| 发明名称 |
ELECTRICAL DISTRIBUTION SYSTEM FOR AN AIRCRAFT |
| 摘要 |
Electrical distribution system for an aircraft comprising at least one electrical supply path comprising at least one power unit capable of opening or closing the connection between at least one electrical energy source and at least one device of the aircraft. The system comprises protection cards (2b, 2n) each comprising at least two microcontrollers each capable of sending a command to each power unit of the electrical supply paths protected by each protection card and, among the set of microcontrollers of the protection cards, at least two microcontrollers are provided with a communication and computation function with all of the microcontrollers of the protection cards (2b, 2n). |
| 申请公布号 |
US2016048186(A1) |
申请公布日期 |
2016.02.18 |
| 申请号 |
US201514826741 |
申请日期 |
2015.08.14 |
| 申请人 |
ZODIAC AERO ELECTRIC |
发明人 |
Pradier Jean-Clair |
| 分类号 |
G06F1/28;G06F13/36 |
主分类号 |
G06F1/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. Electrical distribution system for an aircraft comprising at least one electrical supply path comprising at least one power unit capable of opening or closing the connection between at least one electrical energy source and at least one device of the aircraft, characterized in that it comprises
protection cards (2b, 2n) each comprising at least two microcontrollers each capable of sending a command to each power unit of the electrical supply paths protected by each protection card, and among the set of microcontrollers of the protection cards, at least two microcontrollers are provided with a communication and computation function with all of the microcontrollers of the protection cards (2b, 2n). |
| 地址 |
Montreuil FR |
