GB2117115A - Surface acoustic wave accelerometer - Google Patents

Surface acoustic wave accelerometer Download PDF

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Publication number
GB2117115A
GB2117115A GB08208434A GB8208434A GB2117115A GB 2117115 A GB2117115 A GB 2117115A GB 08208434 A GB08208434 A GB 08208434A GB 8208434 A GB8208434 A GB 8208434A GB 2117115 A GB2117115 A GB 2117115A
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GB
United Kingdom
Prior art keywords
strip
surface acoustic
acoustic wave
acceleration
propagation path
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.)
Granted
Application number
GB08208434A
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GB2117115B (en
Inventor
Douglas Frank George Dwyer
Steven Courtenay Hudson
David Errol Bower
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 GB08208434A priority Critical patent/GB2117115B/en
Publication of GB2117115A publication Critical patent/GB2117115A/en
Application granted granted Critical
Publication of GB2117115B publication Critical patent/GB2117115B/en
Expired legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/02Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
    • G01P15/08Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
    • G01P15/097Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by vibratory elements
    • G01P15/0975Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by vibratory elements by acoustic surface wave resonators or delay lines

Abstract

An accelerometer comprises a resilient strip of quartz 1 on one face of which are formed surface acoustic wave transducers 3, 4 connected in the feedback loop of an amplifier to form an oscillator. The strip 1 is mounted in a support member 2 which is movable in a direction a normal to the plane of the strip whereby the resilient strip will bend because of inertial resistance to acceleration forces. This bending of the strip alters the amplifier loop delay and hence the oscillator frequency f. Arrangements are disclosed for compensating for temperature variations and unwanted coupling (Figs. 3 to 5). Alternatively, a reference frequency may be provided from a surface acoustic wave device mounted on a rigid strip (Fig. 6). A heater may be controllable to maintain the accelerometer at a constant temperature (Fig. 7). <IMAGE>

Description

SPECIFICATION Surface acoustic wave accelerometer This invention relates to a surface acoustic wave accelerometer device.
A typical simple accelerometer comprises a mass maintained in a neutral position in a system by means of springs. It remains in this neutral position so long as the system as a whole remains at rest or is in motion at a constant velocity. When the system is accelerated, i.e. is subjected to a change of velocity, the mass will, because of its inertia, lag behind the system movement. This movement of the mass relative to the rest of the system can be detected and used to control e.g.
an electrical circuit to give a signal representative of the acceleration.
According to the present invention there is provided an accelerometer device comprising a resilient strip substrate of surface acoustic wave material provided with surface acoustic wave transducers arranged on a wave propagation path, at least one end of the strip being secured in a support member whereby acceleration of the support member in a direction normal to the plane of the strip will result in bending of the strip and a change in the propagation path whereby the acceleration can be measured by measuring the change in propagation path.
According to another aspect of the invention there is provided a method of measuring acceleration of a body wherein a resilient strip of surface acoustic wave material provided on at least one face with surface acoustic wave transducers arranged on a wave propagation path is subjected to bending in a direction normal to the plane of the strip in response to acceleration of the body resulting in a change in the propagation path delay and utilising the change to provide a signal which is a measure of the acceleration.
Embodiments of the invention will now be described with reference to the accompanying drawings, in which: Figs. 1 a and 1 b illustrate a simple cantilever or single clamped semi-beam surface acoustic wave accelerometer, Figs. 2a and 2b illustrate a double clamped beam accelerometer, Figs. 3 and 4 illustrate differential output versions of the accelerometers of Figs. 1 and 2, Fig. 5 illustrates an arrangement for decoupling a differential accelerometer, Fig. 6 illustrates an arrangement for obtaining ageing and temperature compensation of a surface acoustic accelerometer, and Fig. 7 illustrates a feedback arrangement for temperature compensation of an accelerometer.
In the arrangement shown in Fig. 1 a a quartz strip 1 is clamped at one end in a support 2 so that the strip forms a cantilever or semi-beam structure. Electroacoustic transducers 3, 4 are provided on the surface of the strip 1 whereby surface acoustic waves can be propagated from transducer 3 in the surface region of the quartz strip to transducer 4. Surface acoustic wave absorption means 5, 6 are provided at each end of the strip. The transducers 3 and 4 are electrically connected in a feedback loop of an amplifier 7 to form an oscillator the frequency of which is dependent on the loop delay.
If the support 2 is moved in a direction normal to the plane of the strip 1, with an acceleration a, the strip 1 bends as shown in Fig. 1 b. This bending causes the surface acoustic wave path length between transducers 3 and 4 to change, resulting in a change in the oscillator frequency f.
Typically a quartz substrate 1 inch long and 500 ym thick will withstand accelerations up to 5000 g. With oscillator frequencies of hundreds of MHz sensitivities of the order of 0.4 ppm/g are attainable whilst a stability of 10-3 ppm can be attained in the neutral condition.
As an alternative to the cantilevered structure of Figs. 1 a and 1 b a double clamped beam can be used, as shown in Figs. 2a and 2b. The structure is generally similar to that Figs. 1 a and 1 b except that the strip 1 is clamped at both ends and both supports 2, 2a will move as one during acceleration. The resultant bending of the strip is symmetrical about its centre, as shown in Fig. 2b.
Fig. 3 shows a cantilever structure similar to that of Fig. 1 a but with two surface acoustic wave paths, one on either face of the strip 1. Each of the paths extending respectively between transducers 3, 4 and 3a, 4a is connected in a separate oscillator loop 7, 7a. When acceleration occurs a differential output is obtained. This has advantages for the subsequent signal processing, as will be readily recognised by those skilled in the art. A similar arrangement for the double clamped beam structure is shown in Fig. 4.If f1=f0[1 ±kAT] and f2=f0[1 --kAT], where f0 is the common neutral frequency of both loops, a is the proportional path length change due to acceleration and kAT is a temperature coefficient of path length change, then f, -f=2f, (independent of AT to first order).
Should there by any problem of unwanted coupling between the two frequencies then a modification as shown in Fig. 5 can be used.
Oscillator loop 7, 3, 4 can have a frequency: f-k f 1- r and loop 7a, 3a, 4a a frequency 2=k2fr where k1 and k2 are positive unequal integers and fr is a nominal reference frequency. The output frequencies are then fed to respective divider networks 8, 8a whose division ratios are k, and k2 respectively.
Thus, during acceleration fi=ki.fr(1 +a) f2=k2'fr(l -8) The differential output is then 2f,.6. In this case there will be a loss of sensitivity as fr is less than fo.
One method of compensating for errors due to temperature and ageing is to provide a reference frequency which although subject to the same errors is invariant during acceleration. This reference frequency can then be compared with the variable frequency to determine the amount of change due solely to acceleration. Fig. 6 shows an arrangement in which two substantially identical surface acoustic wave structures 11, 11 a are mounted side by side in a common support 12.
The surface acoustic wave structure 11 is free to respond to acceleration forces as described above, whilst structure 1 a is constrained to be inflexible by being bonded to a rigid backing 13.
One method of compensating for errors due to temperature and ageing is to provide a reference frequency which although subject to the same errors is invariant during acceleration. This reference frequency can then be compared with the variable frequency to determine the amount of change due soleiy to acceleration. Fig. 6 shows an arrangement in which two substantially identical surface acoustic wave structures 11, 1 a are mounted side by side in a common support 1 2. The surface acoustic wave structure 11 is free to respond to acceleration forces as described above, whilst structure 1 a is constrained to be inflexible by being bonded to a rigid backing 1 3.
Whilst the ageing effects in a surface acoustic wave device can probably be ignored, e.g.
typically less than 10 ppm/year, temperature sensitivity is a factor which must be considered.
Fig. 7 shows an arrangement in which a positive temperature correction is applied. The differential structure of Fig. 3 or Fig. 5 is used to provide a sum output 2fo (1-kAT) which is applied to a phase sensitive detector 14 together with a stable reference frequency from source 1 5 to produce a temperature control signal 1 6. This control signal is passed through a loop filter 1 7 and fed to a power amplifier 18 the output of which is applied to a heater 19. Heater 19 is arranged to keep the surface acoustic wave structure at a constant temperature.
Although the above descriptions refer to a delay-line surface wave oscillator, a practical alternative could employ a surface-wave resonator as the controiling element of an oscillator.

Claims (10)

Claims
1. An accelerometer device comprising a resilient strip substrate of surface acoustic wave material provided with surface acoustic wave transducers arranged on a wave propagation path, at least one end of the strip being secured in a support member whereby acceleration of the support member in a direction normal to the plane of the strip will result in bending of the strip and a change in the propagation path whereby the acceleration can be measured by measuring the change in propagation path.
2. A device according to claim 1 wherein both ends of the strip are secured in support members whereby common movement of both support members in a direction normal to the plane of the strip will result in bending of the strip between the two ends thereof.
3. A device according to claim 1 or 2 wherein the strip is provided on opposing faces with separate substantially identical surface acoustic wave transducer arrangements having the same surface acoustic wave frequencies.
4. A device according to claim 1 or 2 wherein the strip is provided on opposing faces with separate surface acoustic wave transducer arrangements having different surface acoustic wave frequencies.
5. A device according to any preceding claim including a second rigid strip substrate of surface acoustic wave material provided with a substantially identical surface acoustic wave transducer arrangement to a transducer arrangement on the resilient strip.
6. A surface acoustic wave accelerometer device according to any preceding claim including means for obtaining an electrical signal representative of differential changes in frequency of surface acoustic wave propagating simultaneously in propagation paths on opposing faces of the strip and temperature compensating means responsive to said electrical signal to maintain constant the temperature of the device.
7. A device according to any preceding claim wherein the or each transducer arrangement is connected eiectrically in the feedback loop of an amplifier to form an oscillator the frequency of which is dependent on the loop delay.
8. A surface acoustic wave accelerometer device substantially as described with reference to the accompanying drawings.
9. A method of measuring acceleration of a body wherein a resilient strip of surface acoustic wave material provided on at least one face with surface acoustic wave transducers arranged on a wave propagation path is subjected to bending in a direction normal to the plane of the strip in response to acceleration of the body resulting in a change in the propagation path delay and utilising the change to provide a signal which is a measure of the acceleration.
10. A method of measuring acceleration substantially as hereibefore described with reference to the accompanying drawings.
GB08208434A 1982-03-23 1982-03-23 Surface acoustic wave accelerometer Expired GB2117115B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08208434A GB2117115B (en) 1982-03-23 1982-03-23 Surface acoustic wave accelerometer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08208434A GB2117115B (en) 1982-03-23 1982-03-23 Surface acoustic wave accelerometer

Publications (2)

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GB2117115A true GB2117115A (en) 1983-10-05
GB2117115B GB2117115B (en) 1985-11-06

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2140161A (en) * 1983-05-20 1984-11-21 Thomson Csf Elastic surface wave force sensor
FR2557695A1 (en) * 1984-01-03 1985-07-05 Thomson Csf Surface elastic wave force sensor
FR2561383A1 (en) * 1984-03-16 1985-09-20 Thomson Csf Vector force sensor based on elastic surface waves.
US4598587A (en) * 1983-08-04 1986-07-08 Standard Telephones & Cables, Plc Surface acoustic wave accelerometer
US4621530A (en) * 1983-07-14 1986-11-11 Standard Telephones And Cables Public Limited Company Surface acoustic wave accelerometer
US4689992A (en) * 1984-04-04 1987-09-01 Syrinx Innovations Limited Rotation rate sensor
GB2219858A (en) * 1988-06-15 1989-12-20 Nat Res Dev Apparatus and method for detecting small changes in attached mass on piezoelectric devices used as sensors.
DE4135369A1 (en) * 1991-10-26 1993-05-13 Bosch Gmbh Robert Bipolar piezoelectric accelerometer with built-in test facility - has upper and lower electrodes in halves for application of test voltage and measurement of deformation
US6803698B2 (en) * 2000-10-12 2004-10-12 Murata Manufacturing Co., Ltd Acceleration sensor
US7380454B2 (en) * 2005-12-20 2008-06-03 Honeywell International Inc. Load beam for surface acoustic wave accelerometer
US7667369B2 (en) * 2006-11-01 2010-02-23 Delaware Capital Formation, Inc. High sensitivity microsensors based on flexure induced frequency effects
US7886575B2 (en) 2006-11-01 2011-02-15 Delaware Capital Formation, Inc. High sensitivity acoustic wave microsensors based on stress effects

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1432818A (en) * 1972-10-24 1976-04-22 Sperry Rand Corp Transducer means
GB1486377A (en) * 1974-02-25 1977-09-21 United Aircraft Corp Surface acoustic wave transducer
GB1488155A (en) * 1974-01-08 1977-10-05 Hewlett Packard Co Acoustic surface wave oscillator force-sensing devices
EP0012644A1 (en) * 1978-11-30 1980-06-25 Thomson-Csf Surface acoustic wave accelerometer
EP0017554A1 (en) * 1979-03-30 1980-10-15 Thomson-Csf Accelerometer using elastic waves
GB1579113A (en) * 1977-03-18 1980-11-12 United Technologies Corp Differential surface acoustic wave transducer
GB1595445A (en) * 1976-12-20 1981-08-12 Gould Inc Force sensor using surface acoustic waves

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1432818A (en) * 1972-10-24 1976-04-22 Sperry Rand Corp Transducer means
GB1488155A (en) * 1974-01-08 1977-10-05 Hewlett Packard Co Acoustic surface wave oscillator force-sensing devices
GB1486377A (en) * 1974-02-25 1977-09-21 United Aircraft Corp Surface acoustic wave transducer
GB1595445A (en) * 1976-12-20 1981-08-12 Gould Inc Force sensor using surface acoustic waves
GB1579113A (en) * 1977-03-18 1980-11-12 United Technologies Corp Differential surface acoustic wave transducer
EP0012644A1 (en) * 1978-11-30 1980-06-25 Thomson-Csf Surface acoustic wave accelerometer
EP0017554A1 (en) * 1979-03-30 1980-10-15 Thomson-Csf Accelerometer using elastic waves

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2140161A (en) * 1983-05-20 1984-11-21 Thomson Csf Elastic surface wave force sensor
US4621530A (en) * 1983-07-14 1986-11-11 Standard Telephones And Cables Public Limited Company Surface acoustic wave accelerometer
US4598587A (en) * 1983-08-04 1986-07-08 Standard Telephones & Cables, Plc Surface acoustic wave accelerometer
FR2557695A1 (en) * 1984-01-03 1985-07-05 Thomson Csf Surface elastic wave force sensor
FR2561383A1 (en) * 1984-03-16 1985-09-20 Thomson Csf Vector force sensor based on elastic surface waves.
US4689992A (en) * 1984-04-04 1987-09-01 Syrinx Innovations Limited Rotation rate sensor
GB2219858A (en) * 1988-06-15 1989-12-20 Nat Res Dev Apparatus and method for detecting small changes in attached mass on piezoelectric devices used as sensors.
DE4135369A1 (en) * 1991-10-26 1993-05-13 Bosch Gmbh Robert Bipolar piezoelectric accelerometer with built-in test facility - has upper and lower electrodes in halves for application of test voltage and measurement of deformation
US5473930A (en) * 1991-10-26 1995-12-12 Robert Bosch Gmbh Acceleration sensor with oppositely-polarized piezoelectric plates
US6803698B2 (en) * 2000-10-12 2004-10-12 Murata Manufacturing Co., Ltd Acceleration sensor
US7380454B2 (en) * 2005-12-20 2008-06-03 Honeywell International Inc. Load beam for surface acoustic wave accelerometer
US7667369B2 (en) * 2006-11-01 2010-02-23 Delaware Capital Formation, Inc. High sensitivity microsensors based on flexure induced frequency effects
US7886575B2 (en) 2006-11-01 2011-02-15 Delaware Capital Formation, Inc. High sensitivity acoustic wave microsensors based on stress effects

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Publication number Publication date
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PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930323