{"title":"导管翼惯性双旋翼:理论、设计与试验","authors":"G. Gress","doi":"10.4050/f-0077-2021-16708","DOIUrl":null,"url":null,"abstract":"\n This paper describes and reports on the status of an electric vertical take-off and landing (eVTOL) aircraft type being developed at Athena Aero Corp that began life as a concept entry in the Boeing-sponsored GoFly Challenge initiated in Sept. 2017. Known as a duct-winged inertial bicopter, the concept was intended to satisfy the Challenge’s basic requirements of giving the pilot an unobstructed forward view within a 90-degree cone and of being able to: \n1.take off and land (essentially) vertically, \n2.transport a 200 lb. person six times around two pylons a half-mile apart at a speed of at least 30kts, and \n3.stay aloft for 20 minutes with a 10-minute fuel/energy reserve,\nall in a single flight. Additionally, the aircraft could be no larger than 8.5 ft. in any direction and had to be quieter than 85 dB at 50 ft. on take-off. \n","PeriodicalId":273020,"journal":{"name":"Proceedings of the Vertical Flight Society 77th Annual Forum","volume":"29 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-05-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Duct-Winged Inertial Bicopter: Theory, Design and Testing\",\"authors\":\"G. Gress\",\"doi\":\"10.4050/f-0077-2021-16708\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"\\n This paper describes and reports on the status of an electric vertical take-off and landing (eVTOL) aircraft type being developed at Athena Aero Corp that began life as a concept entry in the Boeing-sponsored GoFly Challenge initiated in Sept. 2017. Known as a duct-winged inertial bicopter, the concept was intended to satisfy the Challenge’s basic requirements of giving the pilot an unobstructed forward view within a 90-degree cone and of being able to: \\n1.take off and land (essentially) vertically, \\n2.transport a 200 lb. person six times around two pylons a half-mile apart at a speed of at least 30kts, and \\n3.stay aloft for 20 minutes with a 10-minute fuel/energy reserve,\\nall in a single flight. Additionally, the aircraft could be no larger than 8.5 ft. in any direction and had to be quieter than 85 dB at 50 ft. on take-off. \\n\",\"PeriodicalId\":273020,\"journal\":{\"name\":\"Proceedings of the Vertical Flight Society 77th Annual Forum\",\"volume\":\"29 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-05-10\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the Vertical Flight Society 77th Annual Forum\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.4050/f-0077-2021-16708\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the Vertical Flight Society 77th Annual Forum","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.4050/f-0077-2021-16708","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Duct-Winged Inertial Bicopter: Theory, Design and Testing
This paper describes and reports on the status of an electric vertical take-off and landing (eVTOL) aircraft type being developed at Athena Aero Corp that began life as a concept entry in the Boeing-sponsored GoFly Challenge initiated in Sept. 2017. Known as a duct-winged inertial bicopter, the concept was intended to satisfy the Challenge’s basic requirements of giving the pilot an unobstructed forward view within a 90-degree cone and of being able to:
1.take off and land (essentially) vertically,
2.transport a 200 lb. person six times around two pylons a half-mile apart at a speed of at least 30kts, and
3.stay aloft for 20 minutes with a 10-minute fuel/energy reserve,
all in a single flight. Additionally, the aircraft could be no larger than 8.5 ft. in any direction and had to be quieter than 85 dB at 50 ft. on take-off.