{"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}
引用次数: 0
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.
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