Payload deployment system for a submarine

• US 7,997,224 B2
• Filed: 10/24/2006
• Issued: 08/16/2011
• Est. Priority Date: 10/24/2005
• Status: Active Grant

• Current Assignee: Babcock IP Management (Number One) Limited
• Original Assignee: Babcock Integrated Technology (Korea) Ltd. (Babcock International Group PLC)
• Inventors: Jeffreys, Dale Michael, Clarke, Peter David, Smith, Jeremy William, Owen, Bryan Jeffery
• Primary Examiner(s): Hayes; Bret
• Assistant Examiner(s): TILLMAN, JR, REGINALD S
• Application Number:
  US12/091,198
• Publication Number:
  US 20090158990A1
• Time in Patent Office: 1,757 Days
• Field of Search: 124/57, 124/58, 124/61, 124/71, 42/11.4, 42/54, 89/5, 89/18.09, 89/18.1, 89/18.15, 89/18.16, 89/18.19, 114/238, 114/239, 114/316, 114/319, 244/63
• US Class Current: 114/238
• CPC Class Codes: B63G 8/32 of torpedo-launching means torpedo-launching means per se F41F3/00; of torpedo stores or handlers
• CPC Class Codes: F41F 3/10 from below the surface of the water

Abstract

A payload deployment system for a vessel, such as a submarine, which includes a cable extending between a piston in a piston tube and an ejection element in an ejection tube, wherein the ejection tube is suitable for holding the payload, such as a torpedo. The system is arranged such that movement of the piston in the piston tube causes movement of the cable which, in turn, exerts a force on the ejection element to move it in the ejection tube to eject the payload from the ejection tube.

Claims

1. A payload deployment system for a vessel, the system including:

an ejection tube for holding a payload;

an ejection element in the ejection tube, the ejection element being moveable in the ejection tube and being arranged releasably to engage the payload;

a piston tube containing a piston, being located outside of the ejection tube, and defining a piston chamber on one side of the piston, the piston being moveable in the piston tube;

means for supplying compressed gas or fluid to the piston chamber, thereby to move the piston in the piston tube; and

a cable which extends between the piston and the ejection element, the cable passing through an aperture of the piston tube into the piston chamber; and

wherein the movement of the piston is arranged to cause movement of the cable which causes movement of the ejection element in the ejection tube, thereby to eject the payload from the ejection tube;

wherein the ejection element is moveable in the ejection tube between a rest position, at which the piston chamber is vacant of said compressed gas or fluid, and a deployed position, at which said piston chamber contains said compressed gas or fluid;

wherein the ejection tube includes an opening in the longitudinal surface thereof, which opening defines a fluid flow path between the interior and the exterior of the ejection tube; and

wherein the opening is blocked by a further part of the ejection element when the election element is in the rest position, and is unblocked when the ejection element is moved from the rest position to eject the payload to allow fluid flow between the interior and exterior.

2. A payload deployment system according to claim 1, wherein the cable is fixed to the piston.

3. A payload deployment system according to claim 1, wherein the cable is fixed to the ejection element.

4. A payload deployment system according to claim 1, wherein the cable is fixed to the ejection tube and part of the cable between the piston and the fixing to the ejection tube engages with the ejection element.

5. A payload deployment system according to claim 4, wherein the engagement with the ejection element is via a pulley rotatably mounted on the ejection element.

6. A payload deployment system according to claim 1, wherein the piston tube is fixed relative to the ejection tube.

7. A payload deployment system according to claim 1, including a second opening in the ejection tube and a third opening in the piston tube, which third opening is located on the opposite side of the aperture from the piston, wherein part of the cable passes through the first and third openings.

8. A payload deployment system according to claim 7, including a cable runner located in or adjacent to the second and third openings, wherein part of the cable passes around the cable runner such that the path of the cable is changed by the cable runner, the path of the cable from the ejection element to the second opening in the ejection tube being in the opposite direction from the path of the cable from the third opening in the piston tube to the piston.

9. A payload deployment system according to claim 8, wherein the cable runner is a wheel.

10. A payload deployment system according to claim 1, further including a sealing element in the piston tube through which the cable passes, the sealing element having a profile that conforms with the inner walls of the piston tube, whereby said compressed gas or fluid is deliverable between the sealing element and the piston.

11. A payload deployment system according to claim 1, wherein a part of the ejection element engages the ejection tube and said part has at least one gap therein thereby to define a fluid flow path around the ejection element in the ejection tube.

12. A payload deployment system according to claim 1, wherein the ejection tube includes a retention latch arranged releasably to engage with the payload.

13. A payload deployment system according to claim 12, wherein said retention latch is disengaged from the payload when a duct between said means for supplying compressed gas or fluid and a release mechanism connected to the retention latch contains said compressed gas or fluid.

14. A payload deployment system according to claim 1, wherein a vent is located in the piston tube on the opposite side of the piston from the piston chamber.

15. A payload deployment system according to claim 1, wherein the ejection element is releasably fixed to the walls of the ejection tube via frangible blocks.