{"title":"高速飞机中电子设备冷却要求引起的问题","authors":"Nathan A. Carhart","doi":"10.1109/TANE3.1958.4201573","DOIUrl":null,"url":null,"abstract":"High-speed aircraft require the successful operation of large quantities of electronic equipment. The problem of providing a suitable environment for such equipment is of interest to both airplane and electronic designers. A proposal is offered by which cooling provisions may be standardized for airplanes of widely varying performance. Basic design parameters for the development of such a system are outlined, as are the economic factors involved.","PeriodicalId":332621,"journal":{"name":"IRE Transactions on Aeronautical and Navigational Electronics","volume":"28 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1958-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Problems Arising in High-Speed Aircraft Due to Cooling Requirements of Electronic Equipment\",\"authors\":\"Nathan A. Carhart\",\"doi\":\"10.1109/TANE3.1958.4201573\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"High-speed aircraft require the successful operation of large quantities of electronic equipment. The problem of providing a suitable environment for such equipment is of interest to both airplane and electronic designers. A proposal is offered by which cooling provisions may be standardized for airplanes of widely varying performance. Basic design parameters for the development of such a system are outlined, as are the economic factors involved.\",\"PeriodicalId\":332621,\"journal\":{\"name\":\"IRE Transactions on Aeronautical and Navigational Electronics\",\"volume\":\"28 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1958-03-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IRE Transactions on Aeronautical and Navigational Electronics\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/TANE3.1958.4201573\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IRE Transactions on Aeronautical and Navigational Electronics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/TANE3.1958.4201573","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Problems Arising in High-Speed Aircraft Due to Cooling Requirements of Electronic Equipment
High-speed aircraft require the successful operation of large quantities of electronic equipment. The problem of providing a suitable environment for such equipment is of interest to both airplane and electronic designers. A proposal is offered by which cooling provisions may be standardized for airplanes of widely varying performance. Basic design parameters for the development of such a system are outlined, as are the economic factors involved.