{"title":"飞机机载供电系统用过电压270v变压器整流装置","authors":"D. Gusakov, Denis Masalimov","doi":"10.1109/ICOECS50468.2020.9278413","DOIUrl":null,"url":null,"abstract":"The paper discusses the transition of the aviation industry to the trend of \"all-electric aircraft\", involving the use of electricity to control all subsystems of the aircraft. A numerical calculation of a transformer-rectifier unit was carried out, and a computer model of a rectifier unit with an increased voltage of 270 V was investigated, characteristic oscillograms were obtained, which made it possible to assess the correctness of calculations and the adequacy of the constructed model.","PeriodicalId":363631,"journal":{"name":"2020 International Conference on Electrotechnical Complexes and Systems (ICOECS)","volume":"136 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-10-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Transformer-rectifier unit of overvoltage 270 V for on-board power supply system of aircraft\",\"authors\":\"D. Gusakov, Denis Masalimov\",\"doi\":\"10.1109/ICOECS50468.2020.9278413\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The paper discusses the transition of the aviation industry to the trend of \\\"all-electric aircraft\\\", involving the use of electricity to control all subsystems of the aircraft. A numerical calculation of a transformer-rectifier unit was carried out, and a computer model of a rectifier unit with an increased voltage of 270 V was investigated, characteristic oscillograms were obtained, which made it possible to assess the correctness of calculations and the adequacy of the constructed model.\",\"PeriodicalId\":363631,\"journal\":{\"name\":\"2020 International Conference on Electrotechnical Complexes and Systems (ICOECS)\",\"volume\":\"136 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2020-10-27\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2020 International Conference on Electrotechnical Complexes and Systems (ICOECS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICOECS50468.2020.9278413\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 International Conference on Electrotechnical Complexes and Systems (ICOECS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICOECS50468.2020.9278413","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Transformer-rectifier unit of overvoltage 270 V for on-board power supply system of aircraft
The paper discusses the transition of the aviation industry to the trend of "all-electric aircraft", involving the use of electricity to control all subsystems of the aircraft. A numerical calculation of a transformer-rectifier unit was carried out, and a computer model of a rectifier unit with an increased voltage of 270 V was investigated, characteristic oscillograms were obtained, which made it possible to assess the correctness of calculations and the adequacy of the constructed model.