ACTIVE POWER FACTOR CORRECTION FOR AIRCRAFT POWER SYSTEM HARMONIC MITIGATION
摘要
<p>Active power factor correction can be used to reduce input harmonics in an aircraft power distribution system. In an embodiment, one or more power factor correction (PFC) units can be placed in a power distribution system to profile an input signal. Each PFC unit can include a converter, such as an AC-DC converter, and can be placed in the power system bus on the input side of the load. In an embodiment, a PFC unit can include a boost rectifier topology with active power factor correction for harmonics elimination.</p>
申请公布号
EP2865081(A1)
申请公布日期
2015.04.29
申请号
EP20130713322
申请日期
2013.03.15
申请人
EATON CORPORATION
发明人
MIR, SAYEED, AHMAD;NEELY, JOHN;SEELY, STANLEY;DOUGHERTY, DEREK;THOMPSON, ANDREW;TORRES, PETER;BROADWELL, JAMES;BLAIR, THOMAS