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Control of Torsional Vibrations by Pendulum MassesVarious versions of pendulum masses have been developed abroad within the past few years by means of which resonant vibrations of rotating shafts can be eliminated at a given tuning. They are already successfully employed on radial engines in the form of pendulous counterweights. Compared with the commonly known torsional vibration dampers, the pendulum masses have the advantage of being structurally very simple, requiring no internal damping and being capable of completely eliminating certain vibrations. Unexplained, so far, remains the problem of behavior of pendulum masses in other critical zones to which they are not tuned, their dynamic behavior at some tuning other than in resonance, and their effect within a compound vibration system and at simultaneous application of several differently tuned pendulous masses. These problems are analyzed in the present report. The results constitute an enlargement of the scope of application of pendulum masses, especially for in-line engines. Among other things it is found that the natural frequency of a system can be raised by means of a correspondingly tuned pendulum mass. The formulas necessary for the design of any practical version are developed, and a pendulum mass having two different natural frequencies simultaneously is described.
Document ID
20030065920
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Stieglitz, Albert
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 7, 2013
Publication Date
November 1, 1942
Publication Information
Publication: Jahrbuch 1938 der Deutschen Luftfahrtforschung
Subject Category
Engineering (General)
Report/Patent Number
NACA-TM-1035
Report Number: NACA-TM-1035
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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