Description

The Bently Nevada 3300/20-12-01-00-00-00 135322-01, also cataloged as the 3300/20 Dual Thrust Position Monitor featuring the 135322-01 backplane block assembly, operates as a dedicated hardware component for continuous axial shaft movement tracking within machinery protection systems. Specifically, the module processes DC voltage variations from two independent proximity probe transducers, thereby translating these changes into direct physical shaft displacement measurements relative to the thrust bearing face and generating proportional 4-20 mA recorder outputs.

Suffix Breakdown & Model Matrix

The complete alphanumeric product code structures the specific hardware selection factory-installed into this thrust positioning block assembly:

Hardware Specifications

Machinery Monitoring and Transducer Interface Dynamics

The processing hardware executes real-time eddy-current probe scaling to accurately translate physical displacement into precise electrical potentials. Consequently, gap voltage validation enforces an operational baseline of -10 VDC for standard proximity sensors, which ensures that the transducer maintains its linear range during high-frequency rotor dynamics observations. Furthermore, dynamic signal isolation circuitry constrains cross-talk suppression to under -60 dB across adjacent measurement paths, thereby preventing electrical resonance interference from corrupting critical vibration calculations.

Frequently Asked Questions

Q: What specific hardware function does the 135322-01 backplane block serve?

A: The 135322-01 backplane block provides the physical electrical termination interface on the rear of the 3300 rack. Specifically, it routes raw transducer signals, 4-20 mA recorder loops, and shared rack relay signals from the field wiring directly into the main 3300/20 processing module.

Q: How does the 3300/20 monitor handle dual-channel voting for critical machinery trip interlocks?

A: When integrated into the common rack backplane, the system allows the option for 1oo2 or 2oo2 hardware voting configurations. Under 2oo2 logic, both axial probes must simultaneously breach the Danger setpoint boundary, which drastically minimizes false machinery trips caused by isolated sensor mechanical damage.

Q: What precise diagnostic action occurs when an axial probe moves beyond its linear calibration range?

A: The monitor constantly scans the input DC bias level. If a physical shift pushes the gap voltage outside the internal -2.0 VDC to -18.0 VDC diagnostic window, the internal logic drops the channel OK relay, illuminates the front panel “NOT OK” LED, and automatically locks out the associated safety alarm circuits.

Field Installation Guidelines

1. Field Wiring and Shield Terminal Isolation: Wire the transducer coaxial extension cables directly to the rear 135322-01 backplane terminal block assignment. Next, isolate the outer shield braid completely at the probe junction box, and then terminate the drain wire only at the designated rack ground bar to block induced magnetic field noise loops.
2. Probe Mechanical Gap Centering: Mount the physical thrust proximity probes looking at an integral shaft shoulder or the shaft end. During machine standstill, mechanical adjustments must position the probe to read exactly the zero-center electrical voltage baseline, which matches the chosen 50-0-50 mil span option.
3. Module Retaining Screw Engagement: Slide the monitor firmly along the guide tracks until the edge connectors lock flush with the backplane pin field. Afterwards, torque the upper and lower captive panel fasteners to establish full chassis ground bonding across the aluminum enclosure front plate.