Unmanned aerial vehicle including equipment mounted in recessed seat of apex support structure

1. An unmanned aerial vehicle, comprising:

a chassis;

a power supply mounted to the chassis;

a control system operable to receive power from the power supply;

a plurality of arms extending outward from the chassis, wherein each arm comprises:

an arm inner end portion connected to the chassis;

an arm outer end portion opposite the arm inner end portion;

an arm body extending between and connecting the arm inner end portion and the arm outer end portion; and

a rotor mounted to the arm outer end portion, wherein the rotor is in communication with the control system and is operable to generate lift under control of the control system;

a support structure mounted atop the chassis, the support structure comprising a plurality of struts and an apex region, wherein each strut comprises:

a strut outer end portion connected with the arm inner end portion of a corresponding arm of the plurality of arms;

a strut inner end portion connected with the apex region; and

a strut body extending between and connecting the strut outer end portion and the strut inner end portion; and

a ranging-and-detection device mounted to a recessed seat of the apex region and in communication with the control system.

2. The unmanned aerial vehicle of claim 1 , wherein each strut body comprises an opening defined in part by a reinforcing rib.

3. The unmanned aerial vehicle of claim 1 , wherein each strut body is curved to define at least a portion of an arch.

4. The unmanned aerial vehicle of claim 1 , wherein the plurality of struts define a plurality of arches; and

wherein each arch comprises a corresponding pair of struts in which the strut inner end portions of the pair of struts are connected to one another to define the corresponding arch.

5. The unmanned aerial vehicle of claim 1 , wherein the plurality of arms comprises a first arm, a second arm opposite the first arm, a third arm, and a fourth arm opposite the third arm;

wherein the plurality of struts comprises:

a first strut, wherein the strut outer end portion of the first strut is connected with the arm inner end portion of the first arm;

a second strut opposite the first strut, wherein the strut outer end portion of the second strut is connected with the arm inner end portion of the second arm;

a third strut, wherein the strut outer end portion of the third strut is connected with the arm inner end portion of the third arm; and

a fourth strut opposite the third strut, wherein the strut outer end portion of the fourth strut is connected with the arm inner end portion of the fourth arm;

wherein the strut inner end portions of the first strut and the second strut are joined such that the first strut and the second strut form a first arch; and

wherein the strut inner end portions of the third strut and the fourth strut are joined such that the third strut and the fourth strut form a second arch.

6. An unmanned aerial vehicle, comprising:

a chassis;

a power supply mounted to the chassis;

a control system operable to receive power from the power supply;

a plurality of arms extending outward from the chassis;

a plurality of rotors, wherein each rotor is mounted to a corresponding arm of the plurality of arms, and wherein each rotor is in communication with the control system and is operable to generate lift under control of the control system;

a support structure mounted atop the chassis, the support structure comprising a plurality of arches that connect to one another at an apex region of the support structure; and

a ranging-and-detection device positioned in a recessed seat defined by the apex region of the support structure, wherein the ranging-and-detection device is in communication with the control system.

7. The unmanned aerial vehicle of claim 6 , wherein each arch of the plurality of arches is coupled to the chassis at a location at which a corresponding arm of the plurality of arms extends outward from the chassis.

8. The unmanned aerial vehicle of claim 6 , wherein each arch further comprises a plurality of openings and one or more reinforcing ribs.

9. The unmanned aerial vehicle of claim 6 , wherein the plurality of arches comprises:

a first arch having a first apex; and

a second arch having a second apex joined to the first apex; and

wherein the first apex and the second apex at least partially define the apex region.

10. The unmanned aerial vehicle of claim 9 , wherein the first apex and the second apex are positioned in a recessed seat defined by the plurality of arched struts.

11. The unmanned aerial vehicle of claim 6 , further comprising a curved cap covering the support structure.

12. An unmanned aerial vehicle, comprising:

a chassis;

a power supply mounted to the chassis;

a control system operable to receive power from the power supply;

a plurality of arms extending outward from the chassis, each arm extending along a corresponding arm axis;

a plurality of rotors, wherein each rotor is mounted to a corresponding arm of the plurality of arms, and wherein each rotor is in communication with the control system and is operable to generate lift under control of the control system;

a support structure mounted atop the chassis, the support structure comprising a plurality of arches that connect to one another at an apex region of the support structure; and

a ranging-and-detection device positioned in a recessed seat defined by the apex region of the support structure, wherein the ranging-and-detection device is in communication with the control system;

wherein each arch of the plurality of arches is aligned with the arm axis of a corresponding arm of the plurality of arms.

13. The unmanned aerial vehicle of claim 12 , further comprising an electronic component in communication with the control system, wherein the electronic component is seated in a recessed seat of the apex region.

14. The unmanned aerial vehicle of claim 13 , wherein the electronic component comprises a ranging-and-detection device.

15. The unmanned aerial vehicle of claim 12 , wherein a first arm of the plurality of arms is positioned diametrically opposite a second arm of the plurality of arms such that the axes of the first arm and the second arm are aligned.

16. The unmanned aerial vehicle of claim 12 , wherein each arm axis extends through a vertical central axis of the unmanned aerial vehicle.

17. The unmanned aerial vehicle of claim 12 , further comprising a ranging-and-detection device positioned at the apex region.