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    Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion Cooled Combustor

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 005::page 51501
    Author:
    Andrei, Luca
    ,
    Andreini, Antonio
    ,
    Bianchini, Cosimo
    ,
    Facchini, Bruno
    ,
    Mazzei, Lorenzo
    ,
    Turrini, Fabio
    DOI: 10.1115/1.4028676
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Effusion cooling represents the state of the art of liner cooling technology for modern combustors. This technique consists of an array of closely spaced discrete film cooling holes and contributes to lower the metal temperature by the combined protective effect of coolant film and heat removal through forced convection inside each hole. Despite many efforts reported in literature to characterize the cooling performance of these devices, detailed analyses of the mixing process between coolant and hot gas are difficult to perform, especially when superposition and density ratio effects as well as the interaction with complex gas side flow field become significant. Furthermore, recent investigations on the acoustic properties of these perforations pointed out the challenge to maintain optimal cooling performance also with orthogonal holes, which showed higher sound absorption. The objective of this paper is to investigate the impact of a realistic flow field on the adiabatic effectiveness performance of effusion cooling liners to verify the findings available in literature, which are mostly based on effusion flat plates with aligned cross flow, in case of swirled hot gas flow. The geometry consists of a tubular combustion chamber, equipped with a double swirler injection system and characterized by 22 rows of cooling holes on the liner. The liner cooling system employs slot cooling as well: its interactions with the cold gas injected through the effusion plate are investigated too. Taking advantage of the rotational periodicity of the effusion geometry and assuming axisymmetric conditions at the combustor inlet, steady state RANS calculations have been performed with the commercial code Ansysآ® CFX simulating a single circumferential pitch. Obtained results show how the effusion perforation angle deeply affects the flowfield around the corner of the combustor, in particular, with a strong reduction of slot effectiveness in case of 90 deg angle value.
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      Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion Cooled Combustor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/157936
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    contributor authorAndrei, Luca
    contributor authorAndreini, Antonio
    contributor authorBianchini, Cosimo
    contributor authorFacchini, Bruno
    contributor authorMazzei, Lorenzo
    contributor authorTurrini, Fabio
    date accessioned2017-05-09T01:17:47Z
    date available2017-05-09T01:17:47Z
    date issued2015
    identifier issn1528-8919
    identifier othergtp_137_05_051501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/157936
    description abstractEffusion cooling represents the state of the art of liner cooling technology for modern combustors. This technique consists of an array of closely spaced discrete film cooling holes and contributes to lower the metal temperature by the combined protective effect of coolant film and heat removal through forced convection inside each hole. Despite many efforts reported in literature to characterize the cooling performance of these devices, detailed analyses of the mixing process between coolant and hot gas are difficult to perform, especially when superposition and density ratio effects as well as the interaction with complex gas side flow field become significant. Furthermore, recent investigations on the acoustic properties of these perforations pointed out the challenge to maintain optimal cooling performance also with orthogonal holes, which showed higher sound absorption. The objective of this paper is to investigate the impact of a realistic flow field on the adiabatic effectiveness performance of effusion cooling liners to verify the findings available in literature, which are mostly based on effusion flat plates with aligned cross flow, in case of swirled hot gas flow. The geometry consists of a tubular combustion chamber, equipped with a double swirler injection system and characterized by 22 rows of cooling holes on the liner. The liner cooling system employs slot cooling as well: its interactions with the cold gas injected through the effusion plate are investigated too. Taking advantage of the rotational periodicity of the effusion geometry and assuming axisymmetric conditions at the combustor inlet, steady state RANS calculations have been performed with the commercial code Ansysآ® CFX simulating a single circumferential pitch. Obtained results show how the effusion perforation angle deeply affects the flowfield around the corner of the combustor, in particular, with a strong reduction of slot effectiveness in case of 90 deg angle value.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInvestigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion Cooled Combustor
    typeJournal Paper
    journal volume137
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4028676
    journal fristpage51501
    journal lastpage51501
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 005
    contenttypeFulltext
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