| 发明名称 |
METHOD AND SYSTEM FOR SUPPLYING AN AIRCRAFT WITH ELECTRICAL POWER |
| 摘要 |
A method and a system for supplying electrical energy to an aircraft that is equipped with a plurality of loads to be powered, said power supply system comprising a plurality of power sources and an on-board energy management module, the energy management module being electrically connected to said power sources and to said loads to be powered. The energy management module is arranged so as to control a supply of power to at least one of said loads using at least two different power sources in parallel in the event of increased energy requirements, said load being initially powered by a single power source. |
| 申请公布号 |
US2015360630(A1) |
申请公布日期 |
2015.12.17 |
| 申请号 |
US201414763720 |
申请日期 |
2014.01.20 |
| 申请人 |
MICROTURBO |
发明人 |
Rideau Jean-François;Dalmas Florent |
| 分类号 |
B60R16/03;B64D41/00 |
主分类号 |
B60R16/03 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. Method for supplying electrical energy to an aircraft having a plurality of loads to be powered and a power supply system, the power supply system being equipped with a plurality of power sources and an on-board energy management module, the method comprising: controlling, by the energy management module, a power supply to at least one of said loads using at least two different power sources in parallel in the event of increased energy requirements, said load initially being powered by a single power source. |
| 地址 |
Toulouse FR |
