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contributor authorKurz, Wolfram
contributor authorDullenkopf, Klaus
contributor authorBauer, Hans
date accessioned2017-05-09T00:58:35Z
date available2017-05-09T00:58:35Z
date issued2013
identifier issn1528-8919
identifier othergtp_135_11_112504.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151724
description abstractThe paper presents results from film thickness measurements in a bearing chamber test rig. The measurements were performed at different operating conditions and with two offtake designs. A discussion of the measurement technique using in situ calibrated capacitive sensors shows good accuracy and repeatability. The film thickness results are first compared to measurements with the same chamber in a vented configuration. The analysis of the measurements at various operating conditions shows a strong influence of the shaft speed, the chamber pressure, and the offtake design. In contrast to that, flow rate and scavenge ratio have only minor influence. Furthermore, the momentum flux of the core air flow is proposed as a suitable parameter with which the influence of shaft speed and pressure can be correlated to the film thickness distribution.
publisherThe American Society of Mechanical Engineers (ASME)
titleCapacitive Film Thickness Measurements in a Ventless Aero Engine Bearing Chamber—Influence of Operating Conditions and Offtake Design
typeJournal Paper
journal volume135
journal issue11
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4025067
journal fristpage112504
journal lastpage112504
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 011
contenttypeFulltext


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