ELECTRONIC VIBRATION SENSOR

• US 20070272023A1
• Filed: 05/23/2006
• Published: 11/29/2007
• Est. Priority Date: 05/23/2006
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Hellickson, Dean R., Dwyer, Michael D.
• Application Number:
  US11/419,938
• Publication Number:
  US 20070272023A1
• Time in Patent Office: Days
• US Class Current: 73/649
• CPC Class Codes: G01H 1/003 of rotating machines G01H1/10 takes precedence

Abstract

An electronic sensor is disclosed. The electronic sensor includes a processor, a processor memory coupled to the processor, and at least one input/output block in communication with the processor and with at least one external component monitor. The sensor further includes one or more accelerometers in communication with the processor and coupled directly to at least one component, the one or more accelerometers sensing one or more mechanical vibrations from the at least one component, and the one or more mechanical vibrations oscillating below 1 MHz. The processor compares the one or more mechanical vibrations with a plurality of vibration samples programmed into the processor memory, each vibration sample specific to at least one sensor application.

Claims

1. An electronic sensor, comprising:

a processor;

a processor memory coupled to the processor;

at least one input/output block in communication with the processor and with at least one external component monitor;

one or more accelerometers in communication with the processor and coupled directly to at least one component, the one or more accelerometers sensing one or more mechanical vibrations from the at least one component, the one or more mechanical vibrations oscillating below 1 MHz; and

wherein the processor compares the one or more mechanical vibrations with a plurality of vibration samples programmed into the processor memory, each vibration sample specific to at least one sensor application.

2. The sensor of claim 1, wherein the processor comprises one of a programmable logic device, a microprocessor, an application-specific integrated circuit, a field-programmable gate array, and a field-programmable object array.

3. The sensor of claim 1, wherein the processor memory comprises one of read only memory, random access memory, and flash reprogrammable memory.

4. The sensor of claim 1, wherein the at least one input/output block comprises one or more bi-directional data signal lines and at least one input power signal in communication with the at least one external component monitor.

5. The sensor of claim 1, wherein the at least one input/output block comprises one of a serial wired communication interface connection and a wireless communication interface connection.

6. The sensor of claim 1, wherein the at least one external component monitor comprises an on-board flight management system.

7. The sensor of claim 1, wherein the one or more accelerometers are integrated within the electronic sensor.

8. The sensor of claim 1, wherein the plurality of vibration samples comprise one or more vibration waveform samples indicative of one or more known failures experienced by at least a portion of the component.

9. The sensor of claim 1, wherein the plurality of vibration samples comprise one or more vibration waveform samples indicative of proper operation of at least a portion of the component.

10. A method for monitoring one or more mechanical assemblies, the method comprising:

measuring a plurality of vibration characteristics of each mechanical assembly with at least one vibration sensor, the plurality of vibration characteristics characterized by oscillating below 1 MHz;

comparing the plurality of vibration characteristics with one or more vibration samples; and

notifying a component monitor of a current condition.

11. The method of claim 10, wherein measuring the plurality of vibration characteristics further comprises programming the at least one vibration sensor with one or more vibration waveform samples.

12. The method of claim 10, wherein comparing the plurality of vibration characteristics further comprises determining whether one or more of the plurality of vibration characteristics substantially match at least one failure pattern present in the one or more vibration samples.

13. The method of claim 10, wherein notifying the component monitor further comprises signaling to the component monitor when one or more of the plurality of vibration characteristics substantially match at least one failure pattern present in the one or more vibration samples.

14. The method of claim 10, wherein notifying the component monitor further comprises refreshing the component monitor with normal operating condition information.

15. An apparatus for detecting a failure from at least a portion of a component, the apparatus comprising:

means for sensing vibrations from the component;

means, responsive to the means for sensing, for processing the sensed vibrations for indication of a current operating condition of the at least a portion of the component; and

means, responsive to the means for sensing and the means for processing, for informing at least one component monitor when the at least one failure from the at least a portion of the component is detected.

16. The apparatus of claim 15, wherein the means for sensing vibrations from the component comprises means for sensing mechanical vibrations oscillating below 1 MHz.

17. The apparatus of claim 15, wherein the means for sensing further includes one or more accelerometers integrated within at least one vibration sensor.

18. The apparatus of claim 17, wherein the means for sensing further includes the at least one vibration sensor configured for a particular application of the at least one component.

19. The apparatus of claim 15, wherein the means for processing further includes one of a programmable logic device, a microprocessor, an application-specific integrated circuit, a field-programmable gate array, and a field-programmable object array.

20. The apparatus of claim 15, wherein the means for informing further includes one of a serial wired communications interface and a wireless communications interface.