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Support device assembly for supporting electric strands on fuselage panel of plane, has concave surface, where one support device is arranged at distance equal to or higher than predetermined minimal distance of strands
Support device assembly for supporting electric strands on fuselage panel of plane, has concave surface, where one support device is arranged at distance equal to or higher than predetermined minimal distance of strands
The assembly has a concave surface (40) for partly delimiting a space (45) of advance of electric strands. A fixing unit i.e. screw, is arranged for fixing of a support device on a structural element i.e. fuselage panel, of an aircraft i.e. plane. A contact end (56) is arranged to contact with another support device (18a). One of the support devices is arranged at a distance that is equal to or higher than a predetermined minimal distance of the strands within the space of advance of electric strands. Independent claims are also included for the following: (1) an aircraft (2) a method for fixing strands.
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