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contributor authorJeff Jablin
contributor authorSensor Engineering Manager
contributor authorMichael R. Storar
contributor authorInstrument Maintenance Master Technician
contributor authorPhillip L. Gray
contributor authorStaff Engineer
contributor authorElectrical Instrument
date accessioned2017-05-09T00:02:18Z
date available2017-05-09T00:02:18Z
date copyrightOctober, 2000
date issued2000
identifier issn1528-8919
identifier otherJETPEZ-26800#659_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123629
description abstractThe development of a “stabilized” temperature sensor has led to significant increases in turbine operating efficiency by maximizing output when compared with present sensor technology. These stabilized type K and E thermocouples are superior to existing standard non-stabilized thermocouples because they are not prone to the typical aging effects in the 400 to 600°C (752 to 1112°F) temperature range that can result in measurements errors. A complete set of 18 stabilized type K thermocouples were installed on the exhaust of several gas turbines used for power generation. These thermocouples were subjected to normal operating conditions for a period of one year. During that year, the increase in turbine output has ranged from 0.5 percent to almost 2.0 percent. This increase in output also translates into significant cost savings. In addition, the stabilized thermocouples have given the turbine maintenance technicians more confidence in the accuracy of their temperature measurements and resulted in improved troubleshooting and decision making. [S0742-4795(00)02502-3]
publisherThe American Society of Mechanical Engineers (ASME)
titleImproved Operating Efficiency Through the Use of Stabilized Thermocouples
typeJournal Paper
journal volume122
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1285845
journal fristpage659
journal lastpage663
identifier eissn0742-4795
keywordsThermocouples
keywordsTurbines AND Temperature
treeJournal of Engineering for Gas Turbines and Power:;2000:;volume( 122 ):;issue: 004
contenttypeFulltext


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