A system for detecting and verifying an environmental anomaly within a shipping container (transported on a transit vehicle having an external transceiver) has wireless sensor-based ID nodes at different locations within the container and multiple command nodes mounted to the container. A first command node is programmatically configured to be operative to detect the sensor data broadcasted from the ID nodes; responsively identify the anomaly based upon the sensor data detected by that command node; and transmit a validation request to another command node. The other command node is configured to be operative to also detect the sensor data broadcasted from the ID nodes; receive the validation request from the first command node; verify the anomaly in response to the validation request and based upon the sensor data detected by the second command node; and broadcast a verification message based upon whether the anomaly for the shipping container is verified.

An unmanned Wing In Ground Effect vessel (UWIG) for transporting the cargo with internal cargo hold contained in a seaworthy fuselage. The UWIG is autonomous or semi-autonomous. A pair of wings are attached to the fuselage. An on-board controller controls lift sufficient lift to travel in ground effect. The controller also controls UWIG surface maneuvering, taxiing and flying. The UWIG may be autonomous or semi-autonomous.

A cargo handling system is disclosed. A method for storing and restraining cargo is disclosed. The method includes positioning a unit load device at a parked location on a conveyance surface and in contact with a drive roller, deploying a restraint to engage the unit load device, and verifying engagement of the restraint with the unit load device by activating the drive roller and detecting movement of the unit load device with respect to the conveyance surface.

An unmanned aerial vehicle (UAV) has a wing assembly that is coupled to a cargo carrying pod. The pod has a pallet storage volume and an aerodynamic outer surface. The wing assembly has wings that are coupled to rotor booms that include motors and rotors. A tail assembly is coupled to tail booms that extend back from the wings. Rudders are coupled to the rear portions of the tail booms and an elevator is coupled to top portions of the rudders. The elevator is at least 84 inches high and the rudders are at least 48 apart so that a forklift can drive under the elevator and between the rudders to a rear door of the pod to place cargo on a pallet into the storage area of the pod.

A system for ensuring proper installation of components of a cargo management system within a cargo hold has cleats rigidly attached to a floor of the cargo hold, a first subset of the cleats having insets of a first shape, a second subset of cleats having insets of a second shape, keys and rotatable fasteners attached to the components of the cargo management system, a first subset of the keys having the first shape and a second subset of the keys having the second shape. The first subset of keys can only engage with the first subset of cleats and the second subset of keys can only engage with the second subset of cleats and the rotatable fasteners utilize a rotary movement to secure the components of the cargo management system to a respective cleat, against which the rotary fastener is engaged.

In an aircraft, bi-stable power drive units (PDUs) move and secure cargo within an aircraft cargo hold. Such a PDU includes a frame, by which the PDU is rigidly attached to the cargo hold floor; a body pivotably attached, via a hinge, at a first end of the frame at least one drive roller attached at a second end of the body; and an actuator attached to the body and which causes a pivoting angular movement of the body, relative to the frame, about the hinge. The actuator maintains an angular position of the body relative to the frame even upon a loss of power to the PDU. The body is movable between and including a retracted position and a deployed position. A cargo management system includes a plurality of such PDUs, at least one having a controlled area network (CAN) bus interface to control and communicate with a controller.

Transport pallet consisting of a first and second opposite short side and a first and second opposite long side. The bearing surface is constituted by a framework consisting of a number of mutually parallel extending elongate ribs and a number of mutually parallel extending transversal ribs extending perpendicularly to the elongate ribs. A number of legs are formed as an extension of the ribs and extend downward from the bearing surface and mutually distributed below the same. The short sides are similarly formed with fork lift pockets. The rib extension is formed with an inclination, so that the legs narrow in a direction away from the pallet underside.

There are provided examples of an enhanced cargo capacity aircraft, converted from a datum aircraft. The enhanced cargo capacity aircraft includes the datum aircraft and a cargo module. The datum aircraft includes at least a fuselage having a dorsal fuselage part. The cargo module is affixed to the datum aircraft, thereby converting the datum aircraft to the enhanced cargo capacity aircraft. The datum aircraft is designed for aerodynamic flight capability absent the cargo module. The enhanced cargo capacity aircraft is capable of aerodynamic flight. The cargo module provides enhanced cargo capacity to the datum aircraft. The cargo module includes an external aerodynamic fairing defining an internal cargo volume, and is configured for being conformally affixed in overlying relationship with respect to the dorsal fuselage part. The cargo module includes a cargo handling floor and at least one access door, and a cargo handling system configured for transporting and securing at least one cargo unit within the cargo volume. The cargo unit includes a standard unit load device (ULD).

A bail hook for use with cargo is disclosed. The bail hook can have a base plate, a spacer and a handle. The bail hook can also include a handle plate located between the base plate and the handle. The bail hook can include position markers located along an edge of the base plate and the handle plate. The bail hook can include a handle mount located between the handle plate and the handle. The bail hook can have a first and second flap slot configured to receive a first and second box flap. The bail hook can have a bevel, where the bevel can be located on the handle plate. The bail hook can be made from plastic or a combination of materials, such as metal. A method of use of the bail hook with box cargo is also disclosed.

A spacer assembly includes a shaft, a spacer having a first end and a second end, the spacer configured to receive the shaft; a collar configured to couple with the shaft at the first end to secure the shaft in the spacer when the shaft is received by the spacer, a lever configured to couple with the shaft at the first end, the lever configured to rotate the shaft, and a screw configured to fasten the lever to the spacer.