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contributor authorFlouros, Michael
contributor authorKanarachos, Andreas
contributor authorYakinthos, Kyros
contributor authorSalpingidou, Christina
contributor authorCottier, Francois
date accessioned2017-05-09T01:28:28Z
date available2017-05-09T01:28:28Z
date issued2016
identifier issn1528-8919
identifier othergtp_138_06_062603.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161086
description abstractIn modern aeroengines, the lubrication system holds a key role due to the demand for high reliability standards. An aeroengine bearing chamber contains components like bearings and gears. Oil is used for lubrication and for heat removal. In order to retain the oil in a bearing chamber, pressurized seals are used. These are pressurized using air from the compressor. In order to avoid overpressurization of the bearing chamber, air/oil passages are provided in the bearing chamber. At the top, a vent pipe discharges most of the sealing air and at the bottom, a scavenge pipe is used for discharging the oil by means of a pump (scavenge pump). The scavenge pipe is setup in most cases by tubes of circular or noncircular cross sections. When the scavenge pipe has to be routed in a way that sharp bends or elbows are unavoidable, flexible (corrugated) pipes can be used. Because of the corrugation, considerable flow resistance with highpressure drop can result. This may cause overpressurization of the bearing compartment with oil loss into the turbomachinery with possibility of ignition, coking (carbon formation), or contamination of the aircraft’s air conditioning system. It is therefore important for the designer to be capable to predict the system’s pressure balance behavior. A real engine bearing chamber sealed by brush seals was used for generating different air/oil mixtures thus corresponding to different engine operating conditions. The mixtures were discharged through a scavenge pipe which was partly setup by corrugated tubes. Instead of a mechanical pump, an ejector was used for evacuating the bearing chamber. An extensive survey covering the existing technical literature on corrugated tube pressure drop was performed and is presented in this paper. The survey has covered both singlephase and multiphase flows. Existing methods were checked against the test results. The method which was most accurately predicting lean air test results from the rig was benchmarked and was used as the basis for extending into a twophase flow pressure drop correlation by applying twophase flow multiplier techniques similar to Lockhart and Martinelli. Comparisons of the new twophase flow pressure drop correlation with an existing correlation by Shannak are presented for mixtures like air/oil, air/water, air/diesel, and air/kerosene. Finally, numerical analysis results using ansys cfx version 15 are presented.
publisherThe American Society of Mechanical Engineers (ASME)
titleTwo Phase Flow Pressure Drop in Corrugated Tubes Used in an Aero engine Oil System
typeJournal Paper
journal volume138
journal issue6
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4031627
journal fristpage62603
journal lastpage62603
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 006
contenttypeFulltext


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