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    Two Phase Flow Pressure Drop in Corrugated Tubes Used in an Aero engine Oil System

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 006::page 62603
    Author:
    Flouros, Michael
    ,
    Kanarachos, Andreas
    ,
    Yakinthos, Kyros
    ,
    Salpingidou, Christina
    ,
    Cottier, Francois
    DOI: 10.1115/1.4031627
    Publisher: 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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      Two Phase Flow Pressure Drop in Corrugated Tubes Used in an Aero engine Oil System

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    http://yetl.yabesh.ir/yetl1/handle/yetl/161086
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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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