Cable ground connector for use in fuselage cell structure of aircraft, has mechanical connection taking place over component drill-hole, where ground connector is mechanically decoupled from fuselage cell structure

摘要

The connector (38) has a riveting bolt (27) formed in a component drill-hole (31) and comprising thread sections. A cable (23) is connected to an electrical contact surface production component (13) within a fuselage cell structure using a mechanical connection e.g. rivet connection and screw connection. The mechanical connection takes place over the component drill-hole, where the ground connector is mechanically decoupled from the cell structure. A pull-off nut is screwed onto the thread sections, and a primary insulator is attached to a stud bolt using a spring element.