FIELD: aviation.
SUBSTANCE: clamping system for transport elements contains a lower part, an upper part and a channel system. The lower part has the first set of recesses, and the upper part has the second set of recesses. The lower part is made with the possibility of overlapping the gap between two supporting structures in the aircraft. The upper part is made with the possibility of engagement with the lower part. The channel system is formed by the first set of recesses and the second set of recesses. The channel system is made with the possibility of receiving a set of transport elements when the upper part and the lower part are connected to each other. The clamping system for transport elements electrically isolates a set of transport elements from two supporting structures. A method for stabilizing the transport element in the aircraft and the aircraft are also claimed.
EFFECT: group of inventions is aimed at reducing the time of placement, alignment, processing and sealing of fasteners.
20 cl, 14 dwg
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