Application of SMES-FCL in electric aircraft for stability improvement

Hamoud Alafnan, Mariam Elshiekh, Xiaoze Pei, Shadan Altouq, Seyed Mahdi Fazeli, Qixing Sun, Min Zhang, Weijia Yuan

Research output: Contribution to journalArticle

Abstract

The increase in aircraft passengers and airfreight traffic has given rise to concerns about greenhouse gas emissions for traditional aircraft and the resulting damage to the environment. This has led several companies and organizations, including NASA, to set goals to enhance aircraft efficiency as well as reduce fuel burn, pollution, and noise for commercial aircraft. The most notable electric aircraft (EA) concept is the N3-X, which was developed by NASA to achieve environmental goals while maintaining the annual growth of the aviation industry. However, one of the main challenges that EA is facing is their overall weight. This paper proposes and explores an improved power system architecture for use in EA, based on the N3-X concept. The number of superconducting magnetic energy storage (SMES) and fault current limiter (FCL) devices required can be reduced by utilizing multifunctional superconducting devices that combine the functionalities of both a SMES and a FCL, thus reducing the weight and cost of the EA by eliminating a complete device. The proposed control technique offers greater flexibility in determining the appropriate size of coils to function as a FCL, based on the fault type. The proposed EA power system architecture including the SMES-FCL devices is modelled in Simulink/MATLAB to test the system performance under different failure scenarios.

LanguageEnglish
Article number5000906
Number of pages6
JournalIEEE Transactions on Applied Superconductivity
Volume29
Issue number5
Early online date18 Mar 2019
DOIs
Publication statusPublished - 1 Aug 2019

Fingerprint

fly by wire control
Fault current limiters
magnetic energy storage
Energy storage
Aircraft
aircraft
passenger aircraft
commercial aircraft
superconducting devices
greenhouses
NASA
pollution
aeronautics
traffic
Superconducting devices
flexibility
coils
industries
damage
costs

Keywords

  • electric aircraft (EA)
  • fault current limiter (FCL)
  • superconducting magnetic energy storage (SMES)
  • turboelectric distributed propulsion system (TeDP)

Cite this

Alafnan, Hamoud ; Elshiekh, Mariam ; Pei, Xiaoze ; Altouq, Shadan ; Fazeli, Seyed Mahdi ; Sun, Qixing ; Zhang, Min ; Yuan, Weijia. / Application of SMES-FCL in electric aircraft for stability improvement. In: IEEE Transactions on Applied Superconductivity. 2019 ; Vol. 29, No. 5.
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Application of SMES-FCL in electric aircraft for stability improvement. / Alafnan, Hamoud; Elshiekh, Mariam; Pei, Xiaoze; Altouq, Shadan; Fazeli, Seyed Mahdi; Sun, Qixing; Zhang, Min; Yuan, Weijia.

In: IEEE Transactions on Applied Superconductivity, Vol. 29, No. 5, 5000906, 01.08.2019.

Research output: Contribution to journalArticle

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