초록 ▼

In one embodiment there is provided a radar signature and induced aerodynamic drag minimizing, externally mountable, internally configurable pod structure optimized for internal placement of one or more deployable stores through configuration and optimal kinematic operation of a pod door assembly. T

In one embodiment there is provided a radar signature and induced aerodynamic drag minimizing, externally mountable, internally configurable pod structure optimized for internal placement of one or more deployable stores through configuration and optimal kinematic operation of a pod door assembly. The pod structure has an externally mountable pod housing, a predetermined pod housing cross-sectional configuration optimized to provide a configurable interior volume accommodating multiple different store configurations, and a predetermined pod housing configuration having a cross-sectional configuration optimized to minimize a radar signature and an induced aerodynamic drag. The pod structure further has a pod door assembly integral with the pod housing and having a plurality of pod doors and one or more seal door mechanism assemblies. The pod structure is optimized in kinematic operational combination of the pod doors and seal door mechanism assemblies controlling ejection launch envelopes.

대표청구항 ▼

1. An externally mountable pod structure comprising: an externally mountable pod housing comprising: a configurable interior volume configured to contain one or more deployable stores;a pod housing configuration having a cross-sectional configuration optimized to minimize a radar signature and optim

1. An externally mountable pod structure comprising: an externally mountable pod housing comprising: a configurable interior volume configured to contain one or more deployable stores;a pod housing configuration having a cross-sectional configuration optimized to minimize a radar signature and optimized to minimize an induced aerodynamic drag; and,a pod door assembly integral with the pod housing and comprising a plurality of pod doors comprising at least two main doors and at least two seal doors, and further comprising one or more seal door mechanism assemblies, each seal door mechanism assembly coupling each main door to each seal door, and coupling each main door and each seal door to the pod structure, and when each seal door mechanism assembly is in a closed position, each seal door mechanism assembly holds each seal door against a pod structure skin, wherein the seal door mechanism assemblies operationally linked to the pod doors provide in an open position a clearance independence such that if a store ejector device fails to deploy the one or more deployable stores coupled to the store ejector device, no trapped deployable stores occur within the pod structure. 2. The pod structure of claim 1 wherein the one or more deployable stores comprise a missile, an aerodynamic missile, an air to air missile, an aerial bomb, an air to ground bomb, an extended range air to ground bomb, a small diameter bomb, a miniature aerial vehicle, an unmanned aerial vehicle, a drone, a joint standoff weapon, a joint standoff missile, a micro-satellite, a multi-payload airborne store comprising an expendable electronic counter measure dispenser and a tactical reconnaissance assembly, or a combination thereof. 3. The pod structure of claim 1 further comprising one or more interface elements coupled to an exterior of the pod structure and configured to interface and aid in external mounting of the pod structure to an exterior portion of an aerial vehicle. 4. The pod structure of claim 3 wherein one pod structure is mounted to a centerline pylon on the aerial vehicle. 5. The pod structure of claim 3 wherein one pod structure is mounted to a mid-board pylon under each of two wings of the aerial vehicle. 6. The pod structure of claim 3 further comprising a jettison element coupled to the pod structure and configured to jettison the pod structure from the aerial vehicle. 7. The pod structure of claim 1 wherein each seal door mechanism assembly comprises a crank element coupled to the pod structure, an adjustable pull rod assembly coupled between the crank element and a main door of the pod door assembly, at least one seal door hinge fitting coupled to a seal door of the pod door assembly, and at least two drive links coupling the crank element to the at least one seal door hinge fitting. 8. The pod structure of claim 1 wherein the multiple different store configurations comprise one or more deployable stores and one or more corresponding store ejector devices coupled to the one or more deployable stores. 9. The pod structure of claim 1 wherein the pod structure is configured for coupling to one or more of a door drive system, a pneumatic compressor system, a control system, and a power system. 10. A configurable store stowage and deployment system for an aerial vehicle, the system comprising: an externally mountable, internally configurable pod structure configured for mounting to the aerial vehicle, the pod structure comprising: an externally mountable pod housing comprising: a configurable interior volume configured to contain one or more deployable stores;a pod housing configuration having a cross-sectional configuration optimized to minimize a radar signature and optimized to minimize an induced aerodynamic drag; and,a pod door assembly integral with the pod housing and comprising a plurality of pod doors comprising at least two main doors and at least two seal doors, and further comprising one or more seal door mechanism assemblies, each seal door mechanism assembly coupling each main door to each seal door, and coupling each main door and each seal door to the pod structure, and when each seal door mechanism assembly is in a closed position, each seal door mechanism assembly holds each seal door against a pod structure skin, wherein the seal door mechanism assemblies operationally linked to the pod doors provide in an open position a clearance independence such that if a store ejector device fails to deploy the one or more deployable stores coupled to the store ejector device, no trapped deployable stores occur within the pod structure;a door drive system coupled to the pod structure and configured to drive the pod door assembly;a pneumatic compressor system coupled to the pod structure and configured to deploy one or more deployable stores out of the pod structure;a control system coupled to the pod structure and configured to control operation and deployment of the one or more deployable stores; and,a power system coupled to the pod structure and configured to provide power to the configurable store stowage and deployment system. 11. The system of claim 10 wherein the one or more deployable stores comprise a missile, an aerodynamic missile, an air to air missile, an aerial bomb, an air to ground bomb, an extended range air to ground bomb, a small diameter bomb, miniature aerial vehicle, an unmanned aerial vehicle, a drone, a joint standoff weapon, a joint standoff missile, a micro-satellite, a multi-payload airborne store comprising an expendable electronic counter measure dispenser and a tactical reconnaissance assembly, or a combination. 12. The system of claim 10 wherein the door drive system comprises an energy storage device, a manual drive input, and a drive train comprising a drive unit control valve, a drive unit, one or more door drive shafts, one or more rotary actuators, and a stop module. 13. The system of claim 10 wherein the pneumatic compressor system comprises a hydraulic reservoir and a hydraulic pump. 14. The system of claim 10 wherein the control system comprises an electronic control unit, a computer, and a logical interface, the control system being coupled between a management system on the aerial vehicle managing the one or more deployable stores and the configurable store stowage and deployment system. 15. The system of claim 10 wherein the power system comprises an electrical power system that converts AC (alternating current) power of the aerial vehicle into DC (direct current) of the configurable store stowage and deployment system for use in the door drive system, the pneumatic compressor system, and the one or more deployable stores. 16. A method for minimizing radar signature and induced aerodynamic drag and for optimizing an interior store volume of an externally mountable, internally configurable store stowage and deployment system on an aerial vehicle, the method comprising: providing the externally mountable, internally configurable store stowage and deployment system having a pod structure, the pod structure comprising: an externally mountable pod housing comprising: a configurable interior volume configured to contain one or more deployable stores;a pod housing configuration having a cross-sectional configuration optimized to minimize a radar signature and optimized to minimize an induced aerodynamic drag; and,a pod door assembly integral with the pod housing and comprising a plurality of pod doors comprising at least two main doors and at least two seal doors, each main door being coupled to each respective seal door, and further comprising one or more seal door mechanism assemblies, each seal door mechanism assembly coupling each main door to each seal door, and coupling each main door and each seal door to the pod structure, and when each seal door mechanism assembly is in a closed position, each seal door mechanism assembly holds each seal door against a pod structure skin;installing the one or more deployable stores and one or more corresponding store ejector devices in the configurable interior volume of the pod housing, where the seal door mechanism assemblies operationally linked to the pod doors provide in an open position a clearance independence such that if one store ejector device fails to deploy the one or more deployable stores coupled to the store ejector device, no trapped deployable stores occur within the pod structure; and,mounting to an exterior portion of an aerial vehicle the configurable store stowage and deployment system with the one or more deployable stores installed in the pod structure. 17. The method of claim 16 further comprising reconfiguring the configurable interior volume of the pod housing with a different store configuration. 18. The method of claim 16 further comprising reusing the store stowage and deployment system with a same aerial vehicle or a different aerial vehicle. 19. The method of claim 16 wherein the pod structure is configured for coupling to one or more of a door drive system, an ejector device pneumatic system, a control system, and a power system.