CN108398575B - Electrostatic resonance accelerometer and acceleration measurement method - Google Patents

Electrostatic resonance accelerometer and acceleration measurement method Download PDF

Info

Publication number
CN108398575B
CN108398575B CN201810224198.XA CN201810224198A CN108398575B CN 108398575 B CN108398575 B CN 108398575B CN 201810224198 A CN201810224198 A CN 201810224198A CN 108398575 B CN108398575 B CN 108398575B
Authority
CN
China
Prior art keywords
resonator
mass block
electrostatic
resonators
mass
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.)
Active
Application number
CN201810224198.XA
Other languages
Chinese (zh)
Other versions
CN108398575A (en
Inventor
何高法
周明举
孟杰
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.)
Chongqing University of Science and Technology
Original Assignee
Chongqing University of Science and Technology
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 Chongqing University of Science and Technology filed Critical Chongqing University of Science and Technology
Priority to CN201810224198.XA priority Critical patent/CN108398575B/en
Publication of CN108398575A publication Critical patent/CN108398575A/en
Application granted granted Critical
Publication of CN108398575B publication Critical patent/CN108398575B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Pressure Sensors (AREA)

Abstract

The invention provides an electrostatic resonance type accelerometer, which comprises a mass block and at least one resonator, wherein an electrode is arranged on the resonator, the mass block is a conductor, and a certain direct current voltage is applied between the mass block and the resonator, so that the resonator is subjected to a certain electrostatic force and is in a resonance state at a certain frequency. The invention adopts the design of separating the resonator from the mass block, the acting force between the resonator and the mass block is non-contact long-range electrostatic force, the independent work of the resonator is ensured, and the quality factor and the sensitivity of the resonator are improved. In the invention, the electrostatic force inducing the acceleration variation acts on the transverse direction of the resonator beam (or tuning fork beam), the influence on the resonance frequency is large, and the sensitivity of the accelerometer is high. In the aspect of manufacturing process, the resonator and the mass block are manufactured separately, the structure is simple, and the manufacturing cost is low.

Description

Electrostatic resonance accelerometer and acceleration measurement method
Technical Field
The invention relates to the field of accelerometers, in particular to an accelerometer for detecting linear acceleration values in the fields of inertial navigation and the like.
Background
The inertial navigation system utilizes a gyroscope and an accelerometer to measure the angular velocity and the linear acceleration of the carrier motion at the same time, and calculates navigation information such as the three-dimensional attitude, the speed, the position and the like of the carrier in real time through a computer. The accelerometer is a core instrument of the inertial system, and the technical index directly influences the overall performance of the inertial navigation system, so that the accelerometer technology is an important mark of the inertial technology and is paid great attention to.
Accelerometers have a variety of operating principles including, in principle, from sensors: capacitance, electromagnetic, optical, piezoresistive, piezoelectric, resonant (frequency), etc. The resonant accelerometer can directly convert acceleration into frequency output, avoids error of amplitude measurement, is not easy to be interfered by environmental noise, and the quasi-digital output can simplify an interface circuit, is not easy to generate error in the transmission and processing processes, and the working principle of the resonant accelerometer establishes the advantages of the resonant accelerometer. However, the structure of the resonant accelerometer is generally designed such that inertial force acts on the axial direction of the resonator beam (or tuning fork beam), and detection and excitation are performed by using a comb-tooth structure. This design results in accelerometers that are not highly sensitive, and are very complex in structure and difficult to manufacture. In order to improve the sensitivity, part of the design adopts a micro-lever mechanism to amplify the inertia force, which leads to more complex structure, increased displacement of the mass block and insignificant amplification effect of the inertia force. In addition, the inertial force of the mass block of the accelerometer of the current design directly acts on the resonator, the mass block and the resonator are required to be integrally manufactured and mutually contacted, the mutual influence is achieved, and the quality factor of the resonator is reduced.
Disclosure of Invention
The invention aims to overcome the defects of the prior art and provides an electrostatic resonance accelerometer and an acceleration measuring method.
To achieve the above and other related objects, the present invention provides an electrostatic resonance type accelerometer, which comprises a mass block and at least one resonator, wherein electrodes are arranged on the resonator, the mass block is a conductor, and a certain direct current voltage is applied between the mass block and the resonator, so that the resonator is subjected to a certain electrostatic force and is in a resonance state at a certain frequency.
Preferably, the at least one resonator is a resonator, and is disposed on one side of the mass.
Preferably, the at least one resonator is two resonators, and the two resonators are respectively located at two sides of the mass block.
Preferably, the at least one resonator is two resonators, and the two resonators are located on the same side of the mass block.
Preferably, the at least one resonator is four resonators, each two resonators form a resonant unit, the two resonators are arranged side by side, and two resonant units are respectively arranged on two opposite sides of the mass block.
Preferably, the resonator is a quartz tuning fork resonator.
To achieve the above and other related objects, an acceleration measurement method specifically includes: a conductive mass block and at least one resonator with electrodes are arranged, and a direct current voltage is applied between the mass block and the resonator to enable the resonator to be subjected to a certain electrostatic force and to be in a resonance state at a certain frequency.
As described above, the electrostatic resonance type accelerometer has the following beneficial effects:
the invention adopts the design of separating the resonator from the mass block, the acting force between the resonator and the mass block is non-contact long-range electrostatic force, the independent work of the resonator is ensured, and the quality factor and the sensitivity of the resonator are improved. In the invention, the electrostatic force inducing the acceleration variation acts on the transverse direction of the resonator beam (or tuning fork beam), the influence on the resonance frequency is large, and the sensitivity of the accelerometer is high. In the aspect of manufacturing process, the resonator and the mass block are manufactured separately, the structure is simple, and the manufacturing cost is low.
Drawings
FIG. 1 is a schematic diagram of one embodiment of an electrostatic resonant accelerometer according to the present invention, wherein the direction of the arrow in the diagram is the vibration direction of the mass;
FIG. 2 is a schematic diagram of another embodiment of an electrostatic resonant accelerometer according to the present invention, wherein the direction of the arrow in the diagram is the vibration direction of the mass;
FIG. 3 is a schematic diagram of another embodiment of an electrostatic resonant accelerometer according to the invention;
fig. 4 is a schematic diagram of another embodiment of an electrostatic resonant accelerometer according to the invention.
Detailed Description
Other advantages and effects of the present invention will become apparent to those skilled in the art from the following disclosure, which describes the embodiments of the present invention with reference to specific examples. The invention may be practiced or carried out in other embodiments that depart from the specific details, and the details of the present description may be modified or varied from the spirit and scope of the present invention. It should be noted that the following embodiments and features in the embodiments may be combined with each other without conflict.
It should be noted that the illustrations provided in the following embodiments merely illustrate the basic concept of the present invention by way of illustration, and only the components related to the present invention are shown in the drawings and are not drawn according to the number, shape and size of the components in actual implementation, and the form, number and proportion of the components in actual implementation may be arbitrarily changed, and the layout of the components may be more complicated.
The invention provides an electrostatic resonance type accelerometer, which comprises a mass block 1 and at least one resonator, wherein electrodes 2 and 4 are arranged on the resonator, the mass block is a conductor, and a certain direct current voltage is applied between the mass block and the resonator, so that the resonator is subjected to a certain electrostatic force and is in a resonance state at a certain frequency.
In this embodiment, the resonator is a quartz tuning fork resonator.
The resonant frequency of a quartz tuning fork resonator will vary depending on the amount of force acting on the tuning fork. In this embodiment, a certain bias voltage (direct current) is applied between the tuning fork resonator and the mass while the tuning fork resonator is in a resonant state. When external acceleration acts on the mass block, the mass block supported by the flexible beam can generate certain displacement under the action of inertia force, the displacement can cause the distance between the tuning fork beam of the resonator and the mass block to change, so that the electrostatic force applied to the resonator changes, the resonant frequency of the resonator also changes, and the change of the resonant frequency is detected through the phase-locked loop circuit, so that the acceleration is detected. Then the change of the resonant frequency is detected by the phase-locked loop circuit, so that the acceleration is detected as in the prior art, and the detection will not be described too much.
The number and the positions of the resonators are not further limited, so long as the requirement that an electric field can be formed between the resonators and the mass block, namely the strip, is met.
For example, in this embodiment, as shown in fig. 2, one resonator, i.e., one side of the mass of the first resonator 3, may be provided.
In another embodiment, as shown in fig. 1, two resonators may be provided, one on each of opposite sides of the mass, namely a first resonator 3 and a second resonator.
In another embodiment, as shown in fig. 3, the at least one resonator is two resonators, and the two resonators are located on the same side of the mass.
In another embodiment, as shown in fig. 4, the at least one resonator is four resonators, each two resonators form a resonant unit, the two resonators are arranged side by side, and two opposite sides of the mass block are respectively provided with a resonant unit.
The invention adopts the design of separating the resonator from the mass block, the acting force between the resonator and the mass block is non-contact long-range electrostatic force, the independent work of the resonator is ensured, and the quality factor and the sensitivity of the resonator are improved. In the invention, the electrostatic force inducing the acceleration variation acts on the transverse direction of the resonator beam (or tuning fork beam), the influence on the resonance frequency is large, and the sensitivity of the accelerometer is high. In the aspect of manufacturing process, the resonator and the mass block are manufactured separately, the structure is simple, and the manufacturing cost is low.
In another embodiment of the present invention, there is also provided an acceleration measurement method, which specifically includes: a conductive mass block and at least one resonator with electrodes are arranged, and a direct current voltage is applied between the mass block and the resonator to enable the resonator to be subjected to a certain electrostatic force and to be in a resonance state at a certain frequency.
In this embodiment, the resonator is a quartz tuning fork resonator.
The resonant frequency of a quartz tuning fork resonator will vary depending on the amount of force acting on the tuning fork. In this embodiment, a certain bias voltage (direct current) is applied between the tuning fork resonator and the mass while the tuning fork resonator is in a resonant state. When external acceleration acts on the mass block, the mass block supported by the flexible beam can generate certain displacement under the action of inertia force, the displacement can cause the distance between the tuning fork beam of the resonator and the mass block to change, so that the electrostatic force applied to the resonator changes, the resonant frequency of the resonator also changes, and the change of the resonant frequency is detected through the phase-locked loop circuit, so that the acceleration is detected.
The above embodiments are merely illustrative of the principles of the present invention and its effectiveness, and are not intended to limit the invention. Modifications and variations may be made to the above-described embodiments by those skilled in the art without departing from the spirit and scope of the invention. Accordingly, it is intended that all equivalent modifications and variations of the invention be covered by the claims, which are within the ordinary skill of the art, be within the spirit and scope of the present disclosure.

Claims (6)

1. An electrostatic resonance type accelerometer is characterized by comprising a mass block and at least one resonator, wherein electrodes are arranged on the resonator, the mass block is a conductor, and a certain direct current voltage is applied between the mass block and the resonator, so that the resonator is subjected to a certain electrostatic force and is in a resonance state at a certain frequency;
the resonator is a quartz tuning fork resonator, a certain bias direct current is applied between the tuning fork resonator and the mass block, and the tuning fork resonator is in a resonance state.
2. An electrostatic resonator accelerometer according to claim 1, wherein the at least one resonator is a resonator disposed on one side of the mass.
3. An electrostatic resonator accelerometer according to claim 1, wherein the at least one resonator is two resonators, the two resonators being located on opposite sides of the mass.
4. An electrostatic resonator accelerometer according to claim 1, wherein the at least one resonator is two resonators, the two resonators being located on the same side of the mass.
5. An electrostatic resonator type accelerometer according to claim 1, wherein the at least one resonator is four resonators, each two resonators forming a resonant unit, the two resonators being arranged side by side, one resonant unit being arranged on each of opposite sides of the mass.
6. An acceleration measuring method is characterized in that the method specifically comprises the following steps: a conductive mass block and at least one resonator with electrodes are arranged, and a direct current voltage is applied between the mass block and the resonator to enable the resonator to be subjected to a certain electrostatic force and to be in a resonance state at a certain frequency.
CN201810224198.XA 2018-03-19 2018-03-19 Electrostatic resonance accelerometer and acceleration measurement method Active CN108398575B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810224198.XA CN108398575B (en) 2018-03-19 2018-03-19 Electrostatic resonance accelerometer and acceleration measurement method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810224198.XA CN108398575B (en) 2018-03-19 2018-03-19 Electrostatic resonance accelerometer and acceleration measurement method

Publications (2)

Publication Number Publication Date
CN108398575A CN108398575A (en) 2018-08-14
CN108398575B true CN108398575B (en) 2024-02-27

Family

ID=63092925

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810224198.XA Active CN108398575B (en) 2018-03-19 2018-03-19 Electrostatic resonance accelerometer and acceleration measurement method

Country Status (1)

Country Link
CN (1) CN108398575B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109614661B (en) * 2018-11-19 2023-04-07 北京联合大学 Resonant accelerometer force-frequency relation equation establishing method
CN113702663B (en) * 2021-08-31 2023-02-21 中国科学院空天信息创新研究院 MEMS resonant acceleration sensor

Citations (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69000479D1 (en) * 1989-08-08 1992-12-24 Onera (Off Nat Aerospatiale) ACCELEROMETER WITH BENDING ROCKER AS A CARRIER.
JP2003294786A (en) * 2002-03-29 2003-10-15 National Institute Of Advanced Industrial & Technology Method and device for measuring frequency characteristic for acceleration sensor
CN101089624A (en) * 2007-07-12 2007-12-19 中北大学 Electric tuning resonance differential frequency accelerator
CN101266259A (en) * 2008-05-08 2008-09-17 南京理工大学 Silicon micro-resonance type accelerometer
CN101303365A (en) * 2008-06-23 2008-11-12 中北大学 Resonance type micro accelerometer
CN102778583A (en) * 2012-07-12 2012-11-14 西安交通大学 Silicon substrate-based quartz resonance acceleration sensor chip with four-beam structure
CN103063875A (en) * 2012-12-25 2013-04-24 西安交通大学 Silicon substrate differential motion quartz acceleration sensor
CN103501166A (en) * 2013-10-15 2014-01-08 中国电子科技集团公司第二十六研究所 Quartz resonant element
CN103808961A (en) * 2012-11-08 2014-05-21 中国科学院电子学研究所 Cantilever part and resonant acceleration sensor using the same
CN106352862A (en) * 2016-10-26 2017-01-25 西安交通大学 Digital differential micro-accelerometer
CN106597011A (en) * 2016-12-23 2017-04-26 中北大学 Double-shaft MEMS resonant acceleration transducer structure
CN106629571A (en) * 2016-09-20 2017-05-10 西北工业大学 Weakly coupled MEMS resonance type accelerometer based on mode localization effect
CN106771358A (en) * 2016-11-30 2017-05-31 西安交通大学 A kind of full quartz resonance accelerometer of miniature differential formula
CN107643423A (en) * 2017-10-26 2018-01-30 西北工业大学 A kind of Three Degree Of Freedom weak coupling resonance type accelerometer based on mode localization effect
CN207882297U (en) * 2018-03-19 2018-09-18 重庆科技学院 A kind of electrostatic resonance type accelerometer

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6782748B2 (en) * 2002-11-12 2004-08-31 Honeywell International, Inc. High-G acceleration protection by caging
IT1395419B1 (en) * 2009-09-07 2012-09-14 Milano Politecnico ACCONEROMETER RESONATING MEMS WITH IMPROVED ELECTRIC CHARACTERISTICS

Patent Citations (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69000479D1 (en) * 1989-08-08 1992-12-24 Onera (Off Nat Aerospatiale) ACCELEROMETER WITH BENDING ROCKER AS A CARRIER.
JP2003294786A (en) * 2002-03-29 2003-10-15 National Institute Of Advanced Industrial & Technology Method and device for measuring frequency characteristic for acceleration sensor
CN101089624A (en) * 2007-07-12 2007-12-19 中北大学 Electric tuning resonance differential frequency accelerator
CN101266259A (en) * 2008-05-08 2008-09-17 南京理工大学 Silicon micro-resonance type accelerometer
CN101303365A (en) * 2008-06-23 2008-11-12 中北大学 Resonance type micro accelerometer
CN102778583A (en) * 2012-07-12 2012-11-14 西安交通大学 Silicon substrate-based quartz resonance acceleration sensor chip with four-beam structure
CN103808961A (en) * 2012-11-08 2014-05-21 中国科学院电子学研究所 Cantilever part and resonant acceleration sensor using the same
CN103063875A (en) * 2012-12-25 2013-04-24 西安交通大学 Silicon substrate differential motion quartz acceleration sensor
CN103501166A (en) * 2013-10-15 2014-01-08 中国电子科技集团公司第二十六研究所 Quartz resonant element
CN106629571A (en) * 2016-09-20 2017-05-10 西北工业大学 Weakly coupled MEMS resonance type accelerometer based on mode localization effect
CN106352862A (en) * 2016-10-26 2017-01-25 西安交通大学 Digital differential micro-accelerometer
CN106771358A (en) * 2016-11-30 2017-05-31 西安交通大学 A kind of full quartz resonance accelerometer of miniature differential formula
CN106597011A (en) * 2016-12-23 2017-04-26 中北大学 Double-shaft MEMS resonant acceleration transducer structure
CN107643423A (en) * 2017-10-26 2018-01-30 西北工业大学 A kind of Three Degree Of Freedom weak coupling resonance type accelerometer based on mode localization effect
CN207882297U (en) * 2018-03-19 2018-09-18 重庆科技学院 A kind of electrostatic resonance type accelerometer

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
静电刚度谐振式微加速度计相关技术研究;刘恒;《中国博士电子期刊信息科技辑》;20111215;全文 *

Also Published As

Publication number Publication date
CN108398575A (en) 2018-08-14

Similar Documents

Publication Publication Date Title
CN107643423B (en) Three-degree-of-freedom weak coupling resonant accelerometer based on modal localization effect
CA2883200C (en) Dual and triple axis inertial sensors and methods of inertial sensing
EP2577324B1 (en) Mems inertial sensor and method of inertial sensing
US9097736B2 (en) Micromechanical component and method for manufacturing a micromechanical component
WO2013179647A2 (en) Physical amount sensor
TW201346263A (en) Apparatus and method for providing an in-plane inertial device with integrated clock
CN108398575B (en) Electrostatic resonance accelerometer and acceleration measurement method
US20110259101A1 (en) Vibration-type force detection sensor and vibration-type force detection device
JP2015072277A (en) Mems gyroscope with lowered magnetism sensitivity
CN111521842A (en) Electrostatic rigidity adjustment Z-axis resonant micro-accelerometer based on tunnel magnetic resistance detection
CN105324634B (en) Rotational speed sensor for detecting rotational speeds, having a substrate with a main extension plane
CN101339025B (en) All solid dual spindle gyroscopes possessing square surface cuboid piezoelectric vibrator
CN111071982B (en) Micromechanical inertial sensor
CN207882297U (en) A kind of electrostatic resonance type accelerometer
US6895819B1 (en) Acceleration sensor
CN207395750U (en) Microthrust test device is detected in electromagnetic drive type tunnel magnetoresistive face
CN101339028B (en) All solid dual spindle gyroscopes possessing double nested square shape groove structure piezoelectric vibrator
CN212159843U (en) Electrostatic rigidity adjustment Z-axis resonant micro-accelerometer based on tunnel magnetic resistance detection
CN101339026B (en) All solid dual spindle gyroscopes possessing square through-hole piezoelectric vibrator
CN101339030B (en) Dual spindle piezoelectric detection gyroscope possessing magnetostriction vibrator
CN101339029B (en) Magnetic striction piezoelectric gyroscope possessing double nested square shape column vibrator
CN101339027B (en) All solid dual spindle magnetostriction piezoelectric gyroscope possessing cuboid vibrator
CN103697876A (en) Electrostatic drive bulk acoustic wave solid fluctuating micro gyroscope based on silicon plane processing craft
CN221405744U (en) Resonant accelerometer
CN212158620U (en) Decoupling type full-symmetrical micro gyroscope for in-plane detection of grating

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant