Abstract: In conventional aircraft cargo compartments panels or similar flat floor elements are fastened to floor beams or similar supporting elements that are installed in the body of the aircraft. Subsequently functional units such as roller elements, latches or PDUs are mounted and connected to one another by way of appropriate control conductors. It is proposed to fasten the floor elements permanently to the supporting beams so as to form prefabricated floor modules and to install these floor modules in the aircraft.

Abstract: The application relates to freight loading systems for transporting freight items. Corresponding freight loading system comprises a freight deck having a plurality of freight handling devices, a control device which is communicatively connected to the freight handling devices in order to handle at least one freight item on the freight deck, and a remote control, which is communicatively connected to the control device in order to output control signals to the control device. The control device is intended to comprise a position determination unit for determining a remote control position on the freight deck and/or the orientation of the remote control, wherein the control unit is designed to select a number of freight handling devices and drive same depending on the control signals received and the remote control position and/or orientation of the remote control. This allows easier control of the freight items on the freight deck.

Abstract: Some embodiments of the invention relate to function elements for fixing in seat rails of aircraft. The function element according to the invention may include: a fixing rail with a web running in the x direction and a multiplicity of extensions which protrude beyond the web in a y direction to form a T profile, wherein the fixing rail is formed corresponding to the seat rail such that the fixing rail can be inserted in the seat rail and moved along the x direction into a holding position in which the extensions sit between the holes below the slots, at least one fixing peg which is arranged mobile on the fixing rail and can be brought into a blocking position in which the fixing peg engages in a hole of the seat rail so that the function element is fixed in the x direction.

Abstract: The invention relates to a cargo holding device, in particular cargo container or pallet, for loading aircraft, comprising a bottom element and a plurality of profile elements and corner elements, wherein a bottom element edge portion is connected to the profile elements and corner elements, wherein the profile elements are connected to the corner elements via push-fit connections, wherein at least one profile element is connected to at least one corner element via a push-fit connection which comprises a push-fit connection recess and a corresponding push-fit connection pin, wherein the push-fit connection recess and the push-fit connection pin are configured such that the profile element and the corner element can be connected together by push-fit by a translational movement, wherein a translational movement direction has an angle in relation to a profile longitudinal axis of the profile element.

Abstract: To secure containers in a cargo bay of an aircraft, locking elements are known comprising locking lugs which can move from a locked position to a rest position. The locking lugs engage in engagement recesses of freight items. On movement of the locking lugs from the locked position to the rest position, the locking lugs can seize in the engagement recesses. A locking element is proposed to which a pair of locking lugs is allocated which in the locked position each have a stop surface which can be brought into engagement on a stop edge of the engagement recess, wherein the locking lugs are mounted mobile such that on movement from the locked position to a rest position, the two stop surfaces separate from the stop edges. As a result the space required in the holding direction for the locking lugs and the risk of seizing of the locking lugs in the engagement recess are substantially reduced.

Abstract: A cargo hold floor of an upper and/or a lower deck of an aircraft having a plane of symmetry which divides the cargo hold floor into a first half and a second half is disclosed, said cargo hold floor comprising locking gaps which each encompass all the locking elements located substantially on one level in the longitudinal direction (x direction) of the aircraft, in particular longitudinal locking elements for securing standardized cargo containers, in particular pallets and/or containers, in the longitudinal direction (x direction) of the aircraft whereby all the longitudinal locking elements of at least one locking gap are arranged in only one of the halves.

Abstract: In an aircraft there is customarily provided, for receiving a load in the cargo compartment, a cargo deck that comprises a plurality of ball mats, floor panels or similar flat floor elements. Also provided are a plurality of roller conveyors or similar profile elements mounted in the long direction of the aircraft to accommodate transport rollers, PDUs, latches or similar functional units for moving and fixing the load on the cargo deck.

Abstract: The present invention relates to a latch device for securing and/or guiding at least one cargo item on a cargo deck, wherein the latch device comprises: a sliding guide carriage extending longitudinally; a bearing in which the sliding guide carriage is movably supported in such a way that the sliding guide carriage is pivotable out of a restraining position into an inoperative position; at least one releasing device which is attached to the latch device by way of at least one articulation in such a way that the releasing device can be brought out of a blocking position into a releasing position, wherein in the blocking position the releasing device acts on the sliding guide carriage in such a manner that said carriage is locked in the restraining position, wherein the releasing device has at least one releasing device ramp section which is designed and arranged in such a manner that a cargo item approaching longitudinally pivots the releasing device out of the blocking position into the releasing position

Abstract: The invention concerns a freight receiver device, in particular freight container or pallet, in particular for loading aircraft, comprising at least one floor element and at least one profile element connected with the floor element, characterised in that at least one edge segment of the floor element is detachably connected with the at least one profile element via a connecting device comprising at least one hook.

Abstract: The invention relates to a cargo holding device, in particular cargo container or pallet, for loading aircraft, comprising a bottom element and a plurality of profile elements and corner elements, wherein a bottom element edge portion is connected to the profile elements and corner elements, wherein the profile elements are connected to the corner elements via push-fit connections, wherein at least one profile element is connected to at least one corner element via a push-fit connection which comprises a push-fit connection recess and a corresponding push-fit connection pin, wherein the push-fit connection recess and the push-fit connection pin are configured such that the profile element and the corner element can be connected together by push-fit by a translational movement, wherein a translational movement direction has an angle in relation to a profile longitudinal axis of the profile element.

Abstract: A floor module with roller conveyors which define an aircraft cargo hold floor with a loading level is provided. The floor modules have cross-members to which the roller conveyor is attached. A rail with two side pieces is provided, between which rollers are rotatably mounted in such a way that they protrude above upper edges of the rails. The side pieces are joined to one another by a floor section. To improve the strength of the floor module, the floor section has a bent region inclined in cross-section at an angle to the loading level, the bent region dividing the floor section into one partial section lying higher and one partial section lying lower relative to the upper edges.

Abstract: A cargo holding device, such as a cargo container or pallet, in particular for loading aircraft, comprising at least one bottom element and at least one pultruded profile element of fibre-reinforced plastic.

Abstract: A freight floor having a multilayer construction and that is formed as a composite material, comprising a core layer of carbon-fibre-reinforced and/or glass-fibre-reinforced plastic and a seating layer of a metal alloy, in particular an aluminium alloy.

Abstract: A loading system for loading a cargo hold (2) of an aircraft (1), containers, pallets or like ULDs (20) for accommodating freight being introduced into the cargo hold through an access opening, being transported by means of a transport device (60) and being fastened in transport positions. With the ULDs are identification devices (30), e.g. RFID transponders, which identification devices have storage devices for storing first data, especially identification data. The system comprises at least one first reading device (40) for reading the first data of a ULD introduced into the cargo hold, and at least one first transmitter device (50) for transmitting the first data to at least one first recipient (11).

Abstract: The application relates to freight loading systems for transporting freight items. Corresponding freight loading system comprises a freight deck having a plurality of freight handling devices, a control device which is communicatively connected to the freight handling devices in order to handle at least one freight item on the freight deck, and a remote control, which is communicatively connected to the control device in order to output control signals to the control device. The control device is intended to comprise a position determination unit for determining a remote control position on the freight deck and/or the orientation of the remote control, wherein the control unit is designed to select a number of freight handling devices and drive same depending on the control signals received and the remote control position and/or orientation of the remote control. This allows easier control of the freight items on the freight deck.

Abstract: The present invention relates to a latch device for securing and/or guiding at least one cargo item on a cargo deck, wherein the latch device comprises: a sliding guide carriage extending longitudinally; a bearing in which the sliding guide carriage is movably supported in such a way that the sliding guide carriage is pivotable out of a restraining position into an inoperative position; at least one releasing device which is attached to the latch device by way of at least one articulation in such a way that the releasing device can be brought out of a blocking position into a releasing position, wherein in the blocking position the releasing device acts on the sliding guide carriage in such a manner that said carriage is locked in the restraining position, wherein the releasing device has at least one releasing device ramp section which is designed and arranged in such a manner that a cargo item approaching longitudinally pivots the releasing device out of the blocking position into the releasing position

Abstract: The invention concerns a loading system for an aircraft, wherein the loading system comprises a control computer; a multiplicity of cargo conveying devices for conveying a piece of cargo on a cargo loading deck of the aircraft, wherein to control the cargo conveying devices, the control computer is communicatively connected with the cargo conveying devices; at least one input device which is communicatively connected with the control computer to transfer user inputs to the control computer. An aspect of the invention is that the one input device may be formed as a touchscreen.

Abstract: Fastening elements are known in which locking elements can be swivelled out of a non-operative position and into a fixing position. Usually, each of these locking elements has a locking lug. The known fastening devices are mostly very complex in their structure. The some embodiments of present application propose the provision of a fastening device for at least partially securing a first and a second freight item, which fastening device comprises a frame and comprises a locking claw having a first locking lug and a second locking lug. The locking lugs in this case are aligned along a longitudinal direction of the fastening device, for the purpose of encompassing and holding partial portions of the freight items. The locking claws are pivotally fastened to the frame of the fastening device in such a way that the locking claw can be swivelled out of a fixing position, for securing the freight items, into a non-operative position.

Abstract: Conventional aircraft offer an inadequate solution for handling freight items. The present invention significantly improves the handling of freight items. Inter alia, for this the cargo compartment of an aircraft is equipped with a robot with at least one robot arm, wherein the robot arm comprises a receiver tool to receive freight items and is arranged displaceably on a ceiling construction of the cargo compartment.

Abstract: The present invention concerns a lift for an aircraft. This is used to store freight items and/or transport these between a cargo hold and a passenger cabin. The lift comprises at least one receiver compartment, in particular a lift cabin, to receive a freight item, in particular a suitcase and/or a bag; at least one first opening and at least one second opening for loading and/or unloading the lift, wherein the first opening opens into a passenger cabin and the second opening into a cargo hold; and at least one guide ring in relation to which the receiver compartment is arranged mobile such that the receiver compartment is displaceable along the guide ring in a rotation movement about a rotation axis.