Temperature Measurement for Advanced Gas Turbine Controls
Modern gas turbine engines with turbine inlet temperatures higher than metal melting temperatures must have control systems which provide subsecond response to changes in gas or metal temperatures. High quality data are required to provide for the most efficient engine operation consistent with engi...
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| Veröffentlicht in: | SAE transactions 1975-01, Vol.84, p.782-796 |
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| container_title | SAE transactions |
| container_volume | 84 |
| creator | Rohy, David A. Duffy, T. E. Compton, W. A. |
| description | Modern gas turbine engines with turbine inlet temperatures higher than metal melting temperatures must have control systems which provide subsecond response to changes in gas or metal temperatures. High quality data are required to provide for the most efficient engine operation consistent with engine safety. Recently developed instruments measure individual blade temperature; another non-immersion gas temperature sensor, not yet fully developed, will provide accurate gas temperature data up to 1900°C. These instruments are described with present and potential uses in control systems. |
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A.</creatorcontrib><description>Modern gas turbine engines with turbine inlet temperatures higher than metal melting temperatures must have control systems which provide subsecond response to changes in gas or metal temperatures. High quality data are required to provide for the most efficient engine operation consistent with engine safety. Recently developed instruments measure individual blade temperature; another non-immersion gas temperature sensor, not yet fully developed, will provide accurate gas temperature data up to 1900°C. These instruments are described with present and potential uses in control systems.</description><identifier>ISSN: 0096-736X</identifier><identifier>EISSN: 2577-1531</identifier><language>eng</language><publisher>SOCIETY OF AUTOMOTIVE ENGINEERS, INC</publisher><subject>Electric potential ; Engines ; Gas temperature ; Pyrometers ; Sensors ; Signal detection ; Temperature control ; Temperature measurement ; Turbine blades ; Turbines</subject><ispartof>SAE transactions, 1975-01, Vol.84, p.782-796</ispartof><rights>Copyright © Society of Automotive Engineers, Inc., 1976</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.jstor.org/stable/pdf/44681967$$EPDF$$P50$$Gjstor$$H</linktopdf><linktohtml>$$Uhttps://www.jstor.org/stable/44681967$$EHTML$$P50$$Gjstor$$H</linktohtml><link.rule.ids>314,776,780,799,57992,58225</link.rule.ids></links><search><creatorcontrib>Rohy, David A.</creatorcontrib><creatorcontrib>Duffy, T. E.</creatorcontrib><creatorcontrib>Compton, W. A.</creatorcontrib><title>Temperature Measurement for Advanced Gas Turbine Controls</title><title>SAE transactions</title><description>Modern gas turbine engines with turbine inlet temperatures higher than metal melting temperatures must have control systems which provide subsecond response to changes in gas or metal temperatures. High quality data are required to provide for the most efficient engine operation consistent with engine safety. Recently developed instruments measure individual blade temperature; another non-immersion gas temperature sensor, not yet fully developed, will provide accurate gas temperature data up to 1900°C. These instruments are described with present and potential uses in control systems.</description><subject>Electric potential</subject><subject>Engines</subject><subject>Gas temperature</subject><subject>Pyrometers</subject><subject>Sensors</subject><subject>Signal detection</subject><subject>Temperature control</subject><subject>Temperature measurement</subject><subject>Turbine blades</subject><subject>Turbines</subject><issn>0096-736X</issn><issn>2577-1531</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1975</creationdate><recordtype>article</recordtype><sourceid/><recordid>eNqFybsOgjAUANDGaCI-PsGkP0DSUmhlNMTH4sbARqpcEgi05N5i4t_r4O50hrNgUZIZE8tMySWLhMh1bJSu1mxD1AuhZGaSiOUljBOgDTMCv4OlryO4wFuP_NS8rHtCw6-WeDnjo3PAC-8C-oF2bNXagWD_c8sOl3NZ3OKegsd6wm60-K7TVB9lro369x_tujO3</recordid><startdate>19750101</startdate><enddate>19750101</enddate><creator>Rohy, David A.</creator><creator>Duffy, T. E.</creator><creator>Compton, W. A.</creator><general>SOCIETY OF AUTOMOTIVE ENGINEERS, INC</general><scope/></search><sort><creationdate>19750101</creationdate><title>Temperature Measurement for Advanced Gas Turbine Controls</title><author>Rohy, David A. ; Duffy, T. E. ; Compton, W. A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-jstor_primary_446819673</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1975</creationdate><topic>Electric potential</topic><topic>Engines</topic><topic>Gas temperature</topic><topic>Pyrometers</topic><topic>Sensors</topic><topic>Signal detection</topic><topic>Temperature control</topic><topic>Temperature measurement</topic><topic>Turbine blades</topic><topic>Turbines</topic><toplevel>online_resources</toplevel><creatorcontrib>Rohy, David A.</creatorcontrib><creatorcontrib>Duffy, T. E.</creatorcontrib><creatorcontrib>Compton, W. A.</creatorcontrib><jtitle>SAE transactions</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Rohy, David A.</au><au>Duffy, T. E.</au><au>Compton, W. A.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Temperature Measurement for Advanced Gas Turbine Controls</atitle><jtitle>SAE transactions</jtitle><date>1975-01-01</date><risdate>1975</risdate><volume>84</volume><spage>782</spage><epage>796</epage><pages>782-796</pages><issn>0096-736X</issn><eissn>2577-1531</eissn><abstract>Modern gas turbine engines with turbine inlet temperatures higher than metal melting temperatures must have control systems which provide subsecond response to changes in gas or metal temperatures. High quality data are required to provide for the most efficient engine operation consistent with engine safety. Recently developed instruments measure individual blade temperature; another non-immersion gas temperature sensor, not yet fully developed, will provide accurate gas temperature data up to 1900°C. These instruments are described with present and potential uses in control systems.</abstract><pub>SOCIETY OF AUTOMOTIVE ENGINEERS, INC</pub></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0096-736X |
| ispartof | SAE transactions, 1975-01, Vol.84, p.782-796 |
| issn | 0096-736X 2577-1531 |
| language | eng |
| recordid | cdi_jstor_primary_44681967 |
| source | Jstor Complete Legacy |
| subjects | Electric potential Engines Gas temperature Pyrometers Sensors Signal detection Temperature control Temperature measurement Turbine blades Turbines |
| title | Temperature Measurement for Advanced Gas Turbine Controls |
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