The invention relates to an electrical system (100) having:-an electrical circuit (102) having an electrically insulating flat support (104) and two electrical conductors (106, 108) fixed to the flat support, the two electrical conductors (106, 108) being designed to have different respective potentials during operation of the electrical circuit (102), the two electrical conductors (106, 108) being separated from each other by an air insulation distance (DI); and-an electrically insulating spacer (110) extending between the two electrical conductors (106, 108) over the flat support (104) and having a raised element (112) to define a leakage path (DF) between the two electrical conductors (106, 108) along the spacer (110), the leakage path (DF) passing through the raised element (112).
本发明涉及一种电气系统(100),该电气系统具有:‑电路(102),电路具有电绝缘的平坦支撑件(104)和固定到平坦支撑件的两个电导体(106,108),两个电导体(106,108)被设计成在电路(102)的运行期间具有不同的相应电势,两个电导体(106,108)以空气绝缘距离(DI)彼此分隔开;以及‑电绝缘的间隔件(110),电绝缘的间隔件在平坦支撑件(104)上方在两个电导体(106,108)之间延伸,并且电绝缘的间隔件具有凸起元件(112)以沿着间隔件(110)在两个电导体(106,108)之间限定出泄漏路径(DF),该泄漏路径(DF)穿过凸起元件(112)。
Electrical system of electric propulsion unit of aircraft
飞行器的电推进单元的电气系统
2025-03-28
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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