Extendable fins for a tube-launched projectile

• US 8,415,598 B1
• Filed: 12/20/2010
• Issued: 04/09/2013
• Est. Priority Date: 12/20/2010
• Status: Active Grant

• Current Assignee: United States Secretary of the Army
• Original Assignee: The United States Of America As Represented By The Secretary Of The Army
• Inventors: Hollis, Michael, Terhune, Robert
• Primary Examiner(s): Poon, Peter M.
• Assistant Examiner(s): SCHWARZ, TIMOTHY S
• Application Number:
  US12/973,074
• Time in Patent Office: 841 Days
• Field of Search: 244/3.24, 244/3.27, 244/3.28, 244/3.29, 244/49, 244/63, 244/473, 102/400, 102/473, 102/490, 102/517, 102/524, 102/526, 89/146, 89/18
• US Class Current: 244/3.28
• CPC Class Codes: F42B 10/18 using a longitudinally slidable support member
• CPC Class Codes: F42B 10/20 deployed by combustion gas pressure, or by pneumatic or hydraulic forces

Abstract

A stabilizing fin deployment apparatus may include a base assembly for attachment to the rear end of a projectile. The base assembly may include a base, a spacer, a fin mount, a gas cavity and an opening that extends from the rear end of the base to the gas cavity. A retention nut may engage the base and secure the fin mount and spacer to the base. A retention plug may be disposed in the opening in the base assembly. The retention plug may include at least one gas conduit between an outer surface of the retention plug and the gas cavity. A retention bolt may extend through the retention plug and may be fixed to the base. A plurality of fins hubs may be rotatably fixed to the base. A plurality of fins may be translatably connected to the fin hubs. When deployed, the fin hubs may rotate forward and the fins may translate outward far into the airstream.

Claims

1. A projectile, comprising:

a body;

a base assembly fixed to a rear end of the body, the base assembly including a base, a spacer, a fin mount, a gas cavity and an opening extending from a rear end of the base to the gas cavity;

a retention nut engaged with the base wherein the retention nut secures the fin mount and the spacer to the base;

a retention plug disposed in the opening in the base assembly, the retention plug including at least one gas conduit between an outer surface of the retention plug and the gas cavity;

a retention bolt that extends through the retention plug and is fixed to the base;

a plurality of fins hubs rotatably fixed to the base, each fin hub including a yoke; and

a plurality of fins movably connected to respective ones of the plurality of fin hubs, each fin including a slot formed therein, each fin being inserted in the yoke of a respective fin hub and connected to the respective fin hub by fasteners movably disposed with respect to the slot and fixed to the yoke, wherein the plurality of fin hubs and fins have a stowed position and a deployed position.

2. The projectile of claim 1, further comprising a retention disk disposed in openings in each of the plurality of fins, the retention disk being fixed in place by the retention bolt.

3. The projectile of claim 2, wherein the retention disk includes a plurality of slots formed therein and further wherein, when the fins are in the stowed position, a portion of each fin is disposed in a respective one of the retention disk slots.

4. The projectile of claim 1, wherein each slot includes a central portion that is substantially parallel to a longitudinal axis of the projectile when the fins are in the stowed position, and front and rear portions that are substantially perpendicular to the central portion.

5. The projectile of claim 4, wherein, with respect to the longitudinal axis of the projectile, the rear portion of each slot is radially distant from the front portion of each slot.

6. The projectile of claim 4, wherein a number of the fasteners that movably connect each fin to each fin hub is two and further wherein, in the stowed position of the fins, a first of the two fasteners is disposed in the rear portion of the slot and a second of the two fasteners is disposed in the central portion of the slot.

7. The projectile of claim 6, wherein, in a deployed position of the fins, the first of the two fasteners is disposed in the central portion of the slot and the second of the two fasteners is disposed in the front portion of the slot.

8. The projectile of claim 7, further comprising a spring lever disposed in each yoke, the spring lever having one end fixed to the fin hub and a free end.

9. The projectile of claim 8, wherein each fin includes a notch formed on a front surface and further wherein the free end of the spring lever is disposed in the notch when the fin is in the deployed position.

10. The projectile of claim 1, further comprising an obturator groove formed in the base wherein a rear side of the obturator groove is defined by the spacer.

11. A method, comprising:

providing the projectile of claim 8 in a gun tube;

igniting propellant;

filling the gas cavity in the base assembly with gas produced by combustion of the propellant;

when the projectile exits the gun tube, fracturing the retention bolt and moving the retention plug out of the opening in the base assembly; and

moving the fin hubs to the deployed position and translating the fins with respect to the fin hubs.

12. The method of claim 11, wherein moving the fin hubs to the deployed position includes rotating the fin hubs with respect to the fin mount and not translating the fin hubs with respect to the fin mount.

13. The method of claim 12, further comprising, after moving the fin hubs and translating the fins, locking the fin hubs in the deployed position and locking the fins in the deployed position.

14. The method of claim 11, wherein translating the fins includes moving the two fasteners through the slot.

15. A fin deployment apparatus, comprising:

a base assembly including a base, a spacer, a fin mount, a gas cavity and an opening extending from a rear end of the base to the gas cavity;

a retention nut engaged with the base wherein the retention nut secures the fin mount and spacer to the base;

a retention plug disposed in the opening in the base assembly, the retention plug including at least one gas conduit between an outer surface of the retention plug and the gas cavity;

a retention bolt that extends through the retention plug and is fixed to the base;

a plurality of fins hubs rotatably fixed to the base, each fin hub including a yoke; and

a plurality of fins movably connected to respective ones of the plurality of fin hubs, each fin including a slot formed therein, each fin being inserted in the yoke of a respective fin hub and connected to the respective fin hub by fasteners movably disposed with respect to the slot and fixed to the yoke, wherein the plurality of fin hubs and fins have a stowed position and a deployed position.

16. The apparatus of claim 15, further comprising an obturator groove formed in the base wherein a rear side of the obturator groove is defined by the spacer.

17. The apparatus of claim 15, wherein each slot includes a central portion that is substantially parallel to a longitudinal axis of the projectile when the fins are in the stowed position, and front and rear portions that are substantially perpendicular to the central portion.

18. The apparatus of claim 17, wherein, with respect to the longitudinal axis of the projectile, the rear portion of each slot is radially distant from the front portion of each slot.

19. The apparatus of claim 17, wherein a number of the fasteners that movably connect each fin to each fin hub is two and further wherein, in the stowed position of the fins, a first of the two fasteners is disposed in the rear portion of the slot and a second of the two fasteners is disposed in the central portion of the slot.

20. The apparatus of claim 19, wherein, in a deployed position of the fins, the first of the two fasteners is disposed in the central portion of the slot and the second of the two fasteners is disposed in the front portion of the slot.