Modelling methods for determining fault management requirements in future MEA and MEE platforms

M. Sztykiel; S. D. A. Fletcher; P. J. Norman; S. J. Galloway; G. M. Burt

Modelling methods for determining fault management requirements in future MEA and MEE platforms

M. Sztykiel, S. D. A. Fletcher, P. J. Norman, S. J. Galloway, G. M. Burt

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Abstract

This paper presents a modular transient modelling tool which provides model-based support for the design and technology selection within future MEE and MEA electrical systems. The developed tool is a Matlab/Simulink library consisting of functional sub-system units, which can be rapidly integrated to build complex system architecture models. The paper focusses on the ability of the tool to assess the thermally-defined fault withstand capability of power electronic converters in order to inform on technology trades and derive the operating requirements of the associated power system protection/fault management devices.

Original language	English
Number of pages	4
Publication status	Published - 1 Feb 2017
Event	More Electric Aircraft 2017 - Bordeaux, France Duration: 1 Feb 2017 → 2 Feb 2017

Conference

Conference	More Electric Aircraft 2017
Country/Territory	France
City	Bordeaux
Period	1/02/17 → 2/02/17

Keywords

More-Electric Aircraft
MEA
More-Electric Engine
MEE
aircraft
electrical architecture

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Sztykiel-etal-MEA2017-Modelling-methods-for-determining-fault-management-requirements-in-future-MEA-and-MEE-platformsAccepted author manuscript, 635 KB

Cite this

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title = "Modelling methods for determining fault management requirements in future MEA and MEE platforms",

abstract = "This paper presents a modular transient modelling tool which provides model-based support for the design and technology selection within future MEE and MEA electrical systems. The developed tool is a Matlab/Simulink library consisting of functional sub-system units, which can be rapidly integrated to build complex system architecture models. The paper focusses on the ability of the tool to assess the thermally-defined fault withstand capability of power electronic converters in order to inform on technology trades and derive the operating requirements of the associated power system protection/fault management devices.",

keywords = "More-Electric Aircraft, MEA, More-Electric Engine, MEE, aircraft, electrical architecture",

author = "M. Sztykiel and Fletcher, {S. D. A.} and Norman, {P. J.} and Galloway, {S. J.} and Burt, {G. M.}",

year = "2017",

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note = "More Electric Aircraft 2017 ; Conference date: 01-02-2017 Through 02-02-2017",

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T1 - Modelling methods for determining fault management requirements in future MEA and MEE platforms

AU - Sztykiel, M.

AU - Fletcher, S. D. A.

AU - Norman, P. J.

AU - Galloway, S. J.

AU - Burt, G. M.

PY - 2017/2/1

Y1 - 2017/2/1

N2 - This paper presents a modular transient modelling tool which provides model-based support for the design and technology selection within future MEE and MEA electrical systems. The developed tool is a Matlab/Simulink library consisting of functional sub-system units, which can be rapidly integrated to build complex system architecture models. The paper focusses on the ability of the tool to assess the thermally-defined fault withstand capability of power electronic converters in order to inform on technology trades and derive the operating requirements of the associated power system protection/fault management devices.

AB - This paper presents a modular transient modelling tool which provides model-based support for the design and technology selection within future MEE and MEA electrical systems. The developed tool is a Matlab/Simulink library consisting of functional sub-system units, which can be rapidly integrated to build complex system architecture models. The paper focusses on the ability of the tool to assess the thermally-defined fault withstand capability of power electronic converters in order to inform on technology trades and derive the operating requirements of the associated power system protection/fault management devices.

KW - More-Electric Aircraft

KW - MEA

KW - More-Electric Engine

KW - MEE

KW - aircraft

KW - electrical architecture

M3 - Paper

T2 - More Electric Aircraft 2017

Y2 - 1 February 2017 through 2 February 2017

ER -

Modelling methods for determining fault management requirements in future MEA and MEE platforms

Abstract

Conference

Keywords

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