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contributor authorJuárez, Raquel
contributor authorCreighton, Barry
contributor authorPetersen, Eric L.
date accessioned2025-04-21T10:22:01Z
date available2025-04-21T10:22:01Z
date copyright1/20/2025 12:00:00 AM
date issued2025
identifier issn0742-4795
identifier othergtp_147_07_071015.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306034
description abstractOperational, efficiency, safety, and economic issues may arise from the formation and accumulation of sludge, varnish, and coke deposits that result from the degradation of engine lubricants through oxidation or thermal breakdown processes. Having a good understanding of the limits of lubricant performance may be useful in determining the best way to protect the engines. To this end, experiments were conducted using Mobil DTE 732, a turbine lubricant, that is aerated using a coarse gas dispersion tube. The oil then flows through a heated test section with a known axial temperature distribution. The inlet and outlet bulk oil temperature measurements are collected and used to determine the amount of time required for deposit formation and buildup. The induction times were determined for various surface temperatures, up to 236 °C. It was found that increased temperatures shortened induction times, and exposure to oxygen increased the rate at which deposits accumulate, but the nature of the deposits, soft and easily removed, was different from those formed during higher-temperature experiments completed in an inert environment in previous studies. Oil samples collected during the test were analyzed with Fourier transform infrared (FTIR) spectroscopy, with no significant changes detected.
publisherThe American Society of Mechanical Engineers (ASME)
titleTemperature Dependence of Aerated Turbine Lubricating Oil Degradation From a Lab-Scale Test Rig
typeJournal Paper
journal volume147
journal issue7
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4066787
journal fristpage71015-1
journal lastpage71015-6
page6
treeJournal of Engineering for Gas Turbines and Power:;2025:;volume( 147 ):;issue: 007
contenttypeFulltext


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