Pole-to-Pole Fault Management for Electric Aircraft DC Network with HTS Cables
Full-electric propulsion aircraft is attracting a lot of interests in recent years. To improve the power density of electric propulsion systems, superconducting power devices are attractive due to their high current density and high efficiency. Fault analysis and fault management techniques with the...
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| Veröffentlicht in: | IEEE transactions on applied superconductivity 2024-05, Vol.34 (3), p.1-6 |
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| container_title | IEEE transactions on applied superconductivity |
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| creator | Liu, Peilin Zeng, Xianwu Surapaneni, Ravi-Kiran Galla, Gowtham Nilsson, Emelie Rouquette, Jean-francois Berg, Frederick Ybanez, Ludovic Pei, Xiaoze |
| description | Full-electric propulsion aircraft is attracting a lot of interests in recent years. To improve the power density of electric propulsion systems, superconducting power devices are attractive due to their high current density and high efficiency. Fault analysis and fault management techniques with the combination of superconducting power devices are critically needed to ensure the safety and reliability of electric propulsion systems. In this paper, pole-to-pole fault analysis is carried out for the DC network in electric aircraft. High temperature superconducting (HTS) cable modeling is taken into consideration for the fault characterization. A system-level pole-to-pole fault management strategy is proposed to detect and isolate the faults at different locations. The analytical results are verified by the simulation models using Matlab/Simscape. The studies in this paper provide valuable guidance for the design and setting of protection systems in electric aircraft. |
| doi_str_mv | 10.1109/TASC.2024.3363127 |
| format | Article |
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To improve the power density of electric propulsion systems, superconducting power devices are attractive due to their high current density and high efficiency. Fault analysis and fault management techniques with the combination of superconducting power devices are critically needed to ensure the safety and reliability of electric propulsion systems. In this paper, pole-to-pole fault analysis is carried out for the DC network in electric aircraft. High temperature superconducting (HTS) cable modeling is taken into consideration for the fault characterization. A system-level pole-to-pole fault management strategy is proposed to detect and isolate the faults at different locations. The analytical results are verified by the simulation models using Matlab/Simscape. The studies in this paper provide valuable guidance for the design and setting of protection systems in electric aircraft.</description><identifier>ISSN: 1051-8223</identifier><identifier>EISSN: 1558-2515</identifier><identifier>DOI: 10.1109/TASC.2024.3363127</identifier><identifier>CODEN: ITASE9</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>Aircraft ; Circuit breakers ; Circuit faults ; DC network ; electric aircraft (EA) ; Electric cables ; Electric propulsion ; Electronic devices ; Fault currents ; Fault detection ; Fault location ; fault management ; Fly by wire control ; High temperature ; high temperature superconducting (HTS) cables ; High-temperature superconductors ; Propulsion systems ; Superconducting cables ; Superconductivity ; Voltage</subject><ispartof>IEEE transactions on applied superconductivity, 2024-05, Vol.34 (3), p.1-6</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) 2024</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c246t-6a8c5c431a9a5d87ba26e73c819411ef4f6e084f2c5d06934715f6416e3e90473</cites><orcidid>0000-0001-7912-2999 ; 0000-0002-1218-739X ; 0000-0003-0653-9640 ; 0000-0003-1750-9578 ; 0009-0009-7067-4207 ; 0000-0003-2516-8734</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/10433251$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>314,780,784,796,27924,27925,54758</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/10433251$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Liu, Peilin</creatorcontrib><creatorcontrib>Zeng, Xianwu</creatorcontrib><creatorcontrib>Surapaneni, Ravi-Kiran</creatorcontrib><creatorcontrib>Galla, Gowtham</creatorcontrib><creatorcontrib>Nilsson, Emelie</creatorcontrib><creatorcontrib>Rouquette, Jean-francois</creatorcontrib><creatorcontrib>Berg, Frederick</creatorcontrib><creatorcontrib>Ybanez, Ludovic</creatorcontrib><creatorcontrib>Pei, Xiaoze</creatorcontrib><title>Pole-to-Pole Fault Management for Electric Aircraft DC Network with HTS Cables</title><title>IEEE transactions on applied superconductivity</title><addtitle>TASC</addtitle><description>Full-electric propulsion aircraft is attracting a lot of interests in recent years. To improve the power density of electric propulsion systems, superconducting power devices are attractive due to their high current density and high efficiency. Fault analysis and fault management techniques with the combination of superconducting power devices are critically needed to ensure the safety and reliability of electric propulsion systems. In this paper, pole-to-pole fault analysis is carried out for the DC network in electric aircraft. High temperature superconducting (HTS) cable modeling is taken into consideration for the fault characterization. A system-level pole-to-pole fault management strategy is proposed to detect and isolate the faults at different locations. The analytical results are verified by the simulation models using Matlab/Simscape. The studies in this paper provide valuable guidance for the design and setting of protection systems in electric aircraft.</description><subject>Aircraft</subject><subject>Circuit breakers</subject><subject>Circuit faults</subject><subject>DC network</subject><subject>electric aircraft (EA)</subject><subject>Electric cables</subject><subject>Electric propulsion</subject><subject>Electronic devices</subject><subject>Fault currents</subject><subject>Fault detection</subject><subject>Fault location</subject><subject>fault management</subject><subject>Fly by wire control</subject><subject>High temperature</subject><subject>high temperature superconducting (HTS) cables</subject><subject>High-temperature superconductors</subject><subject>Propulsion systems</subject><subject>Superconducting cables</subject><subject>Superconductivity</subject><subject>Voltage</subject><issn>1051-8223</issn><issn>1558-2515</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><sourceid>RIE</sourceid><recordid>eNpNkE1PAjEURRujiYj-ABMXTVwP9vVrOksygpggmoDrppRXHRwY7JQQ_71DcOHqvsW59yWHkFtgAwBWPCyG83LAGZcDIbQAnp-RHihlMq5AnXc3U5AZzsUluWrbNWMgjVQ9MntrasxSkx2Tjt2-TvTFbd0HbnCbaGgiHdXoU6w8HVbRRxcSfSzpDNOhiV_0UKVPOlnMaemWNbbX5CK4usWbv-yT9_FoUU6y6evTczmcZp5LnTLtjFdeCnCFUyuTLx3XmAtvoJAAGGTQyIwM3KsV04WQOaigJWgUWDCZiz65P-3uYvO9xzbZdbOP2-6l5YUwjAsA01Fwonxs2jZisLtYbVz8scDsUZs9arNHbfZPW9e5O3UqRPzHSyE6leIXkPJmeQ</recordid><startdate>20240501</startdate><enddate>20240501</enddate><creator>Liu, Peilin</creator><creator>Zeng, Xianwu</creator><creator>Surapaneni, Ravi-Kiran</creator><creator>Galla, Gowtham</creator><creator>Nilsson, Emelie</creator><creator>Rouquette, Jean-francois</creator><creator>Berg, Frederick</creator><creator>Ybanez, Ludovic</creator><creator>Pei, Xiaoze</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. 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| source | IEEE Electronic Library (IEL) |
| subjects | Aircraft Circuit breakers Circuit faults DC network electric aircraft (EA) Electric cables Electric propulsion Electronic devices Fault currents Fault detection Fault location fault management Fly by wire control High temperature high temperature superconducting (HTS) cables High-temperature superconductors Propulsion systems Superconducting cables Superconductivity Voltage |
| title | Pole-to-Pole Fault Management for Electric Aircraft DC Network with HTS Cables |
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