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contributor authorPeral, David;Zaid, Ahmed;Benninghoven, Christoph;Araguás-Rodríguez, Silvia;Kluß, David;Karagiannopoulos, Solon;Krewinkel, Robert;Feist, Jörg P.
date accessioned2022-12-27T23:21:10Z
date available2022-12-27T23:21:10Z
date copyright7/21/2022 12:00:00 AM
date issued2022
identifier issn0889-504X
identifier otherturbo_144_11_111007.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4288443
description abstractThe requirement for reduced emissions and the growing demand for gas turbine efficiency are in part met through increasing firing temperatures. However, development budgets leave only limited time for dedicated thermal testing. Consequently, manufacturers are seeking novel temperature measurement technologies to validate new engine designs. This paper will demonstrate how a new temperature mapping technology can be utilized for non-dedicated (multi-cycling) testing while still delivering high-resolution temperature data in a non-dedicated test on a combustor of an industrial gas turbine. Typically, thermocouples are used to monitor the temperature during tests, but they only provide one data point. Color-changing thermal paints are used to deliver measurements over complete surfaces, but they require dedicated testing with short-duration exposure, necessitating dismantling and re-assembling the engine for further testing. Thermal History Coatings (THC) present an alternative solution to providing high-density temperature information. This coating permanently changes consistent with the maximum temperature of exposure during the test. A laser-based instrumentation technique is then used to obtain temperatures. The maximum temperature profile of the surface can be determined through a customized calibration. Given the complex cooling system of a combustor, the high temperatures, and the long-time exposure, this case offers a unique possibility for the testing of the coating under real engine conditions. The coated region covered the external surface of the can. Highly significant is the number of measurement points above 7000 (2 × 2 mm resolution), which enables advanced analysis. This provides insight into the impact of local features, e.g., the region adjacent to a cooling hole. The temperature profile is compared to a computational fluid dynamics-conjugate heat transfer model and thermocouple measurements for the calibration of cooling pre-design methods.
publisherThe American Society of Mechanical Engineers (ASME)
titleHigh-Resolution Thermal Profiling of a Combustor in a Non-Dedicated Test Using Thermal History Coatings
typeJournal Paper
journal volume144
journal issue11
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4054635
journal fristpage111007
journal lastpage111007_12
page12
treeJournal of Turbomachinery:;2022:;volume( 144 ):;issue: 011
contenttypeFulltext


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