UAV-DELIVERED DEPLOYABLE DESCENT DEVICE

• US 20120152654A1
• Filed: 12/15/2010
• Published: 06/21/2012
• Est. Priority Date: 12/15/2010
• Status: Abandoned Application

• Current Assignee: Robert Marcus
• Original Assignee: Robert Marcus
• Inventors: Marcus, Robert
• Application Number:
  US12/969,421
• Publication Number:
  US 20120152654A1
• Time in Patent Office: Days
• US Class Current: 182/129
• CPC Class Codes: A62B 5/00 Other devices for rescuing from fire ladders E06C
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 10/14 with four distinct rotor axes, e.g. quadcopters
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2101/55 for life-saving or rescue operations; for medical use
• CPC Class Codes: B64U 2101/60 for transporting passengers; for transporting goods other than weapons
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/26 Ducted or shrouded rotors
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 80/86 Land vehicles
• CPC Class Codes: E06C 1/36 Ladders suspendable by hooks or the like ladderhooks E06C7/505
• CPC Class Codes: E06C 1/56 Rope or chain ladders
• CPC Class Codes: E06C 5/26 with non-rigid longitudinal members
• CPC Class Codes: E06C 7/505 Anchors being adapted to fix a ladder to a vertical structure, e.g. ladder hooks
• CPC Class Codes: E06C 9/02 rigidly mounted
• CPC Class Codes: E06C 9/14 with non-rigid longitudinal members, e.g. rope or chain ladders, ladders of the lazy-tongs type

Abstract

An unmanned aerial vehicle (UAV) may be used to deliver a descent system to an elevated location at which people await rescue, such as people trapped in an upper story of a burning building. The UAV may deliver the descent system, attach it to the building, and deploy the descent system. After deployment, the descent system may be tensioned to prevent sway and facilitate descent. Standoffs may be installed or integrated into the descent system to provide for adequate handholds for descending individuals. Various equipment and methods used in such systems are described herein.

Claims

1. A method comprising:

delivering a first deployable descent device to an elevated first location with an unmanned aerial vehicle (UAV), the first deployable descent device having a first end and a second end;

anchoring the first end of the first deployable descent device to a feature at the elevated first location by the UAV; and

deploying the first deployable descent device such that the second end of the first deployable descent device is at a lower altitude than the first end of the first deployable descent device after deployment.

2. The method of claim 1, further comprising:

anchoring the second end of the first deployable descent device to a second location at a lower altitude than the altitude of the elevated first location; and

inducing a tensile load in the first deployable descent device between the first end and the second end in addition to any tensile load attributable to the weight of the first deployable descent device.

3. The method of claim 2, further comprising:

providing two or more standoffs configured to offset the first deployable descent device from a surface across a substantial portion of the first deployable descent device, wherein the surface is located between the elevated first location and the second location; and

offsetting the first deployable descent device from the surface with the standoffs.

4. The method of claim 1, further comprising:

equipping the UAV with a second deployable descent device, the second deployable descent device having a first end and a second end;

delivering the second deployable descent device to the second end of the first deployable descent device with the UAV;

attaching the first end of the second deployable descent device to the second end of the first deployable descent device by the UAV; and

deploying the second deployable descent device such that the second end of the second deployable descent device is at a lower altitude than the first end of the second deployable descent device after deployment.

5. The method of claim 1, further comprising:

retrieving the first deployable descent device from the elevated first location after the first deployable descent device has been anchored to the elevated first location, wherein the retrieving is performed by the UAV.

6. A system comprising:

a first deployable descent device, the first deployable descent device having a first end and a second end; and

an unmanned aerial vehicle (UAV), the UAV configured to provide for delivery of the first deployable descent device to an elevated first location and anchoring of the first end of the first deployable descent device to the elevated first location.

7. The system of claim 6, the UAV further configured to provide for anchoring of the second end of the first deployable descent device to a second location at a lower altitude than the elevated first location.

8. The system of claim 7, the UAV further configured to provide for inducement of a tensile load in the first deployable descent device in addition to any tensile load attributable to the weight of the first deployable descent device.

9. The system of claim 7, further comprising two or more standoffs configured to offset the first deployable descent device from a surface across a substantial portion of the first deployable descent device when the first deployable descent device is anchored to the elevated first location and the second location and wherein the surface is located between the elevated first location and the second location.

10. The system of claim 6, further comprising:

a second deployable descent device, the second deployable descent device having a first end and a second end,

wherein the UAV is further configured to provide for delivery of the second deployable descent device to the second end of the first deployable descent device after the first deployable descent device has been anchored to the elevated first location and for attaching of the first end of the second deployable descent device to the second end of the first deployable descent device.

11. The system of claim 6, wherein the UAV is further configured to provide for deployment of the first deployable descent device after the first deployable descent device has been anchored to the elevated first location.

12. The system of claim 6, wherein the UAV is further configured to retrieve the first deployable descent device after the first deployable descent device has been anchored to the elevated first location.

13. The system of claim 9, wherein the first deployable descent device includes a plurality of rungs and wherein the standoffs comprise radially-symmetric spacers mounted onto selected rungs in the plurality of rungs.

14. The system of claim 13, wherein each radially-symmetric spacer is substantially radially centered on the rung onto which the radially-symmetric spacer is mounted.

15. The system of claim 9, wherein the first deployable descent device comprises two or more risers spanning between the first end and the second end of the first deployable descent device, wherein the standoffs comprise a plurality of rungs, wherein each rung in the plurality of rungs is configured to:

span between the two or more risers,

provide a substantially flat stepping surface substantially normal to the two or more risers when the first deployable descent device is anchored to the elevated first location and the second location, and

offset the two or more risers from the surface when the first deployable descent device is anchored to the elevated first location and the second location.

16. A deployable descent device comprising:

unmanned aerial vehicle (UAV) interface features, wherein the UAV interface features are configured to;

allow the deployable descent device to be removably mounted to a mating delivery interface on a UAV, and

support the deployable descent device during delivery to the elevated first location by the UAV;

two or more risers;

a plurality of rungs, each rung spanning between the two or more risers;

a plurality of standoffs, each standoff connected with a rung or a riser;

a first end; and

a second end,

wherein the first end is configured to be anchored to an elevated first location, and

wherein the second end is configured to be anchored to a second location or connected to a chain of one or more other deployable descent devices sequentially connected with one another.

17. The deployable descent device of claim 16, wherein the standoffs comprise radially-symmetric spacers mounted onto selected rungs in the plurality of rungs, wherein each radially-symmetric spacer is substantially radially centered on the rung onto which the radially-symmetric spacer is mounted.

18. The system of claim 17, wherein each radially-symmetric spacer is substantially radially centered on the rung onto which the radially-symmetric spacer is mounted.

19. The deployable descent device of claim 16, wherein the standoffs include an interface material, the interface material selected from the group including rubbers, adhesives, and adhesive tapes, and wherein the interface material forms contact patches between the standoffs and a surface when the deployable descent device is anchored to an elevated first location and a second location and wherein the surface is located between the elevated first location and the second location.

20. The deployable descent device of claim 16, wherein the each standoff is integrated into the rung with which it is connected, and wherein each rung in the plurality of rungs is configured to:

provide a substantially flat stepping surface substantially normal to the two or more risers when the deployable descent device is anchored to the elevated first location and the second location, and

offset the two or more risers from a surface when the deployable descent device is anchored to the elevated first location and the second location, wherein the surface is located between the elevated first location and the second location.

21. The deployable descent device of claim 16, further comprising one or more tensioning devices, the one or more tensioning devices configured to provide for the inducement of a tensile load in the one or more risers when the deployable descent device is anchored to the elevated first location and the second location, wherein the tensile load is in addition to any tensile load generated due to gravity.