Abstract: An airframe apparatus for attaching and selectively releasing multiple payloads suspended from an aircraft. The airframe apparatus includes a collapsible loading frame that is configured to have a stabilized open position and a collapsed closed position. The loading frame is constructed from a plurality of vertical struts and horizontal struts that are hingedly interconnected at corner assemblies to allow the loading frame to be collapsed. A payload hook is connected to each of the corner assemblies by a universal joint. A plurality of legs are rotatably attached to the loading frame and can be extended below the loading frame to support the payload hooks off the ground during landing of the airframe apparatus. Shock absorbing devices are operatively attached to the legs to absorb the impact of the loading frame against the ground during landing. The airframe apparatus is used as part of a cargo management system for transporting multiple payloads suspended from an aircraft.

Abstract: A cargo management system comprising an airframe suspended from an aircraft by a cable assembly. The airframe includes a loading frame which comprises a plurality of horizontal struts and vertical struts which are interconnected at corner assemblies. A payload hook is connected to each of the corner assemblies by a universal joint. A load cell used in combination with the universal joint assists in weighing the payloads attached to each of the payload hooks. The airframe also includes a hub assembly which includes a hub rigidly mounted to the vertical struts and a spindle rotatably disposed within the hub. A U-bolt is connected to the spindle which in turn can be selectively attached to the cable assembly. As such, the hub and loading frame are freely rotatable relative to the spindle and cable assembly.