Rocket propelled barrier defense system

• US 8,399,816 B2
• Filed: 07/01/2008
• Issued: 03/19/2013
• Est. Priority Date: 01/06/2005
• Status: Active Grant

• Current Assignee: Richard Glasson
• Original Assignee: CPI IP LLC
• Inventors: Glasson, Richard O.
• Primary Examiner(s): GREGORY, BERNARR E
• Application Number:
  US12/165,759
• Publication Number:
  US 20120011996A1
• Time in Patent Office: 1,722 Days
• Field of Search: 244 31- 33, 244/1.TD, 244/1.R, 89/11.1, 89/360.1, 89/361.6, 89/361.7, 89/360.4, 89/361.1, 342 5- 9, 102335-340, 102/347, 102/348, 102/401, 102/402, 102/473, 102/501
• US Class Current: 244/3.1
• CPC Class Codes: F41H 11/04 Aerial barrages
• CPC Class Codes: F41H 13/0006 Ballistically deployed systems for restraining persons or animals, e.g. ballistically deployed nets

Abstract

A system providing a physical-barrier defense against rocket-propelled grenades (RPGs) that is suitable for use on aircraft, ground vehicles and ships. The system includes a propulsion device (for example, a rocket) and a barrier that is attached to the propulsion device by one or more tethers. The barrier includes an inflatable frame. When the propulsion device is launched, an inflator inflates the frame to assume an open state, and the propulsion device pulls the tether and the barrier along a trajectory for intercepting an RPG.

Claims

1. A system for intercepting a projectile comprising:

a propulsion device adapted to be launched to propel itself through air,

a barrier comprising an inflatable frame having a compact deflated state and an open inflated state, said barrier including an inflator which when actuated after the propulsion device is launched inflates the inflatable frame to change from said deflated state to said inflated state, and

at least one tether attaching the barrier to the propulsion device,

wherein the propulsion device when launched pulls the at least one tether and the barrier through the air along a trajectory of the propulsion device for intercepting the projectile.

2. The system of claim 1, wherein the barrier further comprises intercrossing steel cables attached to the inflatable frame.

3. The system of claim 2, wherein the steel cables are welded together at the intercrossing locations.

4. The system of claim 2 wherein the steel cables are at least partially encased in a plastic coating.

5. The system of claim 1 wherein the barrier further comprises strain hardened plastic reinforced by steel cable and attached to the inflatable frame.

6. The system of claim 1 wherein the barrier further comprises a plurality of deflecting panels attached to the inflatable frame, wherein ones of the panels define an air-gap in relation to each other.

7. The system of claim 6 wherein ones of the deflecting panels are arranged to overlap in relation to an oncoming projectile.

8. The system of claim 1 wherein the inflator includes a solid propellant.

9. The system of claim 1, wherein the at least one tether comprises at least one tether affixed to a central area of the barrier and at least another tether affixed proximate to the peripheral area of the barrier.

10. The system of claim 1, wherein the at least one tether comprises a plurality of tethers comprised of an energy absorbing material.

11. The system of claim 1 wherein the inflatable frame is in the compact deflated state and the barrier is folded into a plurality of pleats to surround the propulsion device.

12. The system of claim 1 wherein the inflatable frame is in the compact deflated state and the barrier is folded into a plurality of overlapping flaps to surround the propulsion device in the compact deflated state.

13. A system for intercepting a projectile comprising:

a propulsion device adapted to be launched to propel itself through air,

a barrier comprising an inflatable frame having a compact deflated state and an open inflated state, said barrier including an inflator which when actuated after the propulsion device is launched inflates said inflatable frame to change from said deflated state to said inflated state, and

at least one tether attaching the barrier to the propulsion device,

wherein the propulsion device when launched pulls the at least one tether and the barrier through the air along a trajectory of the propulsion device for intercepting the projectile,

said barrier further comprising at least one shock wave generating device for diverting the intercepted projectile.

14. The system of claim 13 wherein the shock wave generating device is affixed to the barrier.

15. The system of claim 13 wherein the shock wave generating device is an explosive device.

16. The system of claim 13 wherein the shock wave generating device creates an electrical shock.

17. The system of claim 16, comprising at least two tethers, wherein one of the at least two tethers has less flexibility than at least another one of the at least two tethers.

18. A host vehicle having an outer surface and having a system for intercepting a projectile, said system comprising:

a propulsion device,

a launch device for launching the propulsion device, the launch device being attached to the host vehicle, and

a barrier releasably affixed to the outer surface of the host vehicle and attached to the propulsion device by means of at least one tether,

wherein the propulsion device when launched by the launching device pulls the at least one tether and the barrier through the air along a trajectory of the propulsion device for intercepting the projectile.

19. The host vehicle as defined in claim 18 wherein the barrier comprises a mesh barrier that is releasably affixed to one or more exterior sides of the outer surface of the host vehicle.