Baffled-tube ram accelerator

Patent metadata

Field	Value
Publication number	US-10132578-B2
Application number	US-201515517942-A
Country	US
Kind code	B2
Filing date	Oct 7, 2015
Priority date	Oct 8, 2014
Publication date	Nov 20, 2018
Grant date	Nov 20, 2018

Abstract

A baffled ram accelerator system includes a ram accelerator tube with an inner surface and an outer surface and a plurality of baffles disposed on the inner surface. The plurality of baffles forms a sequential series of propellant chambers along the longitudinal axis of the ram accelerator tube. An accelerator gun is also disposed on an input end of the ram accelerator tube, and the accelerator gun is positioned to fire a projectile into the ram accelerator tube.

First claim

What is claimed is:

1. A ram accelerator system, the system comprising:
a ram accelerator tube with an inner surface and an outer surface;
a plurality of baffles including uniformly spaced holes disposed on the inner surface of the ram accelerator tube, wherein the plurality of baffles is disposed to form a sequential series of propellant chambers along the longitudinal axis of the ram accelerator tube, and wherein edges of the uniformly spaced holes have a linear taper; and
an accelerator gun disposed on an input end of the ram accelerator tube, wherein the accelerator gun is positioned to fire a projectile into the ram accelerator tube.

2. The ram accelerator system of claim 1 , wherein the plurality of baffles is arranged linearly along the longitudinal axis of the ram accelerator tube.

3. The ram accelerator system of claim 1 , wherein the plurality of baffles is arranged into a helix along the longitudinal axis of the ram accelerator tube.

4. The ram accelerator system of claim 1 , wherein the ram accelerator tube has an output end opposite the input end, and wherein the plurality of baffles is angled toward the output end.

5. The ram accelerator system of claim 1 , wherein the ram accelerator tube has an output end opposite the input end, and wherein the plurality of baffles is angled toward the input end.

6. The ram accelerator system of claim 1 , further comprising a projectile, wherein the length of the projectile is greater than the distance between two neighboring baffles in the ram accelerator tube.

7. The ram accelerator system of claim 6 , wherein the plurality of baffles in the ram accelerator tube is machined to a diameter such that a combustion process in the ram accelerator tube is contained behind the projectile.

8. The ram accelerator system of claim 1 , wherein the plurality of baffles extends along only a portion of the inner surface of the ram accelerator tube.

9. The ram accelerator system of claim 8 , wherein the plurality of baffles extends from the input end of the ram accelerator tube, opposite an output end of the ram accelerator tube, along only a portion of the inner surface of the ram accelerator tube.

10. The ram accelerator system of claim 8 , wherein the plurality of baffles extends from an output end of the ram accelerator tube, opposite the input end of the ram accelerator tube, along only a portion of the inner surface of the ram accelerator tube.

11. The ram accelerator system of claim 1 , further comprising rails to guide a projectile, wherein the rails are disposed on the inner surface of the ram accelerator tube between adjacent baffles in the plurality of baffles.

12. The ram accelerator system of claim 11 , wherein the projectile includes fins disposed along a periphery of the projectile.

13. The ram accelerator system of claim 1 , wherein the plurality of baffles is cut into the inner surface of the ram accelerator tube.

14. The ram accelerator system of claim 13 , wherein the cuts used to form the plurality of baffles extend from the inner surface of the ram accelerator tube through the outer surface of the ram accelerator tube, and wherein the cuts are capped on the outer surface the ram accelerator tube.

15. A baffled ram accelerator tube, the baffled ram accelerator tube comprising:
a first hollow cylinder; and
a second hollow cylinder, wherein the second hollow cylinder is perforated with uniformly spaced holes along the longitudinal axis of the second hollow cylinder, and wherein the second hollow cylinder is disposed within the first hollow cylinder such that the uniformly spaced holes in the second hollow cylinder are capped by the inner surface of the first hollow cylinder to form the baffles, wherein edges of the uniformly spaced holes have a linear taper.

16. The ram accelerator tube of claim 15 , wherein the uniformly spaced holes are angled with respect to surface normal of the inner surface of the second hollow cylinder.

17. The ram accelerator tube of claim 15 , wherein the uniformly spaced holes are arranged linearly along the longitudinal axis of the second hollow cylinder.

18. The ram accelerator tube of claim 15 , wherein the uniformly spaced holes are arranged into a helix along the longitudinal axis of the second hollow cylinder.

19. The ram accelerator tube of claim 15 , wherein the uniformly spaced holes are noncircular.

20. The ram accelerator tube of claim 15 , wherein the uniformly spaced holes are triangular.

21. A baffled ram accelerator tube, the baffled ram accelerator tube comprising:
a first hollow cylinder; and
a second hollow cylinder, wherein the second hollow cylinder is perforated with uniformly spaced holes along the longitudinal axis of the second hollow cylinder, and wherein the second hollow cylinder is disposed within the first hollow cylinder such that the uniformly spaced holes in the second hollow cylinder are capped by the inner surface of the first hollow cylinder to form the baffles, wherein baffle diameter decreases in the direction of a center of the second hollow cylinder such that the baffles form a saw-tooth structure.

Assignees

• Univ Washington

Inventors

• Knowlen Carl
• Bruckner Adam P
• Higgins Andrew J
• Hansen Viggo

Classifications

• Y02P10/25

  Process efficiency · CPC title

• F41F3/00

  Rocket or torpedo launchers · CPC title

• F41F1/00

  Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons (F41F3/00 takes precedence); Harpoon guns · CPC title

• F41A1/02 Primary

  Hypervelocity missile propulsion using successive means for increasing the propulsive force, e.g. using successively initiated propellant charges arranged along the barrel length; Multistage missile propulsion · CPC title