ASSEMBLY, equipotential connecting element branches and NETWORK reverse current With equipotential bonding in a nonconducting DESIGN

摘要

1. A process for the compounds with the reverse current equipotential connection network in an aircraft; wherein this network comprises a primary return current network (110, 120, 130) arranged in a longitudinal direction relative to the fuselage and locally detached from each other, one of which (110) at least formed by structural elements (111, 112, 113 ) located in the transverse direction so that the equipotential connections connect the primary network to form a generally reverse current network, characterized in that the aluminum compounds are the cabling (1) of large cross section, forming integrally ekvipot entsialnoe connection between primary nets (110, 120, 130) and between their structural elements (111, 112, 113) disposed in the transverse direction; wherein the device is electrically connected as close as possible to their location through successive lines of intermediates (2, 2 ', 2' ', 2' '') on the equipotential bonding without breaking the wiring is effected by rigid electrical and mechanical assemblies; wherein each interconnect comprises two sealed zones (22) surrounding the central contact zone (21) by stripping (11) with promezhutkom.2. The compound according to Method. 1, according to which the assembly on the cable of each compound (2, 2 ', 2' ', 2' '') is carried out using the selected rigid connection technologies, including bolting, riveting, soldering, welding, crimping and koltsami.3 bond. Connection method according to Claim. 1, according to which a conductive material is applied to the cleaning sheath (11) prior to performing each interconnect assembly (2, 2 ', 2' ', 2' ''). 4. A method according to Claim compound. 1, according to which a