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PASSIVE VIBRATION CONTROL OF AIRBORNE EQUIPMENT USING A CIRCULAR STEEL RING

โœ Scribed by J. ELLISON; G. AHMADI; M. KEHOE


Book ID
102606461
Publisher
Elsevier Science
Year
2001
Tongue
English
Weight
489 KB
Volume
246
Category
Article
ISSN
0022-460X

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โœฆ Synopsis


Vibration isolation is needed to protect avionics equipment from adverse aircraft vibration environments. Passive isolation is the simplest means to achieve this goal. The system used here consists of a circular steel ring with a lump mass on top and exposed to base excitation. Sinusoidal and "ltered zero-mean Gaussian white noise are used to excite the structure and the acceleration response spectra at the top of the ring are computed. An experiment is performed to identify the natural frequencies and modal damping of the circular ring. Comparison is made between the analytical and experimental results and good agreement is observed. The ring response is also evaluated with a concentrated mass attached to the top of the ring. The e!ectiveness of the ring in isolating the equipment from base excitation is studied. The acceleration response spectra of a single-degree-of-freedom (s.d.o.f.) system attached to the top of the ring are evaluated and the results are compared with those exposed directly to the base excitation. It is shown that a properly designed ring could e!ectively protect the avionics from possible damaging excitation levels.


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