Title:
航空機の一連の電気構成要素を合理化する方法、実施アーキテクチャ、および対応する航空機
Document Type and Number:
Japanese Patent JP2014516004
Kind Code:
A
Abstract:
A chain of components for transmitting electric power of an aircraft includes an auxiliary power unit (APU), main engines and end consumer systems via power networks and electronic connections controlled by a unit. The APU supplies power to a shaft by a connection to at least one energy converter unit, via a transmission unit, each converter unit comprising only one convertible electromechanical component. The transmission of power is effected by a direct connection to the transmission unit and to the end consumer system. The connection between a converter unit and the APU is provided by connecting the shaft of the APU to the shaft of the starter/generator (SG) via a directional transmission of power operating in one direction only from the shaft of the APU to the shaft of the SG.
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Inventors:
Erotic, Jean-Michel
Application Number:
JP2014510862A
Publication Date:
July 07, 2014
Filing Date:
May 15, 2012
Export Citation:
Assignee:
TURBOMECA
International Classes:
B64D41/00; F02C6/00; F02C6/08; F02C7/27; F02C7/275
Domestic Patent References:
| JP2001515825A | 2001-09-25 | |||
| JP2007505261A | 2007-03-08 |
Foreign References:
| WO2010046520A2 | 2010-04-29 | |||
| GB2429500A | 2007-02-28 | |||
| US4456830A | 1984-06-26 | |||
| US20070284939A1 | 2007-12-13 | |||
| EP2202395A2 | 2010-06-30 | |||
| US20070000746A1 | 2007-01-04 | |||
| EP2025899A2 | 2009-02-18 | |||
| US5201798A | 1993-04-13 |
Attorney, Agent or Firm:
Kawaguchi International Patent Office