Abstract: A composite panel assembly including a first panel with a first skin, a second skin, a core, and an assembly flange. A second panel includes a first skin, a second skin, a core, and an assembly flange. A fastening device is adapted to fasten the assembly flange of the first panel to the assembly flange of the second panel, wherein the core of one of the first panel or the second panel includes reinforcing pins and a high-density portion placed along the assembly flange.

Abstract: A method for producing a decorated plastic molded article with the steps: a) providing a base body made of a fiber composite plastic b) providing a decorative film; c) heating the base body; d) joining the base body and the decorative film in a mold.

Abstract: A composite panel assembly including a first panel with a first skin, a second skin, a core, and an assembly flange. A second panel includes a first skin, a second skin, a core, and an assembly flange. A fastening device is adapted to fasten the assembly flange of the first panel to the assembly flange of the second panel, wherein the core of one of the first panel or the second panel includes reinforcing pins and a high-density portion placed along the assembly flange.

Abstract: A method for producing a decorated plastic molded article with the steps: a) providing a base body made of a fiber composite plastic b) providing a decorative film; c) heating the base body; d) joining the base body and the decorative film in a mold.

Abstract: A tool mold, which includes a first tool molding part and a second tool molding part, is provided, wherein the first tool molding part and/or the second tool molding part has a filling channel. At least two insertion elements are arranged in such a way that at least one first insertion element of the at least two insertion elements bears at least in some areas against the inner wall of the first tool molding part or against the inner wall of the second tool molding part, and that at least one second insertion element of the at least two insertion elements is arranged at least in some areas on the side of the at least one first insertion element which faces away from the inner wall of the first tool molding part or the side of the at least one first insertion element which faces away from the inner wall of the second tool molding part.

Abstract: The invention relates to a multilayered film element (1) comprising a first component, more particularly an RFID antenna in the form of a multilayered film element, and to a method for fixing a second component on a film element (1) of this type. The film element (1) has a dielectric layer (10) having a front side (10V) and a rear side (10R). The film element (1) has a layer (11, 12) forming a first component, and at least one component contact area (23, 24) arranged on the front side (10V) and connected to the first component. The film element (1) has at least one thermode contact layer (30) which is arranged on the dielectric layer (10) and which, as seen perpendicularly to the dielectric layer (10), is arranged in the region of the at least one component contact area (23, 24). The thermode contact layer (30) has a thermode contact area (32) on a side facing away from the dielectric layer (10), said thermode contact area forming an outer surface of the film element (1).

Abstract: An air conditioning system for an aircraft for the individual air conditioning of regions of a cabin of an aircraft includes a central air conditioning device, which provides a pressurized and temperature-controlled central air flow. A part of the central air flow is supplied to a first cabin region. Another part of the central air flow is heated in a heating device or cooled in a cooling device and supplied to another cabin region. Water evaporates in the cooling device, in order to cool the air flow to be supplied to the cabin region.

Abstract: A 3D printer system that allows a 3D object to be printed such that each portion or object element is constructed or designed to have a user-defined or user-selected material parameter such as varying elastic deformation. The 3D printer system stores a library of microstructures or cells that are each defined and designed to provide the desired material parameter and that can be combined during 3D printing to provide a portion or element of a printed 3D object having the material parameter. For example, a toy or figurine is printed using differing microstructures in its arms than its body to allow the arms to have a first elasticity (or softness) that differs from that of the body that is printed with microstructures providing a second elasticity. The use of microstructures allows the 3D printer system to operate to alter the effective deformation behavior of 3D objects printed using single-material.

Abstract: A multilayer film element and a method for producing the same. The multilayer film element includes a flexible dielectric carrier layer having a layer thickness of less than 800 ?m and has a first electrically conductive layer, in which a first coil-shaped conductor track is shaped in a first region of the film element, and a second electrically conductive layer, in which a second coil-shaped conductor track is shaped in the first region. The dielectric carrier layer is arranged between the first and second electrically conductive layers, and the first and second conductor tracks overlap at least in regions and are coupled to one another to form an antenna structure.

Abstract: A multilayer film element and a method for producing the same. The multilayer film element includes a flexible dielectric carrier layer having a layer thickness of less than 800 ?m and has a first electrically conductive layer, in which a first coil-shaped conductor track is shaped in a first region of the film element, and a second electrically conductive layer, in which a second coil-shaped conductor track is shaped in the first region. The dielectric carrier layer is arranged between the first and second electrically conductive layers, and the first and second conductor tracks overlap at least in regions and are coupled to one another to form an antenna structure.

Abstract: A multilayer film element and a method for producing the same. The multilayer film element includes a flexible dielectric carrier layer having a layer thickness of less than 800 ?m and has a first electrically conductive layer, in which a first coil-shaped conductor track is shaped in a first region of the film element, and a second electrically conductive layer, in which a second coil-shaped conductor track is shaped in the first region. The dielectric carrier layer is arranged between the first and second electrically conductive layers, and the first and second conductor tracks overlap at least in regions and are coupled to one another to form an antenna structure.

Abstract: In order to increase the air humidity in a cabin region of an aircraft equipped with a plurality of seats, a device includes a plurality of humidifying units each arranged in spatial association with a partial number of the seats and a plurality of outlet openings. The humidifying units are each designed to enrich a supplied air stream with gaseous water. The outlet openings are designed to emit the air streams enriched by the humidifying units into the cabin region, such that a partial number of the outlet openings each receive one of the enriched air streams. The air temperature of the enriched air streams is controlled so that the local temperature in a target region served by the humidifying unit does not fall below a dew point.

Abstract: The invention pertains to an inerting system for an aircraft featuring at least one air separation module with at least one air inlet, a first air outlet and a second air outlet. The air separation module is designed for splitting an input air flow into a first air flow and a second air flow, wherein the first air flow is enriched with oxygen in comparison with the input air flow and discharged at the first air outlet and the second air flow is enriched with nitrogen in comparison with the input air flow and discharged at the second air outlet. In comparison with known inerting systems, the inerting system according to the invention is characterized in that the air inlet can be connected to an air extraction point in an air processing system and the inerting system is designed for routing the first air flow into a cabin to be air-conditioned.

Abstract: The invention relates to a multilayered film element (1) comprising a first component, more particularly an RFID antenna in the form of a multilayered film element, and to a method for fixing a second component on a film element (1) of this type. The film element (1) has a dielectric layer (10) having a front side (10V) and a rear side (10R). The film element (1) has a layer (11, 12) forming a first component, and at least one component contact area (23, 24) arranged on the front side (10V) and connected to the first component. The film element (1) has at least one thermode contact layer (30) which is arranged on the dielectric layer (10) and which, as seen perpendicularly to the dielectric layer (10), is arranged in the region of the at least one component contact area (23, 24). The thermode contact layer (30) has a thermode contact area (32) on a side facing away from the dielectric layer (10), said thermode contact area forming an outer surface of the film element (1).

Abstract: The invention relates to a multilayer film element (1) and to a method for producing the same. The multilayer film element (1) comprises a flexible dielectric carrier layer having a layer thickness of less than 800 ?m. Furthermore, it comprises a first electrically conductive layer, in which a first coil-shaped conductor track (27) is shaped in a first region (71) of the film element, and a second electrically conductive layer, in which a second coil-shaped conductor track (37) is shaped in the first region (71). The dielectric carrier layer is arranged between the first and second electrically conductive layers, and the first and second conductor tracks (27, 37) overlap at least in regions and are coupled to one another to form an antenna structure.

Abstract: In order to increase the air humidity in a cabin region (10) of an aircraft equipped with a plurality of seats (16; 28), a device (12; 14) is provided, comprising a plurality of humidifying units (26) arranged in each case in spatial association with in each case a partial number of the seats (16; 28) and a plurality of outlet openings (120). The humidifying units (26) are in each case designed to enrich a supplied air stream with gaseous water. The outlet openings (120) are designed to emit the air streams enriched by the humidifying units (26) into the cabin region (10), in each case a partial number of the outlet openings (120) each receiving one of the enriched air streams.

Abstract: An air conditioning system for an aircraft for the individual air conditioning of regions of a cabin of an aircraft includes a central air conditioning device, which provides a pressurized and temperature-controlled central air flow. A part of the central air flow is supplied to a first cabin region. Another part of the central air flow is heated in a heating device or cooled in a cooling device and supplied to another cabin region. Water evaporates in the cooling device, in order to cool the air flow to be supplied to the cabin region.

Abstract: The invention pertains to an inerting system for an aircraft featuring at least one air separation module with at least one air inlet, a first air outlet and a second air outlet. The air separation module is designed for splitting an input air flow into a first air flow and a second air flow, wherein the first air flow is enriched with oxygen in comparison with the input air flow and discharged at the first air outlet and the second air flow is enriched with nitrogen in comparison with the input air flow and discharged at the second air outlet. In comparison with known inerting systems, the inerting system according to the invention is characterized in that the air inlet can be connected to an air extraction point in an air processing system and the inerting system is designed for routing the first air flow into a cabin to be air-conditioned.

Abstract: The present invention provides dye mixtures containing one or more dyes of the general formula (I) and one or more dyes of the general formulae (II) where D1, D2, D3 RA, RB, RC, Z1 and M are each as defined in claim 1, processes for their preparation and their use.

Abstract: The present invention relates to a dye mixture which comprises at least one dye of the general formula (I) and at least one dye of the general formula (II) in which D1, D2, W1, W2, Y1, Y2, R1 to R6, M, m and n are defined as indicated in claim 1, to processes for preparing them, to their use, and to inks comprising them for digital printing.