CN107101629A - A kind of silicon micro mechanical graphene beam resonant mode gyroscope - Google Patents

A kind of silicon micro mechanical graphene beam resonant mode gyroscope Download PDF

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Publication number
CN107101629A
CN107101629A CN201710324290.9A CN201710324290A CN107101629A CN 107101629 A CN107101629 A CN 107101629A CN 201710324290 A CN201710324290 A CN 201710324290A CN 107101629 A CN107101629 A CN 107101629A
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graphene
resonance beam
graphene resonance
resonance
gyro
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CN107101629B (en
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樊尚春
卢阳
邢维巍
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Beihang University
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Beihang University
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/56Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
    • G01C19/5607Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using vibrating tuning forks
    • G01C19/5621Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using vibrating tuning forks the devices involving a micromechanical structure
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/56Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
    • G01C19/5642Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using vibrating bars or beams
    • G01C19/5656Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using vibrating bars or beams the devices involving a micromechanical structure
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/56Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
    • G01C19/5705Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using masses driven in reciprocating rotary motion about an axis
    • G01C19/5712Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using masses driven in reciprocating rotary motion about an axis the devices involving a micromechanical structure

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Gyroscopes (AREA)

Abstract

The invention discloses a kind of silicon micro mechanical graphene beam resonant mode gyroscope, including glass substrate, transfer beams, lever transmission part, fixed mass block driving comb, gyro mass, the first graphene resonance beam, the second graphene resonance beam and frame.Using graphene resonance beam as secondary sensitive structure, the change for indirect sensitization axial stress in transfer beams.Resonance sensitive structure is used as using graphene resonance beam, graphene resonance beam in axisymmetric position is during the axial coriolis force change of impression, one is in axial tension state, another is in the state that is compressed axially (in resonant frequency range), and two graphene resonance beams are identical to sensitive capabilities such as temperature fields.By two symmetrical graphene resonance beams and the characteristics of can the giving full play of graphene resonance beam small volume, flexible structure, big fracture strength and high mechanical quality factor of combining closely of silicon micromechanical gyroscope, variate, high sensitivity and the high measurement accuracy of silicon micro mechanical graphene beam resonant mode gyroscope are realized.

Description

A kind of silicon micro mechanical graphene beam resonant mode gyroscope
Technical field
The invention belongs to the technical field of micro-/nano electromechanical systems, and in particular to a kind of silicon micro mechanical graphene beam resonant mode Gyroscope.
Background technology
Gyro can rotate as a kind of sensor for measuring measured object angular speed for discrimination object within the unit interval Angle, have very important effect in gesture stability and navigator fix field.Due to tradition machinery gyro have volume it is big, Cost is high, be not suitable for the undesirable elements such as batch production so that silicon micromechanical gyroscope is so that its small volume, light weight, cost be low, power consumption Small, reliability is high and shows one's talent from the manufacture of numerous gyros the advantages of big measurement range, is obtained in civilian and military industry field It is widely applied.1988, U.S.'s Draper lab designs simultaneously processed first silicon micromechanical gyroscope, and the gyro passes through Measure the differential capacitance variable quantity of a pair of electric capacity collection plates to obtain angular speed, precision is apparently higher than classical spinning top.The gyro makes Capacitance determining method has that temperature drift is small, sensitivity is high, good reliability the characteristics of.But with silicon micro mechanical inertia device structure Continuing to optimize for size, steps into micro-nano rank field so that the Signal-to-Noise exported by capacitance detecting is very low.Cause This, Seshia of University of California-Berkeley in 2002 et al. proposes the imagination of silicon micromachine resonant gyro simultaneously Principle prototype is produced.The clamped tuning fork of both-end (DEFT) is converted into by the change for the coriolis force for producing input angular velocity humorous The change of vibration frequency, can be effectively prevented from the noise jamming produced in capacitance detecting.The resonance sensing unit wherein used With the good characteristics that reproducible, resolving power is high and stability is strong, therefore silicon micromachine resonant gyro is as people's research Emphasis.
The correlation theory research of graphene just has begun to from nineteen forty-seven.Univ Manchester UK physicist in 2004 Andre Geim and Konstantin Novoselov isolate single-layer graphene using micromechanics stripping method success from graphite. Self-existent two-dimensional graphene crystal is obtained in fields such as high-performance nanometer electronic device, composite, resonant transducers It is widely applied.Because the theoretic throat of graphene individual layer is 0.335nm, fracture strength is 40N/m close to theoretical limit, room temperature Lower Young's modulus is 1.0TPa, and Elastic extensibility is much better than the overload capacity of the materials such as silicon, CNT up to 20%.
Because for silicon micro-resonance type gyro, the difference that sensitive material is produced to environmental factors such as temperature, vibrations causes humorous The change of vibration frequency has important influence to the measurement accuracy and job stability of sensor.Therefore graphene resonance beam is in silicon microcomputer It can give full play of as sensitive material that small volume, flexible structure, fracture strength be big and mechanical quality factor in tool gyro High the characteristics of.And the fundamental research of graphene beam resonant mode gyro, key technology break through more than based on empirical theory, tool Body carries out resonance characteristic research using graphene as sensitive structure, and the resonant mode gyroscope exported with differential composite sensing is still located In research blank.
The content of the invention
The technical problem to be solved in the present invention is:Overcome the shortcomings of on existing silicon micro-resonance type gyroscope technology, make full use of There is provided a kind of silicon that a kind of size is small, flexible structure, strong antijamming capability, measurement range are big for the high-quality feature of grapheme material Micromechanics graphene beam resonant mode gyroscope, realizes graphene resonance beam and the close coupling of silicon micromechanical gyroscope.
The technical solution adopted for the present invention to solve the technical problems is:A kind of silicon micro mechanical graphene beam resonant mode gyro Instrument, including glass substrate, transfer beams, lever transmission part, fixed mass block driving comb, gyro mass, the first graphene Resonance beam, the second graphene resonance beam and frame, lever transmission part, fixed mass block driving comb and gyro mass are fixed On a glass substrate;The fixed pedestal of gyro mass can allow gyro mass to have displacement in normal orientation;Lever is passed Pass part to link together with gyro mass, left-right parts are in symmetrical structure;First graphene resonance beam and the second graphite Alkene resonance beam is placed in transfer beams and positioned between lever transmission part and frame, goes into the clamped resonance beam of both-end, and two The geometric identity of graphene resonance beam the first graphene resonance beam and the second graphene resonance beam, is completely in vacuum ring Border.
Wherein, the transfer beams, lever transmission part, fixed mass block driving comb it is identical with gyro quality block of material and It is each attached to above glass substrate, the first graphene resonance beam is identical with the second graphene resonance beam material therefor and is each attached to In transfer beams and positioned between lever transmission part and frame, an entirety is consequently formed.
Wherein, the transfer beams, lever transmission part, fixed mass block driving comb and gyro quality block of material can pass through Material etch mode is formed;First graphene resonance beam and the second graphene resonance beam material therefor can pass through stripping and growth side Formula is obtained.
Wherein, the lever transmission part, fixed mass block driving comb and gyro mass are put in same level Put structure normal orientation fixed mass block driving comb and axial direction lever transmission part it is full symmetric;First graphene Resonance beam and the second graphene resonance beam in same level, be placed on it is on same horizontal line and full symmetric along normal direction, The influence by measuring pressure and environment can be experienced simultaneously.
Wherein, excitation-pick-up mode that the first graphene resonance beam and the second graphene resonance beam are used with And relevant parameter is consistent;
When described excitation-pick-up mode be electrical way when, metal electrode respectively be located at the first graphene resonance beam and Wire is respectively welded on two rectangle short side centers of the second graphene resonance beam, metal electrode;
When described excitation-pick-up mode is optical mode, laser facula should be directed at the first graphene resonance beam and the The center of two graphene resonance beams.
The advantage of the present invention compared with prior art is:
In the present invention, by the way that graphene resonance beam, as the sensitive structure in silicon micromechanical gyroscope key technology, is met Graphene resonance beam sensitive structure high-precision, inexpensive, small volume, reaction is fast, dynamic range is big, adapt to adverse circumstances It is strict with, makes gyroscope that there is the performance that the linearity is good, zero stability is high, drift rate is low, anti-impact force is strong, realize humorous In formula of shaking sensor the characteristics of highly reliable, high mechanical quality factor, symmetrical measurement.Can be in biology, medical treatment, industrial machinery, aviation Space flight, safety protection field have larger application.
Brief description of the drawings
Fig. 1 is a kind of structure top view of silicon micro mechanical graphene beam resonant mode gyroscope of the invention.
Fig. 2 is a kind of stereochemical structure exploded view of silicon micro mechanical graphene beam resonant mode gyroscope of the invention.
Fig. 3 is a kind of sensitive structure profile of silicon micro mechanical graphene beam resonant mode gyroscope of the invention.
Embodiment
Below in conjunction with the accompanying drawings and embodiment further illustrates the present invention.
As Figure 1-3, a kind of silicon micro mechanical graphene beam resonant mode gyroscope angular-rate sensor, including glass substrate 1st, transfer beams 2, lever transmission part 3, fixed mass block driving comb 4, gyro mass 5, the first graphene resonance beam 6, Two graphene resonance beams 7 and frame 8.
The gyroscope structure simple shape, transfer beams 2, lever transmission part 3, fixed mass block in glass substrate 1 Four part of devices thickness of driving comb 4 and gyro mass 5 do not influence on integrally-built intrinsic frequency, therefore select state The Bulk micro machining technology of interior comparative maturity.By using silicon-glass anodic bonding, silicon deep etching process technology, it can be achieved The large-scale mode of production.
Selection N-type silicon or P-type silicon are simultaneously cleaned up, by the two-sided oxidation of silicon chip, and (front side of silicon wafer enters rower in front Know) carry out photoetching process.After photoetching, the silica of developing location is etched away.After removing photoresist, used with silica as mask Downward 3 μm -0.5 μm of the positive silicon face of KOH solution corrosion.Key is formed at fixed mass block driving comb 4 and the anchor point of frame 8 Close.Injected in silicon front and spread phosphorus or boron wait electrostatic bonding.
Go out concave pattern in the photomask surface of glass substrate 1 with silicon similar thermal expansion coefficient, and sputter Au electrodes to be formed Electrode and lead wait electrostatic bonding.
The heat produced in bonding process can be effectively reduced using the glass substrate 1 with silicon chip similar thermal expansion coefficient should Power, the stronger thermal stress produced in traditional heating bonding process is avoided by anode/electrostatic bonding under electric field action and is become Change.In the electric field formed on si-glass contact surface, the nominal price sodium ion in glass drifts about to negative electrode, makes connecing for si-glass Contacting surface is closely combined together.
Silicon wafer turnover is bonded with glass substrate 1 makes the boss of front side of silicon wafer turn into fixed structure, including transfer beams 2, thick stick Bar transmitting portions 3, fixed mass block driving comb 4 and gyro mass 5, and it is connected with lead with electrode, continue to use KOH solution corrosion is thinned, and forms the structure sheaf of silicon micromechanical gyroscope.On silicon chip carry out secondary light quarter, make by lithography transfer beams 2, Two normal orientations in lever transmission part 3, fixed mass block driving comb 4, gyro mass 5 and two transfer beams 2 Groove, the groove is used for building two graphene beams on axial direction.
First graphene resonance beam 6, the second graphene resonance beam 7 are in same level, and placement direction is in axial direction Level is consistent, and the method that can be by mechanically pulling off method and chemical vapor deposition is obtained.The thickness of single layer graphene film is 0.335nm, the first graphene resonance beam 6 of the present invention, the second graphene resonance beam 7 formation clamped resonance beam of both-end, thickness For 1~1000 layer, trench length is 100~10000 times of graphene resonance cantilever thickness, vacuum environment is in, such as Fig. 3 institutes Show.
Excitation-pick-up mode that first graphene resonance beam 6, the second graphene resonance beam 7 are used is identical, metal Electrode is located at two resonance beam short side centers respectively.
The driving force and damping force for realizing that reduction is coupled on detection axle are encapsulated using vacuum, gyroscope is greatly enhanced Quality factor, improve gyroscope performance.
The present invention principle and the course of work be:There are two vibration modes in the micromechanical gyro course of work, one is Normal vibration pattern, that is, drive vibration mode, normally referred to as with reference to vibration mode, and itself is in resonant condition, in coriolis force Additional movement can be produced under effect;Another is axial vibration pattern, i.e., the pattern of sensitive vibration, by reflecting the attached of coriolis force Plus the detection of motion, obtain the angular velocity information being included in coriolis force.
In the present invention, fixed mass block driving comb 4 provides the resonant condition of normal orientation for gyro.When angular speed is defeated Enter into gyro, gyro mass 5 is used for the change for experiencing angular speed, lever transmission part 3 is used to amplify coriolis force, makes transmission Beam 2 produces the change of internal stress in the axial direction.Due to each position axial direction internal stress change all same in transfer beams 2, therefore The two graphene resonance beams (the first graphene resonance beam 6 and the second graphene resonance beam 7) placed in transfer beams 2 at groove can To experience the change of the internal stress in transfer beams 2.By one in one the first graphene in compressive state of extended state The change of the internal stress of 6 and second graphene resonance beam of resonance beam 7, the axial coriolis force that gyro mass is exported to it is converted to Corresponding rate-adaptive pacemaker, by resonant frequency during graphene resonance beam original state and by resonant frequency during axial coriolis force Change can obtain corresponding axial coriolis force, so the angular speed change that can be inputted.

Claims (5)

1. a kind of silicon micro mechanical graphene beam resonant mode gyroscope, including glass substrate (1), transfer beams (2), lever transmission part (3), fixed mass block driving comb (4), gyro mass (5), the first graphene resonance beam (6), the second graphene resonance beam And frame (8) (7), it is characterised in that:Lever transmission part (3), fixed mass block driving comb (4) and gyro mass (5) It is fixed in glass substrate (1);The fixed pedestal of gyro mass (5) can allow gyro mass (5) in normal orientation There is displacement;Lever transmission part (3) links together with gyro mass (5), and left-right parts are in symmetrical structure;First graphite Alkene resonance beam (6) and the second graphene resonance beam (7) are placed in transfer beams (2) and positioned at lever transmission part (3) and frame (8) between, the clamped resonance beam of both-end, and two graphene resonance beam the first graphene resonance beams (6) and the second graphene are gone into The geometric identity of resonance beam (7), is completely in vacuum environment.
2. a kind of silicon micro mechanical graphene beam resonant mode gyroscope as claimed in claim 1, it is characterised in that:The transfer beams (2), lever transmission part (3), fixed mass block driving comb (4) is identical with gyro mass (5) material and is each attached to glass Above, the first graphene resonance beam (6) is identical with second graphene resonance beam (7) material and is each attached to transmission for glass substrate (1) On beam (2) and positioned between lever transmission part (3) and frame (8), an entirety is consequently formed.
3. a kind of silicon micro mechanical graphene beam resonant mode gyroscope as claimed in claim 1, it is characterised in that:The transfer beams (2), lever transmission part (3), fixed mass block driving comb (4) and gyro mass (5) material can pass through material etch etc. Mode is formed;First graphene resonance beam (6) and second graphene resonance beam (7) material can be obtained by the mode such as stripping and growth .
4. a kind of silicon micro mechanical graphene beam resonant mode gyroscope as claimed in claim 1, it is characterised in that:The lever is passed Part (3), fixed mass block driving comb (4) and gyro mass (5) are passed in same level, displacement structure normal orientation Fixed mass block driving comb (4) and axial direction lever transmission part (3) it is full symmetric;First graphene resonance beam (6) and the second graphene resonance beam (7) is in same level, be placed on it is on same horizontal line and full symmetric along normal direction, The influence by measuring pressure and environment can be experienced simultaneously.
5. a kind of silicon micro mechanical graphene beam resonant mode gyroscope as claimed in claim 1, it is characterised in that:First stone Excitation-pick-up the mode and relevant parameter that black alkene resonance beam (6) is used with the second graphene resonance beam (7) are consistent;
When described excitation-pick-up mode is electrical way, metal electrode is located at the first graphene resonance beam (6) and the respectively Wire is respectively welded on two rectangle short side centers of two graphene resonance beams (7), metal electrode;
When described excitation-pick-up mode is optical mode, laser facula should be directed at the first graphene resonance beam (6) and second The center of graphene resonance beam (7).
CN201710324290.9A 2017-05-10 2017-05-10 Silicon micromechanical graphene beam resonant gyroscope Active CN107101629B (en)

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Cited By (3)

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Publication number Priority date Publication date Assignee Title
CN108413953A (en) * 2018-02-27 2018-08-17 郑州轻工业学院 A kind of adjustable gain control surface acoustic wave gyroscope based on graphene film
CN112444239A (en) * 2019-08-30 2021-03-05 北京大学 Geometric compensation type (100) silicon micro-mechanical ring-shaped resonant gyroscope
CN116907463A (en) * 2023-09-08 2023-10-20 华芯拓远(天津)科技有限公司 High-precision full-decoupling triaxial MEMS gyroscope

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CN104215231A (en) * 2013-06-05 2014-12-17 中国科学院地质与地球物理研究所 MEMS high precision resonant beam closed-loop control gyroscope and manufacturing process thereof
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CN104819710A (en) * 2015-05-21 2015-08-05 北京航空航天大学 Resonant mode silicon micro-machined gyroscope with temperature compensation structure
CN106918420A (en) * 2017-04-21 2017-07-04 北京航空航天大学 A kind of pair of Graphene resonance beam type pressure sensor

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Publication number Priority date Publication date Assignee Title
CN1865851A (en) * 2006-06-13 2006-11-22 北京航空航天大学 Resonant-type micro-mechanical optic fiber gyroscope
CN101403615A (en) * 2008-10-24 2009-04-08 北京航空航天大学 Direct frequency-output vibration gyroscope structure
CN102315831A (en) * 2011-05-04 2012-01-11 西安电子科技大学 Preparation method for nano-electromechanical resonator based on graphene
US8683862B2 (en) * 2011-11-03 2014-04-01 The United States Of America As Represented By The Secretary Of The Navy Oscillation apparatus with atomic-layer proximity switch
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Cited By (5)

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Publication number Priority date Publication date Assignee Title
CN108413953A (en) * 2018-02-27 2018-08-17 郑州轻工业学院 A kind of adjustable gain control surface acoustic wave gyroscope based on graphene film
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CN112444239A (en) * 2019-08-30 2021-03-05 北京大学 Geometric compensation type (100) silicon micro-mechanical ring-shaped resonant gyroscope
CN116907463A (en) * 2023-09-08 2023-10-20 华芯拓远(天津)科技有限公司 High-precision full-decoupling triaxial MEMS gyroscope
CN116907463B (en) * 2023-09-08 2023-12-15 华芯拓远(天津)科技有限公司 High-precision full-decoupling triaxial MEMS gyroscope

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