Reverse velocity jet tamper disrupter enhancer
View Patent ↗Provided herein are fluid jet enhancement adapters for use with a propellant driven disrupter. The adapter may comprise: a first end operably connected to a muzzle end of a propellant driven disrupter barrel and a second end, wherein a longitudinal region extends between the first end and the second end. The longitudinal region has: a longitudinal region inner surface that defines a longitudinal region lumen; a longitudinal region outer surface opposably facing the longitudinal region inner surface, with a longitudinal region wall having a wall thickness that separates the longitudinal region inner surface from the longitudinal region outer surface. The longitudinal region lumen has a first end inner diameter that is substantially equivalent to a muzzle inner diameter. The longitudinal region wall forms a continuous surface that radially isolates the longitudinal region lumen from a surrounding environment.
1. A method comprising the steps of:
filling a proximal portion of a disrupter barrel with a liquid projectile so that a distal portion of the disrupter barrel is without the liquid projectile;
plugging a distal end of the liquid projectile by introducing a ram rod into the disrupter barrel to displace a desired amount of liquid projectile; and
propelling the liquid projectile out of the barrel, in a direction toward a target.
2. The method of claim 1 , wherein the distal portion of the disrupter barrel without the liquid projectile has a length that is less than or equal to 50% of a disrupter barrel length.
3. The method of claim 1 , wherein the distal portion of the disrupter barrel without the liquid has a length between 5% and 50% of a disrupter barrel length.
4. The method of claim 3 , wherein the disrupter barrel length is 21.75″.
5. The method of claim 1 , wherein the liquid projectile is encapsulated within a cylindrical container having a diameter configured to provide a tight fit in the disrupter barrel.
6. The method of claim 5 , wherein the liquid projectile comprises solid particles suspended in a liquid.
7. The method of claim 1 , wherein the distal portion of the disrupter barrel without the liquid projectile increases a velocity of a distal end of the liquid projectile under confinement in the disrupter barrel and decreases a velocity of a proximal end of the liquid projectile under confinement in the disrupter barrel compared to an equivalent barrel filled with an equivalent liquid projectile.
8. The method of claim 1 , further comprising the step of exerting a Venturi effect on the liquid projectile by providing a taper in the disrupter barrel, thereby increasing average jet velocity and jet length of the liquid projectile exiting the disrupter barrel.
9. The method of claim 1 , wherein the introducing the ram rod step further comprises seating a muzzle plug at the distal end of the liquid projectile.
10. The method of claim 1 , wherein the ram rod has a user-adjustable length to provide a desired liquid projectile length in the disrupter barrel.
11. The method of claim 10 , wherein the ram rod comprises a plurality of sections, with adjacent sections telescopingly connected to each other.
12. The method of claim 1 , wherein the liquid projectile comprises an encapsulated highly efficient energy transfer (HEET) projectile.
13. The method of claim 1 , wherein said propelling step and said distal portion of the disrupter barrel without the liquid projectile together generate a reduced reverse jet velocity gradient in the propelled fluid, wherein the reduced reverse jet velocity gradient is characterized by a difference between a fluid proximal end velocity and a fluid distal end velocity that is reduced relative to an equivalent disrupter barrel with an equivalent liquid projectile that completely fills the disrupter barrel, thereby improving a fluid jet parameter.
14. The method of claim 13 , wherein the difference in the fluid proximal end velocity and the fluid distal end velocity as the liquid projectile exits the disrupter barrel is within 5% to 20%.
15. The method of claim 13 , wherein the fluid jet parameter is an average jet tip velocity, and the average jet tip velocity is increased by at least 20%.
16. The method of claim 1 , wherein the liquid projectile is water.