GB2142429A - Wide bandwidth surface acoustic wave vibration sensor - Google Patents

Wide bandwidth surface acoustic wave vibration sensor Download PDF

Info

Publication number
GB2142429A
GB2142429A GB08317332A GB8317332A GB2142429A GB 2142429 A GB2142429 A GB 2142429A GB 08317332 A GB08317332 A GB 08317332A GB 8317332 A GB8317332 A GB 8317332A GB 2142429 A GB2142429 A GB 2142429A
Authority
GB
United Kingdom
Prior art keywords
vibration
acoustic wave
surface acoustic
sensor
bearing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
GB08317332A
Other versions
GB8317332D0 (en
Inventor
Douglas Frank George Dwyer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
STC PLC
Original Assignee
Standard Telephone and Cables PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Standard Telephone and Cables PLC filed Critical Standard Telephone and Cables PLC
Priority to GB08317332A priority Critical patent/GB2142429A/en
Publication of GB8317332D0 publication Critical patent/GB8317332D0/en
Publication of GB2142429A publication Critical patent/GB2142429A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01HMEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H1/00Measuring characteristics of vibrations in solids by using direct conduction to the detector
    • G01H1/12Measuring characteristics of vibrations in solids by using direct conduction to the detector of longitudinal or not specified vibrations

Abstract

A vibration sensor comprising a cantilever flexible beam (3) bearing on one surface a surface acoustic wave structure (1,2), the beam being supported for a portion of its length from one end on a rigid support member (4) and carrying on its unsupported portion a mass of damping material (5) whereby during flexural vibration of the beam standing waves in the beam due to flexural waves reflected from the unsupported end of the beam are eliminated, the surface acoustic wave structure being located about the position of maximum flexing of the beam during vibration. The surface acoustic wave structure may be a simple delay line or it may include reflectors (7,8) to form a resonant cavity. The free end of the beam may be mass loaded (9). <IMAGE>

Description

@@@@@@@@@@@@@@@ surface acoustic wave vibratioi sensor This invention relates to vibration sensors using surface acoustic wave technology such as may be used for monitoriny the performance and condition of bearings in engineering equipment.
It is well known that bearings, e.g. ball or roller bearings, can be monitored in use by detecting and measuring vibration in the bearing. The problem is to provide a compact, rigged form of vibration sensor that can be utilised in situ on a bearing.
According to the present invention there is provided a vibration sensor comprising a flexible beam bearing a surface acoustic wave structureRs), the beam being supported for a portion of its length on a rigid support member and including means for damping its unsupported portion(s) whereby during flexural vibration of the beam standing waves in the beam due to flexural waves are eliminated, the surface acoustic wave structure being located about the position of maximum flexing of the beam during vibration.
An embodiment of the invention will now be described with reference to the accompanying drawings, in which: Figure 1 is a plan view of a surface acoustic wave vibration sensor, and Figure 2 is a side view of the sensor of Figure 1.
The vibration sensor is based on a surface acoustic wave accelerometer mounted on a particular configuration of flexible beam. In the embodiment illustrated surface acoustic wave transducers, e.g.
interdigital electrode patterns 1,2 etched in alumi- nium, are formed on one side of a quartz beam 3.
The beam is rigidly supported for a portion member 4, e.g. a quartz spacer. The unsupported portion o the beam 3 is provided with flexural vibration damping rnalerial 5. The transdt.lcers 1,2 are located about the position of maximum flexing when the support member 4 is subject to vibration, e.g. by attachment to a vibrating body 6 such as the housing of bearing. This would normally be above the point at which the unsupported portion of the beam commences.
The transducers 1,2 are connected via leads la, 1 b, 2a, 2b to a circuit (not shown) in which the resonator forms, together with an amplifier, an oscillate maintaining loop. The oscillator output is thus in the form of a carrier frequency modulated by a vibration frequency.
Whilst a simple two transducer delay line may suffice it may be beneficial to incorporate acoustic wave reflectors 7,8 on either side of the resonator.
These have the effect of turning the acoustic wave structure into the equivalent of a resonant cavity.
Further, it may be desirable to mass load the unsupported end of the beam 3, with a weight 9. The choice of dimensions, loading etc is governed by range of vibration frequencies which it is desired to monitor. The sensor is constructed so as to respond to applied vibration with a minimum variation in sensitivity over a frequency band up to, and exceed ing by many octaves, the first flexural resonance frequency. This is achieved by ensuring::- 1) that the sensor active region (the surface acoustic wave delay iine or resonator cavity) is shorter than one quarter of the wavelength of the upper frequency cy of interest, and 2) that the beam is damped for flexural vibration such that virtually no flexural waves are reflected from the unsupported end of the beam.
A characteristic of a sensor such as has been described is that it is also sensitive to temperature changes. For example, m when used to monitor the performance of a bearing not only will vibration in the bearing impose a modulation on the carrier at the frequency of the vibration, there will also be a long-term variation of the modulated carrier in accordance with any temperature variation of the bearing. This is important because usually deterioration in a bearing is accompanied by a temperature rise. Thus even when the vibration ceases, e.g. when the maching running is stopped, the residual temperature change is detectable until the bearing has cooled down to ambient temperature. Differential filtering of the oscillator frequency can be used to detect separately the low frequency (down to d.c.
component imposed on the carrier by temperature change and the relatively high frequency modulation of the carrier due to vibration.
1. A vibration sensor comprising a flexible beam bearing a surface acoustic wave structure(s), the beam being supported for a portion of its length on a rigid support member and including means for damping its unsupported portion(s) whereby during flexural vibration of the beam standing waves in the beam diic to flexural waves are eliminated, the stirface acoustic wave -tructure being located about the position of maximum flexing @@@@@@@@@@@@@@@@@ vibration.
2. A sensor according to claim i rv'brcin the surface acoustic wave structure is configured as a delay line.
3. A sensor according to claim 1 wherein the surface acoustic wave structure includes two acoustic wave reflectors, one on either side of the pair of transducers, to forrn with the transducers a resonant cavity.
4. A sensor according to claim 1,2 or 3 including mass loading of the unsupported end of the beam.
5. A sensor according to any preceding claim wherein the beam is quartz.
6. A sensor according to a precedin; claim wherein the support r1ieniber is quartz.
7. A vibration sensor substantially as described with reference to the accompanying drawious.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (7)

**WARNING** start of CLMS field may overlap end of DESC **. @@@@@@@@@@@@@@@ surface acoustic wave vibratioi sensor This invention relates to vibration sensors using surface acoustic wave technology such as may be used for monitoriny the performance and condition of bearings in engineering equipment. It is well known that bearings, e.g. ball or roller bearings, can be monitored in use by detecting and measuring vibration in the bearing. The problem is to provide a compact, rigged form of vibration sensor that can be utilised in situ on a bearing. According to the present invention there is provided a vibration sensor comprising a flexible beam bearing a surface acoustic wave structureRs), the beam being supported for a portion of its length on a rigid support member and including means for damping its unsupported portion(s) whereby during flexural vibration of the beam standing waves in the beam due to flexural waves are eliminated, the surface acoustic wave structure being located about the position of maximum flexing of the beam during vibration. An embodiment of the invention will now be described with reference to the accompanying drawings, in which: Figure 1 is a plan view of a surface acoustic wave vibration sensor, and Figure 2 is a side view of the sensor of Figure 1. The vibration sensor is based on a surface acoustic wave accelerometer mounted on a particular configuration of flexible beam. In the embodiment illustrated surface acoustic wave transducers, e.g. interdigital electrode patterns 1,2 etched in alumi- nium, are formed on one side of a quartz beam 3. The beam is rigidly supported for a portion member 4, e.g. a quartz spacer. The unsupported portion o the beam 3 is provided with flexural vibration damping rnalerial 5. The transdt.lcers 1,2 are located about the position of maximum flexing when the support member 4 is subject to vibration, e.g. by attachment to a vibrating body 6 such as the housing of bearing. This would normally be above the point at which the unsupported portion of the beam commences. The transducers 1,2 are connected via leads la, 1 b, 2a, 2b to a circuit (not shown) in which the resonator forms, together with an amplifier, an oscillate maintaining loop. The oscillator output is thus in the form of a carrier frequency modulated by a vibration frequency. Whilst a simple two transducer delay line may suffice it may be beneficial to incorporate acoustic wave reflectors 7,8 on either side of the resonator. These have the effect of turning the acoustic wave structure into the equivalent of a resonant cavity. Further, it may be desirable to mass load the unsupported end of the beam 3, with a weight 9. The choice of dimensions, loading etc is governed by range of vibration frequencies which it is desired to monitor. The sensor is constructed so as to respond to applied vibration with a minimum variation in sensitivity over a frequency band up to, and exceed ing by many octaves, the first flexural resonance frequency. This is achieved by ensuring::- 1) that the sensor active region (the surface acoustic wave delay iine or resonator cavity) is shorter than one quarter of the wavelength of the upper frequency cy of interest, and 2) that the beam is damped for flexural vibration such that virtually no flexural waves are reflected from the unsupported end of the beam. A characteristic of a sensor such as has been described is that it is also sensitive to temperature changes. For example, m when used to monitor the performance of a bearing not only will vibration in the bearing impose a modulation on the carrier at the frequency of the vibration, there will also be a long-term variation of the modulated carrier in accordance with any temperature variation of the bearing. This is important because usually deterioration in a bearing is accompanied by a temperature rise. Thus even when the vibration ceases, e.g. when the maching running is stopped, the residual temperature change is detectable until the bearing has cooled down to ambient temperature. Differential filtering of the oscillator frequency can be used to detect separately the low frequency (down to d.c. component imposed on the carrier by temperature change and the relatively high frequency modulation of the carrier due to vibration. CLAIMS
1. A vibration sensor comprising a flexible beam bearing a surface acoustic wave structure(s), the beam being supported for a portion of its length on a rigid support member and including means for damping its unsupported portion(s) whereby during flexural vibration of the beam standing waves in the beam diic to flexural waves are eliminated, the stirface acoustic wave -tructure being located about the position of maximum flexing @@@@@@@@@@@@@@@@@ vibration.
2. A sensor according to claim i rv'brcin the surface acoustic wave structure is configured as a delay line.
3. A sensor according to claim 1 wherein the surface acoustic wave structure includes two acoustic wave reflectors, one on either side of the pair of transducers, to forrn with the transducers a resonant cavity.
4. A sensor according to claim 1,2 or 3 including mass loading of the unsupported end of the beam.
5. A sensor according to any preceding claim wherein the beam is quartz.
6. A sensor according to a precedin; claim wherein the support r1ieniber is quartz.
7. A vibration sensor substantially as described with reference to the accompanying drawious.
GB08317332A 1983-06-29 1983-06-29 Wide bandwidth surface acoustic wave vibration sensor Withdrawn GB2142429A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08317332A GB2142429A (en) 1983-06-29 1983-06-29 Wide bandwidth surface acoustic wave vibration sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08317332A GB2142429A (en) 1983-06-29 1983-06-29 Wide bandwidth surface acoustic wave vibration sensor

Publications (2)

Publication Number Publication Date
GB8317332D0 GB8317332D0 (en) 1983-07-27
GB2142429A true GB2142429A (en) 1985-01-16

Family

ID=10544820

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08317332A Withdrawn GB2142429A (en) 1983-06-29 1983-06-29 Wide bandwidth surface acoustic wave vibration sensor

Country Status (1)

Country Link
GB (1) GB2142429A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7639826B1 (en) 2004-01-08 2009-12-29 New Transducers Limited Bending wave panel loudspeaker
CN110081918A (en) * 2019-04-26 2019-08-02 中北大学 Multi-parameter surface acoustic wave sensing device and preparation method thereof
WO2020215611A1 (en) * 2019-04-26 2020-10-29 中北大学 Multi-parameter surface acoustic wave sensing device, manufacturing method, and aircraft monitoring system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1211809A (en) * 1967-09-29 1970-11-11 Gleason Works Improvements relating to machines for running together bevel or hypoid gears
GB1317152A (en) * 1969-04-16 1973-05-16 Triumph Motor Co Ltd Tevice responsive to the amplitude of vibration at a predetermined frequency of a vibrating body
GB1432818A (en) * 1972-10-24 1976-04-22 Sperry Rand Corp Transducer means
GB1466401A (en) * 1973-05-14 1977-03-09 Trw Inc Gas generating charge for open chamber gas powered tool
GB1525334A (en) * 1975-03-03 1978-09-20 Sperry Rand Corp Transducer means
GB1599727A (en) * 1978-01-18 1981-10-07 Bosch Gmbh Robert Sensor for detecting vibrations in a combustion engine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1211809A (en) * 1967-09-29 1970-11-11 Gleason Works Improvements relating to machines for running together bevel or hypoid gears
GB1317152A (en) * 1969-04-16 1973-05-16 Triumph Motor Co Ltd Tevice responsive to the amplitude of vibration at a predetermined frequency of a vibrating body
GB1432818A (en) * 1972-10-24 1976-04-22 Sperry Rand Corp Transducer means
GB1466401A (en) * 1973-05-14 1977-03-09 Trw Inc Gas generating charge for open chamber gas powered tool
GB1525334A (en) * 1975-03-03 1978-09-20 Sperry Rand Corp Transducer means
GB1599727A (en) * 1978-01-18 1981-10-07 Bosch Gmbh Robert Sensor for detecting vibrations in a combustion engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7639826B1 (en) 2004-01-08 2009-12-29 New Transducers Limited Bending wave panel loudspeaker
CN110081918A (en) * 2019-04-26 2019-08-02 中北大学 Multi-parameter surface acoustic wave sensing device and preparation method thereof
WO2020215611A1 (en) * 2019-04-26 2020-10-29 中北大学 Multi-parameter surface acoustic wave sensing device, manufacturing method, and aircraft monitoring system
EP3967982A4 (en) * 2019-04-26 2022-12-28 North University of China Multi-parameter surface acoustic wave sensing device, manufacturing method, and aircraft monitoring system

Also Published As

Publication number Publication date
GB8317332D0 (en) 1983-07-27

Similar Documents

Publication Publication Date Title
US3878477A (en) Acoustic surface wave oscillator force-sensing devices
US4901586A (en) Electrostatically driven dual vibrating beam force transducer
US4594898A (en) Force sensors
US5113698A (en) Vibrating beam transducer drive system
US4658175A (en) Vibrating beam force transducer with A-frame beam root and frequency adjusting means
EP0244086A2 (en) Resonator device
EP1445579B9 (en) Vibrators and vibratory gyroscopes
FR2435707A1 (en) DEVICE FOR MEASURING THE DENSITY OF A LIQUID
US4333342A (en) Fluid damped saw accelerometer
GB2142429A (en) Wide bandwidth surface acoustic wave vibration sensor
CA1290593C (en) Mounting and isolation system for tuning fork temperature sensor
US4414652A (en) Ultrasonic line sensor
US4949584A (en) Apparatus for measuring depth of a fluid chamber
US4047428A (en) Force measuring transducer with frequency output signal
JPS5594122A (en) Thermometer
SU1578637A1 (en) Vibroacoustic receiving transducer
JPS6122340Y2 (en)
SU883681A1 (en) Pressure transducer with frequency output
SU1578526A1 (en) Force transmitter
SU830163A2 (en) Pressure sensor with frequency output signal
JPS5856406B2 (en) crystal transducer
JPS62147317A (en) Remote measuring apparatus
JPH07109970B2 (en) Structure of twin tuning fork type piezoelectric vibrator
SU690322A1 (en) Method of measuring resonant frequencies of vibrations
RU2026540C1 (en) Pressure gauge

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)