A cargo restraint system may comprise a restraint and an actuator shaft configured to rotate the restraint between a raised position and a stowed position. The restraint may include a head configured to rotate about an axis and a plunger configured to translate between an engaged state and a disengaged state. When the plunger is in the engaged state, the head is rotationally coupled to the actuator shaft. When the plunger is in the disengaged state, the head can rotate independently of the actuator shaft.

A cargo aisle drive system is disclosed. In various embodiments, the system includes a drive track; and a drive car configured for motorized translation along a length of the drive track, the drive car including a first plate, a second plate having an upper surface and a lower surface, the first plate pivotally disposed on the upper surface of the second plate, a drive assembly connected to the lower surface of the second plate, and a first strain gauge sensor configured to detect a pivotal movement between the first plate and the second plate of the drive car.

An apparatus for loading and unloading cargo, capable of loading cargo while distributing the weight of the cargo and unloading the cargo regardless of the loading order of the cargo, is provided. The apparatus for loading and unloading cargo may include: a base portion; a rail installed on the base portion; a plurality of movable plates disposed on the rail, supporting the cargo, and moving along the rail; and a raising-lowering portion connected between the base portion and a body so that the base portion can be raised and lowered.

Systems and methods for extending the interior cargo bay of fixed-wing cargo aircraft into a replaceable tailcone bay are disclosed. The system includes an aircraft and a removable tailcone configured couple to the aft end of the fuselage. The aircraft fuselage includes a cargo bay and an aft end opening into the cargo bay. The tailcone, when attached, encloses the aft end opening the cargo bay. The tailcone can include an interior volume configured to extend the fuselage cargo bay such that the interior volume defines an aft end of a cargo bay of the cargo aircraft. In some examples, the tailcone includes a plurality of segments, which can be configured to extend from the aft end of the aircraft to adjust a length of the cargo extension provided by the tailcone.

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.

An automatic electromechanical braking roller system includes a power drive unit (PDU) comprising a sensor configured to detect a speed of a unit load device (ULD), a controller configured to receive a speed signal corresponding to a speed of the ULD from the sensor, and an electromechanical braking roller (EBR) spaced apart from the PDU and configured to receive a braking signal from the controller in response to the speed of the ULD being greater than a threshold value. In response to the speed of the ULD being less than the threshold value, the EBR is configured to rotate freely about an axis in a first state. In response to the speed of the ULD being greater than the threshold value, the EBR is configured to reduce the speed of the ULD in a second state.

An aircraft including at least one hold configured to store containers along at least one storage line, and at least one opening configured to provide a passage between the hold and the exterior of the aircraft, the opening being positioned in vertical alignment with the storage line or in line with the storage line. The hold comprises at least one loading and unloading device comprising at least one carriage, at least one guiding system configured to move the carriage along the storage line, at least one spreader equipped with at least one system for grasping the containers, and at least one vertical movement system that is configured to move the spreader vertically with respect to the carriage.

Disclosed is a method of operating a Portable Cargo Panel (PCP) for an aircraft, including: detecting a gesture on a display of the PCP; determining that the gesture is a command to view on the display a first cargo compartment; securing a wireless connection with the first control panel therein; receiving, from the first control panel, a health state of each of a plurality of Cargo Handling Units (CHUs) therein; displaying, on the display, the first cargo compartment with the plurality of CHUs and the operational state of the plurality of CHUs; controlling one or more of the CHUs in the first cargo compartment by transmitting, to the first control panel, a command to: run a diagnostic test against the one or more of the plurality of CHUs; or control the plurality of CHUs to move a Unit Load Device (ULD) into, within or out of the first cargo compartment.

An aircraft fuselage assembly includes a primary structure with first and second rows of support elements extending parallel to a longitudinal axis and into an interior space of the fuselage where they have a free end. The free ends of the first and second rows are spaced from one another to from a free space below a common plane of the free ends and extending to the primary structure. A cargo floor assembly with at least one first cargo floor element is fixedly connected to the free ends of the first row in the common plane and at least one second cargo floor element fixedly connected to the free ends of the second row in the common plane. At least one central cargo floor element is arranged between the first and second lines and is releasably connected to the support elements of the first and second rows.

A cargo conveying system for conveying cargo items, in particular containers and/or pallets, in a cargo hold of an aircraft having at least one cargo conveying device, in particular roller conveyors. The cargo conveying device includes at least one frame, at least one roller drive unit having at least one roller for conveying the cargo items, at least one main line strand, in particular a partial cable harness, arranged on the frame, and at least one distributor module for connecting the at least one main line strand to at least one further main line strand. The distributor module is arranged on the frame and is connected to the roller drive unit via at least one secondary line strand.