Title:
航空機に搭載される発電、変換、配電及び始動のためのシステム
Document Type and Number:
Japanese Patent JP2010507526
Kind Code:
A
Abstract:
The system has electrical distribution channels (B) e.g. three phase alternating system, for high power loads and electrical distribution channels (G1) for conventional loads e.g. fuel pump. The distribution channels are separated and are powered by starter-generators (SG-B, SG-B1) e.g. brushless three phase synchronous generator, where the channels for high power loads comprise rectifiers (RU-B1, RU-B2) and inverters (MCU-B1, MCU-B2). The generators are driven by a jet engine (Eng1) of an aircraft.
Inventors:
Marc Deuce
Jean-Louis Land
Etienne Foch
Jean-Louis Land
Etienne Foch
Application Number:
JP2009533845A
Publication Date:
March 11, 2010
Filing Date:
October 25, 2007
Export Citation:
Assignee:
Airbus France
International Classes:
B64D41/00; H02P9/04
Domestic Patent References:
| JPH0374143A | 1991-03-28 | |||
| JP2006516230A | 2006-06-29 | |||
| JPH0374143A | 1991-03-28 |
Foreign References:
| US20060061213A1 | 2006-03-23 | |||
| EP1679784A1 | 2006-07-12 | |||
| US6807076B1 | 2004-10-19 | |||
| US20060061213A1 | 2006-03-23 |
Attorney, Agent or Firm:
Masatake Shiga
Takashi Watanabe
Yasuhiko Murayama
Shinya Mitsuhiro
Takashi Watanabe
Yasuhiko Murayama
Shinya Mitsuhiro