Systems, methods, and vehicles for loading and unloading cargo into or out of a large transport vehicle, such as an aircraft, utilizing a curved path are described. The systems and methods include one or more support structures disposed, either permanently or removably, within a cargo bay of the transport vehicle to form a curved path extending into an aft portion of the cargo bay. During loading, the payload can move in the aft direction while concurrently rotating about a center point of an arc. In some embodiments, the cargo bay can include a kinked portion disposed between a proximal and aft portions of the cargo bay, with the curved path extending at least through the kinked portion and into the aft portion. Methods, systems, and components thereof for assembling a cargo, unloading cargo from a large transport vehicle, and disassembling a cargo are also provided.

A mechanically actuated cargo restraint system for a vehicle includes a rotatable reel in a frame, first and second flexible tethers, and a mechanical device. The first flexible tether has a first end coupled to the rotatable reel and a second end capable of being coupled to a cargo item, the first flexible tether is windable around the rotatable reel. The mechanical device includes a pawl and cog that are movable with respect to each other, the pawl coupled to the rotatable reel for rotatable movement therewith. Movement of a cargo item attached to the first flexible tether that causes the first flexible tether to move in an unwinding direction on the rotatable reel causes movement of the pawl-containing member relative to the cog. Velocity in the unwinding direction such as that encountered during a crash or free-fall engages the pawl into the cog, thereby inhibiting movement of the first flexible tether in an unwinding direction on the rotatable reel.

Systems for restraining palleted cargo within an aircraft are provided. A first system operates to provide vertical and outboard lateral support to cargo at a location where the opposite ends of the system are connected to surfaces that are aligned at different orientations, for example, one end connected to a horizontal floor and the second end connected to a sidewall of the fuselage of the aircraft. A second system operates to provide aft, vertical, and outboard lateral support to cargo upon a pallet proximate to its corner, and at a location where a portion of cargo extends above a stay out zone of the aircraft.

A cargo restraint assembly may comprise a first bracket slidingly coupled to a housing. A retention block may be pivotably coupled to the first bracket. A second bracket may be slidingly coupled to the housing. The first bracket may be coupled to the second bracket via a spring. The first bracket and the second bracket may be configured to attenuate in response to a cargo deck bending during transportation of cargo in an aircraft.

A system for moving loads comprising a cargo compartment floor, at least one roller track comprising rollers arranged one behind the other in the cargo compartment floor, at least one guideway in the floor and extending parallel to the at least one track, and at least one transport vehicle removably accommodated in and movable along the guideway. The transport vehicle comprises at least one connecting element movable between first and second operating positions. In the first operating position, the connecting element is configured so the transport vehicle is positionable beneath a load on the roller track, and in the second operating position, the connecting element is configured to interact with the load to connect the load to the transport vehicle, so the load is entrained when the transport vehicle moves along the guideway. The transport vehicle further comprises a drive mechanism to move the transport vehicle along the guideway.

A cargo airship is disclosed. The cargo airship may include a hull configured to contain a gas and at least one propulsion assembly coupled to the airship and including a propulsion device. The cargo airship may further include a payload bay comprising an external cargo area located outside of the hull. The cargo airship may also include a cargo handling system including at least one hoisting mechanism configured to lift cargo into the external cargo area while the airship is hovering.

The present invention provides a seat adjustment device for an aircraft or spacecraft, comprising: a seat rail for connection to a floor; and a seat connection for connection to at least one seat; and a worm is provided which can be actuated to adjust the seat connection relative to the seat rail.

A multicopter system according to one aspect of the present invention includes a multicopter configured to fly in a state of holding a package and a mooring device that is installed at a target position of a flight of the multicopter and includes a linear member that extends in a predetermined direction from the target position, the multicopter including a reception portion that has the shape of a recess including an opening open toward one direction and is configured to receive the linear member via the opening.

The present invention includes a mobile robot which transports a container configured of having a cargo contained therein to an air vehicle, loads the container at a predetermined loading place of the air vehicle, unloads the container from the air vehicle, identifies the unloaded container, and transports the identified container to a predetermined location.

An embodiment of the invention relates to a system for receiving cargo or passengers in a vehicle. The system includes a bottom beam and several functional units, wherein each functional unit includes a floor segment and a seat row with several passenger seats being attached to the floor segment. Each functional unit is assigned to a pivoting device for pivoting the functional unit relatively to bottom beam. Another embodiment of the invention relates to a vehicle having such a system.