Smart accelerometer

• US 5,309,149 A
• Filed: 02/12/1992
• Issued: 05/03/1994
• Est. Priority Date: 02/12/1992
• Status: Expired due to Fees

• Current Assignee: The United States of America As Represented By The Secretary of Agriculture
• Original Assignee: United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration
• Inventors: Bozeman, Richard J. Jr.
• Primary Examiner(s): RAEVIS, ROBERT R
• Application Number:
  US07/834,451
• Time in Patent Office: 811 Days
• Field of Search: 73/117.4, 73/649, 73/658-661, 73/517 AV, 340/683
• US Class Current: 340/683
• CPC Class Codes: G01H 1/00 Measuring characteristics of vibrations in solids by using direct conduction to the detector G01H9/00, G01H11/00 take precedence
• CPC Class Codes: G01P 15/08 with conversion into electric or magnetic values
• CPC Class Codes: G08B 21/187 Machine fault alarms

Abstract

The invention discloses methods and apparatus for detecting vibrations from machines which indicate an impending malfunction for the purpose of preventing additional damage and allowing for an orderly shutdown or a change in mode of operation. The method and apparatus are especially suited for reliable operation in providing thruster control data concerning unstable vibration in an electrical environment which is typically noisy and in which unrecognized ground loops may exist.

Claims

1. A machinery vibration monitoring apparatus, comprising:

a housing defining an interior;

a transducer physically disposed with said interior of said housing and responsive to vibration in machinery operative to produce an electrical transducer signal functionally related to the magnitude and frequency of said vibration;

a decoding circuit physically disposed within said housing and responsive to said electrical transducer signal greater than a predetermined magnitude within a selected frequency band to produce a first fault signal;

a single power source supplying power to both said transducer and said decoding circuit, said power source further providing a common ground connected to both said transducer and said decoding circuit; and

isolating circuitry responsive to said first fault signal operative to produce a second fault signal for nullifying ground shift effects with respect to said common ground.

2. The apparatus of claim 1, wherein:

said isolating circuitry for producing said second fault signal includes optical isolating circuitry.

3. A machinery vibration monitoring apparatus, comprising:

a housing defining an interior;

a transducer physically disposed within said interior of said housing and responsive to vibration in machinery operative to produce an electrical transducer signal functionally related to the magnitude and frequency of said vibration;

a decoding circuitry physically disposed within said housing and responsive to said electrical transducer signal greater than a predetermined magnitude within a selected frequency band to produce a first fault signal;

a single power source supplying power to both said transducer and said decoding circuit said power source further providing a common ground connected to both said transducer and said decoding circuit;

a capacitor directly connected to said transducer; and

a potentiometer circuit within said housing and directly connected through said capacitor to said transducer for adjusting said predetermined magnitude of said electrical transducer signal.

4. The apparatus of claim 3, further comprising:

a split transducer electrical signal output, one path of said split transducer signal output bypassing said frequency decoder to allow separate monitoring of said transducer electrical signal.

5. The apparatus of claim 3, further comprising:

a bandwidth adjustment means for controlling the width of said frequency band.

6. The apparatus of claim 5, wherein:

said bandwidth adjustment means includes a switch for selectively varying the width of said frequency band.

7. The apparatus of claim 3, further comprising:

loop filter means operative in conjunction with said decoder circuit to produce said fault signal only after a predetermined number of cycles have occurred of said electrical transducer signal within said frequency band.

8. The apparatus of claim 7, further comprising:

adjustment means for selectively varying said predetermined number of cycles needed before said decoding circuit produces said fault signal.

9. The apparatus of claim 3, further comprising:

a voltage regulator powered by said single power source and controlling the voltage applied to said decoding circuit, and

a current regulator powered from said single power source and controlling the current to said transducer.

10. A machinery monitoring apparatus, comprising:

a transducer adapted to be mounted on machinery and operatively responsive to vibration in said machinery to produce an electrical transducer signal functionally related to the magnitude and frequency of said vibration;

a decoding circuit in close physical proximity to said transducer and responsive to said electrical transducer signal greater than a predetermined magnitude within a selected frequency band to produce a first fault signal, said decoding circuit including;

a decoding circuit in close physical proximity to said transducer and responsive to said electrical transducer signal greater than a predetermined magnitude within a selected frequency band to produce a first fault signal, said decoding circuit including;

a single power source supplying power to both said transducer and said decoding circuit, said power source further providing a common ground connected to both said transducer and said decoding circuit; and

a potentiometer circuit coupled to said transducer for adjusting said predetermined magnitude of said electrical transducer signal.

11. The apparatus of claim 10, further comprising:

isolating circuitry responsive to said first fault signal operative to produce a second fault signal for nullifying ground shift effects with respect to said common ground.

12. The apparatus of claim 11, wherein:

said isolating circuitry for producing said second fault signal includes optional isolating circuitry.