Abstract:
A modular assembly and method of installing a modular assembly is provided. The modular assembly can include a plurality of base members made of a plastic composite material. Each base member can be a monolithic structure defined by a top wall, a bottom wall, and opposing side walls, the opposing side walls defining a channel. A heater tray can be configured to be slidably received within the channel of each base member. The heater tray may include a channel that extends longitudinally along the heater tray. A heating element can be configured to heat the heating tray, the heating element received within the channel of the heater tray. Each of the plurality of base members can adjoin one another in an assembled state to form a horizontal platform for traffic.
Abstract:
The disclosure relates to a covering system for a floor, a wall and/or a ceiling. The covering system includes a decorated side, a lower side opposite the decorated side and a plurality of interconnected covering elements. At least one conducting element is arranged between at least two of the covering elements in such a way that the at least one conducting element is at least partially visible on the decorated side. The at least one conducting element is configured to conduct a physical quantity, material or signals. The at least one conducting element includes an interface to a source or a consumer of the physical quantity, material or signals.
Abstract:
A floor panel for an aircraft comprising a panel structure for transmitting forces applied to the floor panel, wherein the panel structure includes an upper cover layer, a lower cover layer, and a core assembly sandwiched between the upper and lower cover layers, and a heater layer for heating the floor panel, wherein the heater layer is provided between the upper and lower cover layers. The object of the present disclosure, to provide a possibly simple heated floor panel for an aircraft, wherein the risk of overheating and at the same time the risk of local hot spots at the heater layer is reduced, is achieved in that the heater layer is formed as a PTC-layer having a plurality of electric conductor paths interconnected to one another by a plurality of PTC-resistor paths comprising a PTC-material, wherein the electric resistance of the PTC-Material increases with increasing temperature.
Abstract:
A support for the heating elements of radiant coverings and floors is disclosed. One example of a support disclosed herein includes bosses having a concave portion. In some examples, defined on the surface of the concave portion is at least one adhering low relief, for example four adhering low reliefs may be provided per concave portion.
Abstract:
Floor and ceiling panels and methods of constructing a floor system for a building are described. In some embodiments, a panel includes a plurality of joists, a corrugated form deck disposed above and attached to the plurality of joists, a ceiling substrate disposed below and attached to the plurality of joists, and an in-floor radiant heat member disposed between the corrugated form deck and the ceiling substrate. In some embodiments, the panel includes a plurality of joists, a corrugated form deck disposed above and attached to the plurality of joists, and a sound dampener disposed between the corrugated form deck and the plurality of joists. In some embodiments, the method includes attaching a pre-assembled panel to a frame of the building and pouring concrete onto the panel so that a radiant heat member is separated from the concrete by a corrugated form deck of the panel.
Abstract:
An aircraft heated floor panel includes a first face sheet, a second face sheet opposite the first face sheet, and core with an electrically conductive core portion. The electrically conductive core portion supports the first face sheet and the second face sheet, and is electrically insulated from the external environment to receive electrical power, resistively generate heat, and communicate heat to the first face sheet.
Abstract:
Disclosed is a heating module and a method of manufacturing thereof. The method comprises arranging a first conductive layer on a first surface of an intermediate insulating layer; making a channel on a second surface of the intermediate insulating layer; arranging a heating cable in the channel; filling the channel with a conductive filling material to cover the heating cable arranged in the channel; and attaching a second conductive layer to the second surface of the intermediate insulating layer with a conductive adhesive coating.
Abstract:
Provided is an infrared electrothermal raised floor piece, comprising a faceplate layer, a carbon fiber far-infrared heat layer, a force support structure layer, at least a pair of electrodes and a plurality of power line connection terminals; wherein the electrodes are connected to the carbon fiber far-infrared heat layer; and the power line connection terminals are connected to the electrode. Also provided is an infrared electrothermal raised floor, comprising a plurality of infrared electrothermal raised floor pieces each comprising a plurality of power line connection terminals, and a supporter; wherein the infrared electrothermal raised floor pieces are transversely or lengthwisely arranged and flexibly installed on the supporter.
Abstract:
A heating wire support meshing and a method of constructing a heated surface, particularly a floor surface therewith, is described. The heating wire support meshing comprises one or more mats formed by transversely spaced parallel rows of wire support bridge elements interconnected together at their crossings. The bridge elements have electric heating wire support slots to receive and guide one or more electric heating wires along one or more desired paths. Bottom support formations extend along a bottom planar surface of the mat. Top support formations lie in a top planar surface of the mat. The wire support slots are adapted to support the one or more electric heating wires spaced below the top support formations. The support meshing also acts as a reinforcement of a sub-floor on which the support meshing is installed.
Abstract:
A method for providing an electrical connection for conductive ink includes direct writing a bus bar onto areas of a desired electrical connection of the conductive ink. The conductive ink is screen printed onto a dielectric film to create a conductive circuit. An aircraft heated floor panel includes at least one floor panel of an aircraft. The one floor panel includes a conductive circuit having a conductive ink including a bus bar directly written onto areas of a desired electrical connection of the conductive ink. The conductive ink is screen printed onto a dielectric film to create a conductive circuit.