{"title":"商用超音速航空运输二次动力系统的研制","authors":"M. Cronin, P. Frankel","doi":"10.1109/TA.1965.4319828","DOIUrl":null,"url":null,"abstract":"A secondary power system in which all secondary power was extracted from the engine by means of large, variable-voltage, variable-frequency generators was proposed for the Lockheed Phase I SST. The quantity of constant frequency power required in the Phase IIA airplane was not favorable to such a system. The selected system uses wing mounted accessory gear boxes, shaft driven from the engine. CSD/generators on the gear boxes generate the 240/416 volt, 400 cycle ac power which is utilized directly by the major loads.","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\":\"The Development of a Secondary Power System for a Commercial Supersonic Air Transport\",\"authors\":\"M. Cronin, P. Frankel\",\"doi\":\"10.1109/TA.1965.4319828\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A secondary power system in which all secondary power was extracted from the engine by means of large, variable-voltage, variable-frequency generators was proposed for the Lockheed Phase I SST. The quantity of constant frequency power required in the Phase IIA airplane was not favorable to such a system. The selected system uses wing mounted accessory gear boxes, shaft driven from the engine. CSD/generators on the gear boxes generate the 240/416 volt, 400 cycle ac power which is utilized directly by the major loads.\",\"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.1965.4319828\",\"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.1965.4319828","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
The Development of a Secondary Power System for a Commercial Supersonic Air Transport
A secondary power system in which all secondary power was extracted from the engine by means of large, variable-voltage, variable-frequency generators was proposed for the Lockheed Phase I SST. The quantity of constant frequency power required in the Phase IIA airplane was not favorable to such a system. The selected system uses wing mounted accessory gear boxes, shaft driven from the engine. CSD/generators on the gear boxes generate the 240/416 volt, 400 cycle ac power which is utilized directly by the major loads.
求助内容：
应助结果提醒方式：
京公网安备 11010802042870号
