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Vibration Analysis
We have experience in performing vibration analysis
and de-tuning to meet the requirements of Mil-STD 810F in machinery
and electronics cabinetry. The military specification identifies
vibration frequencies that equipment will be exposed to in the field.
All equipment that meets the standard must be designed so that it
does not have a resonant frequency in any of the specified areas.
Where machinery is not subject to the military specifications it
is possible to identify the frequencies that the machinery is exposed
to and to detune it so as to reduce wear on the machinery.
It is necessary to determine the fragility specification
for the equipment to be de-tuned. This determines what level of
acceleration the machinery can withstand without damage. The level
of acceleration will also depend upon the frequency of the vibration
the machinery is exposed to during operation and during storage
or transportation.
Phase I
A Sweep test exposes the machinery to a range
of frequencies. A properly designed sweep test will have accelerometers
installed on the machinery at critical points on structures and
subcomponents. As the frequency of vibration changes the accelerometers
will tell you how sensitive that location is to the frequency. The
more sensitive the location the higher the acceleration and the
greater the chance of a failure.
Phase II
An analysis of the results of the sweep test
will determine which areas are critical and need to be de-tuned.
The information from the sweep test will also be fed into a computer
model that can be used to make predictions on the effect of particular
detuning actions.
Phase III
Detuning the equipment involves changing the
mass or the stiffness of the members or components. It can be achieved
by introducing springs or by stressing the members or changing the
stiffness to change their resonant frequencies. Detuning involves
tradeoffs, adding spring components can reduce the resonance at
a high frequency but at the expense of increasing it at a lower
frequency. Detuning a complex device for multiple frequency ranges
also must take into account coupling modes that create new resonant
frequencies. Changing the stress on a component is similar to tightening
a guitar string, the tighter the string the higher the frequency.
The more prestress on a component the higher the resonant frequency.
Predictions are made by making changes to the
computer model, and then these are tested against the actual device
to verify that the model correctly represents the device. A simple
hammer strike test can be used to predict the effects of specific
changes and this can be compared to the computer model to validate
the computer model. If necessary the model can be changed to give
a more accurate representation of the device.
Phase IV
To achieve certification under the military
standard the final detuned device is subjected to two tests, a random
vibration test and a shock test.
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