초록 ▼

Methods and apparatuses are described for determining the operating status of a turbine engine. An eddy current sensor is provided having a sensing field in communication with a plurality of rotating turbine blades during a revolution of a turbine engine. The sensor generates signature data for the

Methods and apparatuses are described for determining the operating status of a turbine engine. An eddy current sensor is provided having a sensing field in communication with a plurality of rotating turbine blades during a revolution of a turbine engine. The sensor generates signature data for the passage of each blade. An analytic waveform is determined from the signature data and blade characteristic data is determined from the analytic waveform.

대표청구항 ▼

What is claimed is: 1. A computerized method of determining the operating status of a turbine engine, comprising the steps of: providing a sensor having a sensing field in communication with a plurality of rotating turbine blades during a revolution of a turbine engine, wherein said sensor generate

What is claimed is: 1. A computerized method of determining the operating status of a turbine engine, comprising the steps of: providing a sensor having a sensing field in communication with a plurality of rotating turbine blades during a revolution of a turbine engine, wherein said sensor generates signature data for the passage of each blade; determining an analytic waveform from said signature data; and determining blade characteristic data from said analytic waveform. 2. The method of claim 1, wherein the analytic waveform comprises a magnitude waveform, and the blade characteristic data comprises a blade crossing point determined by detecting a maximum point of the magnitude waveform. 3. The method of claim 1, wherein the sensor is an eddy current sensor. 4. The method of claim 3, wherein determining said analytic waveform comprises the steps of: performing a forward Fourier transform on said signature data; performing a zeroing out operation on the negative frequencies of said forward Fourier transform of said signature data; and performing an inverse Fourier transform on said zeroed out forward Fourier transform of said signature data. 5. The method of claim 3, wherein said signature data is measured as a function of one of time, rotor speed, tip clearance or blade angle. 6. The method of claim 3, wherein said signature data is measured utilizing a predetermined uniform sampling rate. 7. The method of claim 3, further comprising determining one of magnitude, instantaneous phase and instantaneous frequency from said analytic waveform. 8. The method of claim 3, wherein said blade characteristic data comprises one of blade clearance, vibration, flutter and twist. 9. The method of claim 3, wherein the eddy current sensor is a two pole eddy current sensor. 10. The method of claim 3, further comprising determining whether said blade characteristic data is indicative of an engine stall or surge condition. 11. The method of claim 10, wherein determining whether said blade characteristic data is indicative of an engine stall or surge condition comprises monitoring trends in said blade characteristic data. 12. A computer-readable medium having computer-executable instructions for performing steps comprising: receiving signature data relating to the passage of a plurality of rotating turbine blades during a revolution of a turbine engine; determining an analytic waveform from said signature data; and determining blade characteristic data from said analytic waveform. 13. The computer-readable medium of claim 12, wherein determining said analytic waveform comprises the steps of: performing a forward Fourier transform on said signature data; performing a zeroing out operation on the negative frequencies of said forward Fourier transform of said signature data; and performing an inverse Fourier transform on said zeroed out forward Fourier transform of said signature data. 14. The computer-readable medium of claim 12, wherein said received magnetic field signature data is measured as a function of one of time, rotor speed, tip clearance or blade angle. 15. The computer-readable medium of claim 12, wherein said received magnetic field signature data is measured utilizing a predetermined uniform sampling rate. 16. The computer-readable medium of claim 12, further comprising determining one of magnitude, instantaneous phase and instantaneous frequency from said analytic waveform. 17. The computer-readable medium of claim 12, wherein said blade characteristic data comprises one of blade clearance, vibration, flutter and twist. 18. The computer-readable medium of claim 12, wherein the analytic waveform comprises a magnitude waveform, and the blade characteristic data comprises a blade crossing point determined by detecting a maximum point of the magnitude waveform. 19. The computer-readable medium of claim 12, wherein the signature data is received from an eddy current sensor. 20. The computer-readable medium of claim 12, further comprising determining whether said blade characteristic data is indicative of a predetermined engine stall or surge condition. 21. The computer-readable medium of claim 20, wherein determining whether said blade characteristic data is indicative of a predetermined engine stall or surge condition comprises monitoring trends in said blade characteristic data. 22. A turbine engine monitor, comprising: a sensor with a sensing field in communication with a plurality of rotating turbine blades during a revolution of a turbine engine, wherein said sensor generates signature data for the passage of each blade; and a processor for determining an analytic waveform from said signature data. 23. The turbine engine monitor of claim 22, wherein the processor is further configured to determine blade characteristic data from said analytic waveform. 24. The turbine engine monitor of claim 23, wherein the sensor is an eddy current sensor. 25. The turbine engine monitor of claim 23, wherein said processor determines said analytic waveform by performing a forward Fourier transform on said signature data; performing a zeroing out operation on the negative frequencies of said forward Fourier transform of said signature data; and performing an inverse Fourier transform on said zeroed out forward Fourier transform of said signature data. 26. The turbine engine monitor of claim 23, wherein said processor measures said signature data as a function of one of time, rotor speed, tip clearance or blade angle. 27. The turbine engine monitor of claim 23, wherein said processor determines one of magnitude, instantaneous phase and instantaneous frequency from said analytic waveform. 28. The turbine engine monitor of claim 23, wherein said blade characteristic data comprises one of blade clearance, vibration, flutter and twist. 29. The turbine engine monitor of claim 23, wherein said processor determines whether said blade characteristic data is indicative of a predetermined engine stall or surge condition. 30. The turbine engine monitor of claim 23, wherein said processor measures said signature data utilizing a predetermined uniform sampling rate. 31. The turbine engine monitor of claim 30, wherein determining whether said blade characteristic data is indicative of a predetermined engine stall or surge condition comprises monitoring trends in said blade characteristic data. 32. The turbine engine monitor of claim 30, wherein the analytic waveform comprises a magnitude waveform, and the blade characteristic data comprises a blade crossing point determined by detecting a maximum point of the magnitude waveform.