Abstract: In a method for processing a fiber compound structure, an unhardened fiber layer is arranged on a surface section of the fiber compound structure. A pressure cushion is arranged above the surface section. The pressure cushion has a pressure cap and a pressure-tight cap mat pressure-tightly connected to a circumferential border of the pressure cap such that the cap mat limits a pressure area together with the pressure cap. An overpressure in the pressure area is generated. The pressure cushion is pressed onto the fiber compound structure such that the overpressure presses the cap mat against the fiber layer while supporting the fiber compound structure on a side of the fiber compound structure that is opposed to the surface section.

Abstract: In a method for processing a fibre compound structure, an unhardened fibre layer is arranged on a surface section of the fibre compound structure. A pressure cushion is arranged above the surface section. The pressure cushion has a pressure cap and a pressure-tight cap mat pressure-tightly connected to a circumferential border of the pressure cap such that the cap mat limits a pressure area together with the pressure cap. An overpressure in the pressure area is generated. The pressure cushion is pressed onto the fibre compound structure such that the overpressure presses the cap mat against the fibre layer while supporting the fibre compound structure on a side of the fibre compound structure that is opposed to the surface section.

Abstract: The present invention provides a connecting device for connecting an unhardened fiber layer which is arranged on a surface section of a fiber compound structure to the fiber compound structure. The connecting device comprises pressure cushion comprising a pressure cap for being arranged above the surface section and a pressure tight cap mat which is pressure tightly connected to a circumferential border of the pressure cap, thereby forming a pressure area which is limited by the pressure cap and by the cap mat. The connecting device further comprises a pressure inducing means for inducing an overpressure which presses the cap mat against the fiber layer into the pressure area. According to a further aspect the invention provides a processing method for processing a fiber compound structure. In a first step at least one unhardened fiber layer is arranged on a surface section of the fiber compound structure.

Abstract: The present invention relates to a component, in particular in the field of aviation and spaceflight, having a resin matrix in which carbon nanotubes are embedded for high conductivity of the component.

Abstract: A module for an aircraft for accessing an upper region of the aircraft includes both an ascent region and an accommodation region, with the regions being divided from each other by a divider element. The accommodation region may, for example, be designed as an on-board lavatory. In this way it may be possible to do without the provision of an additional lavatory monument.

Abstract: The present invention provides a connecting device for connecting an unhardened fibre layer which is arranged on a surface section of a fibre compound structure to the fibre compound structure. The connecting device comprises pressure cushion comprising a pressure cap for being arranged above the surface section and a pressure tight cap mat which is pressure tightly connected to a circumferential border of the pressure cap, thereby forming a pressure area which is limited by the pressure cap and by the cap mat. The connecting device further comprises a pressure inducing means for inducing an overpressure which presses the cap mat against the fibre layer into the pressure area. According to a further aspect the invention provides a processing method for processing a fibre compound structure. In a first step at least one unhardened fibre layer is arranged on a surface section of the fibre compound structure.

Abstract: The present invention relates to a component, in particular in the field of aviation and spaceflight, having a resin matrix in which carbon nanotubes are embedded for high conductivity of the component.

Abstract: A module for an aircraft for accessing an upper region of the aircraft includes both an ascent region and an accommodation region, with the regions being divided from each other by a divider element. The accommodation region may, for example, be designed as an on-board lavatory. In this way it may be possible to do without the provision of an additional lavatory monument.