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    Transient Response of Floating Ring Liquid Seals

    Source: Journal of Tribology:;1988:;volume( 110 ):;issue: 003::page 572
    Author:
    R. G. Kirk
    DOI: 10.1115/1.3261688
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The design and analysis of pressure balanced seals are important to the designers and users of turbomachinery which require floating element seals. The design objective for compressor seals differs from that of the engineered pump seal but the common factor includes the ability to predict the dynamic response of the floating ring seal relative to the rotor shaft. Steady-state calculations can be used to study possible operating conditions for compressor designs, but they do not include accurate account of rotor shaft response and ring spin torque. In addition, engineered pump seal applications are such that the ring is expected to track shaft movement during start-up and shut-down transients when reduced pressures and leakage produce laminar flow sealing conditions. The analysis presented in this paper gives the designer the ability to evaluate seal ring dynamic transient response, including friction stick-slip on the axial sealing face and the ring spin torque interaction with the antirotation element. The analysis results presented in this paper were obtained from a personal computer program written specifically for seal transient analysis.
    keyword(s): Transients (Dynamics) , Particle spin , Design , Pumps , Rotors , Torque , Compressors , Sealing (Process) , Laminar flow , Pressure , Friction , Computer software , Dynamic response , Steady state , Stick-slip , Transient analysis , Turbomachinery AND Leakage ,
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      Transient Response of Floating Ring Liquid Seals

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    http://yetl.yabesh.ir/yetl1/handle/yetl/104528
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    contributor authorR. G. Kirk
    date accessioned2017-05-08T23:28:20Z
    date available2017-05-08T23:28:20Z
    date copyrightJuly, 1988
    date issued1988
    identifier issn0742-4787
    identifier otherJOTRE9-28471#572_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/104528
    description abstractThe design and analysis of pressure balanced seals are important to the designers and users of turbomachinery which require floating element seals. The design objective for compressor seals differs from that of the engineered pump seal but the common factor includes the ability to predict the dynamic response of the floating ring seal relative to the rotor shaft. Steady-state calculations can be used to study possible operating conditions for compressor designs, but they do not include accurate account of rotor shaft response and ring spin torque. In addition, engineered pump seal applications are such that the ring is expected to track shaft movement during start-up and shut-down transients when reduced pressures and leakage produce laminar flow sealing conditions. The analysis presented in this paper gives the designer the ability to evaluate seal ring dynamic transient response, including friction stick-slip on the axial sealing face and the ring spin torque interaction with the antirotation element. The analysis results presented in this paper were obtained from a personal computer program written specifically for seal transient analysis.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTransient Response of Floating Ring Liquid Seals
    typeJournal Paper
    journal volume110
    journal issue3
    journal titleJournal of Tribology
    identifier doi10.1115/1.3261688
    journal fristpage572
    journal lastpage577
    identifier eissn1528-8897
    keywordsTransients (Dynamics)
    keywordsParticle spin
    keywordsDesign
    keywordsPumps
    keywordsRotors
    keywordsTorque
    keywordsCompressors
    keywordsSealing (Process)
    keywordsLaminar flow
    keywordsPressure
    keywordsFriction
    keywordsComputer software
    keywordsDynamic response
    keywordsSteady state
    keywordsStick-slip
    keywordsTransient analysis
    keywordsTurbomachinery AND Leakage
    treeJournal of Tribology:;1988:;volume( 110 ):;issue: 003
    contenttypeFulltext
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