| 摘要 |
An electrical insulating system for a line element that forms part of a f luid system subjected to risks of possible external electrical discharges, s uch as the fuel system of an aircraft. Use is made of an insulating insert ( 12) between two parts (14, 16) of said line element, consisting in providing said parts (14, 16) with grooved edges and in forming the insulating insert (12) between them by means, preferably, of an injection technique, such tha t said insulating insert (12) provides an interior conduit for the passage o f fluid between said parts (14, 16) and covers said grooved edges, guarantee ing the leak tight joining of the insulating insert (12) and said parts (14, 16).
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