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    A New Tailpipe Design for GE Frame-Type Gas Turbines to Substantially Lower Pressure Losses

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 001::page 128
    Author:
    Richard Golomb
    ,
    Vivek Sahai
    ,
    Dah Yu Cheng
    DOI: 10.1115/1.1515335
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Many GE frame gas turbines have a unique 90-deg tailpipe exhaust system that contains struts, diffusers, and turning vanes. As confirmed in a recent report by GE and other authors, it is known in the industry that this tailpipe design has large pressure losses. In this recent report a pressure loss as high as 60 in. of water (0.15 kgs/sqcm) was cited. Due to the flow separations they create, the report indicates that the struts can cause very high-pressure losses in the turbine. The report also states that these pressure losses can vary with different turbine load conditions. Cheng Fluid Systems and Cheng Power Systems have conducted a study aimed at substantially reducing these pressure losses. Flow control technology introduced to the refinery industry, i.e., the Cheng Rotation Vane (CRV) and the Large Angle Diffuser (LAD) can be used to mitigate the flow separation and turbulence that occurs in turns, bends, and large sudden expansions. Specifically the CRV addresses the flow separations in pipe turns, and the LAD addresses the flow problems that occur with large sudden expansion areas. The paper will introduce the past experience of the CRV and LAD, and will then use computer simulations to show the flow characteristics around a new design. First, the study meticulously goes through the entire GE exhaust system, starting with the redesign of the airfoil shape surrounding the struts. This new design has a larger angle of attack and minimizes the flow separations over a much wider operating range. Second, the pros and cons of the concentric turning vanes are studied and it is shown that they are more flow restrictive, rather than flow enhancing. Third, it is shown that the highly turbulent rectangular box-type exhaust ducting design, substantially contributes to high noise levels and pressure losses. In this paper a completed design will be shown that incorporates a new airfoil shape for the struts, and by using CRV flow technology in combination with the LAD flow technology, the pressure recovery can be enhanced. If the pressure losses could be reduced by 40 inches of water (0.10 kgs/sqcm), the turbine efficiency could be increased by 5%, and the power output could be increased by 6%.
    keyword(s): Pressure , Flow (Dynamics) , Turbulence , Structural frames , Design , Gas turbines , Turbines , Exhaust systems , Flow separation , Turning vanes , Rotation , Fluids , High pressure (Physics) , Stress , Noise (Sound) AND Diffusers ,
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      A New Tailpipe Design for GE Frame-Type Gas Turbines to Substantially Lower Pressure Losses

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    http://yetl.yabesh.ir/yetl1/handle/yetl/129302
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    contributor authorRichard Golomb
    contributor authorVivek Sahai
    contributor authorDah Yu Cheng
    date accessioned2017-05-09T00:11:46Z
    date available2017-05-09T00:11:46Z
    date copyrightJanuary, 2003
    date issued2003
    identifier issn0889-504X
    identifier otherJOTUEI-28700#128_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129302
    description abstractMany GE frame gas turbines have a unique 90-deg tailpipe exhaust system that contains struts, diffusers, and turning vanes. As confirmed in a recent report by GE and other authors, it is known in the industry that this tailpipe design has large pressure losses. In this recent report a pressure loss as high as 60 in. of water (0.15 kgs/sqcm) was cited. Due to the flow separations they create, the report indicates that the struts can cause very high-pressure losses in the turbine. The report also states that these pressure losses can vary with different turbine load conditions. Cheng Fluid Systems and Cheng Power Systems have conducted a study aimed at substantially reducing these pressure losses. Flow control technology introduced to the refinery industry, i.e., the Cheng Rotation Vane (CRV) and the Large Angle Diffuser (LAD) can be used to mitigate the flow separation and turbulence that occurs in turns, bends, and large sudden expansions. Specifically the CRV addresses the flow separations in pipe turns, and the LAD addresses the flow problems that occur with large sudden expansion areas. The paper will introduce the past experience of the CRV and LAD, and will then use computer simulations to show the flow characteristics around a new design. First, the study meticulously goes through the entire GE exhaust system, starting with the redesign of the airfoil shape surrounding the struts. This new design has a larger angle of attack and minimizes the flow separations over a much wider operating range. Second, the pros and cons of the concentric turning vanes are studied and it is shown that they are more flow restrictive, rather than flow enhancing. Third, it is shown that the highly turbulent rectangular box-type exhaust ducting design, substantially contributes to high noise levels and pressure losses. In this paper a completed design will be shown that incorporates a new airfoil shape for the struts, and by using CRV flow technology in combination with the LAD flow technology, the pressure recovery can be enhanced. If the pressure losses could be reduced by 40 inches of water (0.10 kgs/sqcm), the turbine efficiency could be increased by 5%, and the power output could be increased by 6%.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA New Tailpipe Design for GE Frame-Type Gas Turbines to Substantially Lower Pressure Losses
    typeJournal Paper
    journal volume125
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1515335
    journal fristpage128
    journal lastpage132
    identifier eissn1528-8900
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsTurbulence
    keywordsStructural frames
    keywordsDesign
    keywordsGas turbines
    keywordsTurbines
    keywordsExhaust systems
    keywordsFlow separation
    keywordsTurning vanes
    keywordsRotation
    keywordsFluids
    keywordsHigh pressure (Physics)
    keywordsStress
    keywordsNoise (Sound) AND Diffusers
    treeJournal of Turbomachinery:;2003:;volume( 125 ):;issue: 001
    contenttypeFulltext
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