CN108279320A - One kind is based on Fano resonance nano optical wave guide accelerometer preparation methods - Google Patents

One kind is based on Fano resonance nano optical wave guide accelerometer preparation methods Download PDF

Info

Publication number
CN108279320A
CN108279320A CN201810133315.1A CN201810133315A CN108279320A CN 108279320 A CN108279320 A CN 108279320A CN 201810133315 A CN201810133315 A CN 201810133315A CN 108279320 A CN108279320 A CN 108279320A
Authority
CN
China
Prior art keywords
photoresist
wave guide
accelerometer
soi substrate
silicon
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
CN201810133315.1A
Other languages
Chinese (zh)
Other versions
CN108279320B (en
Inventor
闫树斌
张彦军
韵力宇
李云超
张志东
崔建功
李国洪
冯登超
胡旭文
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.)
North University of China
Original Assignee
North University of China
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 North University of China filed Critical North University of China
Priority to CN201810133315.1A priority Critical patent/CN108279320B/en
Publication of CN108279320A publication Critical patent/CN108279320A/en
Application granted granted Critical
Publication of CN108279320B publication Critical patent/CN108279320B/en
Expired - Fee Related 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

Abstract

Optical field and micro optoelectro mechanical system field are particularly belonged to based on Fano resonance nano optical wave guide accelerometer principles and manufacturing process the present invention relates to a kind of, it is specially a kind of based on Fano resonance nano optical wave guide accelerometer preparation methods.The present invention provides one kind based on Fano resonance nano optical wave guide accelerometer preparation methods, the present invention is using SOI materials as sensing element and base material, based on the feature that high Q optics micro-loop chamber is highly sensitive, and SOI materials high refractive index, the advantages that optical confinement ability is strong, transmission loss is small, easy of integration, using integrated nanometer optical waveguide technique, it proposes the nano optical wave guide accelerometer to resonate based on Fano, the optical accelerometer with highly sensitive impact property is realized by power optical coupling effect.

Description

One kind is based on Fano resonance nano optical wave guide accelerometer preparation methods
Technical field
The present invention relates to one kind based on Fano resonance nano optical wave guide accelerometer principles and manufacturing process, particularly belongs to light Field and micro optoelectro mechanical system field, it is specially a kind of based on Fano resonance nano optical wave guide accelerometer preparation methods.
Background technology
Accelerometer (accelerometer) is a kind of inertia device for measuring acceleration, is to constitute not depending on to defend The core measuring unit of the inertial navigation system of star.From automobile air-bag system control, seismic monitoring, Aeronautics and Astronautics device is arrived And the inertial navigation system of pilotless automobile, then gravity sensing and screen automatic rotation function etc. to mobile phone peace plate computer It is all be unable to do without the effect of accelerometer, accelerometer has become an essential part in our daily lifes.
Traditional mems accelerometer is limited by environment, volume and self attributes, cannot be satisfied modern industry and Demand of the military developments to high-sensitivity accelerometer.And gleam dynamoelectric acceleration gauge MOEMS may be implemented by the characteristic of light Faster than mems accelerometer response device speed, integrated level higher, controllability are stronger, inhibit noise immune and electromagnetism interference Ability system device more outstanding.
Invention content
The present invention provides one kind based on Fano resonance nano optical wave guide accelerometer preparation methods, and the present invention is with SOI materials Material is used as sensing element and base material, based on the highly sensitive feature of high Q optics micro-loop chamber and SOI materials high refractive index, light The advantages that limitation capability is strong, transmission loss is small, easy of integration is learned, using integrated nanometer optical waveguide technique, proposes to resonate based on Fano Nano optical wave guide accelerometer, pass through power-optical coupling effect and realize the optical accelerometer with highly sensitive impact property.
The present invention adopts the following technical scheme that realization:One kind is based on Fano resonance nano optical wave guide accelerometer systems Preparation Method includes the following steps:
The first step, SOI Substrate pretreatment:SOI Substrate is cleaned by ultrasonic, is then rinsed with deionized water, is dried up through nitrogen;
Second step, high temperature modified and stress relieving by annealing:Pretreated SOI Substrate is toasted, to remove on substrate Steam increases the adhesiveness between photoresist and substrate, keeps spin coating more uniform, meanwhile, after the completion of baking will to substrate into The processing of row stress relieving by annealing;
Third walks, spin coating:The resist coating in above-mentioned SOI Substrate top layer silicon;
4th step, front baking:SOI Substrate is toasted after the completion of spin coating, fully evaporates the solvent in photoresist, reduces high speed Photoresist membrane stress when rotation, avoids photoresist from being layered;
5th step, photoetching:The photoresist of electron beam alignment mark is exposed using mask;
6th step, development:SOI Substrate after exposure is put into developer solution and is developed, oxygen plasma is used after the completion of development Resist remover handles substrate, removes the photoresist of exposure, while enhancing the adhesion strength of metal and SOI Substrate;
7th step, electron beam evaporation and stripping:Using electron beam evaporation titanizing and gold, it is then placed in acetone soln and impregnates, then Ultrasonic vibration removes the metal other than alignment mark with tweezers in acetone soln, and removes remaining photoresist, finally obtains double Cross alignment key pattern;
8th step, spin coating and electron beam lithography:Then the spin coating on the SOI Substrate for obtaining diesis alignment key pattern carries out Electron beam exposure is exposed the photoresist at annular chamber and waveguiding structure;
9th step, development:SOI Substrate after above-mentioned exposure is put into developer solution and is developed, oxygen etc. is used after the completion of development Ion resist remover handles substrate, removes the photoresist of exposure;
Tenth step, ICP deep silicon etchings:Using sense coupling, annular chamber and waveguide are obtained in top layer silicon Structure, waveguiding structure include straight wave guide and two Y waveguides, straight wave guide include connect two Y waveguide stem bifurcateds straight wave guide and with The straight wave guide that two Y waveguide tail portions are separately connected is gone wherein a straight wave guide of connection Y waveguide stem bifurcated is coupled with annular chamber Except remaining photoresist;
11st step, spin coating, photoetching, development, ICP deep silicon etchings, grating is obtained on the straight wave guide of two Y waveguides, 2 tail portion;
12nd step, spin coating, photoetching and development:Spin coating, photoetching and development on the SOI Substrate for obtain grating, will be outside annular chamber The photoresist enclosed is got rid of;
13rd step, it is rear to dry:After the completion of development, SOI Substrate is placed in and dries baking processing after progress on platform, removes post-develop photoresist Interior residual solvent improves the adhesiveness of photoresist and anti-etching ability;
14th step, ICP deep silicon etchings:Using sense coupling, the top layer silicon of annular chamber periphery is etched away,
15th step, RIE etchings:The intermediate silicon dioxide layer exposed is performed etching, the inspection being located at below annular chamber is formed Mass metering block and tie-beam(Intermediate silicon dioxide layer after connecting detection mass block and etching), and form the logical of bottom silicon etching Road;
16th step, ICP isotropic deep silicon etchings:ICP isotropics deep silicon etching used, removes passivating process therein, Utilize SF6Gas enters base silicon by the channel previously etched, is performed etching to base silicon, becomes to discharge tie-beam The SiO 2 cantilever detection mass block hanging with formation, removes photoresist;
Modulate circuit is integrated in the arrangements of accelerometers that etching is completed using MEMS technology, realizes nanometer light by the 17th step The preparation of waveguide accelerometer, modulate circuit include electrode 5, input unit 12 and probe unit 7.
Accelerometer basic principle is:Light source is divided into two-way after the straight wave guide grating incidence of side by Y waveguide, wherein Light is exported through straight wave guide all the way;Another way light is coupled through straight wave guide with annular chamber.When in the eigenfrequency and straight wave guide of annular chamber The frequency of transmission light generates resonance when close, and the spectrum of another light path and the spectrum of resonant optical path are interfered in Y waveguide and produced Raw Fano resonance;Annular chamber on a cantilever beam, when force effect outside system senses, annular chamber with wherein the coupling spacing of light is sent out all the way Raw slight change causes Fano Resonance Transmissions spectral line in transmission spectrum that significant changes occur, by the luminous intensity for measuring transmission peak value Variation can calculate acceleration value.
The present invention compared with prior art, has an advantageous effect in that:
(1)The present invention propose a kind of compact-sized, fast response time, high resolution, low-power consumption Fano resonance accelerometers, Especially on piece integrated-type hypersensitivity accelerometer has important meaning for the development of integrated optics accelerometer technology Justice.
(2)Present invention proposition can generate very precipitous Resonance Transmission spectral line using Fano resonator systems, and very little adds Velocity variations will make the luminous intensity of output occur significantly to change the detection, it can be achieved that hypersensitivity acceleration.
(3)Device of the present invention can use integrated nanometer optical waveguide technique to make, at low cost, and performance is high, and loss is small, with tradition CMOS technology perfection compatibility, it is simple in structure, be easy to make, have large-scale production potentiality.
Description of the drawings
Fig. 1 is nano optical wave guide arrangements of accelerometers schematic diagram of the present invention.
Fig. 2 is SOI Substrate schematic diagram.
Fig. 3 is straight wave guide of the present invention and optical grating construction schematic diagram.
Fig. 4 is diesis alignment mark schematic diagram.
Fig. 5 is that cantilever beam prepares schematic diagram.
Description of the drawings:1- straight wave guides;2-Y waveguides;3- cantilever beams;4- detects mass block, 5- electrodes;6- annular chambers;7- is visited Survey unit;8- top layer silicons;9- silicon dioxide layers;10- base silicons;11- gratings;12- input units.
Specific implementation mode
For accelerometer using SOI materials as sensing element and base material, SOI materials include top layer silicon 8, intermediate titanium dioxide Silicon layer 9 and base silicon 10 form straight wave guide 1, Y waveguide 2, annular chamber 6 and grating 11 in top layer silicon 8;Intermediate silicon dioxide layer 9 Upper formation cantilever beam 3 and detection mass block 4;Electrode 5, input unit 12, probe unit 7 form modulate circuit.Straight wave guide 1 hangs Arm beam 3, annular chamber 6 and grating 11 integrate, and the structure of this integral type helps to reduce mutually to be connected by separating component It is lost caused by connecing coupling.
According to the manufacturing process of accelerometer provided by the present invention, it is broadly divided into preparation and the cantilever beam of ring resonator Two flows of release, finally connected together using alignment process, wherein the preparation of ring resonator includes following step Suddenly:
The first step, SOI Substrate pretreatment.Once it is cleaned by ultrasonic with acetone, isopropanol and absolute ethyl alcohol, is cleaned every time 15min, cleaning three times, are then rinsed with deionized water, are dried up through nitrogen.
Second step, high temperature modified and stress relieving by annealing.SOI Substrate is toasted using 100 DEG C of temperature, with removal Steam on substrate increases the adhesiveness between photoresist and substrate, keeps spin coating more uniform.Meanwhile it being wanted after the completion of baking Stress relieving by annealing processing is carried out to substrate, annealing furnace used is RPT-500 quick anneal ovens, time 2min.
Third walks, spin coating.It is 1.2-1.5 μm to select AZ4620 positive photoetching rubbers, spin coating thickness, and the running parameter of sol evenning machine is set It is set to:Spin-coating time 6-8s, rotating speed 2000rad/min.
4th step, front baking.SOI Substrate is placed on 95 DEG C of baking platform after the completion of spin coating and toasts 90s, fully evaporates photoetching Solvent in glue, photoresist membrane stress when reducing high speed rotation, avoids photoresist from being layered.
5th step, photoetching.Litho machine used is the domestic exposure machine of MA6 contacts, and broadband UV light source is 365 ~ 400nm, Resolution ratio is 1 μm.Exposure parameter is set as:6.5s, exposure energy 9mW/cm3
6th step, development.SOI Substrate after exposure is put into dedicated developer solution and is developed, time 60s.It is aobvious Substrate is handled using oxygen plasma resist remover after the completion of shadow, removes the photoresist of exposure, while enhancing metal and SOI bases The adhesion strength of piece.
7th step, electron beam evaporation and stripping.Using the gold of the titanium and 130nm thickness of electron beam evaporation plating 30nm thickness, then It is put into acetone soln and impregnates 30min, then ultrasonic vibration 3min, the gold other than alignment mark is removed with tweezers in acetone soln Belong to, and remove photoresist, finally obtains diesis alignment key pattern, as shown in Figure 4.
8th step, spin coating and electron beam lithography.It is PMMA A4 positive photoresists with photoresist, spin coating thickness is 2 μm, spin coating ginseng Number is set as:Rotating speed is 3000rad/min, spin-coating time 6-8s.Then electron beam exposure is carried out.Instrument is Japan's electricity The JBX5500ZA, exposure dose 600mJ/mm of son3, time for exposure 2min.
9th step, development.SOI Substrate after exposure is put into dedicated developer solution and is developed, time 60s.It is aobvious Substrate is handled using oxygen plasma resist remover after the completion of shadow, removes the photoresist of exposure.
Tenth step, ICP deep silicon etchings.Using sense coupling, instrument is HRM etching machines, etching Gas is SF6, passivation protection gas is C4F8, etching parameters are:ICP power is 2000W, radio-frequency power 10W, SF6Gas stream Amount is 50sccm, and etch period 30s obtains annular chamber 6 and Y waveguide structure.
11st step, spin coating, photoetching, development, ICP deep silicon etchings obtain grating 11 on the straight wave guide 1 at both ends, obtain Optical grating construction is as shown in Figure 3.
The release of cantilever beam mainly comprises the steps of:
12nd step, spin coating, photoetching and development.Mask used layer material is AZ4620, and spin coating thickness is about 20 μm, spin coating parameter It is set as:Rotating speed is 3000rad/min, and spin-coating time is 6 ~ 8s.It is exposed after the completion of spin coating, exposure parameter is:9mW/ cm2, time for exposure 20s.Develop immediately after the completion of exposure, the TMAH that developer solution used is 25% and water 1:3 proportioning solution, Developing time is 90s, then rinses nitrogen drying well with deionized water.
13rd step, it is rear to dry.After the completion of development, SOI Substrate is placed in and dries baking processing after progress on platform, glue after removal development Interior residual solvent improves the adhesiveness of photoresist and anti-etching ability.It is 100 DEG C to dry temperature afterwards, time 90s.
14th step, ICP deep silicon etchings:Using sense coupling, the top layer silicon of 6 periphery of annular chamber is carved Eating away.
15th step, RIE etchings.Etching instrument used is Tegal903e, and etch rate is about 200nm/min, when etching Between be set as 30min.Every 10min, pallet is taken out and carries out cooling processing, leads to photoresist layer to avoid because temperature is excessively high It consumes too fast.
16th step, ICP isotropic deep silicon etchings.ICP isotropics deep silicon etching used is removed therein passivated Journey utilizes SF6Gas enters base silicon by the channel previously etched, is performed etching to silicon, outstanding to discharge silica Arm beam 3 and detection mass block 4.Etching parameters are set as:Rate is 0.6 μm/min, time 90s, preparation process flow such as Fig. 5 It is shown.
Modulate circuit is integrated in the arrangements of accelerometers that etching is completed by the 17th step using MEMS technology, and realization is received The preparation of rice light guide accelerometer.

Claims (1)

1. one kind is included the following steps based on Fano resonance nano optical wave guide accelerometer preparation methods:
The first step, SOI Substrate pretreatment:SOI Substrate is cleaned by ultrasonic, is then rinsed with deionized water, is dried up through nitrogen;
Second step, baking is modified and stress relieving by annealing:Pretreated SOI Substrate is toasted, to remove on substrate Steam increases the adhesiveness between photoresist and substrate, keeps spin coating more uniform, meanwhile, after the completion of baking will to substrate into The processing of row stress relieving by annealing;
Third walks, spin coating:The resist coating in above-mentioned SOI Substrate top layer silicon;
4th step, front baking:SOI Substrate is toasted after the completion of spin coating, fully evaporates the solvent in photoresist, reduces high speed Photoresist membrane stress when rotation, avoids photoresist from being layered;
5th step, photoetching:The photoresist of electron beam alignment mark is exposed using mask;
6th step, development:SOI Substrate after exposure is put into developer solution and is developed, oxygen plasma is used after the completion of development Resist remover handles substrate, removes the photoresist of exposure, while enhancing the adhesion strength of metal and SOI Substrate;
7th step, electron beam evaporation and stripping:Using electron beam evaporation titanizing and gold, it is then placed in acetone soln and impregnates, then Ultrasonic vibration removes the metal other than alignment mark with tweezers in acetone soln, and removes remaining photoresist, finally obtains double Cross alignment key pattern;
8th step, spin coating and electron beam lithography:Then the spin coating on the SOI Substrate for obtaining diesis alignment key pattern carries out Electron beam exposure, to annular chamber(6)And the photoresist at waveguiding structure is exposed;
9th step, development:SOI Substrate after above-mentioned exposure is put into developer solution and is developed, oxygen etc. is used after the completion of development Ion resist remover handles substrate, removes the photoresist of exposure;
Tenth step, ICP deep silicon etchings:Using sense coupling, annular chamber is obtained in top layer silicon(6)And wave Guide structure, waveguiding structure include straight wave guide(1)With two Y waveguides(2), straight wave guide(1)Including connecting two Y waveguides(2)Stem point The straight wave guide of fork and with two Y waveguides(2)The straight wave guide that tail portion is separately connected, wherein connecting Y waveguide(2)One of stem bifurcated is straight Waveguide and annular chamber(6)Coupling, removes remaining photoresist;
11st step, spin coating, photoetching, development, ICP deep silicon etchings, in two Y waveguides(2)The straight wave guide of tail portion(1)On obtain grating (11);
12nd step, spin coating, photoetching and development:Obtaining grating(11)SOI Substrate on spin coating, photoetching and development, will be annular Chamber(6)The photoresist of periphery is got rid of;
13rd step, it is rear to dry:After the completion of development, SOI Substrate is placed in and dries baking processing after progress on platform, removes post-develop photoresist Interior residual solvent improves the adhesiveness of photoresist and anti-etching ability;
14th step, ICP deep silicon etchings:Using sense coupling, by annular chamber(6)The top layer silicon etching of periphery Fall;
15th step, RIE etchings:The intermediate silicon dioxide layer exposed is performed etching, is formed and is located at annular chamber(6)Lower section Detect mass block(4)And tie-beam, and form the channel of bottom silicon etching;
16th step, ICP isotropic deep silicon etchings:With ICP isotropic deep silicon etchings, remove passivating process therein, profit Use SF6Gas enters base silicon by the channel previously etched, is performed etching to base silicon, becomes two to discharge tie-beam Aoxidize silicon cantilever(3)The hanging detection mass block with formation(4), remove photoresist;
Modulate circuit is integrated in the arrangements of accelerometers that etching is completed using MEMS technology, realizes nanometer light by the 17th step The preparation of waveguide accelerometer.
CN201810133315.1A 2018-02-09 2018-02-09 Preparation method of nano optical waveguide accelerometer based on Fano resonance Expired - Fee Related CN108279320B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810133315.1A CN108279320B (en) 2018-02-09 2018-02-09 Preparation method of nano optical waveguide accelerometer based on Fano resonance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810133315.1A CN108279320B (en) 2018-02-09 2018-02-09 Preparation method of nano optical waveguide accelerometer based on Fano resonance

Publications (2)

Publication Number Publication Date
CN108279320A true CN108279320A (en) 2018-07-13
CN108279320B CN108279320B (en) 2020-12-04

Family

ID=62808179

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810133315.1A Expired - Fee Related CN108279320B (en) 2018-02-09 2018-02-09 Preparation method of nano optical waveguide accelerometer based on Fano resonance

Country Status (1)

Country Link
CN (1) CN108279320B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112066975A (en) * 2020-09-25 2020-12-11 中北大学 Gyroscope and accelerometer integrated system based on double resonant cavities and preparation method thereof
CN114509845A (en) * 2022-04-21 2022-05-17 苏州熹联光芯微电子科技有限公司 Micro-ring resonator and electronic device

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060192974A1 (en) * 2005-02-01 2006-08-31 Chian Chiu Li Interferometric MOEMS Sensor
CN101256198A (en) * 2008-03-26 2008-09-03 北京航空航天大学 Gleam dynamoelectric acceleration gauge based on laser feedback interference
CN101609101A (en) * 2009-07-21 2009-12-23 浙江大学 Micro-acceleration gauge based on the wave guide ring shaped resonant cavity of silica-based high speed electrooptical modulation
CN101871950A (en) * 2010-06-21 2010-10-27 中北大学 Optical cavity micro-accelerometer based on integrated input/output terminal
CN102483427A (en) * 2009-06-15 2012-05-30 茨瓦内科技大学 CMOS moems sensor device
CN105445494A (en) * 2015-12-10 2016-03-30 中北大学 MOEMS accelerometer based on planar ring cavity, and manufacturing method of the same
CN106443065A (en) * 2016-07-01 2017-02-22 中国科学院上海微系统与信息技术研究所 High-precision wavelength shape acceleration sensor and preparation method thereof
WO2017055029A1 (en) * 2015-09-29 2017-04-06 Tronic's Microsystems Device for attaching two elements such as a chip, an interposer and a support

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060192974A1 (en) * 2005-02-01 2006-08-31 Chian Chiu Li Interferometric MOEMS Sensor
CN101256198A (en) * 2008-03-26 2008-09-03 北京航空航天大学 Gleam dynamoelectric acceleration gauge based on laser feedback interference
CN102483427A (en) * 2009-06-15 2012-05-30 茨瓦内科技大学 CMOS moems sensor device
CN101609101A (en) * 2009-07-21 2009-12-23 浙江大学 Micro-acceleration gauge based on the wave guide ring shaped resonant cavity of silica-based high speed electrooptical modulation
CN101871950A (en) * 2010-06-21 2010-10-27 中北大学 Optical cavity micro-accelerometer based on integrated input/output terminal
WO2017055029A1 (en) * 2015-09-29 2017-04-06 Tronic's Microsystems Device for attaching two elements such as a chip, an interposer and a support
CN105445494A (en) * 2015-12-10 2016-03-30 中北大学 MOEMS accelerometer based on planar ring cavity, and manufacturing method of the same
CN106443065A (en) * 2016-07-01 2017-02-22 中国科学院上海微系统与信息技术研究所 High-precision wavelength shape acceleration sensor and preparation method thereof

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112066975A (en) * 2020-09-25 2020-12-11 中北大学 Gyroscope and accelerometer integrated system based on double resonant cavities and preparation method thereof
CN112066975B (en) * 2020-09-25 2021-05-14 中北大学 Gyroscope and accelerometer integrated system based on double resonant cavities and preparation method thereof
CN114509845A (en) * 2022-04-21 2022-05-17 苏州熹联光芯微电子科技有限公司 Micro-ring resonator and electronic device
CN114509845B (en) * 2022-04-21 2022-07-12 苏州熹联光芯微电子科技有限公司 Micro-ring resonator and electronic device

Also Published As

Publication number Publication date
CN108279320B (en) 2020-12-04

Similar Documents

Publication Publication Date Title
CN105445494B (en) A kind of MOEMS accelerometers and its manufacturing method based on plane annular chamber
Wang et al. Monolithic integration of pressure plus acceleration composite TPMS sensors with a single-sided micromachining technology
CN108279320A (en) One kind is based on Fano resonance nano optical wave guide accelerometer preparation methods
JP2006247793A (en) Interdigital electrode couple forming method
CN110329982B (en) In-plane accelerometer based on rotating folding beam and nano optical resonant cavity and method
CN105445495B (en) A kind of symmetrical MEMS acceleration sensitives chip and its manufacturing process
CN110308306B (en) MOEMS accelerometer based on fully-differential two-dimensional photonic crystal cavity structure and processing method thereof
CN109557049A (en) A kind of hydrogen gas sensor and preparation method thereof
CN107817364B (en) A kind of two axis accelerometer chip of MEMS straight pull and vertical compression formula and preparation method thereof
Taghavi et al. Simulation, fabrication, and characterization of a sensitive SU-8-based Fabry-Pérot MOEMS accelerometer
CN112433067A (en) Low-cross-axis crosstalk sensitive structure and manufacturing method thereof
CN107799392B (en) Black silicon, preparation process and preparation method of MEMS device based on black silicon
CN107621674A (en) A kind of flexible optical waveguides of SU 8 applied to accelerometer and preparation method thereof
CN213933915U (en) Sensitive structure of low cross axle crosstalk
CN1994860B (en) Silicon micromachine cantilever beam sensor driving structure, production method and uses under torsion mode
CN107478251B (en) A kind of graphene film Fabry-perot optical fiber resonator and preparation method thereof for capableing of stress regulation and control
CN108195366A (en) A kind of micro-nano gyroscope and its processing method based on double-layer nanometer grating
CN201408748Y (en) Silicon deep slot structure with depth-to-width ratio
CN104555893B (en) The method that inductive material film is formed in deep trench
CN110531114A (en) A kind of MEMS three-axis piezoresistance formula accelerometer chip of purely axial deformation and preparation method thereof
CN107703056A (en) SOI micro-loop photon biology sensor preparation methods based on 1-D photon crystal
CN108709549A (en) A kind of single-chip integration gyroscope and its processing method based on nanometer grating
CN209559360U (en) A kind of temperature sensor
CN111024194B (en) Quality detection method of resonance system
CN109239399B (en) Resonant accelerometer based on double-fork resonant beam

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
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20201204

Termination date: 20220209

CF01 Termination of patent right due to non-payment of annual fee