to the central pod and a second end free of any connection;
a set of mechanisms for connecting the connection end of each rotor arm assembly with the central pod enabling each rotor arm assembly to be independent and detached from the central pod; and
a set of shrouds for protecting the rotor arm assemblies.
3. The aerial vehicle of claim 2 wherein the number of shrouds equals the number of rotor arm assemblies so that the set of shrouds protect each one of the set of independent rotor arm assemblies in a one-to-one relationship.
4. The aerial vehicle of claim 2 wherein the set of shrouds include at least two shrouds.
5. The aerial vehicle of claim 4 wherein each of the at least two shrouds includes shroud interconnect features for connecting the at least two shrouds together.
6. An aerial vehicle comprising:
a central pod comprising a central pod frame and a set of receptacles;
a set of independent rotor arm assemblies, each rotor arm assembly having a first end connected to the central pod and a second end free of any connection;
a set of mechanisms for connecting the connection end of each rotor arm assembly with the central pod enabling each rotor arm assembly to be independent and detached from the central pod;
wherein the set of receptacles are configured to receive the first end of each of the set of independent rotor arm assembles; and
wherein each of the set of independent rotor arm assemblies comprises:
a retainer ring for mating with one of the set of receptacles;
a motor;
a motor basket for housing the motor;
a rotor arm, having the retainer ring located at the first end and connected to the motor basket at the second end; and
a set of rotor blades connected to the motor;
wherein the receptacle and the retainer ring form part of the mechanism.
7. The aerial vehicle of claim 6 wherein each of the set of independent rotor arm assemblies further comprises a support arm connecting the rotor arm assembly to a shroud.
8. The aerial vehicle of claim 2 further including apparatus for mounting the set of shrouds to the central pod.
9. The aerial vehicle of claim 8 wherein the apparatus for mounting the set of shrouds comprises:
a female receiving portion located on the central pod; and
a complementary male protrusion portion located on each of the set of shrouds.
10. The aerial vehicle of claim 1 further comprising a processor for communicating with a remote control to receive operational instructions.
11. The hovering unmanned aerial vehicle of claim 1 further comprising power, control signal and information infrastructure within the pod.
12. The hovering unmanned aerial vehicle of claim 11 wherein the power, control signal and information infrastructure is within the frame.
13. The hovering unmanned aerial vehicle of claim 1 wherein the plurality of rotor arm assemblies comprises 3 to 6 rotor arm assemblies.
14. The hovering unmanned aerial vehicle of claim 13 wherein the plurality of rotor arm assemblies comprises 4 rotor arm assemblies.
15. The hovering unmanned aerial vehicle of claim 14 wherein the 4 rotor arm assemblies are mounted to the central pod at evenly spaced intervals around the outside of the central pod.
16. The hovering unmanned aerial vehicle of claim 1 wherein the axis of each of the independent electrically driven rotors are substantially parallel.
17. The hovering unmanned aerial vehicle of claim 1 wherein the independent electrically driven rotors operate in substantially the same plane.
18. The hovering unmanned aerial vehicle of claim 1 wherein each of the independent electrically driven rotors provides a fixed axis of thrust.
19. The hovering unmanned aerial vehicle of claim 1 wherein
each of the rotor arm assemblies includes:
a connecting end connected to the central pod;
a rotor end free of any connection; and
a motor basket at the rotor end including an electric motor secured to the rotor; and
the frame includes a set of attachment mechanisms at the central pod for connecting the connecting end of each of the rotor arm assemblies with the central pod enabling each of the rotor arm assemblies to be independent and detachable from the central pod.
20. The hovering unmanned aerial vehicle of claim 19 wherein the set of attachment mechanisms includes a respective set of receptacles.
21. The hovering unmanned aerial vehicle of claim 20 wherein each of the rotor arms includes a retainer ring for mating with a respective one of the set of receptacles and the receptacles and the retainer rings form part of the set of mechanisms.
22. The hovering unmanned aerial vehicle of claim 19 wherein the set of attachment mechanisms comprises a snap in mechanism for retaining the rotor arm assemblies in connection to the frame.
23. The hovering unmanned aerial vehicle of claim 19 wherein the set of attachment mechanisms comprises a set of sockets and the connecting end of each of the rotor arm assemblies includes ball plungers for mating with the set of sockets.
24. The hovering unmanned aerial vehicle of claim 23 wherein each socket of the set of sockets comprises a set of ball bearings for retaining and aligning an associated rotor arm assembly.
25. The hovering unmanned aerial vehicle of claim 1 further comprising a payload sensor for intelligence gathering.
26. The hovering unmanned aerial vehicle of claim 1 wherein the rotor arm assemblies are removably secured to the vehicle such that the rotor arm assemblies snap off the central pod in response to an outside force that would otherwise cause damage.