Abstract: A computerized method of assisting the routing of a part, comprising the steps of: providing at least one computer; receiving part identifier information; and generating a tag for affixing to the part. The tag has information thereon responsive to the identifier information. A computerized method of assisting the handling of a part, comprising the steps of: providing at least one computer; receiving part identifier information; processing the part identifier information; and generating output from the computer responsive to the part identifier information.

Abstract: A computerized method of assisting the routing of a part, comprising the steps of: providing at least one computer; receiving part identifier information; and generating a tag for affixing to the part. The tag has information thereon responsive to the identifier information. A computerized method of assisting the handling of a part, comprising the steps of: providing at least one computer; receiving part identifier information; processing the part identifier information; and generating output from the computer responsive to the part identifier information.

Abstract: A system for monitoring the structural condition of a helicopter rotor assembly component includes a piezoelectric sensor. Acoustic emission signal techniques allow for recognizing the relatively high frequency stress waves associated with the propagation of cracks or defects in a rotor assembly component. A signal conditioner processes the sensor signal and provides an output signal that includes at least one characteristic that is indicative of the content of the sensor signal and, therefore, the structural condition of the item of interest. A signal analyzer utilizes the output signal from the signal processor to determine the structural condition of the component.

Abstract: A computerized method of assisting the routing of a part, comprising the steps of: providing at least one computer; receiving part identifier information; and generating a tag for affixing to the part. The tag has information thereon responsive to the identifier information. A computerized method of assisting the handling of a part, comprising the steps of: providing at least one computer; receiving part identifier information; processing the part identifier information; and generating output from the computer responsive to the part identifier information.

Abstract: A system for monitoring the structural condition of a helicopter rotor assembly component includes a piezoelectric sensor. Acoustic emission signal techniques allow for recognizing the relatively high frequency stress waves associated with the propagation of cracks or defects in a rotor assembly component. A signal conditioner processes the sensor signal and provides an output signal that includes at least one characteristic that is indicative of the content of the sensor signal and, therefore, the structural condition of the item of interest. A signal analyzer utilizes the output signal from the signal processor to determine the structural condition of the component.

Abstract: A bearing assembly monitoring system provides continuous, real time monitoring of the operating condition of a powertrain support bearing assembly and real time alarm signals indicative of degradation and/or impending catastrophic failure thereof. One embodiment of the monitoring system includes a vibration sensing device, first and second primary temperature sensing devices, an ambient temperature sensing device, vibration and temperature signal processing subcircuits, and an alarm subsystem. The vibration sensing device monitors complex vibration signals emanating from the bearing assembly and provides signals corresponding thereto. The vibration signal processing circuit filters such complex vibration signals to provide a predetermined bandwidth thereof that are converted to stabilized DC voltage signals which are compared to reference voltages corresponding to higher than normal and excessive vibration levels. Exceedance of such reference voltages generates a corresponding vibration alarm signal.

Abstract: A turbine engine debris ingestion monitor has an acoustic emission sensor 18, 18a mounted on a surface 14, 14a disposed in an air flow stream of a turbine engine 12. The sensor converts acoustic emissions 16, generated by particles of debris 10 impacting on the surface, into an electrical signal. A counting circuit 22 (FIG. 2) processes the signal resulting in an output, indicative of the level of debris ingested into the engine, which is recorded in the aircraft's flight data recording system 110.