Frangible tail boom for projectile

• US 9,470,491 B1
• Filed: 09/25/2014
• Issued: 10/18/2016
• Est. Priority Date: 09/25/2014
• 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: Ginetto, Stephen, Moramarco, Andrew, Mohla, Leanne
• Primary Examiner(s): Benedik, Justin
• Application Number:
  US14/496,150
• Time in Patent Office: 754 Days
• US Class Current: 1/1
• CPC Class Codes: F42B 10/14 using fins spread or deployed after launch, e.g. after leaving the barrel
• CPC Class Codes: F42B 8/14 disintegrating in flight or upon impact

Abstract

A frangible tail boom for a gun-launched projectile includes a tail boom housing having a forward end configured to engage a projectile body and a through bore. The tail boom housing has forward and rear portions. The forward portion has a frusto-conical shape and an outer diameter that decreases from the forward end toward the rear portion. The forward portion includes a circumferential groove extending from the outer surface radially inward toward the small diameter segment of the through bore.

Claims

1. A frangible tail boom for a gun-launched projectile, comprising:

a tail boom housing having a central longitudinal axis, a forward end configured to engage a projectile body and a through bore;

the tail boom housing having a forward portion and a rear portion, the forward portion having the general shape of a conical frustum, an outer diameter of the forward portion decreasing from the forward end toward the rear portion;

the through bore in the forward portion including a large diameter segment and a small diameter segment located rearward of the large diameter segment;

the forward portion including a circumferential groove extending from an outer surface radially inward toward the small diameter segment of the through bore wherein after the projectile impacts a target the tail boom is designed to fracture at the circumferential groove.

2. The tail boom of claim 1, wherein the circumferential groove has a depth equal to at least one half a radius of the conical frustum at the groove.

3. The tail boom of claim 1, further comprising:

a cap fixed to a rear end of the boom housing, the cap including an outer cylindrical portion that engages a surface of the through bore in the housing and an inner cylindrical portion having a bore therein;

a piston centered on the central longitudinal axis and translatable in the through bore in the boom housing, the piston having a forward curved surface and a stem that extends rearward, the stem being translatable in and engaging a surface of the bore of the inner cylindrical portion of the cap;

a compression spring disposed around the inner cylindrical portion of the cap, one end of the compression spring bearing on the piston and the other end of the compression spring bearing on the cap to bias the piston in a forward direction; and

a plurality of fins rotatably fixed to the boom housing, each fin including a protruding portion that extends into a forward translation path of the piston in a stowed position of the fins.

4. The tail boom of claim 3, wherein the forward curved surface of the piston is a hemispherical surface.

5. The tail boom of claim 3, wherein the protruding portion of each fin that extends into the forward translation path of the piston is a curved portion.

6. The tail boom of claim 5, wherein, in a deployed position of the fins, each fin includes a planar portion parallel to the central longitudinal axis of the boom housing.

7. The tail boom of claim 6, wherein the piston includes a cylindrical surface that adjoins the forward curved surface.

8. The tail boom of claim 7, wherein, in the deployed position of the fins, the planar portion of each fin abuts the cylindrical surface of the piston.

9. The tail boom of claim 8, wherein the through bore of the tail boom housing includes a chamfer that reduces a diameter of the through bore to less than a diameter of the piston, the chamfer being located at an end of the forward translation path of the piston.

10. The tail boom of claim 9, wherein the tail boom housing includes, for each of the plurality of fins, a stop surface that is angled with respect to the central longitudinal axis.

11. The tail boom of claim 10, wherein, in the deployed position of the fins, a trailing portion of each fin abuts the stop surface.

12. A gun-launched projectile including the tail boom of claim 1.

13. A method, comprising:

providing a projectile having the tail boom of claim 1;

launching the projectile;

impacting a target with the projectile;

fracturing the tail boom at the circumferential groove; and

breaking the tail boom away from the projectile.

14. A tail boom for a gun-launched projectile, comprising:

a tail boom housing having a central longitudinal axis, a forward end for engaging a projectile body and a central through bore;

the tail boom housing having forward and rear portions, the forward portion configured in the shape of a conical frustum, an outer diameter of the forward portion decreasing from the forward end toward the rear portion;

the through bore in the forward portion including a first segment and a second segment, the first segment having a larger diameter than the second segment;

the forward portion including a circumferential groove extending from an outer surface radially inward toward the small diameter segment of the through bore wherein the circumferential groove has a depth equal to at least one half a radius of the conical frustum at the groove.

15. The tail boom of claim 14, further comprising:

a cap fixed to a rear end of the boom housing, the cap including an outer cylindrical portion that engages a surface of the through bore in the housing and an inner cylindrical portion having a bore therein;

a piston centered on the central longitudinal axis and translatable in the through bore in the boom housing, the piston having a forward curved surface and a stem that extends rearward, the stem being translatable in and engaging a surface of the bore of the inner cylindrical portion of the cap;

a compression spring disposed around the inner cylindrical portion of the cap, one end of the compression spring bearing on the piston and the other end of the compression spring bearing on the cap to bias the piston in a forward direction; and

a plurality of fins rotatably fixed to the boom housing, each fin including a protruding portion that extends into a forward translation path of the piston in a stowed position of the fins.

16. The tail boom of claim 15, wherein the protruding portion of each fin that extends into the forward translation path of the piston is a curved portion.

17. The tail boom of claim 16, wherein, in a deployed position of the fins, each fin includes a planar portion parallel to the central longitudinal axis of the boom housing.

18. The tail boom of claim 17, wherein the piston includes a cylindrical surface that adjoins the forward curved surface.

19. The tail boom of claim 18, wherein, in the deployed position of the fins, the planar portion of each fin abuts the cylindrical surface of the piston.

20. A gun-launched projectile including the tail boom of claim 19.