FIELD: aircraft.
SUBSTANCE: invention relates to aircraft engineering. Proposed is a structure containing a nacelle 1 or a thrust reverser 18, wherein the structure comprises a fixed part 2 and a movable part 3, as well as: a first guide provided on or in the fixed part of the structure or the movable part of the structure; a first electrical connector 13 attached to the fixed part 2 of the structure; a second electrical connector 16 attached to the movable part 3 of the structure; and a carriage 6 configured to move along the first guide; wherein the carriage comprises an electric cable 8 with a closed loop, installed in or on the body of the carriage 6 so as to allow the cable 8 with a closed loop to rotate, wherein the first electrical connector 13 is electrically connected with the electric cable 8 with a closed loop, and the electrical cable 8 with a closed loop is electrically connected with the second electrical connector 16, thereby providing an electrical connection between the fixed part 2 of the structure and the movable part 3 of the structure.
EFFECT: possibility of providing a stable and reliable electrical connection between the movable part and the fixed part of the structure.
36 cl, 5 dwg
