Abstract: The invention comprises a structure having at least two separate air chambers (7) enclosed by flexible, flat material (8) and having flexible bars (9) in the interior thereof for stabilizing an external shape of the air chambers (7). The structure is characterized in that the air chambers (7) form a wall structure (4) in the inflated state. By means of such a wall structure (4)—preferably in conjunction with a corresponding ceiling structure (16)—lightweight berths (1), particularly for aircraft crew, flight passengers, or transported injured persons, can be set up quickly and simply.

Abstract: An arrangement for supplying a load with electrical energy from a power source comprises a textile, woven floor covering (101) with longitudinally running warp threads and transversely running weft threads, three or more current conductors (106) that are spaced apart and substantially parallel to one another being woven in either as warp threads or as weft threads, the current conductors replacing part of a filling warp, a binding warp or the weft threads during the weaving operation. The arrangement also comprises a feed for the connection of the current conductors (106) to the power source and a coupling device (130) for picking up electrical energy from the current conductors (106) in the floor covering (101) and transporting it further to the load when the coupling device (130) is brought into a power pick-up area of the floor covering (101).

Abstract: The invention comprises a structure having at least two separate air chambers (7) enclosed by flexible, flat material (8) and having flexible bars (9) in the interior thereof for stabilizing an external shape of the air chambers (7). The structure is characterized in that the air chambers (7) form a wall structure (4) in the inflated state. By means of such a wall structure (4)—preferably in conjunction with a corresponding ceiling structure (16)—lightweight berths (1), particularly for aircraft crew, flight passengers, or transported injured persons, can be set up quickly and simply.

Abstract: The invention relates to a fire-resistant carpet for aircraft interiors, comprising a machine-woven material, forming a working surface, made from a main yarn, essentially of a fire-resistant thermoplastic synthetic fibre material and an active yarn, essentially of a fire-resistant thermoplastic synthetic fibre material, further comprising a non-woven material, in particular, a needled non-woven material, with a specific weight per area of a maximum of 300 g/m2, preferably a maximum of 250 g/m2, essentially made from a fire-resistant thermoplastic synthetic fibre material and an intermediate layer containing adhesive between the non-woven material and the flat material with a specific weight per area of a maximum of 250 g/m2, preferably a maximum of 200 g/m2, in particular 80 g/m2, and particularly preferred, a maximum of 50 g/m2.