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RESEARCH PAPERS

An Investigation of an Impact Vibration Absorber

[+] Author and Article Information
D. M. Egle

School of Aerospace and Mechanical Engineering, University of Oklahoma, Norman, Okla.

J. Eng. Ind 89(4), 653-657 (Nov 01, 1967) (5 pages) doi:10.1115/1.3610127 History: Received December 01, 1966; Online August 25, 2011

Abstract

The impact vibration absorber consists of a small mass, moving unidirectionally, impacting against the ends of a container which is rigidly attached to the primary vibrating system. A simplified theory for the forced steady-state response of a linear, single-degree-of-freedom system with an impact vibration absorber is presented. The assumption of two impacts per cycle at equal time intervals is known to lead to two possible solutions near the resonant frequency of the primary system. A criterion for determining the stability of the solutions is developed. An approximate expression for the maximum displacement of the primary system is given and the theory is compared to experimental results.

Copyright © 1967 by ASME
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