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Airborne Gravity 2010 - Geoscience Australia

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<strong>Airborne</strong> <strong>Gravity</strong> <strong>2010</strong><br />

GT then undertook a detailed study of the design of the main gravimetric sensing element, or vertical<br />

accelerometer, and found that under certain conditions of induced non-orthogonal vibrations, i.e.,<br />

vibrations non-orthogonal relative to the base of the gravimeter, the accelerometer output could be<br />

offset by several tens of mGal. They concluded that the diagonal spring/damper assemblies should be<br />

removed as they could potentially induce non-orthogonal vibrations.<br />

New shock mount design<br />

In order to eliminate the problems associated with vibrations, in particular non-orthogonal vibrations,<br />

and to thus improve the performance of the gravimeter under a wider range of installations and flying<br />

conditions, we designed a totally new shock mount during the fall of 2006.<br />

The new shock mount (Figure 3) has two stages of isolation that make use of special closed-cell<br />

polyurethane foam of a specific density which has exceptional damping properties and durability. We<br />

designed the shock mount, or two-stage vibration isolation module, to specifically remove nonorthogonal<br />

vibrations. We obtained design assistance from two independent consultants in Canada<br />

and <strong>Australia</strong> who are considered experts in the field of vibration isolation.<br />

The natural frequencies of the two isolation stages differ by several Hz which helps to isolate<br />

vibrations, and the new shock mount has a different weight distribution. These two features are both<br />

important attributes of a two-stage vibration isolation system. Both stages are further isolated from<br />

aircraft vibrations by eliminating contact between the main structural bolts and the base-plate. The<br />

prototype shock mount used a heavy steel plate in the centre stage, but we replaced this with two<br />

thinner aluminium plates to remove potential interference with magnetometers which may also be on<br />

board the survey aircraft. The thinner aluminium plates are much lighter and are thus easier to handle,<br />

ship and install.<br />

Figure 3. The prototype of the new two-stage vibration isolation module or ‘shock mount’. The<br />

steel plate seen here above the first stage isolator was later replaced by two lighter aluminium<br />

plates for ease of handling.<br />

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