Abstract: A cargo deck for an aircraft having a center plane extending centrally along a longitudinal direction of the cargo deck. The cargo deck includes one or more perforated rails spaced apart from the center plane. The perforated rails may be arranged parallel to the center plane. The cargo deck may also include one or more roller tracks and/or fitting elements arranged relative to the center plane. The cargo deck may also include a one or more center guide locks having one or more guide claws.

Abstract: An integral floor module for a cargo deck comprising: a first and second support section for (planar) support on support sections of perforated rail device, wherein the support sections extend in a longitudinal direction and define a support plane; a flat functional device receiving section, which is formed (centrally) between the support sections, wherein the functional device receiving section extends in a longitudinal direction and defines a (lower) receiving plane; wherein the floor module is designed in such a way that the receiving plane is clearly spaced apart (downwards) from the support plane. The floor module can be used in a cargo loading system, including with a latch element, and a method for converting a passenger deck into a cargo deck.

Abstract: A side guide for guiding and/or holding cargo items, in particular containers and/or pallets, in an aircraft, comprising a fastening rail extending in the longitudinal direction (v), at least one side guide device, which can be fastened to the fastening rail in the longitudinal direction (v) at different positions (A, B, C, D) and at least one first and at least one second fastening device for fastening the side guide to a cargo deck of the aircraft, in particular in a perforated rail. The first fastening device engages around the fastening rail and/or engages in the fastening rail in such a way that the first fastening device can be displaced in the longitudinal direction (v), in particular relative to the second fastening device.

Abstract: A floor module for an aircraft cargo hold including a cover element and a floor element which is spaced apart from the cover element at least in some segments and which is attached to an underside of the cover element. The cover element includes receiving openings for receiving ball elements. The cover element and the floor element can be formed as a hybrid composite part.

Abstract: A mounting device for mounting functional devices within a cargo hold of an aircraft. The mounting device includes at least one surface unit and a plurality of functional devices which can be mounted on the surface unit in such a way that the surface unit can be inserted together with functional devices mounted thereon into the aircraft cargo hold in the manner of a template in such a way that all the functional devices come to lie in defined mounting locations in the cargo hold and can be mounted on supporting structures of the aircraft or the cargo hold without adjustment in relation to the surface unit.

Abstract: A cargo deck of an aircraft, including a series of at least two floor modules arranged side by side and made of a fiber-composite material. The floor modules each comprise at least one core in the form of a foam core and/or structural core which is interposed between a first cover layer made of fiber-reinforced plastic and a second cover layer made of fiber-reinforced plastic, wherein the floor modules each comprise a coreless peripheral edge region for producing an, in particular laminar, materially bonded connection between the cover layers. The floor modules are arranged in such a way that sections of the coreless edge regions of the floor modules arranged side by side overlap one another, wherein at least one sealing strip, in particular made of silicone foam, is provided between the mutually overlapping edge regions.

Abstract: A side guide for guiding and/or holding cargo items, in particular containers and/or pallets, in an aircraft, comprising a fastening rail extending in the longitudinal direction (v), at least one side guide device, which can be fastened to the fastening rail in the longitudinal direction (v) at different positions (A, B, C, D) and at least one first and at least one second fastening device for fastening the side guide to a cargo deck of the aircraft, in particular in a perforated rail. The first fastening device engages around the fastening rail and/or engages in the fastening rail in such a way that the first fastening device can be displaced in the longitudinal direction (v), in particular relative to the second fastening device.

Abstract: A floor module for an aircraft cargo hold including a cover element and a floor element which is spaced apart from the cover element at least in some segments and which is attached to an underside of the cover element. The cover element includes receiving openings for receiving ball elements. The cover element and the floor element can be formed as a hybrid composite part.

Abstract: A mounting device for mounting functional devices within a cargo hold of an aircraft. The mounting device includes at least one surface unit and a plurality of functional devices which can be mounted on the surface unit in such a way that the surface unit can be inserted together with functional devices mounted thereon into the aircraft cargo hold in the manner of a template in such a way that all the functional devices come to lie in defined mounting locations in the cargo hold and can be mounted on supporting structures of the aircraft or the cargo hold without adjustment in relation to the surface unit.

Abstract: A freight loading system may include: freight transport devices each with at least one roller for transporting freight items in a transport direction and each sensor for detecting the presence of a freight item, wherein the rollers of at least a first freight transport device are mounted rotationally mobile such that the transport direction of the first freight transport device is adjustable, and a control unit which receives signals from sensors of at least two freight transport devices in order to detect a movement, of a freight item, wherein the control unit is designed to calculate from the signals a relative movement of part of the freight item relative to the first freight transport device and align the at least one roller of the first freight transport device taking into account the relative movement of the part of the freight item.

Abstract: A lock is proposed for securing containers or similar freight on a cargo bay floor of an aircraft in a vertical direction perpendicular to the cargo bay floor and in a transverse direction perpendicular to a longitudinal direction of the aircraft. The locking element comprises at least one lock attached to a frame for securing containers or similar freight and with a claw in the transverse direction of the aircraft to surround and hold a part section of the container. At least one lock is arranged mobile and fixable in a guide of the frame in order to adapt the spacing of the locks to containers of different sizes.

Abstract: A cargo gate for holding at least one cargo item at a predetermined position within a cargo hold of an aircraft comprising at least one retaining element at least one fastening device having at least one articulation for articulatedly fastening the retaining element to a cargo hold floor such that the retaining element can be pivoted from an operative position for holding the at least one cargo item into an inoperative position, wherein the retaining element can be traversed by the at least one cargo item in the inoperative position. The retaining element may be provided with a stop which can be operatively connected to a pivotable locking lug of a locking device such that the locking lug holds the retaining element in the operative position thereof.

Abstract: The present invention concerns a cargo hold floor for a cargo hold of an aircraft. The cargo hold floor comprises a multiplicity of panels (110a, 110b) to form the cargo hold floor, wherein the panels have rail segments to form rails extending over several profile panels (120-130, 120?-129?) and arranged in a longitudinal direction of the aircraft. The rail segments comprise full seat rail segments (150, 150b) and partial seat rail segments (155a, 155b, 155b, 155b) for fixing of freight loading components. Such full seat rail segments and partial seat rail segments can be used advantageously to anchor freight items to the cargo hold floor or to fasten function elements there.

Abstract: A locking element is described for securing containers, pallets or similar freight items in the cargo bay of an aircraft, wherein a first and a second locking claw are mounted on a frame swivellable from a lowered loading position into a raised working position for securing containers. A remotely controllable adjustment device is provided to change and adjust the state of the locking claws between the loading state in which the locking claws are in the loading position, a holding state in which the locking claws are in the working position and fixed, and a trigger state in which the locking claws are in the working position but can be swivelled from the working position into the loading position if a force acting on the locking claws exceeds a predetermined amount.

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.

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: 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: 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: 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: 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.