CN104777330A - Single-island multi-electrode quartz accelerometer - Google Patents

Single-island multi-electrode quartz accelerometer Download PDF

Info

Publication number
CN104777330A
CN104777330A CN201410014008.3A CN201410014008A CN104777330A CN 104777330 A CN104777330 A CN 104777330A CN 201410014008 A CN201410014008 A CN 201410014008A CN 104777330 A CN104777330 A CN 104777330A
Authority
CN
China
Prior art keywords
island
single island
pedestal
electrode
screw
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
CN201410014008.3A
Other languages
Chinese (zh)
Other versions
CN104777330B (en
Inventor
田文杰
朴林华
朱嘉林
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.)
Beijing Information Science and Technology University
Original Assignee
Beijing Information Science and Technology University
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 Beijing Information Science and Technology University filed Critical Beijing Information Science and Technology University
Priority to CN201410014008.3A priority Critical patent/CN104777330B/en
Publication of CN104777330A publication Critical patent/CN104777330A/en
Application granted granted Critical
Publication of CN104777330B publication Critical patent/CN104777330B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Piezo-Electric Or Mechanical Vibrators, Or Delay Or Filter Circuits (AREA)

Abstract

A single-island multi-electrode quartz accelerometer of the invention belongs to the field of linear acceleration measurement by using a multi-electrode quartz force-sensitive resonator as a sensitive core component. The accelerometer acts the inertial force generated during accelerated movement on the multi-electrode quartz force-sensitive resonator, and detects the amount of change of the resonant frequency of the resonator to obtain a corresponding acceleration to be detected. The accelerometer is composed of a base, a shell, a circuit board, a sensitive element, and an aerial socket. The base and the shell constitute a closed cavity, the sensitive element is mounted on the base, the circuit board is mounted on the sensitive element, and the socket is mounted on the shell. A single-island base and a sealing cover of the sensitive element are matched to form a sealed cavity, multi-electrode quartz force-sensitive resonators are installed at the two sides of a central single island in the cavity, the single-island base and the central single island are integrally machined, and the single-island base is equipped with limiting screws. The measuring range of the accelerometer is from 10<-4>g to 10<2>g. The accelerometer can be used in detection control systems of aircrafts, vehicles, ships, and the like.

Description

Single island multi-electrode quartz accelerometer
Technical field
List island of the present invention multi-electrode quartz accelerometer belongs to the field utilizing the quick resonator of multi-electrode quartz power to carry out linear acceleration measurement as sensitive core element.This accelerometer is made up of base, shell, circuit board, sensitive element and socket, can be used for the detecting and controlling system of aircraft, vehicle, naval vessel, industrial automation etc.
Background technology
Quartz crystal has good physics, chemical stability, its piezoelectric effect had is widely used in power, stress mornitoring, particularly in digital detection control field, quartz element receives the lasting concern of people always because it has stronger advantage.Such as, the piezoelectric effect of quartz crystal is being applied in acceleration detection, the strategic level quartz accelerometer energy sensitivity that Kearfott company of the U.S. adopts double quality blocks and double resonator to develop goes out the Gravity changer because Yue Qiu sun tidal fluctuations causes, U.S.Army Missile Command and Allied Singal Aerospace Instunment System company adopt the high acceleration high-performance quartz crystal accelerometer of two quality, frequency difference structure, measurement range 1200g, scale-up factor 1.1Hz/g.United States Patent (USP) 5578755 and United States Patent (USP) 5962786 etc. all disclose the quartz accelerometer scheme of different structure.National Aerospace research company of France (ONERA) adopts the quartz accelerometer (VIA) of girder construction development of shaking, for the gesture stability of tactical missile.These quartz accelerometers are structurally general complicated.
Summary of the invention
To the object of the invention is in the application process in order to solve quartz accelerometer the environmental factor such as temperature to the impact of accelerometer performance, providing that a kind of stability is high, antijamming capability is strong, structure simple single island multi-electrode quartz accelerometer.
A kind of single island of the present invention multi-electrode quartz accelerometer, this accelerometer is made up of base, shell, circuit board, sensitive element and socket.Passive base and shell are closely cooperated by screw and are assembled into cavity, the sensitive element screw detected is arranged on base, circuit board is anchored on sensitive element by board support stud and attachment screw, aviation socket is arranged on shell by screw, and power supply and signal are passed in and out from aviation socket by cable.It is characterized in that: (one) sensitive element is made up of single island pedestal, central single island, stop screw, the quick resonator of multi-electrode quartz power and seal closure; (2) single island pedestal and seal closure form seal chamber by screw fastening, and single island pedestal and central single island are by integrally processing; (3) the quick resonator of power as core parts is the quick resonator of multi-electrode quartz crystal power, and its electrode logarithm is two pairs or more.
Accompanying drawing explanation
Tu1Dan island multi-electrode quartz arrangements of accelerometers cut-open view
1-base 2-shell
3-sensitive element 4-aviation socket
5-circuit board 6-board support stud (totally 4)
7-circuit board screw (totally 4) 8-socket screws (totally 4)
9-casing screws (totally 4) 10-base screw (totally 2)
Fig. 2 sensitive element structural representation
11-mono-island pedestal 12-1,12-2-stop screw
The single island of 13-1,13-2-multi-electrode power quick resonator 14-central authorities
15-1,15-2 (not shown)-holding screw 16-seal closure
17-sealing screw (totally 8)
Tu3Dan island pedestal and central single island structure schematic diagram
Pedestal 11-1,11-2-mono-island, 11-mono-island pedestal resonator support platform
11-3,11-4-stop nut hole 11-5-electrode lead hole (totally 4)
11-6-mounting nuts hole (totally 2) 11-7-wire lead slot
The single island of 11-8-seal closure locknut hole 14-central authorities
14-1-flexibly connects 14-2,14-3-central authorities single island resonator support platform
14-4-inertial mass
Fig. 4 seal closure structural representation
16-seal closure 16-1-seals countersunk screw hole (totally 8)
16-2-circuit board mounting nuts hole (totally 4)
Embodiment
Below in conjunction with accompanying drawing, following describing is done to list island of the present invention multi-electrode quartz accelerometer.
The structure of single island multi-electrode quartz accelerometer as shown in Figure 1, it to be closely cooperated by screw 9 by passive base 1 and shell 2 and is assembled into cavity, the sensitive element 3 detected is arranged on base 1 with screw 10, circuit board 5 is supported by circuit board stud 6, and be anchored on sensitive element 3 by circuit board screw 7, aviation socket 4 is arranged on shell 2 by socket screws 8, and power supply and signal are passed in and out from aviation socket 4 by cable; As shown in Figure 2, it is made up of single island pedestal 11, central 14, two stop screw 12-1 and 12-2 in single island, two quick resonator 13-1 and 13-2 of multi-electrode power, seal closures 16 structure of sensitive element 3.
Single island pedestal 11 of sensitive element 3 and seal closure 16 form seal chamber by sealing screw 17 is fastening, central single island 14 is had in cavity, single island pedestal 11 and central authorities' list island 14 are by integrally processing, structure as shown in Figure 3, the cavity of sensitive element is divided into the symmetrical little cavity in two, left and right by the single island 14 of central authorities, two the quick resonator of multi-electrode power 13-1 and 13-2 are embedded in two little cavitys of both sides, central single island 14 symmetrically, the quick resonator of multi-electrode power 13-1's or 13-2 while weld with the support platform 14-2 in the middle part of central authorities single islands 14 or 14-3, another side welds with the support platform 11-1 in the middle part of single island pedestal 11 or 11-2, at inertial mass 14-4 corresponding position limited location screw 12-1 and 12-2 on the single top, island 14 in two ends, left and right and central authorities on pedestal 11 top, single island, stop screw 12-1 and 12-2 is arranged in stop nut hole 11-3 and 11-4 corresponding to pedestal 11 top, single island, and by holding screw 15-1 and the tightening of 15-2 (not shown).
Single island pedestal 11 of the sensitive element 3 shown in Fig. 2 and central single island 14, its structure as shown in Figure 3, single island pedestal 11 and central authorities' list island 14 are by integrally processing, the bottom on the single island 14 of central authorities and the junction 14-1 of single island pedestal 11 are for flexibly connecting, there is symmetric support platform 14-2 and 14-3 inlaying quick resonator 13-1 and 13-2 of multi-electrode power the left and right sides, middle part on the single island 14 of central authorities, and the top on central single island 14 is inertial mass 14-4; Electrode lead hole 11-5 (totally 4), mounting nuts hole 11-6 (totally 2), wire lead slot 11-7 are arranged at the bottom of single island pedestal 11, there is symmetric support platform 11-1 and 11-2 inlaying quick resonator 13-1 or 13-2 of multi-electrode power the left and right sides, middle part of single island pedestal 11, there are nut bore 11-3 and the 11-4 of mounting limit screw 12-1 or 12-2 in the left and right sides, top of single island pedestal 11, and there is the locknut hole 11-8 (totally 8) for installing seal closure 16 left and right sides of single island pedestal 11.
Quick resonator 13-1 or 13-2 of multi-electrode power of the sensitive element 3 shown in Fig. 2, its substrate is quartz crystal circle sheet, same on-chip electrode logarithm is two pairs or more, and electrode position can be symmetrical or asymmetric distribution in on-chip distribution; It is the quick resonator of Quartz Force of three pairs of electrodes shown in the present embodiment.
The seal closure 16 of the sensitive element 3 shown in Fig. 2, its structure as shown in Figure 4, there is the countersunk screw hole 16-1 (totally 8) for installing sealing screw two of seal closure 16, having the support mounting nuts hole 16-2 (totally 4) for mounting circuit boards support column 6 at four adjacent corners.
List island multi-electrode quartz accelerometer resolution < 10 of the present invention -4g, nonlinearity < 0.1%, measurement range is 10 -4g ~ 10 2g, have structure simple, numeral exports, high reliability.This accelerometer can be used for the detecting and controlling system of aircraft, vehicle, naval vessel, industrial automation etc.

Claims (4)

1. a Zhong Dan island multi-electrode quartz accelerometer, to be closely cooperated by screw (9) by passive base (1) and shell (2) and be assembled into cavity, the sensitive element (3) detected is arranged on base (1) with screw (10), circuit board (5) is supported by board support stud (6), and be anchored on sensitive element (3) by circuit board screw (7), aviation socket (4) is arranged on shell (2) by screw (8), and power supply and signal are passed in and out from aviation socket (4) by cable; Sensitive element (3) is made up of single island pedestal (11), central single island (14), stop screw (12-1,12-2), the quick resonator of multi-electrode power (13-1,13-2) and seal closure (16).
2. single island multi-electrode quartz accelerometer described in claim 1, the architectural feature of its sensitive element (3) is: single island pedestal (11) and seal closure (16) form seal chamber by sealing screw (17) is fastening, central single island (14) and two quick resonators of multi-electrode power (13-1) are had in cavity, (13-2), single island pedestal (11) and central authorities' list island (14) are by integrally processing, the cavity of sensitive element is divided into the symmetrical little cavity in two, left and right by central authorities single island (14), two quick resonators of multi-electrode power (13-1), (13-2) be embedded in symmetrically in two little cavitys of central single island (14) both sides, the quick resonator of multi-electrode power (13-1) or (13-2) while weld with the support platform (14-2) at central authorities single island (14) middle parts or (14-3), another side welds with the support platform (11-1) in the middle part of single island pedestal (11) or (11-2), the two ends, left and right limited location screw (12-1) on single pedestal (11) top, island, (12-2), stop screw (12-1), (12-2) the stop nut hole (11-3) that pedestal (11) top, single island is corresponding is embedded in, (11-4) in, and by holding screw (15-1), (15-2) (not shown) tightening.
3. single island multi-electrode quartz accelerometer described in claim 1, single island pedestal (11) of its sensitive element (3) and the architectural feature on central single island (14) are: single island pedestal (11) and central authorities' list island (14) are by integrally processing, the bottom of central authorities single island (14) and the junction (14-1) on single island pedestal (11) are for flexibly connecting, there are the symmetric support platform (14-2) and (14-3) of inlaying the quick resonator of multi-electrode power (13-1) or (13-2) in the left and right sides, middle part of central authorities single island (14), the top of central authorities single island (14) is inertial mass (14-4), electrode lead hole (11-5) (totally 4) is arranged at the bottom of single island pedestal (11), mounting nuts hole (11-6) (totally 2), wire lead slot (11-7), there are the symmetric support platform (11-1) and (11-2) of inlaying the quick resonator of multi-electrode power (13-1) or (13-2) in the left and right sides, middle part of single island pedestal (11), there are stop nut hole (11-3) and (11-4) of mounting limit screw (12-1) or (12-2) in the left and right sides, top of single island pedestal (11), there is the locknut hole (11-8) (totally 8) of installation seal closure (16) left and right sides of single island pedestal (11).
4. single island multi-electrode quartz accelerometer described in claim 1, the quick resonator of multi-electrode power (13-1) of its sensitive element (3) or the architectural feature of (13-2) are: the substrate of the quick resonator of multi-electrode power (13-1,13-2) is quartz crystal circle sheet, same on-chip electrode logarithm is two pairs or more, and electrode position can be symmetrical or asymmetric distribution in on-chip distribution.
CN201410014008.3A 2014-01-14 2014-01-14 Single island multi-electrode quartz accelerometer Expired - Fee Related CN104777330B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410014008.3A CN104777330B (en) 2014-01-14 2014-01-14 Single island multi-electrode quartz accelerometer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410014008.3A CN104777330B (en) 2014-01-14 2014-01-14 Single island multi-electrode quartz accelerometer

Publications (2)

Publication Number Publication Date
CN104777330A true CN104777330A (en) 2015-07-15
CN104777330B CN104777330B (en) 2018-04-10

Family

ID=53618922

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410014008.3A Expired - Fee Related CN104777330B (en) 2014-01-14 2014-01-14 Single island multi-electrode quartz accelerometer

Country Status (1)

Country Link
CN (1) CN104777330B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110441550A (en) * 2019-09-06 2019-11-12 北京信息科技大学 A kind of embedded 12 electrode quartz accelerometer of circuit

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3569749A (en) * 1968-11-06 1971-03-09 List Hans Piezoelectric accelerometer with an internal spherical bearing
CN101082630A (en) * 2007-07-09 2007-12-05 北京信息工程学院 Novel piezoelectric quartz accelerameter
CN101082487A (en) * 2007-07-09 2007-12-05 北京信息工程学院 Novel piezoelectric quartz horizontal attitude sensor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3569749A (en) * 1968-11-06 1971-03-09 List Hans Piezoelectric accelerometer with an internal spherical bearing
CN101082630A (en) * 2007-07-09 2007-12-05 北京信息工程学院 Novel piezoelectric quartz accelerameter
CN101082487A (en) * 2007-07-09 2007-12-05 北京信息工程学院 Novel piezoelectric quartz horizontal attitude sensor

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
鄂然: "单基多电极式石英加速度计的研究", 《万方数据库》 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110441550A (en) * 2019-09-06 2019-11-12 北京信息科技大学 A kind of embedded 12 electrode quartz accelerometer of circuit
CN110441550B (en) * 2019-09-06 2024-06-25 北京信息科技大学 Circuit embedded 12-electrode quartz accelerometer

Also Published As

Publication number Publication date
CN104777330B (en) 2018-04-10

Similar Documents

Publication Publication Date Title
CN100397086C (en) Novel piezoelectric quartz accelerameter
EP2746780B1 (en) Bias reduction in force rebalanced accelerometers
CN103543292A (en) Composite accelerometer based on capacitance effect and tunnel effect
CN203605948U (en) Novel gyroscope based on nano grating detection
CN108089027A (en) Sensor and navigation attitude instrument based on MEMS capacitive micro-acceleration gauge
CN103557854A (en) Novel gyroscope based on nanometer optical grating detection
CN203606385U (en) Combined type accelerometer based on capacitance effect and tunnel effect
CN104596496A (en) Self-adapted time lag feedback control micromechanical gyroscope system
CN101298987B (en) Robustness tuning fork vibrating type micromechanical gyroscope
KR20210110361A (en) Sensor components, inertial measurement components and mobile devices
Nekrasov et al. Influence of translational vibrations, shocks and acoustic noise on MEMS gyro performance
CN104457966A (en) Piezoelectric type decoupling micro-vibration measurement system
CN113639954B (en) Model inclination angle measuring device suitable for 1-meter-scale high-speed wind tunnel test
CN110531407B (en) Acceleration sensor module in seismic intensity meter and measurement application method thereof
CN104777330A (en) Single-island multi-electrode quartz accelerometer
CN113514666B (en) Micromechanical accelerometer based on PT symmetrical resonator and detection method thereof
CN103454449A (en) Three-axis micro-mechanical accelerometer
Cao Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope
CN201828261U (en) Digital display inclinometer
CN113219819B (en) Matlab/Simulink-based electrostatic suspension accelerometer tower-falling experiment simulation system
CN107532903B (en) Rotational rate sensor and method
CN207623364U (en) Sensor based on MEMS capacitive micro-acceleration gauge and navigation attitude instrument
CN211262468U (en) Piezoelectric acceleration and temperature integrated sensor
Yuzawa et al. A 3-axis catch-and-release gyroscope with pantograph vibration for low-power and fast start-up applications
CN209764377U (en) Blunt body split structure model for automobile wind tunnel experiment research

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
EXSB Decision made by sipo to initiate 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
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180410

Termination date: 20190114