US12523455 - Submunition deployment system

The patent describes a payload module for aerial vehicles that efficiently deploys submunition assemblies while maintaining the vehicle’s aerodynamic profile. It features a rotating skin that covers openings post-deployment to restore the outer mold line (OML) of the vehicle.
Claim 1
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. 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.
Google Patents
https://patents.google.com/patent/US12523455
USPTO PDF
https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/12523455