Abstract: A cargo system for an aircraft may include one or more of the following: a cargo deck configured for the receipt of bulk cargo, the cargo deck including at least one deck panel; and a cargo transport system including a track for moving a cargo container; and at least one floor fixture exposed on the cargo deck, where the cargo transport system includes an installed state and an uninstalled state, the track being secured to the floor fixture when the cargo transport system is in the installed state and the track being displaced from the cargo deck when the cargo transport system is in the uninstalled state.

Abstract: A deck system for cargo compartment may including one or more of the following features: a first deck; a second deck, where at least one of the first deck and the second deck divide the cargo compartment into an upper sub-compartment and a lower sub-compartment; and an actuator that is mechanically coupled to the second deck, where operation of the actuator causes at least a portion of the second deck to move vertically relative to the first deck within the cargo compartment.

Abstract: An anchor device for a cargo securement strap includes a frame configured to engage a mounting track. The anchor device further includes a hook receiver coupled to the frame. The hook receiver is configured to receive a hook of the cargo securement strap. The anchor device further includes a keeper coupled to the frame. The keeper includes a keeper body and at least one keeper finger extending from a side of the keeper body. The keeper is configured to move between a first position and a second position. In the first position, the at least one keeper finger contacts a bolt and the keeper body is positioned to retain the hook. In the second position, the keeper body is positioned to allow for removal of the hook from the hook receiver.

Abstract: A deck system for cargo compartment may including one or more of the following features: a first deck; a second deck, where at least one of the first deck and the second deck divide the cargo compartment into an upper sub-compartment and a lower sub-compartment; and an actuator that is mechanically coupled to the second deck, where operation of the actuator causes at least a portion of the second deck to move vertically relative to the first deck within the cargo compartment.

Abstract: Systems and methods are provided for restraining cargo in a cargo compartment. In one embodiment, the system comprises a bracket having a main plate segment. At least one adapter is coupled to the bracket and dimensioned to be releasably secured to a location within the cargo compartment. A hook is disposed along a portion of the bracket, the hook comprising a receiving space formed between a rear segment, an end segment and a front segment. A portion of cargo is dimensioned to be placed within a portion of the receiving space. The system may include a locking member, wherein the portion of cargo is capable of being inserted into the receiving space when the locking member is in an open state, and wherein the portion of cargo is restrained from forward, rearward and lateral movement in the cargo compartment when the locking member is in a closed state.

Abstract: This disclosure provides a bushing for a captive beam system, and specifically a bushing that extends between a track for a captive beam system and a bracket that slides along the track. In some captive beam systems that have automatic moving capability, the bracket (and therefore the captive beam that is rotatably connected to the bracket) is pulled upward or downward by a force applied thereto either directly or indirectly, and this force may result in some rubbing between the bracket and the track, which introduces the possibility of wear. The bushing is provided as a wear surface to prevent track or bracket wear. The disclosure also provides a tensioning system for an automatically movable captive beam.

Abstract: A motorized horizontal support system may include first and second vertical tracks that are configured to be installed upon opposing walls of a cargo compartment; first and second brackets that each slide along the respective first and second vertical tracks; a horizontal support disposed between and fixed with respect to the first and second brackets, where the horizontal support includes a first inner passageway extending along a length of the horizontal support; a first balance cable extending through the first inner passageway of the horizontal support; a motor operatively engaged with the second bracket, where operation of the motor may cause the first and second brackets to slide upwardly or downwardly along the respective first and second vertical tracks; and a controller with user input capability that may selectively control the operation of the motor.

Abstract: A locking assembly is provided including a frame. The frame includes a slot and a recess positioned at a top portion of the frame. The assembly further includes a handle rotatably coupled to an end of the frame that is opposite the slot. The handle is rotatable between an open position and a closed position. The slot is configured to receive an attachment means. When the attachment means is in the slot and the handle is in the closed position, the handle is positioned in the slot on top of the attachment means such that the attachment means is prevented from moving with respect to the frame. A latch may be mounted to the handle. The latch is slidable between a locked position where a pin extending from the latch engages the recess of the frame and an unlocked position where the pin is positioned outside the recess.

Abstract: A deck system for cargo compartment may including one or more of the following features: a first deck; a second deck, where at least one of the first deck and the second deck divide the cargo compartment into an upper sub-compartment and a lower sub-compartment; and an actuator that is mechanically coupled to the second deck, where operation of the actuator causes at least a portion of the second deck to move vertically relative to the first deck within the cargo compartment.

Abstract: A cargo system for an aircraft may include one or more of the following: a cargo deck configured for the receipt of bulk cargo, the cargo deck including at least one deck panel; and a cargo transport system including a track for moving a cargo container; and at least one floor fixture exposed on the cargo deck, where the cargo transport system includes an installed state and an uninstalled state, the track being secured to the floor fixture when the cargo transport system is in the installed state and the track being displaced from the cargo deck when the cargo transport system is in the uninstalled state.

Abstract: Systems and methods are provided for restraining cargo in a cargo compartment. In one embodiment, the system comprises a first track sub-assembly comprising a vertical track secured to at least one horizontal support member. The at least one horizontal support member is dimensioned to span between a plurality of preexisting vertical logistics posts on a first sidewall of a cargo compartment. In one embodiment, the at least one horizontal support member comprises first and second ends, and a center point positioned halfway between the first and second ends, wherein a central longitudinal axis of the vertical track is offset from the center point of the first horizontal support member by a predetermined distance. A first beam assembly having a first end to assembly is movable along the vertical track and configured to be secured at a predetermined height.

Abstract: A winch system may include a winch bar and a winch. The winch may have a base, a spool that is rotatable relative to the base, and a drive hub fixed to the spool such that when the drive hub rotates, the spool also rotates. The winch bar may include a winch engagement portion at an end of a shaft, where the winch engagement portion includes a protrusion configured to engage a socket of the drive hub, where the winch engagement portion includes a first contact surface for contacting an outer surface of the drive hub, where the winch engagement portion includes a second contact surface for contacting the outer surface of the drive hub, and where the first contact surface is substantially parallel to the second contact surface.

Abstract: Systems and methods are provided for restraining cargo in a cargo compartment. In one embodiment, the system comprises a first track sub-assembly comprising a vertical track secured to at least one horizontal support member. The at least one horizontal support member is dimensioned to span between a plurality of preexisting vertical logistics posts on a first sidewall of a cargo compartment. In one embodiment, the at least one horizontal support member comprises first and second ends, and a center point positioned halfway between the first and second ends, wherein a central longitudinal axis of the vertical track is offset from the center point of the first horizontal support member by a predetermined distance. A first beam assembly having a first end to assembly is movable along the vertical track and configured to be secured at a predetermined height.

Abstract: An anchor device for a cargo securement strap includes a frame configured to engage a mounting track. The anchor device further includes a hook receiver coupled to the frame. The hook receiver is configured to receive a hook of the cargo securement strap. The anchor device further includes a keeper coupled to the frame. The keeper includes a keeper body and at least one keeper finger extending from a side of the keeper body. The keeper is configured to move between a first position and a second position. In the first position, the at least one keeper finger contacts a bolt and the keeper body is positioned to retain the hook. In the second position, the keeper body is positioned to allow for removal of the hook from the hook receiver.

Abstract: A system and method for automatically and remotely adjusting the position of a captive beam is provided. The system includes a motor that moves a bracket along a vertical track, with the bracket supporting an end of the captive beam. The bracket rotatably supports a latch that engages an aperture in a track when aligned therewith to allow track to support the load of the captive beam and the load supported by the captive beam.

Abstract: An anchor device for a cargo securement strap includes a frame configured to engage a mounting track. The anchor device further includes a hook receiver coupled to the frame. The hook receiver is configured to receive a hook of the cargo securement strap. The anchor device further includes a keeper coupled to the frame. The keeper includes a keeper body and at least one keeper finger extending from a side of the keeper body. The keeper is configured to move between a first position and a second position. In the first position, the at least one keeper finger contacts a bolt and the keeper body is positioned to retain the hook. In the second position, the keeper body is positioned to allow for removal of the hook from the hook receiver.

Abstract: A system and method for automatically and remotely adjusting the position of a captive beam is provided. The system includes a motor that moves a bracket along a vertical track, with the bracket supporting an end of the captive beam. The bracket rotatably supports a latch that engages an aperture in a track when aligned therewith to allow track to support the load of the captive beam and the load supported by the captive beam.

Abstract: Systems and methods are provided for restraining cargo in a cargo compartment. In one embodiment, the system comprises a first track sub-assembly comprising a vertical track secured to at least one horizontal support member. The at least one horizontal support member is dimensioned to span between a plurality of preexisting vertical logistics posts on a first sidewall of a cargo compartment. In one embodiment, the at least one horizontal support member comprises first and second ends, and a center point positioned halfway between the first and second ends, wherein a central longitudinal axis of the vertical track is offset from the center point of the first horizontal support member by a predetermined distance. A first beam assembly having a first end to assembly is movable along the vertical track and configured to be secured at a predetermined height.

Abstract: A bulkhead is provided. The bulkhead includes a panel that extends between first and second primary and secondary edges that are perpendicular to each other. The first primary edge includes a plurality of cutouts, and the second primary edge includes a first plurality of fingers and a second plurality of fingers. Each of the first plurality of fingers includes a first tongue extending from a first side of the second primary edge and away from a primary centerline and also includes a first groove extending from a second side of the second primary edge and toward the primary centerline. Each of the second plurality of fingers includes a second tongue extending from the second side of the second primary edge and away from the primary centerline and also includes a second groove extending from the first side of the second primary edge and toward the primary centerline.

Abstract: A bulkhead is provided. The bulkhead includes a panel that extends between first and second primary and secondary edges that are perpendicular to each other. The first primary edge includes a plurality of cutouts, and the second primary edge includes a first plurality of fingers and a second plurality of fingers. Each of the first plurality of fingers includes a first tongue extending from a first side of the second primary edge and away from a primary centerline and also includes a first groove extending from a second side of the second primary edge and toward the primary centerline. Each of the second plurality of fingers includes a second tongue extending from the second side of the second primary edge and away from the primary centerline and also includes a second groove extending from the first side of the second primary edge and toward the primary centerline.