{"title":"两种高温液态金属压力测量系统的分析","authors":"A. J. Cassano","doi":"10.1109/TA.1965.4319837","DOIUrl":null,"url":null,"abstract":"A design approach to a high-temperature pressure transducer system for use in closed cycle liquid metal facilities utilizes the displacement of a diaphragm member by the liquid metal pressure. The displacement is then monitored by a suitable transduction device whose output indicates the pressure. A main problem area involves the pertinent characteristics of the transducer. This paper presents the analyses of two transduction system approaches based on (1) thermionic and (2) variable impedance phenomena.","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\":\"Analysis of Two High-Temperature Liquid Metal Pressure Measuring Systems\",\"authors\":\"A. J. Cassano\",\"doi\":\"10.1109/TA.1965.4319837\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A design approach to a high-temperature pressure transducer system for use in closed cycle liquid metal facilities utilizes the displacement of a diaphragm member by the liquid metal pressure. The displacement is then monitored by a suitable transduction device whose output indicates the pressure. A main problem area involves the pertinent characteristics of the transducer. This paper presents the analyses of two transduction system approaches based on (1) thermionic and (2) variable impedance phenomena.\",\"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.1965.4319837\",\"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.1965.4319837","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Analysis of Two High-Temperature Liquid Metal Pressure Measuring Systems
A design approach to a high-temperature pressure transducer system for use in closed cycle liquid metal facilities utilizes the displacement of a diaphragm member by the liquid metal pressure. The displacement is then monitored by a suitable transduction device whose output indicates the pressure. A main problem area involves the pertinent characteristics of the transducer. This paper presents the analyses of two transduction system approaches based on (1) thermionic and (2) variable impedance phenomena.
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