{"title":"基于倾斜尾桨垂直起降鸭式改型三旋翼机的试制","authors":"K. Hayama, Tomohiro Kudou, H. Irie","doi":"10.12792/icisip2021.035","DOIUrl":null,"url":null,"abstract":"The trial production of a new concept vertical take-off and landing (VTOL) canard aircraft based on the modified tricopter with tilt tail rotor was carried out for aerial, observation and research. Continuous transition from vertical to horizontal flight can be done by tilting the tail rotor supported with canard wing. The lift of wing during horizontal flight supported the weight of the aircraft, and its causes the reduction of power consumption and extend the flight area.","PeriodicalId":431446,"journal":{"name":"The Proceedings of The 8th International Conference on Intelligent Systems and Image Processing 2021","volume":"25 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Trial Production of Modified Tricopter Based Vertical Take-off Landing Canard Aircraft with Tilt Tail Rotor\",\"authors\":\"K. Hayama, Tomohiro Kudou, H. Irie\",\"doi\":\"10.12792/icisip2021.035\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The trial production of a new concept vertical take-off and landing (VTOL) canard aircraft based on the modified tricopter with tilt tail rotor was carried out for aerial, observation and research. Continuous transition from vertical to horizontal flight can be done by tilting the tail rotor supported with canard wing. The lift of wing during horizontal flight supported the weight of the aircraft, and its causes the reduction of power consumption and extend the flight area.\",\"PeriodicalId\":431446,\"journal\":{\"name\":\"The Proceedings of The 8th International Conference on Intelligent Systems and Image Processing 2021\",\"volume\":\"25 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"The Proceedings of The 8th International Conference on Intelligent Systems and Image Processing 2021\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.12792/icisip2021.035\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"The Proceedings of The 8th International Conference on Intelligent Systems and Image Processing 2021","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.12792/icisip2021.035","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Trial Production of Modified Tricopter Based Vertical Take-off Landing Canard Aircraft with Tilt Tail Rotor
The trial production of a new concept vertical take-off and landing (VTOL) canard aircraft based on the modified tricopter with tilt tail rotor was carried out for aerial, observation and research. Continuous transition from vertical to horizontal flight can be done by tilting the tail rotor supported with canard wing. The lift of wing during horizontal flight supported the weight of the aircraft, and its causes the reduction of power consumption and extend the flight area.
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