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    Stability of a Rotor Partially Filled With Fluid: Test Facility and Experimental Results

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 145 ):;issue: 004::page 41019-1
    Author:
    Kasprzyk, Marie
    ,
    Sentmanat, John
    ,
    Delgado, Adolfo
    DOI: 10.1115/1.4055946
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fluid trapped in a hollow, rotating component may lead to subsynchronous vibrations, resulting in high vibration amplitudes. This asynchronous response is observed around 0.55–0.92× after passing through the first critical frequency and affects large rotating equipment such as centrifuges, fluid-cooled gas turbines, and jet engines. A test rig is designed to evaluate this self-excited asynchronous vibration. The high-speed rig comprises of a flexibly-mounted rotor partially filled with fluid, with an overhung test chamber providing an unobstructed view of the liquid surface. A squeeze film damper provides external damping and allows operation through the asynchronous response when the test chamber contains a large amount of fluid. The results show the rotor response with different fluid depths and external damping values as the rotor-bearing system transverses the first critical speed (cylindrical mode). The experiments show that only a small amount of oil (∼20 mL) is required to induce asynchronous excitations, and increasing the fluid depth increases the amplitude of vibration. External damping slightly decreases the response, but it also expands the range of frequencies where asynchronous vibrations occur. At a given speed ratio, the vibrations reach a limit cycle, and subsequently, begin to drop as the rotor speed increases past the first critical speed.
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      Stability of a Rotor Partially Filled With Fluid: Test Facility and Experimental Results

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    contributor authorKasprzyk, Marie
    contributor authorSentmanat, John
    contributor authorDelgado, Adolfo
    date accessioned2023-08-16T18:22:26Z
    date available2023-08-16T18:22:26Z
    date copyright12/13/2022 12:00:00 AM
    date issued2022
    identifier issn0742-4795
    identifier othergtp_145_04_041019.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291871
    description abstractFluid trapped in a hollow, rotating component may lead to subsynchronous vibrations, resulting in high vibration amplitudes. This asynchronous response is observed around 0.55–0.92× after passing through the first critical frequency and affects large rotating equipment such as centrifuges, fluid-cooled gas turbines, and jet engines. A test rig is designed to evaluate this self-excited asynchronous vibration. The high-speed rig comprises of a flexibly-mounted rotor partially filled with fluid, with an overhung test chamber providing an unobstructed view of the liquid surface. A squeeze film damper provides external damping and allows operation through the asynchronous response when the test chamber contains a large amount of fluid. The results show the rotor response with different fluid depths and external damping values as the rotor-bearing system transverses the first critical speed (cylindrical mode). The experiments show that only a small amount of oil (∼20 mL) is required to induce asynchronous excitations, and increasing the fluid depth increases the amplitude of vibration. External damping slightly decreases the response, but it also expands the range of frequencies where asynchronous vibrations occur. At a given speed ratio, the vibrations reach a limit cycle, and subsequently, begin to drop as the rotor speed increases past the first critical speed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStability of a Rotor Partially Filled With Fluid: Test Facility and Experimental Results
    typeJournal Paper
    journal volume145
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4055946
    journal fristpage41019-1
    journal lastpage41019-8
    page8
    treeJournal of Engineering for Gas Turbines and Power:;2022:;volume( 145 ):;issue: 004
    contenttypeFulltext
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