| 发明名称 | Electrical system for an aircraft | ||
| 摘要 | An electrical system for an aircraft is provided. The system comprises an inverter for transforming a first alternating current from an on-board network having a variable frequency into a second alternating current, and at least a first electrical load and at least a second electrical load, which are configured to be operated simultaneously by the second alternating current. | ||
| 申请公布号 | US9302636(B2) | 申请公布日期 | 2016.04.05 |
| 申请号 | US201213718836 | 申请日期 | 2012.12.18 |
| 申请人 | AIRBUS OPERATIONS GMBH | 发明人 | Schult Jens;Everth Henning;Kraus Fabian |
| 分类号 | B60R16/03;H02J4/00 | 主分类号 | B60R16/03 |
| 代理机构 | Ingrassia Fisher & Lorenz, P.C. | 代理人 | Ingrassia Fisher & Lorenz, P.C. |
| 主权项 | 1. An electrical system for an aircraft, the electrical system being configured to drive a group of electric motors which drive a fluid conveying device, the electrical system comprising: an inverter for transforming a first alternating current from an on-board network having a variable frequency into a second alternating current; at least a first electrical load and at least a second electrical load, which are operated simultaneously by the second alternating current; wherein the first electrical load comprises the group of electric motors; wherein the electrical system is configured to, if an electric motor of the group of electric motors is out of operation, increase the frequency of the second alternating current and operate the remaining electric motors at a higher frequency. | ||
| 地址 | Hamburg DE | ||