Two Phase Flow Pressure Drop in Corrugated Tubes Used in an Aero engine Oil SystemSource: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 006::page 62603Author:Flouros, Michael
,
Kanarachos, Andreas
,
Yakinthos, Kyros
,
Salpingidou, Christina
,
Cottier, Francois
DOI: 10.1115/1.4031627Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In 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.
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contributor author | Flouros, Michael | |
contributor author | Kanarachos, Andreas | |
contributor author | Yakinthos, Kyros | |
contributor author | Salpingidou, Christina | |
contributor author | Cottier, Francois | |
date accessioned | 2017-05-09T01:28:28Z | |
date available | 2017-05-09T01:28:28Z | |
date issued | 2016 | |
identifier issn | 1528-8919 | |
identifier other | gtp_138_06_062603.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/161086 | |
description abstract | In 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. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Two Phase Flow Pressure Drop in Corrugated Tubes Used in an Aero engine Oil System | |
type | Journal Paper | |
journal volume | 138 | |
journal issue | 6 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.4031627 | |
journal fristpage | 62603 | |
journal lastpage | 62603 | |
identifier eissn | 0742-4795 | |
tree | Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 006 | |
contenttype | Fulltext |