CA2413447A1 - A mechano-electrical sensor for sensing force or vibration - Google Patents
A mechano-electrical sensor for sensing force or vibration Download PDFInfo
- Publication number
- CA2413447A1 CA2413447A1 CA002413447A CA2413447A CA2413447A1 CA 2413447 A1 CA2413447 A1 CA 2413447A1 CA 002413447 A CA002413447 A CA 002413447A CA 2413447 A CA2413447 A CA 2413447A CA 2413447 A1 CA2413447 A1 CA 2413447A1
- Authority
- CA
- Canada
- Prior art keywords
- sensor
- framework
- inner body
- dimensional
- vibration
- 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.)
- Abandoned
Links
- 239000000725 suspension Substances 0.000 claims abstract description 11
- 239000013013 elastic material Substances 0.000 claims abstract description 6
- 239000011888 foil Substances 0.000 claims description 31
- 239000000463 material Substances 0.000 claims description 8
- 229920001971 elastomer Polymers 0.000 claims description 3
- 239000012528 membrane Substances 0.000 claims 1
- 230000001133 acceleration Effects 0.000 description 4
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 230000010355 oscillation Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 230000003534 oscillatory effect Effects 0.000 description 2
- 229910052729 chemical element Inorganic materials 0.000 description 1
- 230000000875 corresponding effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 229920002379 silicone rubber Polymers 0.000 description 1
- 239000004945 silicone rubber Substances 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
- G01H11/00—Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by detecting changes in electric or magnetic properties
- G01H11/06—Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by detecting changes in electric or magnetic properties by electric means
- G01H11/08—Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by detecting changes in electric or magnetic properties by electric means using piezoelectric devices
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/004—Mounting transducers, e.g. provided with mechanical moving or orienting device
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/18—Methods or devices for transmitting, conducting or directing sound
- G10K11/24—Methods or devices for transmitting, conducting or directing sound for conducting sound through solid bodies, e.g. wires
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Acoustics & Sound (AREA)
- Multimedia (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
- Force Measurement Appropriate To Specific Purposes (AREA)
- Piezo-Electric Transducers For Audible Bands (AREA)
Abstract
A mechano-electrical sensor for sensing force or vibration comprises an inner body (1) supported by a piezoelectric support structure (3) that in its turn is suspended in a surrounding framework (2), and signal leads from oppositely polarizable sides of the support structure (3). Alternatively, the surrounding framework (2) may be provided with piezoelectric areas situated at the suspension positions on the framework (2) for the support structure. The framework (2) may be further suspended in an outer frame (5) by means of an elastic material (4).
Description
Mechano-electrical Sensor The present invention relates to sensing of force or vibration, delivering electrical signals representative of the sensed force or a parameter of a vibration s state. More particularly, the invention relates to a mechano-electrical sensor for sensing force or vibration and delivering at least one electrical signal that is a function of the sensed force or vibration.
Force sensors, acceleration sensors and vibration sensors have many uses, and exist in many embodiments. Usually, two or three separate sensors are to utilized e.g. to sense acceleration in three orthogonal directions, by allowing mas-sive bodies, suspended in spring systems, to move relative to respective reference frames. Rotation is usually sensed with a gyroscope device.
The present invention aims at providing a sensor that, better than previously known solutions, is able to operate with a directional effect and provide good mea-~s surements regarding translation as well as rotation, by means of one movable body only.
Therefore, in accordance with the invention there is provided a mechano-electrical sensor such as precisely defined in the appended claim 1.
Advantageous embodiments of the invention appear from the attached dependent claims.
zo In the following, the invention shall be illuminated further by describing exemplary embodiments of the invention, and in this connection it is also referred to the appended drawings, wherein Fig. 1 shows a two-dimensional embodiment of the sensor in accordance with the invention;
Zs Fig. 2 shows the same embodiment as Fig. 1, however suspended in an outer frame;
Fig. 3 shows another two-dimensional embodiment of the sensor in accor-dance with the invention;
Fig. 4 shows the same embodiment as Fig. 3, however suspended in an so outer frame;
Fig. 5 shows a three-dimensional embodiment of the sensor in accordance with the invention, with foil-shaped support structures, in a partially cut-away view;
and Fig. 6 shows another three-dimensional embodiment with filament-shaped support structures, this drawing also in a partially cut-away view.
In Fig. 1 appears a relatively simple, two-dimensional embodiment of the sensor of the invention. An inner body 1 is supported by means of piezoelectric foils 3 in a framework 2, and non-appearing signal wires connected e.g. to respec-tive sides of a foil 3, are able to deliver electrical signals generated when the foils are subject to deformation due to shift of the inner body 1 relative to a relaxed centre position. The figure shows three foils tautened in a hexagonal opening, however one single foil may be used, or a larger number of foils. The choice of inner body will depend on the use field of the sensor. The inner body may, in uses including recording from soft surfaces, consist of e.g. plastic or silicone rubber with various shore values. In other applications, for example industrial diamond mate-rial may be used. Combinations of material and geometrical shape of the inner body is important. The inner body may also exhibit openings to provide a possibi-~s lity for air passage therethrough, for example in microphone applications.
The foils may possibly be attached between two metallic frame parts that are insulated from each other and possibly from other frame parts along the periphery, so that signals can be collected from the metallic frame parts. When foils 3 are used such as indi-Gated in the figure, the stretch directions of the foils may be e.g. along the longitu-ao dinal direction for each foil strip, and this provides an opportunity to collect a hig-her, summed total signal compared to the case of only one single foil, either as a strip across the opening, or as a complete "diaphragm" covering the whole opening.
Centering of the inner body 1 is not necessary, one may visualize embodi-as ments with an inner body arranged in an eccentric position. Nor is the shape of framework 2 crucial, as long as the frame is rigid and suitable for attaching the piezoelectric foils.
Such a two-dimensional sensor will clearly be most sensitive with regard to force or vibratory influence in a direction perpendicular to the plane spanned by so the sensor, but it will also be possible (when using several foils with separate sig-nal wires) to sense a force in the support plane, i.e. lateral movement of the inner body.
In Fig. 2 appears the same embodiment as in Fig. 1, however the whole basic sensor is suspended in an outside framework 5. The suspension is by means of elastic elements 4, e.g. rubber elements, and such an embodiment of the invention will be particularly favourable e.g. when using the sensor as a sensor s element in a microphone. The main purpose of the outside framework 5 is noise attenuation, i.e. attenuation of noise in the form of vibrations that may bring the piezo elements of the sensor into oscillation. When the sensor is attached to an outer frame 5, there will be two oscillatory systems, of which the inner system is the sensor itself. The design must then be so as to give the outer system a reson-ant frequency that is low relative to the resonant frequency of the system compris-ing inner frame/piezoelectric suspension structure/inner body. One will then achi-eve the effect that the frame works as a low pass filter. This relates primarily to the two-dimensional solution.
Further, it will be of great importance whether it is the framework 2 or the ~s inner body 1 that is supposed to oscillate in relation to the surroundings.
Ideally, it is desirable to maintain the framework 2 at rest in relation to the surroundings, while the inner body oscillates relative to the framework. In practice, the suspen-sion of the sensor frame will normally provide "good" acoustic coupling between the surroundings and the sensor elements, and normally this is not desirable.
Gen-ao erally, the mass of the inner body will influence the characteristic (the frequency response) most strongly, but design and material choice will also be of importance regarding the coupling between the "sensed medium" and the sensor. Due to the coupled oscillatory systems, the characteristic must be optimized as a function of mass ratios, stiffnesses etc.
as In an application in a microphone that is supposed to be good at high fre-quencies, the oscillations in the air will bring the suspension diaphragms (see Fig. 4) into oscillation, and the framework 2 will then oscillate around the inner body 1. In such a case, the vibrating part of the sensor must be as light as possible.
3o In Fig. 3 appears an alternative embodiment of the sensor in accordance with the invention, still in a two-dimensional version. Here appears an inner body 1 suspended in a number of sector-shaped piezoelectric foils 3, and preferably the stretch direction for every foil sector is arranged in the same manner in relation to the radius in the respective position, e.g. pointing substantially in a radial direction.
There are small openings between foils in this case, which for example in connec-tion with use in a microphone, may be favourable regarding air passage through the openings. Moreover, connection of signal leads is made in a similar manner as mentioned regarding Fig. 1, and it appears that it may be possible to achieve high s sum voltages with appropriate coupling of signal leads from each respective foil sector, if this is desirable. Alternatively, of course separate signals can be collec-ted from each respective sector.
Fig. 4 shows suspension in an outer frame 5 in the same manner as in Fig. 2, however in this case the suspension structures are elastic, sector-shaped diaphragms made of e.g. rubber.
In Fig. 5 appears an embodiment of a three-dimensional type. The inner body 1 is held suspended at the centre of a spherical frame 2, by means of piezo-electric foil pieces 3 arranged in such a manner that a relative shifting of the inner body 1, or a rotation for that matter, will be detectable by means of voltages cre-~s ated in the foils 3, and that can be collected by means of (not shown) signal wires connected to the two sides of the foil pieces projecting out through the frame. Of course, framework 2 does not have to be spherical, nor does it need to be closed, but it is important that it is rigid, in order to constitute a reference for the position of the inner body.
ao Fig. 6 shows a similar design, but the piezoelectric foils have been replaced by filaments, and the filaments are either of a piezoelectric type with correspond-ing function as the foil pieces in Fig. 5, or the filaments are taut and substantially inelastic, but attached to piezoelectric areas (not shown) of the framework, so that these areas generate voltages depending on the translation or rotation of the inner as body relative to framework 2.
Such a three-dimensional force/vibration sensor as shown in Fig. 5 and Fig. 6, is based upon a rigid coupling between the framework and the body for which force or possibly acceleration shall be measured, and thereby the inertia of the inner body will create the measurable voltages in the suspension structures 3 30 or in their attachment areas. Hence, with signal leads coupled to suitable process-ing equipment, such an acceleration/vibration sensor may constitute a main ele-ment in e.g. an inertia navigation system.
Also the three-dimensional embodiments shown in Figs. 5 and 6 can be suspended in an outer framework via an elastic material in two or three dimen-sions.
The foil pieces shown in the embodiment of Fig. 5 may come in other sha-s pes, for example more sector-like or possibly as approximations to full circle areas, and the planes to be spanned, do not necessarily have to be orthogonal like in the figure.
Besides, foil materials or filament materials are not the only possible materi-als in this application, the suspension structures between inner body and frame-work may possibly be piezoelectric bimorph elements or similar elements.
The invention is also intended to accommodate the variant that has already been mentioned, namely the variant with suspension structures that are not piezo-electric, but attached to piezoelectric areas of the framework.
Force sensors, acceleration sensors and vibration sensors have many uses, and exist in many embodiments. Usually, two or three separate sensors are to utilized e.g. to sense acceleration in three orthogonal directions, by allowing mas-sive bodies, suspended in spring systems, to move relative to respective reference frames. Rotation is usually sensed with a gyroscope device.
The present invention aims at providing a sensor that, better than previously known solutions, is able to operate with a directional effect and provide good mea-~s surements regarding translation as well as rotation, by means of one movable body only.
Therefore, in accordance with the invention there is provided a mechano-electrical sensor such as precisely defined in the appended claim 1.
Advantageous embodiments of the invention appear from the attached dependent claims.
zo In the following, the invention shall be illuminated further by describing exemplary embodiments of the invention, and in this connection it is also referred to the appended drawings, wherein Fig. 1 shows a two-dimensional embodiment of the sensor in accordance with the invention;
Zs Fig. 2 shows the same embodiment as Fig. 1, however suspended in an outer frame;
Fig. 3 shows another two-dimensional embodiment of the sensor in accor-dance with the invention;
Fig. 4 shows the same embodiment as Fig. 3, however suspended in an so outer frame;
Fig. 5 shows a three-dimensional embodiment of the sensor in accordance with the invention, with foil-shaped support structures, in a partially cut-away view;
and Fig. 6 shows another three-dimensional embodiment with filament-shaped support structures, this drawing also in a partially cut-away view.
In Fig. 1 appears a relatively simple, two-dimensional embodiment of the sensor of the invention. An inner body 1 is supported by means of piezoelectric foils 3 in a framework 2, and non-appearing signal wires connected e.g. to respec-tive sides of a foil 3, are able to deliver electrical signals generated when the foils are subject to deformation due to shift of the inner body 1 relative to a relaxed centre position. The figure shows three foils tautened in a hexagonal opening, however one single foil may be used, or a larger number of foils. The choice of inner body will depend on the use field of the sensor. The inner body may, in uses including recording from soft surfaces, consist of e.g. plastic or silicone rubber with various shore values. In other applications, for example industrial diamond mate-rial may be used. Combinations of material and geometrical shape of the inner body is important. The inner body may also exhibit openings to provide a possibi-~s lity for air passage therethrough, for example in microphone applications.
The foils may possibly be attached between two metallic frame parts that are insulated from each other and possibly from other frame parts along the periphery, so that signals can be collected from the metallic frame parts. When foils 3 are used such as indi-Gated in the figure, the stretch directions of the foils may be e.g. along the longitu-ao dinal direction for each foil strip, and this provides an opportunity to collect a hig-her, summed total signal compared to the case of only one single foil, either as a strip across the opening, or as a complete "diaphragm" covering the whole opening.
Centering of the inner body 1 is not necessary, one may visualize embodi-as ments with an inner body arranged in an eccentric position. Nor is the shape of framework 2 crucial, as long as the frame is rigid and suitable for attaching the piezoelectric foils.
Such a two-dimensional sensor will clearly be most sensitive with regard to force or vibratory influence in a direction perpendicular to the plane spanned by so the sensor, but it will also be possible (when using several foils with separate sig-nal wires) to sense a force in the support plane, i.e. lateral movement of the inner body.
In Fig. 2 appears the same embodiment as in Fig. 1, however the whole basic sensor is suspended in an outside framework 5. The suspension is by means of elastic elements 4, e.g. rubber elements, and such an embodiment of the invention will be particularly favourable e.g. when using the sensor as a sensor s element in a microphone. The main purpose of the outside framework 5 is noise attenuation, i.e. attenuation of noise in the form of vibrations that may bring the piezo elements of the sensor into oscillation. When the sensor is attached to an outer frame 5, there will be two oscillatory systems, of which the inner system is the sensor itself. The design must then be so as to give the outer system a reson-ant frequency that is low relative to the resonant frequency of the system compris-ing inner frame/piezoelectric suspension structure/inner body. One will then achi-eve the effect that the frame works as a low pass filter. This relates primarily to the two-dimensional solution.
Further, it will be of great importance whether it is the framework 2 or the ~s inner body 1 that is supposed to oscillate in relation to the surroundings.
Ideally, it is desirable to maintain the framework 2 at rest in relation to the surroundings, while the inner body oscillates relative to the framework. In practice, the suspen-sion of the sensor frame will normally provide "good" acoustic coupling between the surroundings and the sensor elements, and normally this is not desirable.
Gen-ao erally, the mass of the inner body will influence the characteristic (the frequency response) most strongly, but design and material choice will also be of importance regarding the coupling between the "sensed medium" and the sensor. Due to the coupled oscillatory systems, the characteristic must be optimized as a function of mass ratios, stiffnesses etc.
as In an application in a microphone that is supposed to be good at high fre-quencies, the oscillations in the air will bring the suspension diaphragms (see Fig. 4) into oscillation, and the framework 2 will then oscillate around the inner body 1. In such a case, the vibrating part of the sensor must be as light as possible.
3o In Fig. 3 appears an alternative embodiment of the sensor in accordance with the invention, still in a two-dimensional version. Here appears an inner body 1 suspended in a number of sector-shaped piezoelectric foils 3, and preferably the stretch direction for every foil sector is arranged in the same manner in relation to the radius in the respective position, e.g. pointing substantially in a radial direction.
There are small openings between foils in this case, which for example in connec-tion with use in a microphone, may be favourable regarding air passage through the openings. Moreover, connection of signal leads is made in a similar manner as mentioned regarding Fig. 1, and it appears that it may be possible to achieve high s sum voltages with appropriate coupling of signal leads from each respective foil sector, if this is desirable. Alternatively, of course separate signals can be collec-ted from each respective sector.
Fig. 4 shows suspension in an outer frame 5 in the same manner as in Fig. 2, however in this case the suspension structures are elastic, sector-shaped diaphragms made of e.g. rubber.
In Fig. 5 appears an embodiment of a three-dimensional type. The inner body 1 is held suspended at the centre of a spherical frame 2, by means of piezo-electric foil pieces 3 arranged in such a manner that a relative shifting of the inner body 1, or a rotation for that matter, will be detectable by means of voltages cre-~s ated in the foils 3, and that can be collected by means of (not shown) signal wires connected to the two sides of the foil pieces projecting out through the frame. Of course, framework 2 does not have to be spherical, nor does it need to be closed, but it is important that it is rigid, in order to constitute a reference for the position of the inner body.
ao Fig. 6 shows a similar design, but the piezoelectric foils have been replaced by filaments, and the filaments are either of a piezoelectric type with correspond-ing function as the foil pieces in Fig. 5, or the filaments are taut and substantially inelastic, but attached to piezoelectric areas (not shown) of the framework, so that these areas generate voltages depending on the translation or rotation of the inner as body relative to framework 2.
Such a three-dimensional force/vibration sensor as shown in Fig. 5 and Fig. 6, is based upon a rigid coupling between the framework and the body for which force or possibly acceleration shall be measured, and thereby the inertia of the inner body will create the measurable voltages in the suspension structures 3 30 or in their attachment areas. Hence, with signal leads coupled to suitable process-ing equipment, such an acceleration/vibration sensor may constitute a main ele-ment in e.g. an inertia navigation system.
Also the three-dimensional embodiments shown in Figs. 5 and 6 can be suspended in an outer framework via an elastic material in two or three dimen-sions.
The foil pieces shown in the embodiment of Fig. 5 may come in other sha-s pes, for example more sector-like or possibly as approximations to full circle areas, and the planes to be spanned, do not necessarily have to be orthogonal like in the figure.
Besides, foil materials or filament materials are not the only possible materi-als in this application, the suspension structures between inner body and frame-work may possibly be piezoelectric bimorph elements or similar elements.
The invention is also intended to accommodate the variant that has already been mentioned, namely the variant with suspension structures that are not piezo-electric, but attached to piezoelectric areas of the framework.
Claims (15)
1. Mechano-electrical sensor for sensing force or vibration and delivering at least one electrical signal that is a function of sensed force or vibration, said sensor comprising one single inner body (1) supported by piezoelectric support structures (3) that are in their turn suspended in a surrounding framework (2), and signal leads from oppositely polarizable sides of said support structures (3), characterized in that said support structures are constituted by a num-ber of separate foils (3) in sector-shape, attached peripherally to the framework (2) and centrally to said inner body (1).
2. The sensor of claim 1, characterized in that each separate foil (3) is arranged with its stretch direction in one and the same relation to a respective radial direction, and that the signal leads are connected to add the respective output signals from each separate foil (3).
3. The sensor of claim 1, characterized in that the inner body (1) is arranged eccentrically.
4. The sensor of claim 1, characterized in that the framework (2) is two-dimensional, i.e. lies substantially in a plane.
5. The sensor of claim 1, characterized in that the framework (2) is three-dimensional, and in that the foil (3) planes span a three-dimensional space.
6. The sensor of claim 5, characterized in that the number of foil (3) planes is three, said planes being orthogonal.
7. The sensor of claim 5, characterized in that each foil plane comprises a number of foils (3) with gaps therebetween outside the inner body (1).
8. The sensor of claim 1, characterized in that the framework (2) is further suspended in an outer frame (5) by means of an elastic material (4).
9. The sensor of claim 8, characterized in that the elastic material is a membrane material.
10. Mechano-electrical sensor for sensing force or vibration and delivering at least one electrical signal that is a function of sensed force or vibration, characterized in that the sensor comprises at least one inner body (1) supported in at least one support structure (3) which in its turn is suspended in a surrounding framework (2) having respective piezoelectric areas at least closely surrounding or situated close by respective suspension positions on the framework (2) for the at least one support structure (3), and signal leads from oppositely polarizable sides of every area.
11. The sensor of claim 10, characterized in that said at least one support structure is constituted by a number of taut and substantially inelastic filaments (3), each attached to said at feast one inner body (1) and to attachment points on the framework (2), and that the piezoelectric areas are arranged as separate areas centered around every attachment point.
12. The sensor of claim 11, characterized in that the framework (2) is two-dimensional, whereby the filaments (3) run substantially like spokes in a wheel between the inner body (1) and the framework (2), possibly with different filament lengths for an eccentric inner body position.
13. The sensor of claim 11, characterized in that the framework (2) is three-dimensional.
14. The sensor of claim 10, characterized in that the framework (2) is further suspended in an outer frame (5) by means of an elastic material (4).
15. The sensor of claim 14, characterized in that the elastic material is a three-dimensional material having rubber characteristics.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NO20003311A NO312792B1 (en) | 2000-06-23 | 2000-06-23 | Mechanoelectric sensor |
| NO20003311 | 2000-06-23 | ||
| PCT/NO2001/000252 WO2002001167A1 (en) | 2000-06-23 | 2001-06-15 | A mechano-electrical sensor for sensing force or vibration |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2413447A1 true CA2413447A1 (en) | 2002-01-03 |
Family
ID=19911307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002413447A Abandoned CA2413447A1 (en) | 2000-06-23 | 2001-06-15 | A mechano-electrical sensor for sensing force or vibration |
Country Status (11)
| Country | Link |
|---|---|
| EP (1) | EP1311811A1 (en) |
| JP (1) | JP2004502158A (en) |
| KR (1) | KR20030071618A (en) |
| CN (1) | CN1302267C (en) |
| AU (1) | AU2001274687A1 (en) |
| BR (1) | BR0112277A (en) |
| CA (1) | CA2413447A1 (en) |
| EA (1) | EA200300054A1 (en) |
| NO (1) | NO312792B1 (en) |
| PL (1) | PL360483A1 (en) |
| WO (1) | WO2002001167A1 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104181330B (en) * | 2013-05-24 | 2018-03-20 | 北京嘉岳同乐极电子有限公司 | Acceleration transducer |
| CN110445415B (en) * | 2019-08-06 | 2020-07-17 | 合肥工业大学 | Rotary piezoelectric driver |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2880333A (en) * | 1954-11-17 | 1959-03-31 | Gulton Ind Inc | Accelerometer |
| US4051395A (en) * | 1975-08-08 | 1977-09-27 | Minnesota Mining And Manufacturing | Weight actuated piezoelectric polymeric transducer |
| US4051351A (en) | 1976-11-10 | 1977-09-27 | Westinghouse Electric Corporation | Electronic system for monitoring pneumatic tool performance |
| GB2055018B (en) | 1979-07-11 | 1983-11-16 | Kureha Chemical Ind Co Ltd | Vibration detector |
| FR2540325A1 (en) * | 1983-01-28 | 1984-08-03 | Thomson Csf | SPEED HYDROPHONE |
| GB8519026D0 (en) * | 1985-07-27 | 1985-09-04 | Laing J | Piezo electrical inertia sensitive device |
| US4727279A (en) * | 1987-04-29 | 1988-02-23 | General Motors Corporation | Piezoelectric knock sensor |
| FR2615682B1 (en) * | 1987-05-19 | 1989-07-13 | Thomson Csf | GEOPHONE COMPRISING A SENSITIVE ELEMENT IN PIEZOELECTRIC POLYMER |
| CN2257019Y (en) * | 1995-09-08 | 1997-06-25 | 陕西青华机电研究所 | Differential vibrating cord accelerometer |
-
2000
- 2000-06-23 NO NO20003311A patent/NO312792B1/en not_active IP Right Cessation
-
2001
- 2001-06-15 JP JP2002506054A patent/JP2004502158A/en active Pending
- 2001-06-15 CN CNB01811623XA patent/CN1302267C/en not_active Expired - Fee Related
- 2001-06-15 AU AU2001274687A patent/AU2001274687A1/en not_active Abandoned
- 2001-06-15 PL PL36048301A patent/PL360483A1/en unknown
- 2001-06-15 EP EP01941327A patent/EP1311811A1/en not_active Withdrawn
- 2001-06-15 CA CA002413447A patent/CA2413447A1/en not_active Abandoned
- 2001-06-15 EA EA200300054A patent/EA200300054A1/en unknown
- 2001-06-15 KR KR1020027017589A patent/KR20030071618A/en not_active Application Discontinuation
- 2001-06-15 WO PCT/NO2001/000252 patent/WO2002001167A1/en active Application Filing
- 2001-06-15 BR BR0112277-0A patent/BR0112277A/en not_active Application Discontinuation
Also Published As
| Publication number | Publication date |
|---|---|
| BR0112277A (en) | 2003-12-30 |
| PL360483A1 (en) | 2004-09-06 |
| CN1302267C (en) | 2007-02-28 |
| KR20030071618A (en) | 2003-09-06 |
| EP1311811A1 (en) | 2003-05-21 |
| NO312792B1 (en) | 2002-07-01 |
| NO20003311D0 (en) | 2000-06-23 |
| WO2002001167A1 (en) | 2002-01-03 |
| EA200300054A1 (en) | 2003-06-26 |
| AU2001274687A1 (en) | 2002-01-08 |
| NO20003311L (en) | 2001-12-24 |
| JP2004502158A (en) | 2004-01-22 |
| CN1437701A (en) | 2003-08-20 |
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| Date | Code | Title | Description |
|---|---|---|---|
| FZDE | Discontinued |