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| Application Notes |
Considerations when using Eddy Current Proximity Probes for Overspeed Protection Applications | ||||||||||||||||||||||||||
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Introduction |
Since overspeed is one of the most dangerous conditions that can occur in a turbine, it is essential that overspeed protection systems are properly installed. Bently Nevada manufactures eddy current proximity transducers and monitors that constitute an electronic overspeed detection system. Such a detection system is one part of an overall overspeed protection system. In the sections below are issues you should consider when applying eddy current proximity transducers in such an application. Figure 1 shows the terms used in this document for describing gear geometry. | |||||||||||||||||||||||||
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Signal Amplitude at Overspeed |
A transducer system viewing a gear generates a complex signal. In other words the signal may contain a vibration and/or runout component as well as the speed component (Figure 2). Other signal variations could come from inconsistencies in gear tooth dimensions. Normally these components of the signal are small compared to the speed component of the signal. However, when a machine approaches overspeed there must be no doubt which component of the signal represents the speed of the gear. In order to insure that the speed signal is the dominant signal component, we recommend that the amplitude of the speed signal be greater than 7 Vpp at the overspeed setpoint (200 mV/mil transducer system). The signal amplitude at overspeed is dependent on factors such as probe gap, gear dimensions, target material, and signal frequency. The general approach to estimating signal amplitude at overspeed is:
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How Gear Geometry Affects the Signal |
Different gear geometries create different types of signals from the transducer. This section describes three types of gear geometries and shows how each type affects the signal amplitude at slow roll. In each of the following examples the tooth depth is beyond the range of the probe, the face width is greater than 16mm, and the system used was a 3300 8mm probe with a 330100 Proximitor®. Small-geometry Gear: A small-geometry gear has a tooth width and space width that are both smaller than the diameter of the probe. Small-geometry gears produce sinusoidal signals but the signal amplitudes may be smaller than desired as shown in Figure 3. Large-geometry Gear: A gear with tooth widths and space widths larger than the probe diameter is a large-geometry gear. Large-geometry gears produce signals best described as "clipped sinusoids". (Figure 4) These signals may become sinusoidal at higher speeds depending on the gear geometry and the amount of signal attenuation. Large-geometry gears with tooth depths beyond the linear range of the probe produce the largest slow roll signal amplitudes. Figure 4 shows a signal generated from a large-geometry gear. The probe is gapped at -8 Vdc when viewing the tooth. Since the tooth depth is beyond the linear range of the probe, the signal is railed at the supply voltage (-24 Vdc) when viewing the space. Asymmetrical-geometry Gear: A gear with tooth widths that are larger than the diameter of the probe and space widths that are smaller than the diameter of the probe (or vice-versa) is an asymmetrical-geometry gear. For a 3300 8 mm probe a gear with 4 mm teeth and 10 mm spaces is an asymmetrical-geometry gear. Figure 5 shows a signal generated from an asymmetrical-geometry gear. When viewing the large tooth the output is -8 Vdc. When viewing the space the output does not go to the supply voltage rail (-24 Vdc) because the probe 'sees' the teeth on either side of the space (tooth depth is beyond the linear range of the probe). Signal amplitudes of asymmetrical-geometry gears vary greatly depending on the gear geometry. The three types of gears described in this section are very general. It is easy to see that every gear will have its own unique signal. That is why one of the most important things you can do to insure the reliability of your system is to verify the characteristics of the transducer signal. One of the most important of these characteristics is the slow roll signal amplitude. | |||||||||||||||||||||||||
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Finding the Slow Roll Signal Amplitude |
Since gears come in a variety of sizes, the best way to find the slow roll signal amplitude is to measure it with the
transducer system observing the actual gear. If you cannot measure the amplitude directly, you may be able to use the
gear geometry and the data in Figure 6 to estimate the slow roll signal amplitude.
The test setup shown in Figure 8 was used to gather the data shown in Figure 6 and
Figure 7. The results shown in Figure 6 are especially useful because they illustrate the relationships that exist between the output voltage, the tooth width, and the space width. Given a certain gear geometry, you can use the graph in Figure 6 to approximate the output voltage (Vpp) of an 8mm probe gapped at 40 mils. Do not use the graph (Figure 6) to predict exact voltage levels for a specific gear geometry. It may provide a reasonable estimate but remember that each system differs depending on gap, tooth geometry, target material, probe viewing angle, etc. The slow roll signal amplitude is an important parameter because it is used in calculating the signal amplitude at overspeed and it is easily verified. Once the slow roll signal amplitude is known, the signal amplitude at overspeed is calculated based on the speed signal frequency and the frequency response of the transducer system. | |||||||||||||||||||||||||
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Estimating the Amount of Signal Attenuation |
In order to estimate the amount of signal attenuation, the signal frequency at overspeed must be known. For most gears
this is easily calculated. However, the signal frequency at overspeed of an asymmetrical gear must be computed more
carefully. For example, Figure 9 shows two transducer signals at slow roll. The asymmetrical-geometry gears being observed both have large teeth and small spaces. Gear 2 has slightly larger teeth and slightly smaller spaces than gear 1. Otherwise, the gears are the same size with the same EPR. Normally, the frequency of the signal is computed as F=RPM/60 x EPR. This is equivalent to F=1/T (T=Period of the signal). Computed in this manner, these two signals have the same frequency (T1=T2). However, these signals will not behave the same at high speeds. Frequency is a function of how much the signal is changing over time. Over the full period both signals change the same amount. However, signal 2 makes the transition from -8 Vdc to -24 Vdc to -8 Vdc in less time than signal 1. Therefore, over this portion of the waveform, signal 2 changes more over time. At high speeds signal 2 will attenuate more than signal 1. In order to deal with the problem of calculating the signal frequency, two equations are suggested. For small gears and for symmetrical gears equation 1 is most appropriate. ![]() For asymmetrical gears equation 2 is more appropriate. ![]() A = smaller of tooth or space dimension B = larger of tooth or space dimension (Figure 10) When using equation 2, the frequency computed is not the actual frequency (1/T) of the signal. It is a worst case frequency, based on the portion of the gear that causes the transducer signal to change the most over the smallest amount of time. In other words, it is the frequency of the signal when the probe is viewing the smallest gear dimension. For asymmetrical gears, equation 2 is more appropriate. Equation 1 gives a best case estimate and equation 2 gives a worst case estimate. Combine these two methods to provide an approximation of the frequency response required for your transducer system. When using these formulas, signal frequencies up to 6 kHz (330100 Proximitor®) should pose no problems if cable lengths between the overspeed monitor and the transducer are kept below 1000 feet (300 Metres). For frequencies near or above 6 kHz, approximate the signal amplitude of the transducer system using equation 3. ![]() Equation 3 uses 6000 Hz for the frequency response (-3dB) of the transducer system (using p/n 330100). This number is conservative because frequency response changes with gap. In general, frequency response improves at smaller gaps and declines at larger gaps. The following section shows how to use these equations for a specific system. | |||||||||||||||||||||||||
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Example |
An AISI 4140 gear with 120 EPR is shown in Figure 11. The transducer system is a 3300 8 mm 5-M system. The probe gap is 50 mils from the tooth. The operating speed is 3600 RPM and the overspeed setpoint is 3978 RPM. What is the estimated output voltage (Vpp) at the overspeed setpoint?
At the overspeed setpoint the output voltage will be somewhere between 4.133 Vpp and 4.817 Vpp. The estimated frequency response of the transducer system was 6 kHz. If the probe gap is safely reduced, the frequency response will improve. If the frequency response improved to 8.0 kHz at 20 mils gap then the estimated output is between 5.67 and 5.01 Vpp. In this example, the amplitude of the speed signal is less than 7 Vpp. However, this may be acceptable depending on your monitoring system and the amplitude of other signal components such as vibration and runout. The next section provides specific guidelines concerning vibration and runout signal components. | |||||||||||||||||||||||||
| Distinguishing Speed from Vibration Signal Amplitude |
The signal generated by a transducer with a 200 mV/mil scale factor should output at least 7 Volts peak to peak (Vpp) at the overspeed setpoint. A speed signal with this amplitude should be sufficient to differentiate the speed signal from any other signal present. Most applications will easily meet these requirements. | |||||||||||||||||||||||||
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Large Vibration and/or Runout Signals |
For gears with large amounts of vibration or runout, the amplitude of the speed signal should be at least twice as large as the vibration or runout signal present at the speed measurement location. Figure 12 shows an 8.0 Vpp speed signal with a 4.0 Vpp vibration signal present at the speed measurement location. The threshold of the monitoring system is set at -15 Vdc and the hysteresis is set at 2 Volts. If the amplitude of the speed signal is reduced, or if the vibration signal increases, the monitor could start missing events. In the previous section it was shown that the transducer signal attenuates at high frequencies. It is important to note that vibration and runout signals will not attenuate the same as the speed signal. This is because the vibration and runout signal components are at different frequencies. For example, a small gear with 60 EPR rotating at 3600 RPM has a speed signal frequency of 3600 Hz. The 1X vibration component of the rotational speed is 60 Hz, much slower than the 3600 Hz speed signal. | |||||||||||||||||||||||||
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Installation Issues Minimum Gear Dimensions |
Tables 1 and 2 show the signal amplitudes from a 3300 8 mm probe and a 3300 11 mm probe while observing the gears in Figure 13 and Figure 14 respectively. Tooth dimensions smaller than those shown may no longer provide sufficient signal amplitude.
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Signal Threshold of the Monitoring System |
The ideal threshold of the monitoring system is the value that is midway between the most positive peak and the most negative peak of the transducer signal (see Figure 12). When using proximity transducers, the midway voltage at operating speed is usually unknown because the midpoint depends on gap, gear geometry, speed and vibration. Therefore, Auto Threshold is recommended when using proximity transducers. | |||||||||||||||||||||||||
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Load Impedance/Cable Length |
Bently Nevada eddy current proximity transducers can drive up to 1000 feet of twisted pair cable into a 10 K Ohm load with no appreciable degradation in frequency response. Therefore it is recommended to keep cable length between monitor and transducer below 1000 feet (300 metres). | |||||||||||||||||||||||||
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Probe Location |
Any transducer used in overspeed protection applications must be mounted on the driver side of the coupling. Also, any target observed should be an integral part of the rotating shaft. | |||||||||||||||||||||||||
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Probe Gap |
If the tooth depth is greater than the linear range of the probe then the signal amplitude can be increased by gapping the probe closer to the gear (Figure 15). Larger gaps, however, improve safety by decreasing the chance of the probe contacting the gear. Smaller probe gaps will also improve the frequency response of the transducer system. | |||||||||||||||||||||||||
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Conclusion |
Eddy current proximity transducers work well in most overspeed protection applications, but it is important to understand that there are limitations to their use. Bently Nevada is ready to help you engineer and install the proper proximity transducer to provide a reliable and effective signal for your electronic overspeed detection system. | |||||||||||||||||||||||||
![]() Figure 1: Terms used for describing gear geometry. Return to article ![]() Figure 2: Signals from the transducer may contain a vibration and/or runout signal as well as a speed signal. Return to article ![]() Figure 3: Signals from 3300 8 mm systems viewing small-geometry gears. The tooth depth is beyond the linear range of the probe on both gears. Return to article ![]() Figure 4: A typical signal generated from a 3300 8 mm system viewing a large-geometry gear. The probe is gapped at -8 Vdc (approx. 45 mils) when viewing the tooth. Since the tooth depth is beyond the linear range of the probe, the signal is railed at the supply voltage (-24 Vdc) when the probe is viewing the space. Return to article ![]() Figure 5: A signal generated from an asymetrical-geometry gear. When viewing the large tooth the output is -8 Vdc (approx. 45 mil gap). The tooth depth is beyond the range of the probe, but when viewing the space the output does not go to the supply voltage rail (-24 Vdc) because the probe sees the teeth on either side of the space. Return to article ![]() Figure 6: An E4140 gear with a 2 mm tooth and a 5.3 mm space viewed by a 3300 8 mm probe at 40 mils gap will have an output voltage of approx. 7 Vpp at slow roll. Return to article ![]() Figure 7: An E4140 gear with a 4 mm tooth and a 10mm space viewed by a 3300 11 mm probe at 80 mils gap will have an output voltage of approx. 7 Vpp at slow roll. Return to article ![]() Figure 8: Test setup to obtain the data shown in Figure 6. A 3300 8 mm system was used with a physical gap of 40 mils. The tooth depths and face widths are greater than 16 mm. Return to article ![]() Figure 9: Signals from two similar gears. Although T1 = T2, these signals will not behave the same at high frequencies. Return to article ![]() Figure 10: A = smaller of tooth or space dimension B = larger of tooth or space dimension Return to article ![]() Figure 11 Return to article ![]() Figure 12: A 4.0 Vpp vibration signal superimposed on an 8.0 Vpp speed signal. The threshold of the monitoring system is -15 Vdc and the hysteresis is 2 Volts. If the amplitude of the speed is reduced, or if the vibration signal increases, the monitor could start missing events. Return to article ![]() Figure 13: When using an 8 mm probe, tooth dimensions smaller than those shown may not provide sufficient signal amplitude (this does not include the 3 mm tooth depth dimension). Return to article ![]() Figure 14: When using an 11 mm probe, tooth dimensions smaller than those shown may not provide sufficient signal amplitude (this does not include the 6 mm tooth depth dimension). Return to article ![]() Figure 15: A smaller gap will provide a larger signal amplitude when the tooth depth is beyond the range of the probe. This data was taken with a 3300 8 mm system: the tooth width was 2.85 mm, the space width was 4.83 mm, and the face width was greater than 16 mm. Return to article |
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