| 摘要 |
The present invention relates to a lip unit for a turbojet engine nacelle provided with at least one electrical deicing system (10) including at least one electric heating element (4), which is electrically powered by means of at least one power-supply conductor (P1, P2, P3), each power-supply conductor being associated with a neutral (N) or ground conductor arranged adjacent to the corresponding power-supply conductor, such that said conductors are grouped together. The invention also relates to a nacelle provided with such a unit. |
