Projectile tail boom with self-locking fin

Patent metadata

Field	Value
Publication number	US-9702673-B1
Application number	US-201414495023-A
Country	US
Kind code	B1
Filing date	Sep 24, 2014
Priority date	Sep 24, 2014
Publication date	Jul 11, 2017
Grant date	Jul 11, 2017

Abstract

A tail boom for a gun-launched projectile includes a boom housing and a cap fixed to a rear end of the boom housing. A piston is translatable in the housing by the force of a compression spring. A plurality of fins are rotatably fixed to the boom housing. Each fin includes a protruding portion that extends into a translation path of the piston. The cap includes a guide bore for the piston stem to maintain alignment of the piston. The piston presses on the protruding portion of the fins, causing the fins to rotate about their hinge points into a deployed position.

First claim

What is claimed is:

1. A tail boom for a gun-launched projectile, comprising:
a boom housing having a central longitudinal axis, a forward end configured to engage a projectile body and a through bore;
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.

2. The tail boom of claim 1 , wherein the forward curved surface of the piston is a hemispherical surface.

3. The tail boom of claim 1 , wherein the boom housing, cap, fins and piston are made of an aluminum alloy.

4. The tail boom of claim 1 , wherein the protruding portion of each fin that extends into the forward translation path of the piston is a curved portion.

5. The tail boom of claim 4 , wherein, in a deployed position of the fins, each fin includes a planar portion parallel to the central longitudinal axis of the boom housing.

6. The tail boom of claim 5 , wherein the piston includes a cylindrical surface that adjoins the forward curved surface.

7. The tail boom of claim 6 , wherein, in the deployed position of the fins, the planar portion of each fin abuts the cylindrical surface of the piston.

8. The tail boom of claim 7 , 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.

9. The tail boom of claim 8 , 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.

10. The tail boom of claim 9 , wherein, in the deployed position of the fins, a trailing portion of each fin abuts the stop surface.

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

12. A tail boom for a gun-launched projectile, comprising:
a boom housing having a central longitudinal axis, a forward end configured to engage a projectile body and a through bore;
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 hemispherical 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 curved portion that extends into a forward translation path of the piston in a stowed position of the fins.

13. The tail boom of claim 12 , wherein the piston includes a cylindrical surface that adjoins the forward curved surface.

14. The tail boom of claim 13 , 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.

15. The tail boom of claim 14 , wherein, in a deployed position of the fins, each fin includes a planar portion parallel to the central longitudinal axis of the boom housing.

16. The tail boom of claim 15 , wherein, in the deployed position of the fins, the planar portion of each fin abuts the cylindrical surface of the piston.

Assignees

• Ginetto Stephen
• Moramarco Andrew
• Mohla Leanne
• Us Army

Inventors

• Ginetto Stephen
• Moramarco Andrew
• Mohla Leanne

Classifications

• F42B10/20 Primary

  deployed by combustion gas pressure, or by pneumatic or hydraulic forces · CPC title

• F42B10/14 Primary

  using fins spread or deployed after launch, e.g. after leaving the barrel · CPC title