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Title:
An electric power system for airplanes which has a dual hybrid energy source
Document Type and Number:
Japanese Patent JP2016535579
Kind Code:
A
Abstract:
航空機用の電力システムは、複数の電力消費構成要素を有し、電力消費構成要素のうちのいくつかが平均電力要求量よりも大きい過渡電力要求量を求め、電力システムは、少なくとも１つの発電機と、電力分配バスと、非電池電源と、電池電源と、過渡電力要求量を満足させるために電力分配バスに非電池電源および電池電源を選択的につなげる電力コントローラとを含む。【選択図】図２

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Inventors:
Radun, Arthur Vorwork
Ips, Philip Henry Richard
Application Number:
JP2016540863A
Publication Date:
November 10, 2016
Filing Date:
September 09, 2013
Export Citation:
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Assignee:
GE Aviation Systems LLC
International Classes:
H02J1/00; B64D41/00; H02J7/34
Domestic Patent References:
JP2009171759A2009-07-30
JP2011114899A2011-06-09
Foreign References:
US20090302153A12009-12-10
WO2012111508A12012-08-23
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka



 
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