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.
Application of the Principle of Reciprocity to Flexible Rotor Balancing
M. S. Darlow
Mechanical Technology Inc., Latham, N.Y.
A. J. Smalley
Southwest Research Institute, San Antonio, Tex.
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Darlow, M. S., and Smalley, A. J. (April 1, 1982). "Application of the Principle of Reciprocity to Flexible Rotor Balancing." ASME. J. Mech. Des. April 1982; 104(2): 329–333. https://doi.org/10.1115/1.3256347
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