Modular unmanned aerial vehicle system for adaptable parcel delivery
A modular unmanned aerial vehicle (UAV) system comprises a body module, a rotor module, and a wing module. The body module includes a flight controller and a power distribution device. The body module is releasably attachable to the rotor module or the wing module, and the body module is releasably attachable to the rotor module. The rotor module includes one or more motors and electronic speed controllers (ESCs), while the wing module includes a wing having a flap, elevator, aileron, or rudder. Various UAV configurations can be formed from the body module, the rotor module, and the wing module. Each configuration includes different advantages for flight time, distance, battery life, and payload capacity. A UAV can be configured to a particular configuration to optimize parcel delivery.
1. A modular unmanned aerial vehicle (UAV) system comprising:
a configuration of motors;
a body module comprising a flight controller and a body connection member, wherein the body connection member comprises a first releasable cable connection joint;
a rotor module comprising a first rotor connection member and a rotor connection hub, wherein:
the first rotor connection member comprises a second releasable cable connection joint,
the rotor connection hub is configured to accommodate the configuration of motors for the UAV system,
the body connection member is configured to be removably coupled to the first rotor connection member, and
the configuration of motors comprises a plurality of arms that removably connects to the rotor connection hub to enable a respective motor of the configuration of motors coupled to each arm of the plurality of arms to be automatically identified and enabled by the flight controller; and
a wing module and a plurality of wings, wherein:
the wing module comprises a wing connection member comprising a fourth releasable cable connection joint,
the wing module is configured to accommodate the plurality of wings for the UAV system,
the rotor module comprises a second rotor connection member comprising a third releasable cable connection joint and the wing connection member is configured to be removably coupled to the second rotor connection member,
the plurality of wings is configured to removably connect to the wing connection member to enable the plurality of wings to be automatically identified and enabled by the flight controller, and
the body connection member is configured to be removably coupled to the first rotor connection member and the second rotor connection member is configured to be removably coupled to the wing connection member to connect the first releasable cable connection joint to the second releasable cable connection joint and the third releasable cable connection joint to the fourth releasable cable connection joint to establish communication between the flight controller and the plurality of wings.
2. The UAV system of claim 1 , wherein the plurality of arms for the configuration of motors comprises a unique combination of at least one of a certain number of arms and motors or a certain size of motors.
3. The UAV system of claim 1 , wherein at least one of the body module or the rotor module comprises a battery and the motor for each arm of the plurality of arms is configured to be automatically powered by the battery.
4. The UAV system of claim 1 , wherein the rotor module comprises a plurality of electronic speed controllers, each electronic speed controller of the plurality of electronic speed controllers is paired with an arm of the plurality of arms to control a speed of the motor coupled to the arm.
5. The UAV system of claim 1 , wherein the plurality of wings comprises a unique combination of at least one of a certain number of wings, a certain size of wings, or a certain design of wings.
6. The UAV system of claim 1 , wherein at least one of the body module, the rotor module, or the wing module comprises a battery and the plurality of wings is configured to be automatically powered by the battery.
7. A modular unmanned aerial vehicle (UAV) system comprising:
a configuration of motors
a body module comprising a flight controller and a body connection member; and
a rotor module comprising a rotor connection member and configured to accommodate the configuration of motors for the UAV system, wherein:
the body connection member is configured to be coupled to the rotor connection member so that the rotor module is stacked on top of the body module,
the configuration of motors comprises a plurality of arms that removably connects to the rotor module to enable a respective motor of the configuration of motors coupled to each arm of the plurality of arms to be automatically identified and enabled by the flight controller.
8. The UAV system of claim 7 , wherein the plurality of arms for the configuration of motors comprises a unique combination of at least one of a certain number of arms and motors or a certain size of motors.
9. The UAV system of claim 7 , wherein:
the body module comprises a first releasable cable connection joint,
the rotor module comprises a second releasable cable connection joint, and
the body module is configured to be coupled to the rotor module to connect the first releasable cable connection joint to the second releasable cable connection joint to establish communication between the flight controller and the plurality of arms.
10. The UAV system of claim 7 , wherein the rotor module comprises a plurality of electronic speed controllers, each electronic speed controller of the plurality of electronic speed controllers is paired with an arm of the plurality of arms to control a speed of the motor coupled to the arm.
11. The UAV system of claim 7 further comprising a wing module and a plurality of wings, the wing module configured to accommodate the plurality of wings for the UAV system, wherein:
the wing module is configured to be coupled to the rotor module, and
the plurality of wings removably connects to the wing module to enable the plurality of wings to be automatically identified and enabled by the flight controller.
12. The UAV system of claim 11 , wherein the plurality of wings comprises a unique combination of at least one of a certain number of wings, a certain size of wings, or a certain design of wings.
13. The UAV system of claim 11 , wherein:
the body module comprises a first releasable cable connection joint,
the rotor module comprises a second releasable cable connection joint,
the rotor module comprises a third releasable cable connection joint,
the wing module comprises a fourth releasable cable connection joint, and
the body module is configured to be coupled to the rotor module and the rotor module is configured to be coupled to the wing module to connect the first releasable cable connection joint to the second releasable cable connection joint and the third releasable cable connection joint to the fourth releasable cable connection joint to establish communication between the flight controller and the plurality of wings.
14. A method of assembling a modular unmanned aerial vehicle (UAV) system, the method comprising:
connecting a plurality of arms for a configuration of motors to a rotor module of the UAV system;
coupling a first rotor connection member of the rotor module of the UAV system to a body connection member of a body module of the UAV system to stake the rotor module on top of the body module, wherein:
the body module comprises a flight controller; and
automatically identifying and enabling, by the flight controller, a respective motor of the configuration of motors coupled to each arm of the plurality of arms.
15. The method of claim 14 further comprising:
coupling a second rotor connection member of the rotor module to a wing connection member of a wing module of the UAV system;
coupling a plurality of wings to the wing module, wherein:
the wing module is configured to accommodate the plurality of wings for the UAV system; and
automatically identifying and enabling, by the flight controller, the plurality of wings.