Abstract: A quick-connect fitting for a convertible cargo handling assembly may comprise a fixed portion and a coupling component. The fixed portion may be secured to an aircraft frame structure. The coupling component may be coupled to a removable cargo handling component. The coupling component may be configured to rotate relative to the fixed portion.

Abstract: A cargo handling system includes a conveyance surface; a first power drive unit having a first drive roller, a first restraint device; one or more sensors configured to provide positional data corresponding to a current location of a unit load device on the conveyance surface; and a first power drive unit agent configured for communication with the one or more sensors, the first power drive unit agent configured to selectively activate and deactivate the first drive roller and the first restraint device based on the positional data.

Abstract: A cargo restraint system comprises a plurality of cargo restraint assemblies. Each cargo restraint assembly in the plurality of cargo restraint assemblies may be removably coupled to a cargo deck in various configurations. The plurality of cargo restraint assemblies may be reconfigurable based on a size of a plurality of unit load devices (ULDs) to be loaded and restrained. Each cargo restraint assembly may restrain four or fewer corners of respective ULDs simultaneously.

Abstract: A cargo restraint system comprises a plurality of cargo restraint assemblies. Each cargo restraint assembly in the plurality of cargo restraint assemblies may be removably coupled to a cargo deck in various configurations. The plurality of cargo restraint assemblies may be reconfigurable based on a size of a plurality of unit load devices (ULDs) to be loaded and restrained. Each cargo restraint assembly may restrain four or fewer corners of respective ULDs simultaneously.

Abstract: A quick-connect fitting for a convertible cargo handling assembly may comprise a fixed portion and a coupling component. The fixed portion may be secured to an aircraft frame structure. The coupling component may be coupled to a removable cargo handling component. The coupling component may be configured to rotate relative to the fixed portion.

Abstract: A quick-connect fitting for a convertible cargo handling assembly may comprise a fixed portion and a coupling component. The fixed portion may be secured to an aircraft frame structure. The coupling component may be coupled to a removable cargo handling component. The coupling component may be configured to rotate relative to the fixed portion.

Abstract: A convertible cargo handling assembly may comprise a mat, a fitting, and a removable cargo handling component. The fitting may include a fixed component and a coupling component. The fixed component may be located in an opening defined by the mat. The removable cargo handling component may be located over the mat and removably coupled to the fixed portion of the fitting via a coupling between the coupling component and the fixed component.

Abstract: A tire may comprise a hub and a plurality of discrete traction elements coupled to the hub. Each of the traction elements may comprise a backing plate and an elastomeric material bonded to the backing plate. Circumferentially adjacent traction elements may axially overlap.

Abstract: A cargo handling system may comprise a plurality of trays and a topskin. The plurality of trays may structurally support the topskin. The plurality of trays may be contiguously covered. The plurality of trays may be partially covered by the topskin. At least one of a ball transfer unit (BTU) or a roller assembly may be configured to be coupled to the topskin and/or disposed within a groove of a tray in the plurality of trays.

Abstract: A cargo restraint system comprises a plurality of cargo restraint assemblies. Each cargo restraint assembly in the plurality of cargo restraint assemblies may be removably coupled to a cargo deck in various configurations. The plurality of cargo restraint assemblies may be reconfigurable based on a size of a plurality of unit load devices (ULDs) to be loaded and restrained. Each cargo restraint assembly may restrain four or fewer corners of respective ULDs simultaneously.

Abstract: A cargo handling system includes a conveyance surface; a first power drive unit having a first drive roller; a first restraint device; one or more sensors configured to provide positional data corresponding to a current location of a unit load device on the conveyance surface; and a first power drive unit agent configured for communication with the one or more sensors, the first power drive unit agent configured to selectively activate and deactivate the first drive roller and the first restraint device based on the positional data.

Abstract: A roller assembly comprises a first axle having a first inner shaft and a second axle having a second inner shaft. The roller assembly may further comprise a plurality of roller elements between the first inner shaft and the second inner shaft. The roller assembly may further comprise a roller disposed between a first tension strap and a second tensions strap.

Abstract: A cargo handling system includes a conveyance surface; a first power drive unit having a first drive roller; a first restraint device; one or more sensors configured to provide positional data corresponding to a current location of a unit load device on the conveyance surface; a first power drive unit controller configured for communication with the one or more sensors, the first power drive unit configured to selectively activate and deactivate the first drive roller and the first restraint device based on the positional data and a second power drive unit and a second power drive unit controller configured for communication with the sensor, the second power drive unit controller configured to selectively activate and deactivate a second drive roller based on the positional data.

Abstract: A cargo handling system is disclosed. In various embodiments, the cargo handling system includes a conveyance surface having a tray defining an interior section and a rail section; a power drive unit disposed within the interior section; and a power bus routed along a length of the rail section and configured to supply power to the power drive unit.

Abstract: A quick-connect fitting for a convertible cargo handling assembly may comprise a fixed portion and a coupling component. The fixed portion may be secured to an aircraft frame structure. The coupling component may be coupled to a removable cargo handling component. The coupling component may be configured to rotate relative to the fixed portion.

Abstract: A convertible cargo handling assembly may comprise a mat, a fitting, and a removable cargo handling component. The fitting may include a fixed component and a coupling component. The fixed component may be located in an opening defined by the mat. The removable cargo handling component may be located over the mat and removably coupled to the fixed portion of the fitting via a coupling between the coupling component and the fixed component.

Abstract: A cargo handling system is disclosed. In various embodiments, the cargo handling system includes a conveyance surface; a first power drive unit having a first drive roller; a first restraint device; one or more sensors configured to provide positional data corresponding to a current location of a unit load device on the conveyance surface; and a first power drive unit agent configured for communication with the one or more sensors, the first power drive unit agent configured to selectively activate and deactivate the first drive roller and the first restraint device based on the positional data.

Abstract: A cargo handling system is disclosed. In various embodiments, the cargo handling system includes a conveyance surface having a tray defining an interior section and a rail section; a power drive unit disposed within the interior section; and a power bus routed along a length of the rail section and configured to supply power to the power drive unit.

Abstract: A tire may comprise a hub and a plurality of discrete traction elements coupled to the hub. Each of the traction elements may comprise a backing plate and an elastomeric material bonded to the backing plate. Circumferentially adjacent traction elements may axially overlap.

Abstract: The present disclosure relates to an apparatus to be used in a system that adapts a pallet to cargo handling system. This includes the use of adaptor panels to alter the length of the pallet so that it may conform to a standard pallet length. The present disclosure also relates to a method of use for the adaptor system in applying it to a pallet.