| 发明名称 |
BUS CONDITIONER FOR AN AIRCRAFT POWER SYSTEM |
| 摘要 |
A bus conditioner for an electrical power system having at least one bus couplable to an electric power generation device driven by a prime mover includes a first energy storage device, a bi-directional power converter including a first converter input electrically connected to the first energy storage device and a converter output for connection to the bus, and a controller operatively coupled to the bi-directional power converter. The controller is configured to maintain a substantially constant load on the power generation device by commanding the power converter to divert excess power into the first energy storage device or use energy from the first storage device to provide power to the bus. |
| 申请公布号 |
US2016105030(A1) |
申请公布日期 |
2016.04.14 |
| 申请号 |
US201514878454 |
申请日期 |
2015.10.08 |
| 申请人 |
Parker-Hannifin Corporation |
发明人 |
Neuhaus Donald;Nedic Velimir |
| 分类号 |
H02J5/00;H02M3/04;H02M7/06;H02M7/44;G06F13/42;G06F1/26 |
主分类号 |
H02J5/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A bus conditioner for an electrical power system having at least one bus couplable to an electric power generation device driven by a prime mover, comprising:
a first energy storage device; a bi-directional power converter including a first converter input electrically connected to the first energy storage device and a converter output for connection to the bus; and a controller operatively coupled to the power converter, the controller configured to maintain a substantially constant load on the power generation device by commanding the power converter to divert excess power into the first energy storage device or use energy from the first storage device to provide power to the bus. |
| 地址 |
Cleveland OH US |
