Projectile launch apparatus for use in fluid environments

Patent metadata

Field	Value
Publication number	US-12281875-B2
Application number	US-202118252739-A
Country	US
Kind code	B2
Filing date	Nov 11, 2021
Priority date	Nov 16, 2020
Publication date	Apr 22, 2025
Grant date	Apr 22, 2025

Abstract

Projectile launch apparatus (20) for use in a fluid environment. The apparatus (20) comprises a launch tube (21) having a supercavitating projectile (24) with cavitator (29) received within the launch tube (21). A means for generating expulsion gas (not visible) is arranged to provide expulsion gas to propel the projectile (24) from the launch tube (21), with means for bleeding expulsion gas (31, 32) being provided to bleed a portion of expulsion gas around the projectile (24). This allows expulsion gases to contribute to the formation of the gas cavity around the supercavitating projectile (24) as the projectile (24) is launched from the launch tube (21). Particularly suited to the deployment of supercavitating projectiles underwater, such as in underwater mine disposal applications.

First claim

The invention claimed is:

1. Projectile launch apparatus for use in a fluid environment, comprising a launch tube having a closed end and an open end, a supercavitating projectile received between the ends separating the launch tube into a forward section comprising the open end and a rear section comprising the closed end, and gas generation means arranged to provide expulsion gas into the rear section of the launch tube, such that in-use trapped expulsion gases within the rear section generate a pressure increase that acts on the supercavitating projectile to propel the projectile through the open end, wherein the supercavitating projectile comprises a nose section and a tail section, the nose section having a cavitator for generating a gas cavity around the supercavitating projectile when the projectile is launched,
wherein the projectile launch apparatus further comprises means for bleeding expulsion gas around the projectile from the rear section of the launch tube into the forward section and thereby to the open end, such that in-use, expulsion gases can contribute to a formation of the gas cavity around the supercavitating projectile as the projectile is launched through the open end.

2. The projectile launch apparatus of claim 1 , wherein the supercavitating projectile is banded with at least one discrete band to form a bore riding projectile, the at least one discrete band being conformal to an interior surface of the launch tube.

3. The projectile launch apparatus of claim 2 , wherein the supercavitating projectile is banded with at least two discrete bands.

4. The projectile launch apparatus of claim 2 , wherein the bands are formed from Nylon or PTFE.

5. The projectile launch apparatus of claim 2 , wherein the means for bleeding expulsion gas comprises conduits extending through the discrete bands for a flow of expulsion gases from the rear section to the forward section of the launch tube.

6. The projectile launch apparatus of claim 2 , wherein the means for bleeding expulsion gas comprises a clearance gap between an exterior surface of the supercavitating projectile and the interior surface of the launch tube.

7. The projectile launch apparatus of claim 6 , wherein the clearance gap is less than 2 mm.

8. The projectile launch apparatus of claim 6 , wherein the clearance gap is less than or equal to 100 μm between the at least one discrete band and interior surface of the launch tube.

9. The projectile launch apparatus of claim 1 , wherein the means for bleeding expulsion gas comprises a groove in an exterior surface of the supercavitating projectile and/or an interior surface of the launch tube, the groove extending between the rear section and the forward section such that the exterior surface of the supercavitating projectile and interior surface of the launch tube define a channel through which expulsion gases can flow.

10. The projectile launch apparatus of claim 1 , wherein the supercavitating projectile comprises an internal conduit connecting the rear section of the launch tube with the forward section, through which expulsion gases can flow.

11. The projectile launch apparatus of claim 10 , wherein the internal conduit takes the form of a spiral about the major axis of the supercavitating projectile.

12. The projectile launch apparatus of claim 1 , further comprising initiation means for initiating the means for bleeding expulsion gas when the pressure in the rear section of the launch tube exceeds a predetermined threshold pressure value.

13. The projectile launch apparatus of claim 12 , wherein the initiation means comprises a shear band attached to the tail section of the supercavitating projectile.

14. The projectile launch apparatus of claim 12 , wherein the initiation means comprises an internal tapering of the rear section of the launch tube and a conformal tapering of the tail section of the supercavitating projectile.

15. The projectile launch apparatus of claim 1 , wherein the cavitator comprises a plurality of stacked sections increasing in diameter in a nose-to-tail direction.

16. The projectile launch apparatus of claim 15 , wherein each stacked section in the plurality of stacked sections is a cylindrical stacked section.

17. The projectile launch apparatus of claim 16 , wherein the cavitator comprises an annular recess extending around a periphery of an interface between each stacked section.

18. The projectile launch apparatus of claim 1 , further comprising an inflatable bladder having an opening for receiving a gas, the inflatable bladder being releasably mounted to the launch tube and arranged to receive through the opening a portion of the expulsion gas from the gas generation means when the projectile launch apparatus is in-use, such that the inflatable bladder can be deployed as a marker buoy.

19. The projectile launch apparatus of claim 18 , wherein the opening of the inflatable bladder is arranged to collect expulsion gas exiting the open end of the launch tube when the projectile launch apparatus is in use.

20. The projectile launch apparatus of claim 18 , wherein the buoy is attached to the launch tube or supercavitating projectile using rope or wire means.

21. The projectile launch apparatus of claim 1 , wherein the supercavitating projectile further comprises decoupling means for rotationally decoupling the nose section from the tail section.

22. A torpedo comprising the projectile launch apparatus of claim 1 .

23. The torpedo of claim 22 comprising a plurality of projectile launch apparatuses.

24. A method of launching a supercavitating projectile in a fluid environment, the method comprising:
(a) Locating the projectile launch apparatus of claim 1 in a fluid environment;
(b) Initiating the gas generation means to provide expulsion gas into the rear section of the launch tube;
(c) Bleeding expulsion gas around the projectile from the rear section of the launch tube into the forward section of the launch tube and thereby to the open end; and then
(d) Launching the supercavitating projectile through the open end of the launch tube, such that expulsion gases can contribute to formation of the gas cavity around the supercavitating projectile as the projectile is launched through the open end.

Assignees

• Secr Defence

Inventors

• Rushforth Peter Richard
• Newell David Timothy

Classifications

• F42B19/125

  Torpedoes provided with drag-reducing means (projectiles with drag-reducing means F42B10/38) · CPC title

• F42B17/00

  Rocket torpedoes, i.e. missiles provided with separate propulsion means for movement through air and through water (F42B12/00 takes precedence) · CPC title

• F42B14/02

  Driving bands; Rotating bands (F42B14/04 takes precedence) · CPC title

• F42B10/38

  Range-increasing arrangements (F42B10/34, F42B14/06 {and F42B15/105} take precedence) · CPC title

• F41F3/08

  for marine torpedoes {(F41A23/22 takes precedence)} · CPC title