The invention relates to an electrical system (100) having: - an electric circuit (102) having a electrically insulating flat support (104) and two electric conductors (106, 108) secured to the flat support, the two electric conductors (106, 108) being designed to have different respective electric potentials during operation of the electric circuit (102), the two electric conductors (106, 108) being separated from one another by an air insulation distance (DI); and - an electrically insulating spacer (110) extending over the flat support (104), between the two electric conductors (106, 108), and having raised elements (112) so as to define a leakage path (DF) between the two electric conductors (106, 108) along the spacer (110), this leakage path (DF) passing via the raised elements (112).
SYSTEME ELECTRIQUE D'UNE PROPULSION ELECTRIQUE D'UN AERONEF
ELECTRICAL SYSTEM OF AN ELECTRIC PROPULSION UNIT OF AN AIRCRAFT
ELEKTRISCHES SYSTEM EINER ELEKTRISCHEN ANTRIEBSEINHEIT EINES FLUGZEUGS
2025-06-18
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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