Devices and methods for facilitating blast and dispersion mitigation
Containment vessels are adapted to facilitate blast and dispersion mitigation. According to one example, a containment vessel may include at least one containment layer. At least one expansion member may be coupled to the at least one containment layer to apply a force sufficient to expand a perimeter of the containment layer(s) laterally outward. A closure system may be coupled with the containment layer(s), where the closure system is configured to cinch the perimeter of the containment layer(s) around a target object without manual intervention. Unmanned aerial vehicle (UAV) including a containment vessel, as well as methods of making a containment vessel are also disclosed. Other aspects, embodiments, and features are also included.
1. A blast and dispersion mitigation device, comprising:
at least one containment layer;
at least one expansion member comprising a rod forming a hoop shape coupled to the at least one containment layer proximate the perimeter thereof, the at least one expansion member applying a force to the at least one containment layer sufficient to expand a perimeter of the at least one containment layer laterally outward when deployed; and
a closure system configured to cinch the perimeter of the at least one containment layer around a target object without manual intervention.
2. The device of claim 1 , wherein the at least one containment layer comprises at least one containment layer selected from a group of containment layers comprising:
a blast layer;
a non-porous layer; and
a conductive layer.
3. The device of claim 2 , wherein the blast layer comprises:
at least one portion of blast material; and
at least one exhaust section.
4. The device of claim 3 , wherein the blast layer comprises:
a first portion of blast material;
a second portion of blast material;
an exhaust section located between the first portion of blast material and the second portion of blast material; and
at least one cord member coupled to the first portion of blast material and the second portion of blast material, the at least one cord member extending between the first portion of blast material and the second portion of blast material, and extending across the exhaust section.
5. The device of claim 1 , wherein the closure system includes a cinching mechanism that cinches a component coupled proximate the perimeter of the at least one containment layer.
6. The device of claim 5 , wherein the cinching mechanism cinches the rod of the at least one expansion member.
7. The device of claim 5 , wherein the cinching mechanism cinches an end of a cord to tighten the perimeter of the at least one containment layer.
8. An unmanned aerial vehicle (UAV); comprising:
an airframe;
a propulsion system coupled to the airframe;
a netting system coupled to the airframe, the netting system configured to launch a net toward a target; and
a containment vessel separate from the net of the netting system and coupled to the airframe, the containment vessel comprising at least one containment layer selected from a group of containment layers comprising a blast layer, a non-porous layer, and a conductive layer.
9. The UAV of claim 8 , further comprising a tether including a first longitudinal end coupled to the net of the netting system, and a second, opposing longitudinal end coupled to the airframe, wherein the tether passes through an aperture in the containment vessel.
10. The UAV of claim 8 , wherein the at least one containment layer comprises a blast layer comprising:
at least one portion of blast material; and
at least one exhaust section.
11. The UAV of claim 10 , wherein the blast layer comprises:
a first portion of blast material;
a second portion of blast material;
an exhaust section located between the first portion of blast material and the second portion of blast material; and
at least one cord member coupled to the first portion of blast material and the second portion of blast material, the at least one cord member extending between the first portion of blast material and the second portion of blast material, and extending across the exhaust section.
12. The UAV of claim 8 , wherein the containment vessel further comprises:
at least one expansion member coupled to the at least one containment layer, the at least one expansion member applying a force to the at least one containment layer sufficient to expand a perimeter of the at least one containment layer laterally outward when deployed; and
a closure system configured to close the perimeter of the at least one containment layer around a target object without manual intervention.
13. The UAV of claim 12 , wherein the at least one expansion member comprises:
a rod formed into a hoop shape and coupled to the at least one containment layer proximate the perimeter thereof.
14. The UAV of claim 12 , wherein the at least one expansion member comprises:
a plurality of rods coupled to the at least one containment layer, each rod of the plurality of rods extending across a surface of the at least one containment layer.