IP Library › Granted Patent US 8,413,570
Granted Patent B2
US 8,413,570 · App. 13/118,233 · Granted Apr 9, 2013

Disrupter ejection and recovery system and method therefor

Inventor: F. Richard Langner (Fountain Hills, AZ)
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Quick Facts
Patent No.
US 8,413,570
App. No.
13/118,233
Granted
Apr 9, 2013
Kind
B2
Abstract

An ejection and recovery system for a disrupter barrel has a parachute. A housing having a channel formed there through is provided wherein the disrupter barrel is positioned in the channel. A tube is coupled to the housing for storing the parachute. A lanyard is coupled to the parachute and to the disrupter barrel.

Claims (35)

1. An ejection and recovery system for a provided disrupter barrel, the system comprising:

a parachute;

a housing having a channel formed there through, the disrupter barrel positioned in the channel;

a tube coupled to the housing for storing the parachute; and

a lanyard coupled to the parachute and to the disrupter barrel.

2. An ejection and recovery system for a disrupter barrel in accordance with claim 1 , further comprising a groove formed around a rear section of the disrupter barrel to secure the lanyard to the disrupter barrel.

3. An ejection and recovery system for a disrupter barrel in accordance with claim 1 , further comprising a non-stick coating applied on an interior surface of the channel.

4. An ejection and recovery system for a disrupter barrel in accordance with claim 1 , further comprising a coating of PTFE applied on an interior surface of the channel.

5. An ejection and recovery system for a disrupter barrel in accordance with claim 1 , further comprising attachment devices to secure the disrupter barrel positioned in the channel.

6. An ejection and recovery system for a disrupter barrel in accordance with claim 5 , wherein the attachment devices comprise adjustable tension devices.

7. An ejection and recovery system for a disrupter barrel in accordance with claim 1 , further comprising a mounting device formed on a bottom section of the housing for mounting the housing on a support stand.

8. An ejection and recovery system for a disrupter barrel in accordance with claim 1 , further comprising a rail mount attached to the housing for securing the tube to the housing.

9. An ejection and recovery system for a provided disrupter barrel, the system comprising:

a parachute;

a housing having a channel formed there through, the disrupter barrel positioned in the channel;

a non-stick coating applied on an interior surface of the channel;

a rail mount attached to the housing;

a tube coupled to the rail mount, the tube for holding the parachute; and

an attachment device coupled to the parachute and to the disrupter barrel.

10. An ejection and recovery system for a disrupter barrel in accordance with claim 9 , wherein the attachment device comprises a lanyard.

11. An ejection and recovery system for a disrupter barrel in accordance with claim 10 , further comprising a groove formed around a rear section of the disrupter barrel to secure the lanyard to the disrupter barrel.

12. An ejection and recovery system for a disrupter barrel in accordance with claim 9 , wherein the non-stick coating comprises a coating of PTFE applied on the interior surface of the channel.

13. An ejection and recovery system for a disrupter barrel in accordance with claim 9 , further comprising securing devices to secure the disrupter barrel positioned in the channel.

14. An ejection and recovery system for a disrupter barrel in accordance with claim 13 , wherein the securing devices comprise adjustable tension devices.

15. An ejection and recovery system for a disrupter barrel in accordance with claim 9 , further comprising a mounting device formed on a bottom section of the housing for mounting the housing on a support stand.

16. A system for holding a provided disrupter prior to firing the disrupter, the disrupter includes a barrel, the system comprising:

a housing having a channel through a first side and a second side of the housing, the channel open at the first side and at the second side of the housing, the channel having an axis along a length of the channel from the first side to the second side, the barrel for positioning in the channel, the barrel for extending beyond the first side and the second side of the housing along the axis of the channel;

at least one securing device positioned at least partially in the channel, the at least one securing device for holding the barrel in the channel prior to firing the disrupter;

an aerodynamic brake for limiting travel of the barrel after firing the disrupter, the aerodynamic braking having a stowed position and a deployed position, the aerodynamic brake in the stowed position prior to firing the disrupter; and

a lanyard, the lanyard coupled to the aerodynamic brake and to the barrel, the lanyard for moving the aerodynamic brake from the stowed position to the deployed position responsive to movement of the barrel out of the channel along the axis after firing the disrupter.

17. The system of claim 16 wherein:

the at least one securing device comprises two or more securing devices;

the two or more securing devices are distributed around the channel.

18. The system of claim 16 further comprising a tube coupled to the housing, the tube for holding the aerodynamic brake while in the stowed position.

19. The system of claim 16 wherein the aerodynamic brake comprises a parachute.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 18, 2019
From: LANGNER, F. RICHARD
To: CONCEPT DEVELOPMENT CORPORATION
Reel/Frame 051035/0080 →
Continuity (2)
Provisional Application 61396526 · Jun 1, 2010
Related Publication 20120180644A1 · Jul 19, 2012