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    On Damping Entire Bladed Disks Through Dampers on Only a Few Blades

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 009::page 92503
    Author:
    Javier Avalos
    ,
    Marc P. Mignolet
    DOI: 10.1115/1.3078792
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The focus of this paper is on demonstrating the potential to damp entire bladed disks using dampers on only a fraction of the blades. This problem is first considered without the presence of random mistuning, and it is demonstrated that a few dampers at optimized locations can lead to a significant reduction in the forced response of the entire bladed disk. Unfortunately, this optimum design may not be robust with respect to random mistuning and a notable fraction of the reduction in forced response obtained may disappear because of mistuning. To regain the reduction in forced response but with mistuning present, robustness to mistuning is enhanced by using intentional mistuning in addition to dampers. The intentional mistuning strategy selected here is the A/B pattern mistuning in which the blades all belong to either type A or B. An optimization effort is then performed to obtain the best combination of A/B pattern and damper location to minimize the mistuned forced response of the disk. The addition of intentional mistuning in the system is shown to be very efficient, and the optimum bladed disk design does indeed exhibit a significant reduction in mistuned forced response as compared with the tuned system. These findings were obtained on both single-degree-of-freedom per blade-disk models and a reduced order model of a blisk.
    keyword(s): Dampers , Damping , Optimization , Disks AND Blades ,
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      On Damping Entire Bladed Disks Through Dampers on Only a Few Blades

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    contributor authorJavier Avalos
    contributor authorMarc P. Mignolet
    date accessioned2017-05-09T00:37:32Z
    date available2017-05-09T00:37:32Z
    date copyrightSeptember, 2010
    date issued2010
    identifier issn1528-8919
    identifier otherJETPEZ-27131#092503_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143105
    description abstractThe focus of this paper is on demonstrating the potential to damp entire bladed disks using dampers on only a fraction of the blades. This problem is first considered without the presence of random mistuning, and it is demonstrated that a few dampers at optimized locations can lead to a significant reduction in the forced response of the entire bladed disk. Unfortunately, this optimum design may not be robust with respect to random mistuning and a notable fraction of the reduction in forced response obtained may disappear because of mistuning. To regain the reduction in forced response but with mistuning present, robustness to mistuning is enhanced by using intentional mistuning in addition to dampers. The intentional mistuning strategy selected here is the A/B pattern mistuning in which the blades all belong to either type A or B. An optimization effort is then performed to obtain the best combination of A/B pattern and damper location to minimize the mistuned forced response of the disk. The addition of intentional mistuning in the system is shown to be very efficient, and the optimum bladed disk design does indeed exhibit a significant reduction in mistuned forced response as compared with the tuned system. These findings were obtained on both single-degree-of-freedom per blade-disk models and a reduced order model of a blisk.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn Damping Entire Bladed Disks Through Dampers on Only a Few Blades
    typeJournal Paper
    journal volume132
    journal issue9
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3078792
    journal fristpage92503
    identifier eissn0742-4795
    keywordsDampers
    keywordsDamping
    keywordsOptimization
    keywordsDisks AND Blades
    treeJournal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 009
    contenttypeFulltext
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