Transducer testing system for low frequency vibrations

• US 5,435,168 A
• Filed: 08/17/1993
• Issued: 07/25/1995
• Est. Priority Date: 08/17/1993
• Status: Expired due to Fees

• Current Assignee: Global Associates, Ltd.
• Original Assignee: Scientific-Atlanta Incorporated (Cisco Systems, Inc.)
• Inventors: Granere, Verne R.
• Primary Examiner(s): Williams, Hezron E.
• Assistant Examiner(s): MILLER, ROSE MARY
• Application Number:
  US08/107,012
• Time in Patent Office: 707 Days
• Field of Search: 73/1 DV, 73/667, 73/662, 73/663, 73/668, 73/579, 73/517 R
• US Class Current: 73/1.84
• CPC Class Codes: G01P 21/00 Testing or calibrating of apparatus or devices covered by the preceding groups
• CPC Class Codes: G01P 21/02 of speedometers

Abstract

A transducer testing system for low frequency vibrations incorporates an electric motor/gearbox assembly 16 with an output shaft 18 and mechanical means for converting low frequency shaft rotation of the output shaft 18 to uniform low frequency sinusoidal excitation of an accelerometer 10. Simultaneously, a data processing unit 14 measures the response of the accelerometer 10 to the uniform low frequency excitation within predetermined frequency ranges. The data processing unit 14 then compares the measured response with predetermined accelerometer response limits to ascertain whether the accelerometer 10 is functional. The transducer testing system overcomes the limitations of electrodynamic testers to provide a means for accurately testing the low frequency response of the accelerometer 10.

Claims

1. A transducer testing system having vibrating means for vibrating a transducer that translates mechanical energy to electrical energy and measuring means for measuring a response of said transducer within predetermined frequency ranges, wherein the improvement is characterized by:

said vibrating means having an electric motor, a first output shaft, and mechanical converting means for converting low frequency shaft rotation of said first output shaft to a uniform low frequency sinusoidal excitation of said transducer;

said vibrating means further having a gearbox that converts shaft rotation of a second shaft of said electric motor at a first frequency to shaft rotation of said first output shaft at a second frequency; and

said transducer testing system further comprising synchronization means for providing a synchronization signal at a third frequency that corresponds to said second frequency of said first output shaft, wherein said measuring means is responsive to said synchronization signal.

2. A transducer testing system as recited in claim 1 further characterized in that said mechanical converting means includes

an eccentric hub affixed to said first output shaft, said eccentric hub having an outer first cylindrical surface;

an annular bearing having an inner race and an outer race, said inner race secured to said first cylindrical surface;

a piston having a second cylindrical surface, first and second end surfaces, biasing means for biasing said first end surface to said outer race of said annular bearing, and means for fastening said transducer to said second end surface in alignment with a sliding motion of said piston; and

a piston bearing block having an inner sleeve which slidably mates to said second cylindrical surface to guide said sliding motion of said piston.

3. A transducer testing system as recited in claim 2 further characterized in that said piston includes a notch in said first end surface that engages said outer race of said bearing, and said biasing means includes a spring clip that fits securely in a groove in said second cylindrical surface, and a spring surrounding said second cylindrical surface mounted between said spring clip and said piston bearing block to bias said notch to said outer race of said annular bearing.

4. A transducer testing system as recited in claim 1 further comprising synchronization means for providing a synchronization signal at said frequency of excitation of said transducer provided by said vibrating means.

5. A transducer testing system as recited in claim 4 further characterized in that said synchronization means includes a magnetic sensor, and a member affixed to said first output shaft formed from iron or a suitable magnetic material with a size and shape such that said member passes in close proximity to said magnetic sensor once during every rotation of said first output shaft to provide said synchronization signal.

6. A transducer testing system as recited in claim 1 further characterized in that said synchronization means includes a magnetic sensor, and a member affixed to said first output shaft formed from iron or a suitable magnetic material with a size and shape such that said member passes in close proximity to said magnetic sensor once during every rotation of said first output shaft to provide said synchronization signal.

7. The transducer testing system as recited in claim 1 further characterized in that said low frequency of said sinusoidal excitation of said transducer corresponds to a frequency of rotation of a helicopter rotor under normal operating conditions.

8. The transducer testing system as recited in claim 7 further characterized in that said frequency of rotation of a helicopter rotor is within a range from 192 to 288 revolutions per minute.

9. A transducer testing system having vibrating means for vibrating a transducer that translates mechanical energy to electrical energy and measuring means for measuring a response of said transducer within predetermined frequency ranges, wherein the improvement is characterized by:

said vibrating means having an electric motor, a first output shaft, and mechanical converting means for converting low frequency shaft rotation of said first output shaft to a uniform low frequency sinusoidal excitation of said transducer;

said mechanical converting means including

an eccentric hub affixed to said first output shaft, said eccentric hub having an outer first cylindrical surface;

an annular beating having an inner race and an outer race, said inner race secured to said first cylindrical surface;

a piston having a second cylindrical surface, first and second end surfaces, biasing means for biasing said first end surface to said outer race of said annular bearing, and means for fastening said transducer to said second end surface in alignment with a sliding motion of said piston; and

a piston beating block having an inner sleeve which slidably mates to said second cylindrical surface to guide said sliding motion of said piston.

10. A transducer testing system as recited in claim 9 further characterized in that said piston includes a notch in said first end surface that engages said outer race of said bearing, and said biasing means includes a spring clip that fits securely in a groove in said second cylindrical surface, and a spring surrounding said second cylindrical surface mounted between said spring clip and said piston bearing block to bias said notch to said outer race of said annular bearing.

11. A transducer testing system comprising:

an electric motor and gearbox assembly with an output shaft;

an eccentric hub affixed to said output shaft, said eccentric hub having an outer first cylindrical surface;

an annular bearing having an inner race and an outer race, said inner race secured to said first cylindrical surface;

a piston having a second cylindrical surface, first and second end surfaces, a notch in said first end surface that engages said outer race of said bearing, a spring clip that fits securely in a groove in said second cylindrical surface, a spring surrounding said second cylindrical surface mounted between said spring clip and said piston bearing block to bias said notch to said outer race of said annular bearing, and means for fastening said transducer to said second end surface in alignment with a sliding motion of said piston;

a piston bearing block having an inner sleeve which slidably mates to said second cylindrical surface of said piston to guide said sliding motion of said piston and vibrate said transducer; and

measuring means for measuring a response of said transducer to said vibration within predetermined frequency ranges, said measuring means having first circuit means for performing Fast Fourier Transforms to the response of said transducer.

12. The transducer testing system as recited in claim 11 wherein said transducer is an accelerometer and said measuring means has second circuit means for integrating the response of said accelerometer.

13. The transducer testing system as recited in claim 11 wherein said transducer is a velocity transducer.

14. A transducer testing system as recited in claim 11 further comprising a magnetic sensor, a member affixed to said output shaft and formed from iron or a suitable magnetic material with a size and shape such that said member passes in close proximity to said magnetic sensor once during every rotation of said output shaft to provide a synchronization signal, and said predetermined frequency ranges of said measuring means being dependent upon said synchronization signal.

15. The transducer testing system as recited in claim 14 further comprising comparing means for comparing the response of said transducer with predetermined limits.

16. The transducer testing system as recited in claim 11 further comprising comparing means for comparing the response of said transducer with predetermined limits.

17. A vibrator for exciting a transducer that translates mechanical energy to electrical energy at a uniform low frequency sinusoidal excitation, the vibrator comprising:

an electric motor;

a first output shaft; and

mechanical converting means for converting low frequency shaft rotation of said first output shaft to a uniform low frequency sinusoidal excitation of said transducer, wherein mechanical convening means comprises

an eccentric hub affixed to said first output shaft, said eccentric hub having an outer first cylindrical surface,

an annular beating having an inner race and an outer race, said inner race secured to said first cylindrical surface,

a piston having a second cylindrical surface, first and second end surfaces, biasing means for biasing said first end surface to said outer race of said annular beating, and means for fastening said transducer to said second end surface in alignment with a sliding motion of said piston, and

a piston bearing block having an inner sleeve which slidably mates to said second cylindrical surface to guide said sliding motion of said piston.

18. A vibrator as recited in claim 17 further comprising a gearbox that converts shaft rotation of a second shaft of said electric motor at a first frequency to shaft rotation of said first output shaft at a second frequency.

19. The vibrator as recited in claim 18 wherein said biasing means includes a notch in said first end surface that engages said outer race of said bearing, a spring clip that fits securely in a groove in said second cylindrical surface, and a spring surrounding said second cylindrical surface mounted between said spring clip and said piston bearing block to bias said notch to said outer race of said annular bearing.

20. The vibrator as recited in claim 18 further comprising a synchronization means for providing a synchronization signal at a third frequency that corresponds to said second frequency of said output shaft.

21. The vibrator as recited in claim 20 wherein said synchronization means includes a magnetic sensor, and a member affixed to said first output shaft formed from iron or a suitable magnetic material with a size and shape such that said member passes in close proximity to said magnetic sensor once during every rotation of said first output shaft to provide said synchronization signal.

22. The vibrator as recited in claim 18 wherein said low frequency of said sinusoidal excitation of said transducer corresponds to a frequency of rotation of a helicopter rotor under normal operating conditions.

23. The vibrator as recited in claim 22 wherein said frequency of rotation of a helicopter rotor is within a range from 192 to 288 revolutions per minute.

24. The vibrator as recited in claim 17 wherein said biasing means includes a notch in said first end surface that engages said outer race of said bearing, a spring clip that fits securely in a groove in said second cylindrical surface, and a spring surrounding said second cylindrical surface mounted between said spring clip and said piston bearing block to bias said notch to said outer race of said annular bearing.

25. The vibrator as recited in claim 17 further comprising a synchronization means for providing a synchronization signal at said frequency of excitation of said transducer provided by said converting means.

26. The vibrator as recited in claim 25 wherein said synchronization means includes a magnetic sensor, and a member affixed to said first output shaft formed from iron or a suitable magnetic material with a size and shape such that said member passes in close proximity to said magnetic sensor once during every rotation of said first output shaft to provide said synchronization signal.

27. The vibrator as recited in claim 17 wherein said low frequency of said sinusoidal excitation of said transducer corresponds to a frequency of rotation of a helicopter rotor under normal operating conditions.

28. The vibrator as recited in claim 27 wherein said frequency of rotation of a helicopter rotor is within a range from 192 to 288 revolutions per minute.

29. A vibrator for exciting a transducer that translates mechanical energy to electrical energy at a uniform low frequency sinusoidal excitation, the vibrator comprising:

a housing;

an electric motor and gearbox assembly with an output shaft;

a mounting means secured to said housing for affixing said motor and gearbox assembly to said housing;

an eccentric hub affixed to said output shaft, said eccentric hub having an outer first cylindrical surface;

an annular bearing having an inner race and an outer race, said inner race secured to said first cylindrical surface;

a piston having a second cylindrical surface, first and second end surfaces, a notch in said first end surface that engages said outer race of said bearing, a spring clip that fits securely in a groove in said second cylindrical surface, a spring surrounding said second cylindrical surface mounted between said spring clip and said piston bearing block to bias said notch to said outer race of said annular bearing, and means for fastening said transducer to said second end surface in alignment with a sliding motion of said piston; and

a piston bearing block having an inner sleeve which slidably mates to said second cylindrical surface of said piston to guide said sliding motion of said piston and vibrate said transducer, said piston bearing block affixed to said mounting means.

30. The vibrator as recited in claim 29 wherein said housing has a hinged top having a carrying handle coupled to said hinged top and a top surface with a beveled opening that allows said piston to protrude therefrom and a first mating connector/switch connected to the power inputs of the electric motor/gearbox assembly integral to said top surface.

31. The vibrator as recited in claim 29 wherein said housing has a top surface with a beveled opening that allows said piston to protrude therefrom and a hinged top that covers said top surface, said piston slidably oscillating in a vertical direction perpendicular to said top surface of said housing.

32. A vibrator as recited in claim 29 further comprising a magnetic sensor affixed to said mounting means, and a member affixed to said output shaft and formed from iron or a suitable magnetic material with a size and shape such that said member passes in close proximity to said magnetic sensor once during every rotation of said output shaft to provide a synchronization signal, said magnetic sensor having an adjusting means for adjusting the spacing between said magnetic sensor and said member.

33. A method of operating a transducer tester,

said transducer tester having vibrating means for sinusoidally exciting a transducer that translates mechanical energy to electrical energy,

said transducer tester also having measuring means for measuring and storing a response of said transducer within predetermined frequency ranges, said vibrating means having an electric motor, a first output shaft, and mechanical converting means for converting low frequency shaft rotation of said first output shaft to a uniform low frequency sinusoidal excitation of said transducer,

said transducer tester further having comparing means for comparing the response of said transducer with predetermined limits, the method comprising the steps of:

sinusoidally exciting said transducer at a low frequency with said vibrating means;

simultaneously measuring and storing the response of said transducer to said excitation within said predetermined frequency ranges with said measuring means; and

comparing the response of said transducer with said predetermined limits in order to ascertain whether said transducer is functional.

34. The method of operating a transducer tester as recited in claim 33 wherein said low frequency of excitation of said transducer corresponds to a frequency of rotation of a helicopter rotor under normal operating conditions.

35. The method of operating a transducer tester as recited in claim 34 wherein said frequency of rotation of a helicopter rotor is within a range from 192 to 288 revolutions per minute.

36. A method of operating a transducer tester,

said transducer tester having vibrating means for sinusoidally exciting a transducer that translates mechanical energy to electrical energy,

said transducer tester also having measuring means for measuring and storing a response of said transducer within predetermined frequency ranges, said vibrating means having an electric motor, a first output shaft, mechanical converting means for converting low frequency shaft rotation of said first output shaft to a uniform low first frequency sinusoidal excitation of said transducer, and a synchronization means for providing a synchronization signal at a second frequency that corresponds to said first frequency,

said transducer tester further having comparing means for comparing the response of said transducer with predetermined limits, the method comprising the steps of:

sinusoidally exciting said transducer at said first frequency and producing said synchronization signal at said second frequency with said vibrating means;

simultaneously measuring and storing the response of said transducer to said excitation within said predetermined frequency ranges with said measuring means, said predetermined frequency ranges dependent upon said second frequency of said synchronization signal; and

comparing the response of said transducer with said predetermined limits in order to ascertain whether said transducer is functional.

37. The method of operating a transducer tester as recited in claim 36 wherein said low frequency of excitation of said transducer corresponds to a frequency of rotation of a helicopter rotor under normal operating conditions.

38. The method of operating a transducer tester as recited in claim 37 wherein said frequency of rotation of a helicopter rotor is within a range from 192 to 288 revolutions per minute.

39. A method of operating a transducer tester,

said transducer tester having vibrating means for sinusoidally exciting a transducer that translates mechanical energy to electrical energy,

said transducer tester also having measuring means for measuring and storing a response of said transducer within predetermined frequency ranges, said vibrating means having an electric motor, a first output shaft, mechanical converting means for converting low frequency shaft rotation of said first output shaft to a uniform low first frequency sinusoidal excitation of said transducer, and a synchronization means for providing a synchronization signal at a second frequency that corresponds to said first frequency,

said transducer tester further having a means for computing an average of the response of said transducer during each cycle of said synchronization signal and subtracting said computed average from each stored response, the method comprising the steps of:

sinusoidally exciting said transducer at said first frequency and producing said synchronization signal at said second frequency with said vibrating means;

simultaneously measuring and storing the response of said transducer to said excitation within said predetermined frequency ranges with said measuring means, said predetermined frequency ranges dependent .upon said second frequency of said synchronization signal; and

computing said average of the response of said transducer during each cycle of said synchronization signal and then subtracting said computed average from each stored response in order to eliminate harmonic components from the response of said transducer.

40. A method of operating a transducer tester as recited in claim 39, said transducer tester having comparing means for comparing the response of said transducer with predetermined limits, the method having an additional step of comparing the response of said transducer with said predetermined limits in order to ascertain whether said transducer is functional.

41. A transducer tester comprising

vibrating means for sinusoidally exciting a transducer that translates mechanical energy to electrical energy,

said vibrating means having an electric motor, a first output shaft, and mechanical converting means for converting low frequency shaft rotation of said first output shaft to a uniform low frequency sinusoidal excitation of said transducer;

measuring means for measuring and storing a response of said transducer within predetermined frequency ranges; and

comparing means for comparing the response of said transducer with predetermined limits to thereby ascertain whether said transducer is functional.

42. The transducer tester of claim 41 further comprising a synchronization means for providing a synchronization signal at the frequency of excitation of said transducer produced by said vibrating means.

43. The transducer tester of claim 42 wherein said synchronization means includes a magnetic sensor, and a member affixed to said first output shaft formed from iron or a suitable magnetic material with a size and shape such that said member passes in close proximity to said magnetic sensor once during every rotation of said first output shaft to provide said synchronization signal.

44. The transducer tester of claim 41 wherein said vibrating means further has a gearbox that converts shaft rotation of a second shaft of said electric motor at a first frequency to shaft rotation of said first output shaft at a second frequency.

45. The transducer tester of claim 44 further comprising a synchronization means for providing a synchronization signal at a third frequency that corresponds to said second frequency of said first output shaft, and wherein said measuring means is responsive to said synchronization signal.

46. The transducer tester of claim 45 wherein said synchronization means includes a magnetic sensor, and a member affixed to said first output shaft formed from iron or a suitable magnetic material with a size and shape such that said member passes in close proximity to said magnetic sensor once during every rotation of said first output shaft to provide said synchronization signal.

47. The transducer tester of claim 41 wherein said mechanical converting means includes

an eccentric hub affixed to said first output shaft, said eccentric hub having an outer first cylindrical surface;

an annular bearing having an inner race and an outer race, said inner race secured to said first cylindrical surface;

a piston having a second cylindrical surface, first and second end surfaces, biasing means for biasing said first end surface to said outer race of said annular bearing, and means for fastening said transducer to said second end surface in alignment with a sliding motion of said piston; and

a piston beating block having an inner sleeve which slidably mates to said second cylindrical surface to guide said sliding motion of said piston.

48. The transducer tester of claim 47 wherein said piston includes a notch in said first end surface that engages said outer race of said bearing, wherein said biasing means includes a spring clip that fits securely in a groove in said second cylindrical surface, and wherein a spring surrounding said second cylindrical surface is mounted between said spring clip and said piston bearing block to bias said notch to said outer race of said annular beating.