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    Windage Power Losses From Spiral Bevel Gears With Varying Oil Flows and Shroud Configurations

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 004::page 41019
    Author:
    Graham Johnson
    ,
    Budi Chandra
    ,
    Colin Foord
    ,
    Kathy Simmons
    DOI: 10.1115/1.3072519
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In many aero-engines, the power to drive accessories is transmitted through high speed bevel gears in a chamber in the center of the engine. The windage power loss (WPL) associated with these gears makes a significant contribution to the overall heat generation within the chamber. Shrouding the gears provides an effective method of reducing this WPL and managing the flow of lubricating oil. Experimental and computational programs at the University of Nottingham Technology Centre in Gas Turbine Transmission Systems are providing an improved understanding of shroud performance and design. This paper presents the results from a pair of shrouded meshing gears run at representative speeds and oil flow in a rig with speed and torque measurement. A previously published study of a single bevel gear operating in air (, 2007, “Experimental Investigation Into Windage Power Loss From a Shrouded Spiral Bevel Gear” ASME Paper No. GT2007-27885) found a reduction in torque of up to 70% from shrouding. In this work, the addition of oil and the pinion gear did not lead to high torque due to the buildup of oil under the shrouds, but the reduction in torque due to fitting the shrouds is significantly less than was found for the same gear in air alone. In order to isolate the various parameters, further testing with a single gear was carried out. A fully (360 deg) shrouded gear shows a big improvement over an unshrouded gear when running in air alone, but much of this benefit disappears as soon as a very small amount of oil is introduced under the shroud. This implies that the oil is recirculating under the shroud. Increasing the oil flow beyond this initial level increases the torque by the amount required to accelerate the oil mass flow up to the peripheral speed of the gear. Providing a full width slot in the shroud downstream of the oil jet allows the oil to escape without any recirculation and restores much of the benefit of the shroud. Further insight into the oil behavior is obtained from torque measurements and observations through a transparent shroud and with various slot configurations. Video observation shows evidence of a vortex flow under the shroud that carries some of the oil toward the inner diameter of the gear. The three main windage contributors, air alone, recirculation of oil under the shroud, and acceleration of the feed oil, are quantified and methods for achieving the optimum design are discussed.
    keyword(s): Torque , Flow (Dynamics) , Gears , Transparency AND Testing ,
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      Windage Power Losses From Spiral Bevel Gears With Varying Oil Flows and Shroud Configurations

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    https://yetl.yabesh.ir/yetl1/handle/yetl/142150
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    • Journal of Turbomachinery

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    contributor authorGraham Johnson
    contributor authorBudi Chandra
    contributor authorColin Foord
    contributor authorKathy Simmons
    date accessioned2017-05-09T00:35:46Z
    date available2017-05-09T00:35:46Z
    date copyrightOctober, 2009
    date issued2009
    identifier issn0889-504X
    identifier otherJOTUEI-28758#041019_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142150
    description abstractIn many aero-engines, the power to drive accessories is transmitted through high speed bevel gears in a chamber in the center of the engine. The windage power loss (WPL) associated with these gears makes a significant contribution to the overall heat generation within the chamber. Shrouding the gears provides an effective method of reducing this WPL and managing the flow of lubricating oil. Experimental and computational programs at the University of Nottingham Technology Centre in Gas Turbine Transmission Systems are providing an improved understanding of shroud performance and design. This paper presents the results from a pair of shrouded meshing gears run at representative speeds and oil flow in a rig with speed and torque measurement. A previously published study of a single bevel gear operating in air (, 2007, “Experimental Investigation Into Windage Power Loss From a Shrouded Spiral Bevel Gear” ASME Paper No. GT2007-27885) found a reduction in torque of up to 70% from shrouding. In this work, the addition of oil and the pinion gear did not lead to high torque due to the buildup of oil under the shrouds, but the reduction in torque due to fitting the shrouds is significantly less than was found for the same gear in air alone. In order to isolate the various parameters, further testing with a single gear was carried out. A fully (360 deg) shrouded gear shows a big improvement over an unshrouded gear when running in air alone, but much of this benefit disappears as soon as a very small amount of oil is introduced under the shroud. This implies that the oil is recirculating under the shroud. Increasing the oil flow beyond this initial level increases the torque by the amount required to accelerate the oil mass flow up to the peripheral speed of the gear. Providing a full width slot in the shroud downstream of the oil jet allows the oil to escape without any recirculation and restores much of the benefit of the shroud. Further insight into the oil behavior is obtained from torque measurements and observations through a transparent shroud and with various slot configurations. Video observation shows evidence of a vortex flow under the shroud that carries some of the oil toward the inner diameter of the gear. The three main windage contributors, air alone, recirculation of oil under the shroud, and acceleration of the feed oil, are quantified and methods for achieving the optimum design are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleWindage Power Losses From Spiral Bevel Gears With Varying Oil Flows and Shroud Configurations
    typeJournal Paper
    journal volume131
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3072519
    journal fristpage41019
    identifier eissn1528-8900
    keywordsTorque
    keywordsFlow (Dynamics)
    keywordsGears
    keywordsTransparency AND Testing
    treeJournal of Turbomachinery:;2009:;volume( 131 ):;issue: 004
    contenttypeFulltext
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