초록 ▼

Unmanned aerial vehicles and methods for providing the same are disclosed. The unmanned aerial vehicles may have various configurations related to a support frame. The unmanned aerial vehicles may have various configurations with a continuous track for ground propulsion. The unmanned aerial vehicles

Unmanned aerial vehicles and methods for providing the same are disclosed. The unmanned aerial vehicles may have various configurations related to a support frame. The unmanned aerial vehicles may have various configurations with a continuous track for ground propulsion. The unmanned aerial vehicles may have various configurations related to payload clamps.

대표청구항 ▼

1. An unmanned aerial vehicle comprising: a frame portion comprising a first assembly, a second assembly, and a third assembly;two or more air propulsion devices arranged on the first assembly, the air propulsion devices configured to propel the frame portion through the air; andone or more ground p

1. An unmanned aerial vehicle comprising: a frame portion comprising a first assembly, a second assembly, and a third assembly;two or more air propulsion devices arranged on the first assembly, the air propulsion devices configured to propel the frame portion through the air; andone or more ground propulsion devices configured to propel the frame portion along the ground;wherein: the third assembly is disposed between the first assembly and the second assembly;the third assembly is coupled to the first assembly at a location of the first assembly between two of the air propulsion devices on the first assembly;the first assembly comprises a generally rigid frame section that supports the two or more air propulsion devices at a fixed spacing relative to each other;the first assembly has at least one annular shape; andthe two or more air propulsion devices are disposed in at least one opening in the at least one annular shape of the first assembly. 2. The unmanned aerial vehicle of claim 1, wherein the third assembly is substantially perpendicular to the first assembly and the second assembly; andwherein the first assembly and the second assembly are substantially parallel to one another. 3. The unmanned aerial vehicle of claim 2, wherein the third assembly has a longitudinal dimension; andwherein the longitudinal dimension of the third assembly is perpendicular to a first axis on which the air propulsion devices of the first assembly are supported. 4. The unmanned aerial vehicle of claim 2, wherein the third assembly has a longitudinal dimension; andwherein the longitudinal dimension of the third assembly is perpendicular to a second axis on which the air propulsion devices of the second assembly are supported. 5. The unmanned aerial vehicle of claim 1, wherein at least one of the one or more ground propulsion devices is coupled to the first assembly; andwherein at least one of the one or more ground propulsion devices is coupled to the second assembly. 6. The unmanned aerial vehicle of claim 5, further comprising: two or more further air propulsion devices arranged on the second assembly; andthe third assembly is coupled to the second assembly at a location between two of the further air propulsion devices. 7. The unmanned aerial vehicle of claim 6, wherein a first air propulsion device of the two or more air propulsion devices is provided on a first end of the at least one annular shape of the first assembly in a front direction;wherein a second air propulsion device of the two or more air propulsion devices is provided on a second end of the at least one annular shape of the first assembly in a rear direction;wherein a third air propulsion device of the two or more air propulsion devices is provided on a first end of the at least one annular shape of the second assembly in a front direction; andwherein a fourth air propulsion device of the two or more air propulsion devices is provided on a second end of the at least one annular shape of the second assembly in a rear direction. 8. The unmanned aerial vehicle of claim 5, wherein the second assembly has at least one annular shape and wherein the two or more further air propulsion devices are disposed in at least one opening in the at least one annular shape of the second assembly. 9. The unmanned aerial vehicle of claim 8, wherein the at least one of the one or more ground propulsion devices coupled to the first assembly comprises a continuous track disposed around the at least one annular shape of the first assembly; andwherein the at least one of the one or more ground propulsion devices coupled to the second assembly comprises a continuous track disposed around the at least one annular shape of the second assembly. 10. The unmanned aerial vehicle of claim 9, wherein the first assembly is formed in at least a second annular shape on at least the first plane; andwherein the second assembly is formed in at least a second annular shape on at least the second plane. 11. The unmanned aerial vehicle of claim 9, wherein the continuous track of the first assembly is around the two or more air propulsion devices of the first assembly; and the continuous track of the second assembly is around the two or more air propulsion devices of the second assembly. 12. The unmanned aerial vehicle of claim 8, wherein the at least one annular shape of the first assembly and the at least one annular shape of the second assembly are configured to receive a battery inserted through an opening of the respective annular shape of the first assembly and the annular shape of the second assembly. 13. The unmanned aerial vehicle of claim 5, wherein the at least one of the one or more ground propulsion devices coupled to the first assembly comprises a continuous track disposed around the first assembly; andwherein the at least one of the one or more ground propulsion devices coupled to the second assembly comprises a continuous track disposed around the second assembly. 14. The unmanned aerial vehicle of claim 1, wherein the first assembly is attachable to and detachable from the third assembly; andwherein the second assembly is attachable to and detachable from the third assembly. 15. The unmanned aerial vehicle of claim 1, wherein the first assembly is formed as a double wall structure;wherein the second assembly is formed as a double wall structure;wherein the first assembly supports wheels of at least one of the one or more ground propulsion devices between two walls of the double wall structure of the first assembly; andwherein the second assembly supports wheels of at least one of the one or more ground propulsion devices between two walls of the double wall structure of the second assembly. 16. The unmanned aerial vehicle of claim 1, wherein component pieces of the frame assembly are from a single sheet of a rigid source material; andwherein the rigid source material is printed circuit board. 17. The unmanned aerial vehicle of claim 16, wherein one or more of the component pieces of the frame assembly include conductive tracks printed on the pieces; andwherein the conductive tracks provide an electrical connection between at least one of the air propulsion devices and a controller provided as part of the unmanned aerial vehicle. 18. The unmanned aerial vehicle of claim 1, wherein the third assembly is coupled to the second assembly at a location of the second assembly between two additional air propulsion devices on the second assembly. 19. The unmanned aerial vehicle of claim 1, wherein: each of the one or more ground propulsion devices comprises a continuous track configured to move along an annular path having at least one axis;the third assembly has a first dimension and a second dimension, the first dimension of the third assembly being greater than the second dimension of the third assembly; andthe first dimension of the third assembly is transverse to the at least one axis of the annular path. 20. The unmanned aerial vehicle of claim 1, wherein: each of the one or more ground propulsion devices is configured to propel the frame portion in at least one first direction along the ground;the first assembly has a lengthwise dimension extending along the first direction; andthe two or more air propulsion devices are spaced apart along the first direction, and the third assembly being coupled to the first assembly at the location along the first direction, between the spaced apart air propulsion devices. 21. The unmanned aerial vehicle of claim 1, wherein the first assembly comprises a generally rigid frame section that supports the two or more air propulsion devices at a fixed spacing relative to each other, the second assembly comprises a generally rigid frame section that supports two or more air propulsion devices at a fixed spacing relative to each other, and the third assembly is connected to each of the first and second assemblies at a location within a space between the two or more air propulsion devices on each of the first and second assemblies. 22. A method of manufacturing an unmanned aerial vehicle comprising: providing a frame portion that comprises a first assembly, a second assembly, and a third assembly;providing two or more air propulsion devices arranged on the first assembly configured to propel the frame portion through the air; andproviding one or more ground propulsion devices, the one or more ground propulsion devices configured to propel the frame portion along the ground;wherein: the third assembly is disposed between and coupled to the first assembly and the second assembly;the third assembly is coupled to the first assembly at a location of the first assembly between two of the air propulsion devices on the first assembly;the first assembly comprises a generally rigid frame section that supports the two or more air propulsion devices at a fixed spacing relative to each other;the first assembly has at least one annular shape; andthe two or more air propulsion devices are disposed in at least one opening in the at least one annular shape of the first assembly. 23. The method of manufacturing an unmanned aerial vehicle of claim 22, wherein at least one of the one or more ground propulsion devices is coupled to the first assembly;wherein at least one of the one or more ground propulsion devices is coupled to the second assembly;wherein the first assembly is formed in at least one annular shape on at least a first plane; andwherein the second assembly is formed in at least one annular shape on at least a first plane. 24. The method of manufacturing an unmanned aerial vehicle of claim 23, wherein the two or more air propulsion devices are disposed in an opening of the at least one annular shape of the first assembly. 25. The method of manufacturing an unmanned aerial vehicle of claim 22, wherein the at least one of the one or more ground propulsion devices coupled to the first assembly comprises a continuous track disposed around the first assembly. 26. An unmanned aerial vehicle comprising: frame means comprising a first assembly, a second assembly, and a third assembly;air propulsion means comprising two or more air propulsion devices arranged on the first assembly, the air propulsion devices configured to propel the frame means through the air; andground propulsion means for propelling the frame means along the ground;wherein: the third assembly is disposed between the first assembly and the second assembly;the third assembly is coupled to the first assembly at a location of the first assembly between two of the air propulsion means on the first assembly;the first assembly comprises a generally rigid frame section that supports the two or more air propulsion devices at a fixed spacing relative to each otherthe first assembly has at least one annular shape; andthe two or more air propulsion devices are disposed in at least one opening in the at least one annular shape of the first assembly. 27. An unmanned aerial vehicle comprising: a frame portion comprising a first assembly, a second assembly, and a third assembly;two or more air propulsion devices arranged on the first assembly, the air propulsion devices configured to propel the frame portion through the air; andone or more ground propulsion devices configured to propel the frame portion along the ground;wherein: the third assembly is disposed between the first assembly and the second assembly;the third assembly is coupled to the first assembly at a location of the first assembly between two of the air propulsion devices on the first assemblya first propeller of a first air propulsion device of the two or more air propulsion devices on the first assembly defines a first circular area of rotation;a second propeller of a second air propulsion device of the two or more air propulsion devices on the first assembly defines a second circular area of rotation;the location at which the third assembly is coupled to the first assembly is between and outside of the first circular area of rotation and the second circular area of rotationthe first assembly has at least one annular shape; andat least one of the first circular area of rotation or the second circular area of rotation is disposed in at least one opening in the at least one annular shape of the first assembly. 28. An unmanned aerial vehicle comprising: a frame portion comprising a first assembly, a second assembly, and a third assembly;two or more air propulsion devices arranged on the first assembly, the air propulsion devices configured to propel the frame portion through the air; andone or more ground propulsion devices configured to propel the frame portion along the ground;wherein: the third assembly is disposed between the first assembly and the second assembly;the third assembly is coupled to the first assembly at a location of the first assembly between two of the air propulsion devices on the first assemblya first air propulsion device of the two or more air propulsion devices on the first assembly comprises a first propeller guard;a second air propulsion device of the two or more air propulsion devices on the first assembly comprises a second propeller guard; andthe location at which the third assembly is coupled to the first assembly is between the first propeller guard and the second propeller guardthe first assembly has at least one annular shape; andat least one of the first propeller guard or the second propeller guard is disposed in at least one opening in the at least one annular shape of the first assembly. 29. The unmanned aerial vehicle of claim 28, wherein the third assembly contacts one or more of the first propeller guard and the second propeller guard.