Abstract: A method for manufacturing a cladding element for a passenger cabin of a vehicle is provided. A first layer is introduced into a forming shell. A support layer is provided onto the first layer, such that the first layer extends beyond an edge of the support layer. An elastic material strip is provided onto a portion of the first layer hat extends beyond the support layer, such that the material strip is flush with the edge of the support layer. A second layer is provided onto the support layer, such that a portion of the second layer extends beyond the edge of the support layer and is superimposed on the material strip. The forming shell is closed and a pressure is exerted on the layer arrangement accommodated in the forming shell at a temperature between 50° C. to 100° C., to form a sandwich structure.

Abstract: An aircraft system carrier element includes a basic body made of a sound- and heat-insulating material, in which are formed an air conditioning duct, which is connectable to an aircraft air conditioning system and provided for supplying an aircraft compartment, and a line duct for receiving lines that are provided for supplying the aircraft compartment. The basic body includes a rear wall and a line duct cover that is fastened detachably to the rear wall. The detachable fastening of the line duct cover enables easy access to the lines for maintenance purposes, when necessary, while also protecting the lines against environmental effects in normal operation.

Abstract: The invention relates to a method for the manufacturing of a cladding element for a passenger cabin of a vehicle, in particular of a land vehicle, an aircraft, or a watercraft, comprising the following steps: introducing a first layer, which is provided with first fibres and impregnated with a resin, into a forming shell, layering of a support layer, which is sheet-like and reinforced with second fibres, onto the first layer, such that the first layer extends beyond at least one edge of the support layer, layering of an elastic material strip onto that portion of the first layer that extends beyond the support layer, such that the material strip bears flushly against the edge of the support layer, layering of a second layer, which is provided with the first fibres and impregnated with the resin, onto the support layer, such that a portion of the second layer extends beyond the edge and lies over the material strip, and closing the forming shell and exerting a pressure on the layer arrangement, which is ac

Abstract: A differential pressure-controlled locking mechanism (10) comprises a housing (12), as well as a first pressure chamber (14) which is arranged in the housing (12) and which is connectable to a first ambient zone. A second pressure chamber, arranged in the housing (12), is connectable to a second ambient zone and is separated from the first pressure chamber (14) by a mobile separating device (18). The separating device (18) is in an inactive position when the pressure in the first pressure chamber (14) is equal to the pressure in the second pressure chamber. Conversely, the separating device (18) is movable from its inactive position into a differential pressure position when a predetermined differential pressure acts on the separating device (18). An actuation element (22), which is held in a first position by the separating device (18) when the separating device (18) is in its inactive position, is movable into a second position when the mobile separating device (18) is in its differential pressure position.

Abstract: An aircraft system carrier element (10) comprises a basic body (12) made of a sound- and heat-insulating material, in which are formed an air conditioning duct (14), which is connectable to an aircraft air conditioning system and provided for supplying an aircraft compartment (22), and a line duct (16) for receiving lines (20) that are provided for supplying the aircraft compartment (22).

Abstract: A differential pressure-controlled locking mechanism (10) comprises a housing (12), as well as a first pressure chamber (14) which is arranged in the housing (12) and which is connectable to a first ambient zone. A second pressure chamber, arranged in the housing (12), is connectable to a second ambient zone and is separated from the first pressure chamber (14) by a mobile separating device (18). The separating device (18) is in an inactive position when the pressure in the first pressure chamber (14) is equal to the pressure in the second pressure chamber. Conversely, the separating device (18) is movable from its inactive position into a differential pressure position when a predetermined differential pressure acts on the separating device (18). An actuation element (22), which is held in a first position by the separating device (18) when the separating device (18) is in its inactive position, is movable into a second position when the mobile separating device (18) is in its differential pressure position.