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    A Gas-Operated Bearing Damper for Turbomachinery

    Source: Journal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 002::page 383
    Author:
    J. M. Vance
    ,
    A. F. Storace
    ,
    B. P. Cardon
    ,
    L. A. San Andres
    DOI: 10.1115/1.2906720
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A gas-operated bearing damper for turbomachinery has been designed, analyzed, and experimentally investigated in the laboratory. The damper utilizes air bled off from the compressor to power an actuator through orifices with area modulated by the vibratory displacement at the bearing support. The design objective for this passive device is to make the actuating dynamic gas pressure phase lead the vibratory displacement by 90 deg. Several variations of the basic concept have been tested. An analysis was performed to guide the experiments. All of the designs tested to date can produce positive damping, and one particular design has produced a damping coefficient of 8756 N-s/m (50 lb-sec/in.) with a power penalty of 5.2 kW (7 hp) at 310 KPa (45 psi). This design was installed on a laboratory rotor with flexibly supported ball bearings, and significant damping of the critical speed response was demonstrated. The experimental results to date suggest that further research can produce significant improvements in performance, and the device appears to be especially adaptable to high-temperature applications for aircraft engines.
    keyword(s): Bearings , Dampers , Turbomachinery , Damping , Design , Displacement , Orifices , Pressure , Compressors , Actuators , Rotors , Ball bearings , Aircraft engines AND High temperature ,
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      A Gas-Operated Bearing Damper for Turbomachinery

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/111944
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. M. Vance
    contributor authorA. F. Storace
    contributor authorB. P. Cardon
    contributor authorL. A. San Andres
    date accessioned2017-05-08T23:41:20Z
    date available2017-05-08T23:41:20Z
    date copyrightApril, 1993
    date issued1993
    identifier issn1528-8919
    identifier otherJETPEZ-26715#383_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111944
    description abstractA gas-operated bearing damper for turbomachinery has been designed, analyzed, and experimentally investigated in the laboratory. The damper utilizes air bled off from the compressor to power an actuator through orifices with area modulated by the vibratory displacement at the bearing support. The design objective for this passive device is to make the actuating dynamic gas pressure phase lead the vibratory displacement by 90 deg. Several variations of the basic concept have been tested. An analysis was performed to guide the experiments. All of the designs tested to date can produce positive damping, and one particular design has produced a damping coefficient of 8756 N-s/m (50 lb-sec/in.) with a power penalty of 5.2 kW (7 hp) at 310 KPa (45 psi). This design was installed on a laboratory rotor with flexibly supported ball bearings, and significant damping of the critical speed response was demonstrated. The experimental results to date suggest that further research can produce significant improvements in performance, and the device appears to be especially adaptable to high-temperature applications for aircraft engines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Gas-Operated Bearing Damper for Turbomachinery
    typeJournal Paper
    journal volume115
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906720
    journal fristpage383
    journal lastpage389
    identifier eissn0742-4795
    keywordsBearings
    keywordsDampers
    keywordsTurbomachinery
    keywordsDamping
    keywordsDesign
    keywordsDisplacement
    keywordsOrifices
    keywordsPressure
    keywordsCompressors
    keywordsActuators
    keywordsRotors
    keywordsBall bearings
    keywordsAircraft engines AND High temperature
    treeJournal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 002
    contenttypeFulltext
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