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    Experimental Characterization of a Bladeless Air Compressor

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 004::page 41020-1
    Author:
    Tiwari, Ravi Nath
    ,
    Reggio, Federico
    ,
    Ferrari, Mario Luigi
    ,
    De Paepe, Ward
    ,
    Traverso, Alberto
    DOI: 10.1115/1.4066732
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The Tesla compressor is an innovative technology that offers a unique approach to fluid compression. Unlike traditional compressors that use rotating blades, bladeless compressors utilize closely spaced disks to create compression. The purpose of this article is to design a prototype Tesla air compressor with optimal design parameters and investigate the performance and loss characteristics based on numerical analysis and experimental demonstration. The prototype model has been numerically investigated at different rotational speeds, and the results have been compared with those obtained in experiments. Computational fluid dynamics (CFD) simulations indicate that the rotor-only efficiency is greater than 90% at very low mass flowrates, while the coupling of the rotor and volute leads to a total-to-static efficiency of approximately 58% (without losses) at 14 g/s. At a nominal mass flow of 4 g/s, the highest total-to-static pressure ratio would be around 1.27. Experimental results indicate leakage losses greatly reduce net mass flow, while pressure ratio values are in good agreement with CFD predictions. During this experiment, a maximum isentropic efficiency of 32.4% is measured. Indeed, the prototype included ventilation and leakage losses, which were not modeled in the CFD analysis. It is remarkable that the compressor does not show any unstable behavior down to zero mass flow (closed valve test), where the CFD and the experiment show consistent pressure ratios. An estimation of the losses from end-wall friction and leakage flow is carried out using numerical simulations at different exit radial clearances. Increasing radial clearance results in an increase in leakage and end-wall power loss, the latter being driven mainly by the axial clearance with the casing, which remained unchanged. To minimize leakage, a Teflon ring has been used as a first measure. Numerical calculations have indicated that the leakage rate is approximately 6 g/s at design speed. A brush seal-type solution can improve the sealing system to reduce leakage.
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      Experimental Characterization of a Bladeless Air Compressor

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    contributor authorTiwari, Ravi Nath
    contributor authorReggio, Federico
    contributor authorFerrari, Mario Luigi
    contributor authorDe Paepe, Ward
    contributor authorTraverso, Alberto
    date accessioned2025-04-21T10:36:45Z
    date available2025-04-21T10:36:45Z
    date copyright11/5/2024 12:00:00 AM
    date issued2024
    identifier issn0742-4795
    identifier othergtp_147_04_041020.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306549
    description abstractThe Tesla compressor is an innovative technology that offers a unique approach to fluid compression. Unlike traditional compressors that use rotating blades, bladeless compressors utilize closely spaced disks to create compression. The purpose of this article is to design a prototype Tesla air compressor with optimal design parameters and investigate the performance and loss characteristics based on numerical analysis and experimental demonstration. The prototype model has been numerically investigated at different rotational speeds, and the results have been compared with those obtained in experiments. Computational fluid dynamics (CFD) simulations indicate that the rotor-only efficiency is greater than 90% at very low mass flowrates, while the coupling of the rotor and volute leads to a total-to-static efficiency of approximately 58% (without losses) at 14 g/s. At a nominal mass flow of 4 g/s, the highest total-to-static pressure ratio would be around 1.27. Experimental results indicate leakage losses greatly reduce net mass flow, while pressure ratio values are in good agreement with CFD predictions. During this experiment, a maximum isentropic efficiency of 32.4% is measured. Indeed, the prototype included ventilation and leakage losses, which were not modeled in the CFD analysis. It is remarkable that the compressor does not show any unstable behavior down to zero mass flow (closed valve test), where the CFD and the experiment show consistent pressure ratios. An estimation of the losses from end-wall friction and leakage flow is carried out using numerical simulations at different exit radial clearances. Increasing radial clearance results in an increase in leakage and end-wall power loss, the latter being driven mainly by the axial clearance with the casing, which remained unchanged. To minimize leakage, a Teflon ring has been used as a first measure. Numerical calculations have indicated that the leakage rate is approximately 6 g/s at design speed. A brush seal-type solution can improve the sealing system to reduce leakage.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental Characterization of a Bladeless Air Compressor
    typeJournal Paper
    journal volume147
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4066732
    journal fristpage41020-1
    journal lastpage41020-12
    page12
    treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 004
    contenttypeFulltext
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