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    Application of the Principle of Reciprocity to Flexible Rotor Balancing

    Source: Journal of Mechanical Design:;1982:;volume( 104 ):;issue: 002::page 329
    Author:
    M. S. Darlow
    ,
    A. J. Smalley
    DOI: 10.1115/1.3256347
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The least desirable feature of most flexible rotor balancing procedures is the considerable number of trial mass runs required. This is of particular importance in the balancing of machines which require a substantial stabilization time during start-up. Using an adaptation of the principle of reciprocity, it is possible to significantly reduce the required number of trial mass runs for certain rotors when using either influence coefficient balancing or the Unified Balancing Approach. When applied to flexible rotor balancing, the principle of reciprocity states that, given two rotor axial locations, A and B (at which both balancing planes and vibration sensors are located), the influence coefficient relating the vibration level at A to the unbalance at B is identical to that relating the vibration level at B to the unbalance at A. This is true even in the presence of damping. This paper begins with a theoretical discussion of the principle of reciprocity and its application to flexible rotor balancing. The particular means by which reciprocity can be applied to improve the influence coefficient and Unified Balancing Approach procedures are then described in detail. A numerical study was conducted to verify this application of reciprocity, as well as to investigate any possible limitations. The results of this study are reported along with those of a similar experimental study using two substantially different test rotors.
    keyword(s): Rotor balancing , Rotors , Vibration , Sensors , Machinery balancing AND Damping ,
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      Application of the Principle of Reciprocity to Flexible Rotor Balancing

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    http://yetl.yabesh.ir/yetl1/handle/yetl/96204
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    contributor authorM. S. Darlow
    contributor authorA. J. Smalley
    date accessioned2017-05-08T23:14:01Z
    date available2017-05-08T23:14:01Z
    date copyrightApril, 1982
    date issued1982
    identifier issn1050-0472
    identifier otherJMDEDB-27998#329_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/96204
    description abstractThe least desirable feature of most flexible rotor balancing procedures is the considerable number of trial mass runs required. This is of particular importance in the balancing of machines which require a substantial stabilization time during start-up. Using an adaptation of the principle of reciprocity, it is possible to significantly reduce the required number of trial mass runs for certain rotors when using either influence coefficient balancing or the Unified Balancing Approach. When applied to flexible rotor balancing, the principle of reciprocity states that, given two rotor axial locations, A and B (at which both balancing planes and vibration sensors are located), the influence coefficient relating the vibration level at A to the unbalance at B is identical to that relating the vibration level at B to the unbalance at A. This is true even in the presence of damping. This paper begins with a theoretical discussion of the principle of reciprocity and its application to flexible rotor balancing. The particular means by which reciprocity can be applied to improve the influence coefficient and Unified Balancing Approach procedures are then described in detail. A numerical study was conducted to verify this application of reciprocity, as well as to investigate any possible limitations. The results of this study are reported along with those of a similar experimental study using two substantially different test rotors.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleApplication of the Principle of Reciprocity to Flexible Rotor Balancing
    typeJournal Paper
    journal volume104
    journal issue2
    journal titleJournal of Mechanical Design
    identifier doi10.1115/1.3256347
    journal fristpage329
    journal lastpage333
    identifier eissn1528-9001
    keywordsRotor balancing
    keywordsRotors
    keywordsVibration
    keywordsSensors
    keywordsMachinery balancing AND Damping
    treeJournal of Mechanical Design:;1982:;volume( 104 ):;issue: 002
    contenttypeFulltext
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