Submunition deployment system

Patent metadata

Field	Value
Publication number	US-12523455-B2
Application number	US-202418731889-A
Country	US
Kind code	B2
Filing date	Jun 3, 2024
Priority date	Jun 3, 2024
Publication date	Jan 13, 2026
Grant date	Jan 13, 2026

Abstract

A payload module for an aerial vehicle stores and deploys one or more submunition assemblies, which provide a portion of the vehicle's OML when stored, in a manner that preserves the aerodynamics of the aerial vehicle post-deployment. Pre-deployment a skin is aligned to a strongback such that the submunition assemblies are exposed through openings in the skin. Post-deployment, the skin rotates to cover any openings in the strongback exposed by the deployment of the submunition assemblies to restore the OML.

First claim

We claim:

1 . A payload module for use with an aerial vehicle, the payload module comprising:
a strongback having a cylindrical shape about an axis, said strongback having at least one opening formed therein; at least one submunition assembly positioned inside the strongback within the at least one opening, each said submunition assembly having a conformal surface, a skin having a cylindrical shape about the axis, said skin having at least one opening and at least one panel formed therein, each of said at least one opening and said at least one panel having sufficient area to cover the at least one opening in the strongback; a bearing assembly configured to allow for rotation of the skin relative to the strongback about the axis; wherein pre-deployment the skin is aligned such that the at least one opening in the strongback and the conformal surface of the submunition positioned therein are exposed through the at least one opening in the skin such that the skin and conformal surface of the submunition assembly complete an outer mold line (OML); a deployment assembly configured to deploy the at least one submunition assembly through the aligned openings in the strongback and skin, and a rotation assembly configured such that once the at least one submunition assembly clears the payload module, the rotation assembly rotates the skin relative to the strongback such that the at least one panel covers the at least one opening in the strongback and exposed surfaces of the strongback and the skin complete the OML.

2 . The payload module of claim 1 , wherein the submunition has a length/width ratio of at least 1:1 where length is measured along the axis.

3 . The payload module of claim 1 , wherein the length/width ratio is at least 2:1.

4 . The payload module of claim 1 , wherein the conformal surface of the at least one submunition assembly extends through the at least one opening in the strongback into the at least one opening in the skin and level with the skin to complete the OML.

5 . The payload module of claim 4 , wherein pre-deployment rotation is prevented by interference of the skin with the conformal surface of the at least one submunition assembly.

6 . The payload module of claim 4 , wherein longitudinal edges of the at least one opening in the skin are configured to interface with the conformal surface of the submunition assembly to complete the OML pre-deployment and to taper to the strongback post-deployment to complete the OML.

7 . The payload module of claim 1 , wherein an outer diameter of the strongback is at least 5 times a thickness of the skin.

8 . The payload module of claim 1 , wherein at least one panel of the strongback is pre-biased with a spring force such that post-deployment and rotation of the skin, the at least one panel moves outward into the at least one opening in the skin to complete the OML.

9 . The payload module of claim 1 ,
wherein the deployment assembly includes at least one spring per submunition assembly positioned and pre-biased to exert an outward force on the submunition assembly and a locking unit to secure the submunition assembly, wherein at deployment the locking unit releases the submunition assembly and the spring exerts the outward force on the submunition to deploy the submunition assembly through the aligned openings in the strongback and skin, and wherein the rotation assembly includes a rotational spring configured to pre-bias rotation of the skin relative to the strongback and rotate the skin once the at least one submunition assembly clears the payload module.

10 . The payload module of claim 9 , wherein the locking unit comprises:
a lock bracket on one end of the submunition assembly positioned forward in the opening in the strongback, said lock bracket including a receptacle; a rod positioned to move into and out of the receptacle; and an actuator configured to move the rod.

11 . The payload module of claim 9 , wherein the deployment assembly comprises:
a hinge bracket positioned aft in the opening in the strongback; a pivot bracket at one end of the submunition assembly below the conformal surface positioned aft in the opening in the strongback to engage the hinge bracket, wherein at deployment, submunition assembly pivots radially outward away from the strongback and separates from the hinge bracket.

12 . The payload module of claim 1 , wherein the at least one submunition assembly comprises:
a container having separable first and second walls that define a volume, at least a portion of one of the first and second walls have an exterior shape that provides the conformal surface of the submunition assembly; a submunition positioned within the volume inside the container; and a mechanism on the container to hold the first and second walls together to secure the volume and upon receipt of a command signal to separate the first and second walls to open the container and release the submunition.

13 . The payload module of claim 12 , wherein said submunition comprising a control unit configured to issue the command signal to the mechanism to open the container and release the submunition.

14 . The payload module of claim 13 , wherein the control unit includes a processor and memory to process data to issue the command signal, wherein any and all processors or memory or data stored in memory or processed by the processor resides only with the submunition.

15 . A payload module for use with an aerial vehicle, the payload module comprising:
a strongback having a cylindrical shape about an axis, said strongback having at least one opening formed therein; at least one submunition assembly positioned inside the strongback within the at least one opening, each said submunition assembly having a conformal surface, a skin having a cylindrical shape about the axis, said skin having at least one opening and at least one panel formed therein, each of said at least one opening and said at least one panel having sufficient area to cover the at least one opening in the strongback; a bearing assembly configured to allow for rotation of the skin relative to the strongback about the axis; wherein pre-deployment the skin is aligned such that the at least one opening in the strongback and the conformal surface of the submunition positioned therein are exposed through the at least one opening in the skin such that the skin and conformal surface of the submunition assembly complete an outer mold line (OML); a deployment assembly including at least one spring per submunition assembly positioned and pre-biased to exert an outward force on the submunition assembly and at least one locking unit to secure the submunition assembly, wherein at deployment the locking unit releases the submunition assembly and the spring exerts the outward force on the submunition assembly to deploy the at least one submunition assembly through the aligned openings in the strongback and skin; and a rotation assembly including a rotational spring configured to pre-bias rotation of the skin relative to the strongback, pre-deployment rotation is prevented by interference of the skin with at least one of the submunition assembly's conformal surface, wherein once the at least one submunition assembly clears the payload module, the rotational spring rotates the skin relative to the strong back such that the at least one panel covers the at least one opening in the strongback and exposed surfaces of the strongback and the skin complete the OML.

16 . The payload module of claim 15 , wherein the deployment assembly comprises:
at least one hinge

Assignees

• Raytheon Co

Inventors

• Macdonald Paul S
• Jones Jaylan S
• Polanco Jessie A
• Burke Shawn P

Classifications

• F42B15/01

  Arrangements thereon for guidance or control ({steering arrangements F42B10/60}; aircraft flight control B64C; guidance systems other than those installed aboard F41G7/00, F41G9/00; locating by use of radio or other waves G01S; flight control in general G05D1/00; computer aspects G06]) · CPC title

• B64D1/06

  Bomb releasing; Bomb doors · CPC title

• B64D1/04

  the articles being explosive, e.g. bombs · CPC title

• F42B10/56

  of parachute {or paraglider} type · CPC title

• F42B12/60

  the submissiles being ejected radially · CPC title