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FIFTH CANADIAN CONFERENCE ON NONDESTRUCTIVE ... - IAEA

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- 265 -<br />

Sensors used on the major metallic components will have a maximum sensitivity in<br />

the range 100-400 kHz. However, attenuation in frp at these frequencies would<br />

demand an unacceptable number of sensors necessary for coverage of the complete<br />

boom. For this reason, it is more usual to employ sensors for the boom with<br />

peak response in the 20-50 kHz range. This is strictly a compromise as the<br />

lower frequency increases the susceptibility to extraneous mechanical noise.<br />

It is rare to use "time of flight" source location on either the boom or metal<br />

components. Sources of acoustic emission that may occur are simply identified<br />

with the particular component. In this way, two sensors may be fed into a<br />

single amplifier chain. This reduces the capital cost of equipment at the<br />

expense of discrimination.<br />

Sensor spacing may be quite important. An artificial acoustic emission source,<br />

such as a puiser or pencil lead break [5], must be used to ensure that the<br />

required degree of coverage is achieved. However, this rigorous process need<br />

only be performed once for a given model of aerial lift truck. Sensitivity,<br />

which includes sensor performance, couplant and amplifier gain, must be checked<br />

and equalized for each test. This is a simple process of stimulating each channel<br />

with the artificial source and adjusting amplifier gains for equal<br />

response. Figure 7 illustrates commonly used sensor locations.<br />

The boom is then deployed in a manner such that it is representative of working<br />

configurations and such that a controlled load may be applied to the bucket<br />

end. in Figure 8 the load is applied through a cable winch and load cell.<br />

A predetermined load regime is followed consisting of the gradual imposition of<br />

load which is then held for a few minutes and then repeated [6], The applied<br />

load must be consistent with the total vehicle design [7], but this may be as<br />

high as three times, but more typically twice, rated load [8].<br />

TEST RESULTS<br />

For each stage of the load profile acoustic emission activity is recorded for<br />

each channel. The data are plotted in a number of ways, but would normally<br />

include count versus load, Figure 9, amplitude distributions, Figure 10 and<br />

perhaps an indication of individual channel activity through the test.<br />

Experience plays a large part in both conducting the test itself and in interpreting<br />

the results. At the present, there are no solid, universal accept/<br />

reject criteria. However, if acoustic emission continues into the hold period<br />

or recurs on the second load, there is strong indication that a problem exists.<br />

If the general activity, that is the overall count, is unusually high, concern<br />

would depend on which channels were active. For example, this type of indication<br />

could be due to a worn or poorly lubricated pin. The shape of the count<br />

versus load plot is also a significant factor used in interpretation.<br />

Fibre breakage represents high energy acoustic emission generation. By observation<br />

of the amplitude distribution, Figure 10, some assessment of fibre breakage<br />

during the test is available.

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