Title:
航空機用ユニバーサル電力コンバータ
Document Type and Number:
Japanese Patent JP6444079
Kind Code:
B2
Abstract:
A power supply system suitable for use by an aircraft is disclosed. The power system converts power from an unregulated DC power source to multiple AC and DC voltage outputs. The power supply system comprises an interleaved buck converter, and interleaved full-bridge converter, an interleaved inverter, and a control system. In one configuration, the interleaved inverter uses high-voltage DC generated by the interleaved four-bridge converter as its power input to generate a high-voltage AC output.
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Inventors:
Karimi, Camial
Riu, Shoi
Wang, Toan Yang
De leon, francisco
Tan, Qing Chuen
Kuh, Durghong
Tsarkowski, Darius
Chorac, Kelim
Boyarski, Mariusz
Riu, Shoi
Wang, Toan Yang
De leon, francisco
Tan, Qing Chuen
Kuh, Durghong
Tsarkowski, Darius
Chorac, Kelim
Boyarski, Mariusz
Application Number:
JP2014143490A
Publication Date:
December 26, 2018
Filing Date:
July 11, 2014
Export Citation:
Assignee:
The Boeing Company
International Classes:
H02J1/00; B64D41/00; H02M3/155; H02M3/28; H02M7/493
Domestic Patent References:
| JP2013124097A | ||||
| JP2006296185A | ||||
| JP3106876U | ||||
| JP2008001316A | ||||
| JP2001119856A | ||||
| JP2013081362A |
Foreign References:
| US20120232728 | ||||
| US20080123375 |
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori
Kobayashi Yoshinori