G. W. Ernsberger, H. R. Howell, F. Gourash, J. L. Klingenberger
{"title":"航空航天静态逆变器并联运行","authors":"G. W. Ernsberger, H. R. Howell, F. Gourash, J. L. Klingenberger","doi":"10.1109/TA.1965.4319800","DOIUrl":null,"url":null,"abstract":"Load division was accomplished by locking both static inverters in-phase and automatically controlling the magnitude of each inverter's internal voltage. Mathematical analysis shows (1) that the inverter internal impedance determines design of load division circuit, and (2) any reasonable load division accuracy can be obtained by using sufficient load division circuit gain. This paralleling method can be used with any number of static inverters and offers unique adaptability, reliability, and high power capability for aerospace applications.","PeriodicalId":13050,"journal":{"name":"IEEE Transactions on Aerospace","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"1965-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Parallel Operation of Aerospace Static Inverters\",\"authors\":\"G. W. Ernsberger, H. R. Howell, F. Gourash, J. L. Klingenberger\",\"doi\":\"10.1109/TA.1965.4319800\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Load division was accomplished by locking both static inverters in-phase and automatically controlling the magnitude of each inverter's internal voltage. Mathematical analysis shows (1) that the inverter internal impedance determines design of load division circuit, and (2) any reasonable load division accuracy can be obtained by using sufficient load division circuit gain. This paralleling method can be used with any number of static inverters and offers unique adaptability, reliability, and high power capability for aerospace applications.\",\"PeriodicalId\":13050,\"journal\":{\"name\":\"IEEE Transactions on Aerospace\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1965-06-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Transactions on Aerospace\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/TA.1965.4319800\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Aerospace","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/TA.1965.4319800","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Load division was accomplished by locking both static inverters in-phase and automatically controlling the magnitude of each inverter's internal voltage. Mathematical analysis shows (1) that the inverter internal impedance determines design of load division circuit, and (2) any reasonable load division accuracy can be obtained by using sufficient load division circuit gain. This paralleling method can be used with any number of static inverters and offers unique adaptability, reliability, and high power capability for aerospace applications.
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