Abstract: A rail system for a cabin of the vehicle comprises a rail with a main extension direction, a fixing element which can be fixed at various positions of the rail to hold a mounting element on the rail, and a cover device for covering the rail. The cover device has several planar cover elements arranged in continuous series extending along the rail, wherein the cover elements are each mounted so as to be pivotable between a closed state in which the respective cover element lies on the rail and an open state in which the respective cover element is removed from the rail. The fixing element has an engagement element which is configured, on displacement of the fixing element along the rail, to reach below a cover element and move the cover element from the closed state to the open state.

Abstract: A connection system for electrically connecting a fixture in a vehicle has at least one cable, and a housing with a cable inlet and a cable outlet, and with a receiving space which is formed in the housing and extends helically along a housing axis with a receiving space cross section from the cable inlet towards the cable outlet. The cable has a cable cross section and runs completely through the receiving space from the cable inlet towards the cable outlet, with cable coils being formed. A radial extent of the cable cross section is smaller than a radial extent of the receiving space cross section. Therefore, different lengths of the at least one cable can be accommodated in the receiving space with different coil diameters being formed.

Abstract: A vehicle cabin seat rail system includes a seat rail having a top side having a plurality of raster openings and mechanically couplable with a cabin floor, a plurality of holding devices positionable on the top side, each being selectively engageable with at least one first raster opening or at least one second raster opening for arresting the holding device and configured for holding an object on the seat rail, and a plurality of marking devices couplable with the seat rail, and configured for optically or mechanically indicating approaching of a first position on the seat rail corresponding to the first raster opening of a respective holding device and of a second position of the same holding device corresponding to the second raster opening, in relation to another object arrested on the seat rail, to prevent an arresting of the holding device on the seat rail on other positions.

Abstract: A connection system for electrically connecting a fixture in a vehicle has at least one cable, and a housing with a cable inlet and a cable outlet, and with a receiving space which is formed in the housing and extends helically along a housing axis with a receiving space cross section from the cable inlet towards the cable outlet. The cable has a cable cross section and runs completely through the receiving space from the cable inlet towards the cable outlet, with cable coils being formed. A radial extent of the cable cross section is smaller than a radial extent of the receiving space cross section. Therefore, different lengths of the at least one cable can be accommodated in the receiving space with different coil diameters being formed.

Abstract: A rail system for a cabin of the vehicle comprises a rail with a main extension direction, a fixing element which can be fixed at various positions of the rail to hold a mounting element on the rail, and a cover device for covering the rail. The cover device has several planar cover elements arranged in continuous series extending along the rail, wherein the cover elements are each mounted so as to be pivotable between a closed state in which the respective cover element lies on the rail and an open state in which the respective cover element is removed from the rail. The fixing element has an engagement element which is configured, on displacement of the fixing element along the rail, to reach below a cover element and move the cover element from the closed state to the open state.

Abstract: A connection box for a system of an aircraft is provided, which includes a plurality of connection boxes, with a holder for holding a line connector for the supply of the system of the aircraft, wherein the system includes, in addition to this connection box, a further connection box with a holder for holding a line connector for the supply of the system of the aircraft. The connection box is configured to receive the further connection box in such a way that both connection boxes can be mounted under an opening in the floor of the aircraft so that both connection boxes are accessible from the opposite side of the floor through the opening in the floor.

Abstract: An apparatus for manufacturing components from a fiber-reinforced composite material by a generative layer construction process including a control device and a tool head fastened to a carrier arm movable via the carrier arm in three spatial directions. The tool head comprises a feed device configured to feed to the tool head a semi-finished layer comprising reinforcing fibers impregnated with a curable plastic material. A shaping device, via movement of the tool head, applies a force to shape the semi-finished layer. A curing device introduces energy into the semi-finished layer, the energy curing the plastic material in the semi-finished layer. The control device controls the movement of the tool head as well as the operations of the feed device, the shaping device and the curing device wherein semi-finished layers are repeatedly fed, shaped, cured and stacked one on top of another to construct the component layer by layer.

Abstract: A connection box for a system of an aircraft is provided, which includes a plurality of connection boxes, with a holder for holding a line connector for the supply of the system of the aircraft, wherein the system includes, in addition to this connection box, a further connection box with a holder for holding a line connector for the supply of the system of the aircraft. The connection box is configured to receive the further connection box in such a way that both connection boxes can be mounted under an opening in the floor of the aircraft so that both connection boxes are accessible from the opposite side of the floor through the opening in the floor.

Abstract: A construction group of an aircraft for feeding a line to a connector section of the cabin module includes a flex zone for providing of at least one cabin module having a connector section for physical connection to a line of the aircraft. The flex zone is configured to receive different cabin modules and/or a cabin module at different positions. The construction group further includes a guide element for guiding the line to be connected to the connector section along the fuselage of the aircraft, and a support element extending along the flex zone for feeding the line from the guide element to the connector section, wherein during the receiving of the construction group in the aircraft, the longitudinal axis of the support element includes a component in direction of the attitudinal axis of the aircraft.

Abstract: A vehicle cabin seat rail system includes a seat rail having a top side having a plurality of raster openings and mechanically couplable with a cabin floor, a plurality of holding devices positionable on the top side, each being selectively engageable with at least one first raster opening or at least one second raster opening for arresting the holding device and configured for holding an object on the seat rail, and a plurality of marking devices couplable with the seat rail, and configured for optically or mechanically indicating approaching of a first position on the seat rail corresponding to the first raster opening of a respective holding device and of a second position of the same holding device corresponding to the second raster opening, in relation to another object arrested on the seat rail, to prevent an arresting of the holding device on the seat rail on other positions.

Abstract: An apparatus for manufacturing components from a fiber-reinforced composite material by a generative layer construction process including a control device and a tool head fastened to a carrier arm movable via the carrier arm in three spatial directions. The tool head comprises a feed device configured to feed to the tool head a semi-finished layer comprising reinforcing fibers impregnated with a curable plastic material. A shaping device, via movement of the tool head, applies a force to shape the semi-finished layer. A curing device introduces energy into the semi-finished layer, the energy curing the plastic material in the semi-finished layer. The control device controls the movement of the tool head as well as the operations of the feed device, the shaping device and the curing device wherein semi-finished layers are repeatedly fed, shaped, cured and stacked one on top of another to construct the component layer by layer.