Modular Pods for Use with an Unmanned Aerial Vehicle

• US 20120153087A1
• Filed: 08/06/2008
• Published: 06/21/2012
• Est. Priority Date: 08/06/2008
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Collette, Daniel Ross, Helsing, Joseph Scott Jr.
• Application Number:
  US12/186,693
• Publication Number:
  US 20120153087A1
• Time in Patent Office: Days
• US Class Current: 244/23.A
• CPC Class Codes: B64C 2211/00 Modular constructions of airplanes or helicopters
• CPC Class Codes: B64C 27/20 Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 2101/00 UAVs specially adapted for particular uses or applications
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/26 Ducted or shrouded rotors
• CPC Class Codes: B64U 50/12 using turbine engines, e.g. turbojets or turbofans
• CPC Class Codes: B64U 50/14 ducted or shrouded
• CPC Class Codes: B64U 60/55 the legs being also used as ground propulsion
• CPC Class Codes: B64U 70/80 Vertical take-off or landing, e.g. using rockets rotorcrafts B64U10/10; VTOL aircraft B64U10/20
• CPC Class Codes: B64U 80/60 by wearable objects, e.g. garments or helmets

Abstract

A pod for an unmanned aerial vehicle is provided that may be removed and re-attached to the vehicle. The pod comprises an outer shell, within which a variety of payloads may be carried. A first surface on the vehicle frame comprises a plurality of connects or electrical traces. The plurality of attachments are used to removably attach the pods to the first surface. Thus, a wide variety of payloads may be delivered using the same unmanned aerial vehicle, simply by removing and attaching different pods to a fixed vehicle core. These pods may be shaped so as to form part of the vehicle exterior, and when the pods are attached to the frame, they enhance the aerodynamics of the vehicle.

Claims

1. A module for an unmanned air vehicle, the module comprising:

an outer shell, comprising;

an external surface;

an internal surface;

a base, wherein the base comprises a plurality of attachments configured to removably attach the outer shell to a frame of the unmanned air vehicle; and

a leading edge; and

an interior within the outer shell, wherein the interior is configured to contain a payload.

2. The module of claim 1, wherein the leading edge forms a convex curve.

3. The module of claim 1, wherein the outer shell is configured such that when the base is attached to the frame, the internal surface is flush with a duct of the unmanned air vehicle.

7. The module of claim 1, wherein the plurality of attachments comprises gas connects.

8. The module of claim 1, wherein the plurality of attachments comprises electric connects.

9. The module of claim 1, wherein the payload comprises at least one camera.

10. The module of claim 1, wherein the payload comprises fuel.

4-6. -6. (canceled)

11. An unmanned aerial vehicle comprising:

a ducted fan core comprising a duct portion and a plurality of attachments; and

a plurality of payload pods configured to be attached to the ducted fan core via the plurality of attachments, wherein each of the plurality of payload pods comprises;

a base, and

a lip comprising an internal lip portion and an external lip portion,

wherein each payload pod defines a perimeter, and a plurality of cross-sections along the perimeter,

wherein the internal lip portion is curved so as to follow a circumference of the duct portion, and

wherein at least two cross-sections of the plurality of cross-sections have a different shape.

12. The unmanned aerial vehicle of claim 11, wherein at least one pod of the plurality of payload pods further comprises a payload.

13. The unmanned aerial vehicle of claim 11, wherein the plurality of payload pods are configured to be removably attached to the ducted fan core via the plurality of attachments.

14. The unmanned aerial vehicle of claim 11, wherein when at least one pod of the plurality of payload pods is attached to the ducted fan core, the at least one pod forms a portion of an external surface of the unmanned aerial vehicle.

15. The unmanned aerial vehicle of claim 11, wherein each cross-section of each pod of the plurality of payload pods has a lip highlight location comprising an axial height and a location of maximum radial thickness having a radial distance from a center of the unmanned aerial vehicle.

16. The unmanned aerial vehicle of claim 15, wherein, for at least one pod of the plurality of payload pods, the radial distance from the center of the unmanned vehicle varies for the plurality of cross-sections around the perimeter of the at least one pod.

17. The unmanned aerial vehicle of claim 11, wherein the plurality of attachments comprises gas connects.

18. The unmanned aerial vehicle of claim 11, wherein the plurality of attachments comprises at least one of mechanical connects or electric connects.

19. The unmanned aerial vehicle of claim 11, wherein at least one pod of the plurality of payload pods comprises an integrated sensor.

21. The unmanned aerial vehicle of claim 11, wherein when the base of each pod of the plurality of pods is attached to the ducted fan core, an internal surface of the base is flush with the duct portion.

22. The unmanned aerial vehicle of claim 11, wherein an internal surface of each pod of the plurality of pods is shaped so that air flows along the internal surface and strikes the ducted fan core.

20. An unmanned aerial vehicle comprising:

a ducted fan core; and

a plurality of pods, wherein each pod of the plurality of pods comprises;

a base; and

a leading edge having an axial height and a plurality of radial locations having radial distances from a center of the ducted fan core;

wherein when the pods are attached to the ducted fan core, the pods form a circumference around the ducted fan core;

wherein the axial height varies for a plurality of cross-sections of each pod such that when the pods are attached to the ducted fan core, there are a plurality of peaks along the circumference and a plurality of troughs along the circumference; and

wherein the base of each of the plurality of pods is removably attachable to the ducted fan core.

23. The unmanned aerial vehicle of claim 20, wherein the duct fan core comprises a duct wall, and each pod of the plurality of pods comprises a lip comprises an internal lip portion and an external lip portion, wherein when the pod is attached to the duct fan core, the internal lip location is integral with the duct wall.