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124382

REMEDIAL STRATEGIES OF THE FAULTS IN THE DRIVE CIRCUIT OF AIRCRAFT FUEL PUMP

Article

Last updated: 26 Dec 2024

Subjects

-

Tags

Electrical Engineering, Computer Engineering and Electrical power and machines engineering.

Abstract

This paper is aimed at examining the performance of H-bridges supplying fault-tolerant Permanent magnet machine in the aircraft fuel pump under short circuit condition. A significant DC component flows in the windings with a subsequent of saturation and higher iron losses, which possibly deteriorates the performance of the fuel pump. Expressions are derived to predict the inverter current during the fault. Also, the paper discusses all the possible remedial actions and highlights the most suitable one.

DOI

10.21608/jesaun.2010.124382

Authors

First Name

Ahmed AbdEl-malek

Last Name

AbdEl-hafez

MiddleName

-

Affiliation

Lecturer in Electrical department, faculty of engineering, Assiut University P.O. 71561

Email

elhafez@aun.edu.eg

City

-

Orcid

-

Volume

38

Article Issue

No 2

Related Issue

16739

Issue Date

2010-03-01

Receive Date

2009-11-03

Publish Date

2010-03-01

Page Start

547

Page End

554

Print ISSN

1687-0530

Online ISSN

2356-8550

Link

https://jesaun.journals.ekb.eg/article_124382.html

Detail API

https://jesaun.journals.ekb.eg/service?article_code=124382

Order

13

Type

Research Paper

Type Code

1,438

Publication Type

Journal

Publication Title

JES. Journal of Engineering Sciences

Publication Link

https://jesaun.journals.ekb.eg/

MainTitle

REMEDIAL STRATEGIES OF THE FAULTS IN THE DRIVE CIRCUIT OF AIRCRAFT FUEL PUMP

Details

Type

Article

Created At

23 Jan 2023