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Title:
METHOD FOR HIGH FIDELITY MODELING OF AIRCRAFT ELECTRICAL POWER SYSTEM
Document Type and Number:
Japanese Patent JP2014078227
Kind Code:
A
Abstract:

To provide a method for modeling an electrical power system of an aircraft.

A method 100 of modeling an electrical power system of an aircraft comprises: among others, identifying electrical characteristics 110, mechanical characteristics 112, thermal characteristics 114, and EMI characteristics 116 of the electrical power system; applying at least one circuit-based solver 120 to model at least one of the electrical characteristics; and applying, simultaneously with the circuit-based solver and in real time, a field-based solver to model the remaining electrical characteristics 166, mechanical characteristics 168, thermal characteristics 170, and EMI characteristics 172.


Inventors:
FANG HAO
JIA XIAOCHUAN
Application Number:
JP2013208697A
Publication Date:
May 01, 2014
Filing Date:
October 04, 2013
Export Citation:
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Assignee:
GE AVIAT SYSTEMS LLC
International Classes:
G06F17/50; B64D41/00; B64F5/00
Domestic Patent References:
JPH0876814A1996-03-22
Other References:
大島聡史、外3名: "三次元有限要素法アプリケーションのCUDA向け実装と性能評価", 情報処理学会研究報告 平成23年2月、3月研究発表会開催分 [DVD−ROM], JPN6017037048, 15 April 2011 (2011-04-15), pages pp.1〜6(2011-HPC-129-20)
WU, THOMAS ET AL.: "Electromagnetic Design of Aircraft Synchronous Generator with High Power-Density", 50TH AIAA AEROSPACE SCIENCES MEETING INCLUDING THE NEW HORIZONS FORUM AND AEROSPACE EXPOSITION, JPN6017037045, 12 January 2012 (2012-01-12), pages p.1
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka