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    Investigation of Entropy Noise in Aero-Engine Combustors

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002::page 370
    Author:
    Friedrich Bake
    ,
    Ulf Michel
    ,
    Ingo Roehle
    DOI: 10.1115/1.2364193
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Strong evidence is presented that entropy noise is the major source of external noise in aero-engine combustion. Entropy noise is generated in the outlet nozzles of combustors. Low-frequency entropy noise, which was predicted earlier in theory and numerical simulations, was successfully detected in a generic aero-engine combustion chamber. It is shown that entropy noise dominates even in the case of thermo-acoustic resonances. In addition to this, a different noise generating mechanism was discovered that is presumably of even higher relevance to jet engines: There is strong evidence of broad band entropy noise at higher frequencies (1 to 3kHz in the reported tests). This unexpected effect can be explained by the interaction of small scale entropy perturbations (hot spots) with the strong pressure gradient in the outlet nozzle. The direct combustion noise of the flame zone seems to be of minor importance for the noise emission to the ambiance. The combustion experiments were supplemented by experiments with electrical heating. Two different methods for generating entropy waves were used, a pulse excitation and a sinusoidal excitation. In addition, high-frequency entropy noise was generated by steady electrical heating.
    keyword(s): Combustion chambers , Noise (Sound) , Nozzles , Entropy , Waves , Microphones , Signals , Aircraft engines , Heating AND Flow (Dynamics) ,
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      Investigation of Entropy Noise in Aero-Engine Combustors

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    http://yetl.yabesh.ir/yetl1/handle/yetl/135732
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    contributor authorFriedrich Bake
    contributor authorUlf Michel
    contributor authorIngo Roehle
    date accessioned2017-05-09T00:23:42Z
    date available2017-05-09T00:23:42Z
    date copyrightApril, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26949#370_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135732
    description abstractStrong evidence is presented that entropy noise is the major source of external noise in aero-engine combustion. Entropy noise is generated in the outlet nozzles of combustors. Low-frequency entropy noise, which was predicted earlier in theory and numerical simulations, was successfully detected in a generic aero-engine combustion chamber. It is shown that entropy noise dominates even in the case of thermo-acoustic resonances. In addition to this, a different noise generating mechanism was discovered that is presumably of even higher relevance to jet engines: There is strong evidence of broad band entropy noise at higher frequencies (1 to 3kHz in the reported tests). This unexpected effect can be explained by the interaction of small scale entropy perturbations (hot spots) with the strong pressure gradient in the outlet nozzle. The direct combustion noise of the flame zone seems to be of minor importance for the noise emission to the ambiance. The combustion experiments were supplemented by experiments with electrical heating. Two different methods for generating entropy waves were used, a pulse excitation and a sinusoidal excitation. In addition, high-frequency entropy noise was generated by steady electrical heating.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInvestigation of Entropy Noise in Aero-Engine Combustors
    typeJournal Paper
    journal volume129
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2364193
    journal fristpage370
    journal lastpage376
    identifier eissn0742-4795
    keywordsCombustion chambers
    keywordsNoise (Sound)
    keywordsNozzles
    keywordsEntropy
    keywordsWaves
    keywordsMicrophones
    keywordsSignals
    keywordsAircraft engines
    keywordsHeating AND Flow (Dynamics)
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002
    contenttypeFulltext
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