| TELAIR INTERNATIONAL GMBH Patent applications |
| Patent application number | Title | Published |
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| 20120132744 | LOCKING ELEMENT - 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. | 05-31-2012 |
| 20120126058 | LOCKING ELEMENT - 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. | 05-24-2012 |
| 20120126057 | FLOOR FOR AN AIRCRAFT CARGO COMPARTMENT AND METHOD FOR THE ASSEMBLY THEREOF - 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. | 05-24-2012 |
| 20120119052 | FUNCTION ELEMENT, METHOD FOR PRODUCING A FUNCTION ELEMENT - 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. | 05-17-2012 |
| 20120119027 | FLOOR ELEMENT FOR A LOADING DECK OF AN AIRCRAFT - Floor elements for a loading deck of an aircraft may be provided. The floor elements may include a hollow profiled element having a cover plate and a base plate which are connected to each other by webs. In order to collect water and/or to heat the loading deck, the hollow profiled element is designed at least in some sections as a conduit for conducting liquids and/or gases. In this way, the cargo deck thus formed by the floor elements simultaneously has several functions, namely the actual cargo deck function and the function of a liquid collecting trough which can be heated or is used as a heater for the cargo hold. | 05-17-2012 |
| 20120119026 | LOCKING ELEMENT - 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. | 05-17-2012 |
| 20120101636 | FREIGHT LOADING SYSTEM AND METHOD FOR DETERMINING MOVEMENT OF A FREIGHT ITEM ON A CARGO DECK - 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. | 04-26-2012 |
| 20120061511 | CARGO HOLD FLOOR AND AIRCRAFT HAVING A CARGO HOLD FLOOR - 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 standardised 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. | 03-15-2012 |
| 20120037753 | LATERAL GUIDE, LATERAL GUIDE ASSEMBLY, CARGO DECK - The present invention relates to a lateral guide for guiding cargo items in an aircraft. Such lateral guides are used to guide containers or pallets during their transport from the tail to the nose and to secure them in their final position. The proposed lateral guide has a mounting frame extending in the longitudinal direction and at least one lateral guide device having a sliding carriage, whereby the lateral guide device is movably supported in the mounting frame in the longitudinal direction. The sliding carriage has at least one guide roller for supporting the cargo items. | 02-16-2012 |
| 20120027534 | FASTENING DEVICE FOR AT LEAST PARTIALLY SECURING A FIRST AND A SECOND FREIGHT ITEM - 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. | 02-02-2012 |
| 20110313563 | Loading System and Method for Loading a Cargo Hold of an Aircraft - A loading system for loading a cargo hold ( | 12-22-2011 |
| 20100230545 | Roller Conveyor - 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. | 09-16-2010 |
| 20100230544 | Fastening Device of a Floor Module - A fastening device of a floor module in an aircraft hull is provided. The fastening device comprises an intermediate element that on one hand can be fastened to the aircraft hull using a joining device and on the other comprises a receiving device for a holding portion of the floor module. In this case the fastening device is designed in such a way that mobility of the holding portion relative to the aircraft is guaranteed in the aircraft's longitudinal direction by means of which it is possible to guarantee stress-free installation inside the aircraft hull. | 09-16-2010 |
| 20100230537 | Floor Module of a Cargo Deck in the Hull of an Aircraft - Floor modules of a cargo deck in a hull of an aircraft which comprise support devices for carrying functional elements, e.g. panels, roller conveyors or ball mats, are provided. The support devices are attachable in the hull of the aircraft directly or by way of intermediate elements. To improve stability at reduced weight, end support devices, as seen in the aircraft's longitudinal direction, have a thickness reduced in such a way compared to the other support devices of the floor module that only together with the end support devices of a floor module installed adjacently in the hull do they ensure a loading capacity that corresponds to at least the loading capacity of the other support devices. | 09-16-2010 |
| 20100230535 | Cargo Hold Floor for a Cargo Hold of an Aircraft and Method for the Installation Thereof - Cargo hold floors are provided, and comprise panels or similar two-dimensional floor elements for the attachment of roller elements, ball elements, locking bar elements or similar functional elements. Support elements, in particular floor beams, are provided which support the two-dimensional floor elements whereby the floor elements are permanently joined to the support elements to make pre-fabricated floor modules and the floor modules are installable in the aircraft. To make installation work easier, separate load-bearing elements, for supporting the floor modules on and joining the floor modules to a body or a skin of the aircraft, are provided which, before the floor modules are installed in the aircraft, are joinable to the body or skin of the aircraft, and, when the floor modules are installed in the aircraft, are joinable to the support elements. As a result, it is possible in particular cases to make installation significantly easier. | 09-16-2010 |
| 20100230230 | Roller Conveyor - Roller conveyors of an aircraft cargo deck, including rollers for transporting freight packages, particularly containers, and a channel with side walls and a base for the installation of locking bar elements to hold the freight packages, are provided. The side walls have reinforcing sections with recesses in which the rollers are installed, whereby axles on which the rollers are rotatably mounted are fixed in each of the side walls. This results in an extremely sturdy but nevertheless lightweight construction | 09-16-2010 |
