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Conceptual Design and Numerical Analysis of 10 MW Fully Superconducting Synchronous Generators Installed With a Novel Casing Structure
Currently, feasibility studies on fully turboelectric propulsion systems for electric aircrafts are being conducted worldwide. A fully superconducting rotating machine can realize fully turboelectric propulsion systems with light weight and high power density. In the simple casing model considered i...
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Published in: | IEEE transactions on applied superconductivity 2020-06, Vol.30 (4), p.1-7 |
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creator | Komiya, Masataka Sugouchi, Ryota Sasa, Hiromasa Miura, Shun Iwakuma, Masataka Yoshida, Takashi Sasayama, Teruyoshi Yamamoto, Kaoru Tomioka, Akira Konno, Masayuki Izumi, Teruo |
description | Currently, feasibility studies on fully turboelectric propulsion systems for electric aircrafts are being conducted worldwide. A fully superconducting rotating machine can realize fully turboelectric propulsion systems with light weight and high power density. In the simple casing model considered in a previous study, the field winding forms a large percentage of the generator weight. Therefore, to reveal the relationship between the operation temperature of the field winding and output power density, we compared an inner cryostat model having a field winding operation temperature of 20 K with the simple casing model having a field winding operation temperature of 64 K in terms of the output power density, efficiency, and increasing temperature. The stator and rotor rooms of the inner cryostat model were insulated by introducing the vacuum layer. The inner cryostat casing structure can have a lower refrigerant gas temperature, e.g., 20 K. Consequently, the temperature of the simple model increased from 5.4 to 7.1 K and that of the inner cryostat model increased from 3.0 to 6.1 K. The simple and inner cryostat models' power densities were 18.8 and 21.7 kW/kg, respectively. Both models achieved 99% efficiency. No major difference was observed between both models in terms of efficiency and output power density. |
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A fully superconducting rotating machine can realize fully turboelectric propulsion systems with light weight and high power density. In the simple casing model considered in a previous study, the field winding forms a large percentage of the generator weight. Therefore, to reveal the relationship between the operation temperature of the field winding and output power density, we compared an inner cryostat model having a field winding operation temperature of 20 K with the simple casing model having a field winding operation temperature of 64 K in terms of the output power density, efficiency, and increasing temperature. The stator and rotor rooms of the inner cryostat model were insulated by introducing the vacuum layer. The inner cryostat casing structure can have a lower refrigerant gas temperature, e.g., 20 K. Consequently, the temperature of the simple model increased from 5.4 to 7.1 K and that of the inner cryostat model increased from 3.0 to 6.1 K. The simple and inner cryostat models' power densities were 18.8 and 21.7 kW/kg, respectively. Both models achieved 99% efficiency. No major difference was observed between both models in terms of efficiency and output power density.</description><identifier>ISSN: 1051-8223</identifier><identifier>EISSN: 1558-2515</identifier><identifier>DOI: 10.1109/TASC.2020.2989746</identifier><identifier>CODEN: ITASE9</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>Atmospheric modeling ; Conceptual design ; Efficiency ; Electric aircraft ; Feasibility studies ; Fully superconducting generator ; Gas temperature ; Generators ; Mathematical model ; Numerical analysis ; Propulsion systems ; REBCO ; Refrigerants ; Rotating machinery ; Rotating machines ; Rotors ; scribing ; Superconductivity ; Thermal analysis ; Weight reduction ; Winding ; Windings</subject><ispartof>IEEE transactions on applied superconductivity, 2020-06, Vol.30 (4), p.1-7</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) 2020</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c293t-264404e5bcbb514c6702b4d96f86c71b073e17e88d381a7037ebc52c6b20d4a13</citedby><cites>FETCH-LOGICAL-c293t-264404e5bcbb514c6702b4d96f86c71b073e17e88d381a7037ebc52c6b20d4a13</cites><orcidid>0000-0002-7700-3555 ; 0000-0003-3560-3613 ; 0000-0002-6307-7940 ; 0000-0002-5470-1190 ; 0000-0003-2841-286X ; 0000-0003-1097-2869 ; 0000-0003-1888-3529</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/9076878$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>314,780,784,27924,27925,54796</link.rule.ids></links><search><creatorcontrib>Komiya, Masataka</creatorcontrib><creatorcontrib>Sugouchi, Ryota</creatorcontrib><creatorcontrib>Sasa, Hiromasa</creatorcontrib><creatorcontrib>Miura, Shun</creatorcontrib><creatorcontrib>Iwakuma, Masataka</creatorcontrib><creatorcontrib>Yoshida, Takashi</creatorcontrib><creatorcontrib>Sasayama, Teruyoshi</creatorcontrib><creatorcontrib>Yamamoto, Kaoru</creatorcontrib><creatorcontrib>Tomioka, Akira</creatorcontrib><creatorcontrib>Konno, Masayuki</creatorcontrib><creatorcontrib>Izumi, Teruo</creatorcontrib><title>Conceptual Design and Numerical Analysis of 10 MW Fully Superconducting Synchronous Generators Installed With a Novel Casing Structure</title><title>IEEE transactions on applied superconductivity</title><addtitle>TASC</addtitle><description>Currently, feasibility studies on fully turboelectric propulsion systems for electric aircrafts are being conducted worldwide. A fully superconducting rotating machine can realize fully turboelectric propulsion systems with light weight and high power density. In the simple casing model considered in a previous study, the field winding forms a large percentage of the generator weight. Therefore, to reveal the relationship between the operation temperature of the field winding and output power density, we compared an inner cryostat model having a field winding operation temperature of 20 K with the simple casing model having a field winding operation temperature of 64 K in terms of the output power density, efficiency, and increasing temperature. The stator and rotor rooms of the inner cryostat model were insulated by introducing the vacuum layer. The inner cryostat casing structure can have a lower refrigerant gas temperature, e.g., 20 K. Consequently, the temperature of the simple model increased from 5.4 to 7.1 K and that of the inner cryostat model increased from 3.0 to 6.1 K. The simple and inner cryostat models' power densities were 18.8 and 21.7 kW/kg, respectively. Both models achieved 99% efficiency. No major difference was observed between both models in terms of efficiency and output power density.</description><subject>Atmospheric modeling</subject><subject>Conceptual design</subject><subject>Efficiency</subject><subject>Electric aircraft</subject><subject>Feasibility studies</subject><subject>Fully superconducting generator</subject><subject>Gas temperature</subject><subject>Generators</subject><subject>Mathematical model</subject><subject>Numerical analysis</subject><subject>Propulsion systems</subject><subject>REBCO</subject><subject>Refrigerants</subject><subject>Rotating machinery</subject><subject>Rotating machines</subject><subject>Rotors</subject><subject>scribing</subject><subject>Superconductivity</subject><subject>Thermal analysis</subject><subject>Weight reduction</subject><subject>Winding</subject><subject>Windings</subject><issn>1051-8223</issn><issn>1558-2515</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNo9kEtOwzAQhiMEEuVxAMTGEuuUsWPHzrIKFJB4LApiGTnOlKZK7WLHSD0B1-AsnIyUIlbza_R_I82XJGcUxpRCcfk8mZVjBgzGrFCF5PleMqJCqJQJKvaHDIKmirHsMDkKYQlAueJilHyWzhpc91F35ApD-2aJtg15jCv0rRmWE6u7TWgDcXNC4fvr4ZVMY9dtyCyu0Rtnm2j61r6R2caahXfWxUBu0KLXvfOB3NnQ667Dhry2_YJo8ug-sCOlDr9Q7wc8ejxJDua6C3j6N4-Tl-n1c3mb3j_d3JWT-9SwIutTlnMOHEVt6lpQbnIJrOZNkc9VbiStQWZIJSrVZIpqCZnE2ghm8ppBwzXNjpOL3d21d-8RQ18tXfTDj6FiHCRwYJwNLbprGe9C8Div1r5dab-pKFRb39XWd7X1Xf35HpjzHdMi4n-_AJkrqbIfh7R95Q</recordid><startdate>20200601</startdate><enddate>20200601</enddate><creator>Komiya, Masataka</creator><creator>Sugouchi, Ryota</creator><creator>Sasa, Hiromasa</creator><creator>Miura, Shun</creator><creator>Iwakuma, Masataka</creator><creator>Yoshida, Takashi</creator><creator>Sasayama, Teruyoshi</creator><creator>Yamamoto, Kaoru</creator><creator>Tomioka, Akira</creator><creator>Konno, Masayuki</creator><creator>Izumi, Teruo</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. 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A fully superconducting rotating machine can realize fully turboelectric propulsion systems with light weight and high power density. In the simple casing model considered in a previous study, the field winding forms a large percentage of the generator weight. Therefore, to reveal the relationship between the operation temperature of the field winding and output power density, we compared an inner cryostat model having a field winding operation temperature of 20 K with the simple casing model having a field winding operation temperature of 64 K in terms of the output power density, efficiency, and increasing temperature. The stator and rotor rooms of the inner cryostat model were insulated by introducing the vacuum layer. The inner cryostat casing structure can have a lower refrigerant gas temperature, e.g., 20 K. Consequently, the temperature of the simple model increased from 5.4 to 7.1 K and that of the inner cryostat model increased from 3.0 to 6.1 K. The simple and inner cryostat models' power densities were 18.8 and 21.7 kW/kg, respectively. Both models achieved 99% efficiency. No major difference was observed between both models in terms of efficiency and output power density.</abstract><cop>New York</cop><pub>IEEE</pub><doi>10.1109/TASC.2020.2989746</doi><tpages>7</tpages><orcidid>https://orcid.org/0000-0002-7700-3555</orcidid><orcidid>https://orcid.org/0000-0003-3560-3613</orcidid><orcidid>https://orcid.org/0000-0002-6307-7940</orcidid><orcidid>https://orcid.org/0000-0002-5470-1190</orcidid><orcidid>https://orcid.org/0000-0003-2841-286X</orcidid><orcidid>https://orcid.org/0000-0003-1097-2869</orcidid><orcidid>https://orcid.org/0000-0003-1888-3529</orcidid></addata></record> |
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subjects | Atmospheric modeling Conceptual design Efficiency Electric aircraft Feasibility studies Fully superconducting generator Gas temperature Generators Mathematical model Numerical analysis Propulsion systems REBCO Refrigerants Rotating machinery Rotating machines Rotors scribing Superconductivity Thermal analysis Weight reduction Winding Windings |
title | Conceptual Design and Numerical Analysis of 10 MW Fully Superconducting Synchronous Generators Installed With a Novel Casing Structure |
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