Fault detection using skewed transducers

Patent metadata

Field	Value
Publication number	US-9494426-B2
Application number	US-201214361437-A
Country	US
Kind code	B2
Filing date	Nov 27, 2012
Priority date	Nov 29, 2011
Publication date	Nov 15, 2016
Grant date	Nov 15, 2016

Abstract

A vibratory gyroscope is provided comprising a plurality of secondary pickoff transducers which are each sensitive to the secondary response mode, wherein: at least two of the secondary pickoff transducers comprise skew transducers designed to be sensitive to the primary mode which produce an induced quadrature signal in response thereto. A method of using the gyroscope is provided comprising the steps of arranging electrical connections between the secondary pickoff transducers and a pickoff amplifier so that in use the induced quadrature signal is substantially rejected by the amplifier in the absence of a fault condition, and the amplifier outputs an induced quadrature signal when a fault condition disconnects one of the skew transducers from the amplifier, and a comparator compares the quadrature output from the pickoff amplifier with a predetermined threshold value and provides a fault indication when the predetermined threshold is exceeded.

First claim

The invention claimed is:

1. A ring vibratory gyroscope comprising:
a plurality of secondary pickoff transducers which are each sensitive to the secondary response mode, at least two of the secondary pickoff transducers comprising skew transducers designed to be sensitive to the primary mode which produce an induced quadrature signal in response thereto; and
a pickoff amplifier and electrical connections between the secondary pickoff transducers and the pickoff amplifier wherein:
the secondary pickoff transducers, electrical connections and pickoff amplifier are arranged so that in use:
the induced quadrature signal is substantially rejected by the amplifier in the absence of a fault condition, and
the amplifier outputs an induced quadrature signal when a fault condition disconnects one of the skew transducers from the amplifier wherein a comparator compares the quadrature output from the pickoff amplifier with a predetermined threshold value and provides a fault indication when the predetermined threshold is exceeded.

2. The gyroscope of claim 1 , wherein a first skew transducer and a second skew transducer have induced quadrature signals with substantially the same phase and magnitude that are combined at inverting and non-inverting inputs to the pickoff amplifier.

3. The gyroscope of claim 2 , wherein the secondary pickoff transducers comprise positive and negative pickoff transducers which produce outputs in response to the secondary mode which have substantially 180 degrees phase difference, and the first skew transducer is a positive secondary pickoff transducer and the second skew transducer is a negative secondary pickoff transducer.

4. The gyroscope of claim 1 , wherein a skew transducer is electrically connected to another secondary pickoff transducer and/or the pickoff amplifier by a wire bond.

5. The gyroscope of claim 4 , wherein a skew transducer is electrically connected to the pickoff amplifier by a series arrangement of wire bonds, so that failure of any single connection of the series arrangement will result in a fault indication.

6. The gyroscope of claim 4 , wherein each wire bond connecting the secondary pickoff transducers to the pickoff amplifier is made in parallel, and skew transducers are associated with each wire bond so that the failure of any wire bond results in a fault indication.

7. The gyroscope of claim 1 , wherein a failure of any single electrical connection results in a fault indication.

8. The gyroscope of claim 1 , wherein the comparator comprises a demodulator/filter that filters and demodulates the output of the pickoff amplifier to remove the rate output, leaving the quadrature component.

9. The gyroscope of claim 8 , wherein the comparator further comprises an analogue to digital convertor that converts the analogue output of the demodulator/filter to a digital output.

10. The gyroscope of claim 9 , wherein the comparator further comprises a digital processor that stores predetermined values and/or ranges of quadrature output that correspond to various fault conditions, and compares the digital output of the analogue to digital convertor with the predetermined values and/or ranges to identify fault conditions.

11. The gyroscope of claim 1 , wherein the secondary pickoff transducers are capacitive, piezoelectric or inductive.

12. A method of using the gyroscope of claim 1 , comprising the steps of:
arranging electrical connections between the secondary pickoff transducers and a pickoff amplifier so that in use:
the induced quadrature signal is substantially rejected by the amplifier in the absence of a fault condition, and
the amplifier outputs an induced quadrature signal when a fault condition disconnects one of the skew transducers from the amplifier, and

a comparator compares the quadrature output from the pickoff amplifier with a predetermined threshold value and provides a fault indication when the predetermined threshold is exceeded.

13. The method of claim 12 , wherein the electrical connections comprise a first electrical connection connecting a first skew transducer to an inverting input of the pickoff amplifier, and a second electrical connection connecting a second skew transducer to a non-inverting input of the pickoff amplifier.

14. The method of claim 13 , wherein the first and second skew transducers produce an induced quadrature signal of substantially the same phase and magnitude.

15. The method of claim 12 , wherein each electrical connection between the secondary pickoff transducers to the pickoff amplifier is made in parallel, and skew transducers are associated with each connection so that the failure of any connection results in a fault indication.

16. The method of claim 12 , wherein the phase and magnitude of the quadrature output from the pickoff amplifier is compared with a pre-determined range of values to identify the fault.

Assignees

• Atlantic Inertial Systems Ltd
• Sumitomo Prec Products Company Ltd

Inventors

• Durston Michael
• Moriguchi Takafumi
• Araki Ryuta

Classifications

• G01C19/5684 Primary

  the devices involving a micromechanical structure · CPC title