Abstract: The invention relates to a heat insulating element (1) comprising: a plate-type main part (2) with a first flat face and a second flat face and comprising a vacuum insulating body (3), in particular a foil-encased vacuum insulating body which is arranged between the first flat face and the second flat face, wherein the first flat face and the second flat face are made of a respective cover layer (4, 5), and on at least one of the two flat faces, the corresponding cover layer (4) is only partially connected to the vacuum insulating body (3), in particular in an adhered or melted manner. The invention is characterized in that the cover layer (4) which is only partially connected has a relief structure (6) in all of, a plurality of, or the majority of the regions which are not connected to the vacuum insulating body (3), said relief structure being designed to compensate for a thermal expansion or a thermal contraction.

Abstract: A structural element for a passenger cabin of an aircraft is built using biomimicry methods. The structural element includes a generative structure, and a functional component. The generative structure includes at least one accommodating space. The functional component is arranged within the at least one accommodating space. The generative structure includes a load topology optimized structure based on a bioinspired generative design that is configured to enable the structural integrity of the structural element while simultaneously providing integrated functionalities via the functional component. Further, an interior component for an aircraft is disclosed that includes at least one such structural element, and an aircraft including at least one structural element. For example, an aircraft galley may include a structural component that may therefore, for example, include integrated wiring, plumbing or other functionalities.

Abstract: Described herein is a method for examining a coating of a probe surface, including the steps of providing sensing data indicative of a depth of the coating at each of a predetermined subset of probe surface points, determining a depth representation of the coating from the sensing data, and deriving a coating property based on the depth representation. The coating property carries objective information about a geometric constitution or structure of the coating, which can be used for assessing the coating with respect to a functionality that is due to its geometric constitution or structure.

Abstract: The invention relates to a heat insulating element (1) comprising: a plate-type main part (2) with a first flat face and a second flat face and comprising a vacuum insulating body (3), in particular a foil-encased vacuum insulating body which is arranged between the first flat face and the second flat face, wherein the first flat face and the second flat face are made of a respective cover layer (4, 5), and on at least one of the two flat faces, the corresponding cover layer (4) is only partially connected to the vacuum insulating body (3), in particular in an adhered or melted manner. The invention is characterized in that the cover layer (4) which is only partially connected has a relief structure (6) in all of, a plurality of, or the majority of the regions which are not connected to the vacuum insulating body (3), said relief structure being designed to compensate for a thermal expansion or a thermal contraction.

Abstract: An aircraft cabin dismantling and recycling system including: a device (10) for transferring aircraft cabin parts to secondary utilization is provided that includes a data input (12), a data processor (14) and an output interface (16). The data input provides cabin base types from a database and initial equipment installation states of the aircraft cabin from an installation state database. The data processor is configured to identify a cabin base type for a current part of the aircraft cabin; assign an initial equipment installation state of the aircraft cabin; estimate changes of the current part and determine a current parameter; identify implementable transferring options for the current part of the aircraft cabin from a database of transferring options based on the current parameter, and select one of the identified transferring options.

Abstract: A system for stock management for on-board catering for a vehicle, in particular for an aircraft, includes a galley which is provided with a control unit for controlling the galley, wherein the control unit is designed to make available stock management data of the galley; a service unit for transporting supplies within the vehicle, wherein the stock management data comprise a stock record of the supplies transported with the service unit; and at least one operator control element which is communicatively connected to the control unit of the galley via a wireless data connection and is designed to record removal of a supply item from the service unit and/or reception of a supply item into the service unit, and to bring about updating of the stock record of the transported supplies on the basis thereof.

Abstract: A system for automatically adapting operating parameters of a galley device on the basis of provided supply items for on-board catering for a vehicle, in particular an aircraft, includes a galley device that has an identification device that is designed to identify a supply item; and a control device for controlling the galley device, wherein the control device is designed to provide operating parameters for the identified supply item and to operate the galley device in accordance with the operating parameters.

Abstract: Described herein is a method for examining a coating of a probe surface, including the steps of providing sensing data indicative of a depth of the coating at each of a predetermined subset of probe surface points, determining a depth representation of the coating from the sensing data, and deriving a coating property based on the depth representation. The coating property carries objective information about a geometric constitution or structure of the coating, which can be used for assessing the coating with respect to a functionality that is due to its geometric constitution or structure.

Abstract: The present invention relates to a refrigerant circuit for a refrigerator and/or freezer, with at least one body and with at least one cooled interior space arranged in the body, wherein the refrigerant circuit includes at least one evaporator and at least one condenser as well as at least one compressor, wherein the condenser is partly or completely arranged in a liquid bath that at least partly absorbs the condensation heat in operation of the refrigerant circuit.

Abstract: The invention relates to a thermally insulated receptacle, preferably a refrigeration and/or a freezing appliance, comprising at least one temperature-controlled, preferably chilled interior and at least one thermoelectric element (20), especially at least one Peltier element (20), for controlling the temperature in the interior, preferably for generating cold in the chilled interior; further comprising at least one solid (10, 12) which is disposed in such a way that heat is conducted to the thermoelectric element (20), especially heat is dissipated from the chilled interior to the thermoelectric element (20) and/or heat is dissipated from the thermoelectric element (20) by having the solid (10, 12) conduct heat.

Abstract: The present invention relates to an apparatus for the vacuum-tight leading of an electric line through a high barrier film. The apparatus comprises a hollow pipe 1 having a collar 2 projecting therefrom; a high barrier film 3 having a passage hole 4 through which the hollow pipe 1 runs; and a pressing element 5 that is arranged at the side of the high barrier film 3 that is remote from the collar 2, and that urges the high barrier film 3 toward the collar 2, with the high barrier film 3 being arranged between the collar 2 of the hollow pipe 1 and the pressing element 5. The apparatus is furthermore characterized in that an electric line runs in the hollow pipe 1 that leads from the one side of the high barrier film 3 to the other side and in that a sealant is present in the hollow pipe 1 for the vacuum-tight closing of the hollow pipe 1.

Abstract: The present invention relates to a method of applying a film to a body. In this respect, a film is first applied to and positioned at a transfer mold and the body to be film coated is introduced into the transfer mold to which the film to be attached is applied or the transfer mold to which the film to be attached is applied is introduced into the body to be film coated so that the film is located between the body and the transfer mold. In the further course, a vacuum is applied in a region between the body and the film and/or an excess pressure is applied in a region between the transfer mold and the film so that the film moves from the transfer mold onto the body. A particularly simple method that is fast to be carried out is thereby provided for applying a film to a surface.

Abstract: The present invention relates to a vacuum insulation body with at least one vacuum-tight casing and with at least one vacuum region which is surrounded by the casing, wherein the casing is provided with at least one opening, in particular with at least one evacuation port, for evacuating the vacuum region, and wherein in the vacuum insulation body at least one adsorbent material is disposed, which partly or entirely is arranged in the region of said opening, wherein around the opening and within the vacuum range at least one plate is arranged, which forms a wall of the space in which the adsorbent material is disposed.

Abstract: The present invention comprises a vacuum insulation body comprising a vacuum-tight covering that surrounds an evacuated region, wherein a core material is arranged in the evacuated region, wherein the covering has an outer region and an inner region at least partially surrounded by the outer region, wherein the inner region and the outer region are formed by a common film bag and wherein the inner region is formed by inverting the film bag.

Abstract: A system for stock management for on-board catering for a vehicle, in particular for an aircraft, includes a galley which is provided with a control unit for controlling the galley, wherein the control unit is designed to make available stock management data of the galley; a service unit for transporting supplies within the vehicle, wherein the stock management data comprise a stock record of the supplies transported with the service unit; and at least one operator control element which is communicatively connected to the control unit of the galley via a wireless data connection and is designed to record removal of a supply item from the service unit and/or reception of a supply item into the service unit, and to bring about updating of the stock record of the transported supplies on the basis thereof.

Abstract: A vacuum insulation body includes at least one vacuum-tight casing and at least one vacuum region surrounded by the casing. The casing is provided with at least one opening, in particular with at least one evacuation port, for evacuating the vacuum region. At least one adsorbent material is present in the vacuum insulation body. The adsorbent material is partly or completely arranged in the region of the opening.

Abstract: The present invention relates to a vacuum insulation body comprising a vacuum-tight casing which surrounds an evacuated region, wherein a core material is arranged in the evacuated region, wherein the casing includes an opening for filling the casing with the core material, which is covered by a vacuum-tight cover film, wherein the casing is folded inwards in the edge region protruding towards the opening, so that the opening is reduced in size, and subsequently again is folded outwards, wherein the region folded outwards and a region of the cover film are vacuum-tightly connected with each other all around.

Abstract: The present invention relates to a refrigerant circuit for a refrigerator and/or freezer, with at least one body and with at least one cooled interior space arranged in the body, wherein the refrigerant circuit includes at least one evaporator and at least one condenser as well as at least one compressor, wherein the condenser is partly or completely arranged in a liquid bath that at least partly absorbs the condensation heat in operation of the refrigerant circuit.

Abstract: The invention relates to a refrigerator and/or freezer device having at least one body with at least one full vacuum insulation body element, and having at least one cooled inner chamber arranged inside said body, the device comprising at least one coolant circuit for cooling the inner chamber, and the entire coolant circuit being made as an assembly that is inserted into the body.

Abstract: The present invention relates to a refrigerator and/or freezer with at least one body and with at least one cooled interior space arranged in the body, wherein the appliance includes at least one refrigerant circuit that serves for cooling the interior space, wherein the refrigerant circuit includes at least one condenser, wherein at least one heat pipe is provided that is in direct or indirect thermal contact with the condenser and that is arranged such that it forms at least a part of a frame heater of the appliance and/or is in thermal contact with the outer skin of the appliance.