CN103900548A - Silicon micro full-decoupling dual-mass dual-line vibratory gyroscope - Google Patents
Silicon micro full-decoupling dual-mass dual-line vibratory gyroscope Download PDFInfo
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- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
- G01C19/5719—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using planar vibrating masses driven in a translation vibration along an axis
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- G01C19/574—Structural details or topology the devices having two sensing masses in anti-phase motion
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Abstract
The invention discloses a silicon micro full-decoupling dual-mass dual-line vibratory gyroscope which comprises a base, a first substructure, a second substructure and a substructure connecting device, wherein the first substructure and the second substructure are connected through the substructure connecting device; the first substructure and the second substructure are angular velocity measurement structures; each angular velocity measurement structure comprises a mass block, a first fixing base fixed on the base, a second fixing base fixed on the base, a third fixing base fixed on the base, a fourth fixing base fixed on the base, a first driving mechanism, a second driving mechanism, a first detection mechanism, a second detection mechanism, a first driving parallel beam, a second driving parallel beam, a first detection parallel beam, a second detection parallel beam and multiple U-shaped folded beams.
Description
Technical field
The invention belongs to microelectromechanical systems and micro-inertia measuring technology, particularly the two mass doublet vibration gyroscopes of the micro-full decoupling of a kind of silicon.
Background technology
Silicon micromechanical gyroscope is a kind of inertial sensor of measuring rotational angular velocity, the Coriolis effect that utilizes oscillating mass piece to produce when by pedestal driven rotary is measured the angular velocity of pedestal rotation, compare with photoelectricity class gyro with traditional electrical category gyro, have that volume is little, cost is low, lightweight, high reliability, have important use value and wide application prospect in dual-use field.
From last century end, Duo Jia research institution has just started the research of silicon micro-gyroscope both at home and abroad, and the silicon micro-gyroscope of most of mechanism research and development adopts the version of simple substance amount and the design proposal of not decoupling zero or half decoupling zero.For simple substance amount silicon micro-gyroscope, in the situation that axial acceleration is disturbed existence, be easy to cause the saturated inefficacy of electronic circuit as common mode interference, finally make the work of silicon micro-gyroscope be had a strong impact on.In recent years, minority mechanism has carried out preliminary theory and Test Study to two quality silicon micro-gyroscopes, also mostly adopt the design of not decoupling zero or half decoupling zero, due to the existence of various mismachining tolerances, silicon micromechanical gyroscope is without Coriolis effect in the situation that, the vibrational energy of its driven-mode also can be coupled to sensed-mode, produce orthogonal coupling error signal and skew coupling error signal, and the impact that not decoupling zero design proposal produces these two kinds of signals cannot reduce at all, the design proposal of half decoupling zero also only can partly reduce this two kinds of signals impact on silicon micromechanical gyroscope performance.
Summary of the invention
Goal of the invention: the object of the present invention is to provide a kind of low in energy consumption, antijamming capability is strong, two mass doublet vibrating micromechanical gyroscopes of highly sensitive, Highgrade integration, motion full decoupling.
Technical scheme: the two mass doublet vibration gyroscopes of the micro-full decoupling of a kind of silicon of the present invention, comprise pedestal, the first minor structure, the second minor structure and minor structure coupling arrangement, connect by minor structure coupling arrangement between the first minor structure and the second minor structure, and described the first minor structure and the second minor structure are angular velocity measurement minor structure, and described angular velocity measurement minor structure comprises mass, be fixed on the first fixed pedestal on pedestal, be fixed on the second fixed pedestal on pedestal, be fixed on the 3rd fixed pedestal on pedestal, be fixed on the 4th fixed pedestal on pedestal, the first driving mechanism, the second driving mechanism, the first testing agency, the second testing agency, first drives parallel girder, second drives parallel girder, first detects parallel girder, second detects parallel girder, the first affixed U-shaped folded beam, the second affixed U-shaped folded beam, the 3rd affixed U-shaped folded beam, the 4th affixed U-shaped folded beam, the 5th affixed U-shaped folded beam, the 6th affixed U-shaped folded beam, the 7th affixed U-shaped folded beam, the 8th affixed U-shaped folded beam, the first driving mechanism by the first affixed U-shaped beam be connected to the first fixed pedestal, the first driving mechanism is connected to the second fixed pedestal by the second affixed U-shaped beam, the second testing agency by the 3rd affixed U-shaped beam be connected to the second fixed pedestal, the second testing agency is connected to the 3rd fixed pedestal by the 4th affixed U-shaped beam, the second driving mechanism by the 5th affixed U-shaped beam be connected to the 3rd fixed pedestal, the second driving mechanism is connected to the 4th fixed pedestal by the 6th affixed U-shaped beam, the first testing agency by the 7th affixed U-shaped beam be connected to the 4th fixed pedestal, the first testing agency is connected to the first fixed pedestal by the 8th affixed U-shaped beam, the first driving mechanism is arranged on a side of mass, the second driving mechanism is arranged on the opposite side that mass is relative, between the first driving mechanism and mass, drive parallel girder to be connected by first, between the second driving mechanism and mass, drive parallel girder to be connected by second, to drive this mass to vibrate at left and right directions from a driving direction, the first testing agency is arranged on a side of mass, the second testing agency is arranged on the opposite side that mass is relative, between the first testing agency and mass, detecting parallel girder by first is connected, between the second testing agency and mass, detect parallel girder by second and be connected, to detect the vibration of mass at the mass perpendicular on driving direction.Further, described minor structure coupling arrangement connects and comprises the first U-shaped folded beam and the second U-shaped folded beam, the first minor structure and the second minor structure mutually against, be respectively arranged with in both next-door neighbours' the top and bottom of driving mechanism the first U-shaped folded beam with the second U-shaped folded beam to be connected the first minor structure and the second minor structure.
Further, described the first fixed pedestal, the second fixed pedestal, the 3rd fixed pedestal, the 4th fixed pedestal is arranged at respectively one foursquare four jiaos, mass is arranged at this foursquare central authorities, the first driving mechanism, the first testing agency, the second driving mechanism, the second testing agency are arranged at respectively the outside on these square four limits, wherein the first driving mechanism and the second driving mechanism are arranged at the outside on relative both sides, and the first testing agency and the second testing agency are arranged at the outside on relative other both sides.
Further, between the first driving mechanism and the second driving mechanism, be connected with the second framework by the first framework respectively, the first described driving mechanism and the second driving mechanism are micro drives capacitor mechanism, and described micro drives capacitor mechanism comprises and drives movable comb braces, drive feedback movable comb braces, is arranged at driving fixed pedestal on pedestal, is arranged at the driving fixed fingers that drives on fixed pedestal, is arranged at the drive feedback fixed pedestal on pedestal and is arranged at the drive feedback fixed fingers on drive feedback fixed pedestal.
Further, the first described testing agency and the second testing agency are miniature Detection capacitance mechanism, described miniature Detection capacitance mechanism comprises the first motion detection broach frame, the second motion detection broach frame, the first detection comb fixed pedestal and be arranged on the first fixed test broach on the first detection comb fixed pedestal, the second detection comb fixed pedestal and be arranged on the second fixed test broach on the second detection comb fixed pedestal, wherein the first motion detection broach frame matches with the first fixed test broach and forms the first broach electric capacity, the second motion detection broach frame matches with the second fixed test broach and forms the second broach electric capacity, the first broach electric capacity and the second broach electric capacity are arranged in parallel, and the first broach electric capacity is positioned at the side near mass.
Further, described angular velocity measurement minor structure is also provided with public electrode lead-in wire, driving input lead, drive feedback lead-in wire, detection signal lead-in wire positive pole, detection signal lead-in wire negative pole; Wherein public electrode lead-in wire is communicated to the first fixed pedestal; Drive input lead to be communicated to the driving fixed fingers of the first driving mechanism and the driving fixed fingers of the second driving mechanism; Drive feedback lead-in wire is communicated to the drive feedback fixed fingers of the first driving mechanism and the drive feedback fixed fingers of the second driving mechanism; Anodal the first fixed test broach of the first testing agency and the second fixed test broach of the second testing agency of being communicated to of detection signal lead-in wire; Detection signal lead-in wire negative pole is communicated to the second fixed test broach of the first testing agency and the first fixed test broach of the second testing agency.
The present invention compared with prior art, its beneficial effect is: (1) two minor structure adopts identical tower structure, be symmetrically arranged, realized gyroscope line motion planar, make whole micro-gyro be subject to the impact of temperature and stress to be close to identical; (2) in each minor structure, adopt folded beam and parallel girder combination that drive part and test section are separated, realized the full decoupled of drive part and test section motion, reduced cross-linked impact; (3) employing folded beam connects two minor structures in left and right, has reduced the phase mutual interference between the part of left and right, makes two minor structures move to the line in opposite directions in driving and detection side when motion, has guaranteed the consistance of two the sub-structure motion frequencies in left and right; (4) by suitable lead-in wire mode, form and detect differential output, not only can eliminate pedestal along detecting axial acceleration noise signal, because the impact of the factors such as temperature also can be reduced to bottom line by differential output, thereby improve the signal to noise ratio (S/N ratio) of whole gyro; (5) adopt the mode that becomes overlapping area drive and detect, can increase the vibration amplitude of gyroscope, can significantly improve the quality factor of driving and sensed-mode, and the sensitivity that improves gyroscope; (6) movable broach is arranged on broach frame, can effectively utilize space, the convenient broach of arranging; (7) folded beam being connected with pedestal all adopts the structure of U-shaped beam, can effectively reduce the unrelieved stress that processing is introduced, and micro-gyro is operated within the scope of the linear elastic deformation of beam, and vibration steadily, increases motion amplitude, has improved detection sensitivity.Design in this invention is also relevant, similar design at home.
Accompanying drawing explanation
Fig. 1 is for being the two mass doublet vibration gyroscope schematic diagram of the micro-full decoupling of silicon of the present invention;
Fig. 2 is the driving mechanism schematic diagram of the two mass doublet vibration gyroscopes of the micro-full decoupling of silicon of the present invention;
Fig. 3 is testing agency's schematic diagram of the two mass doublet vibration gyroscopes of the micro-full decoupling of silicon of the present invention;
Fig. 4 is the signal lead schematic diagram in the two mass doublet vibration gyroscope of the micro-full decoupling of silicon of the present invention lower floor glass pedestal.
Embodiment
Below technical solution of the present invention is elaborated, but protection scope of the present invention is not limited to described embodiment.
Embodiment 1:
In conjunction with Fig. 1, the two mass doublet vibration gyroscopes of the micro-full decoupling of silicon of the present invention, for measuring the input angular velocity perpendicular to micro-gyroscope structure plane.Gyroscope one-piece construction is made up of two parts, comprises and is manufactured with the glass pedestal of electric signal extension line and is placed in the micro-gyro physical construction layer in glass pedestal.Gyroscope upper strata physical construction is made up of a pair of identical the first minor structure 1a, the second minor structure 1b, the first minor structure 1a, the symmetrical distribution of the second minor structure 1b, and connect by the first U-shaped folded beam 2a, the second U-shaped folded beam 2b, minor structure 1a is by the first affixed U-shaped folded beam 6a1, the second affixed U-shaped folded beam 6a2, the 3rd affixed U-shaped folded beam 7a2, the 4th affixed U-shaped folded beam 7a4, the 5th affixed U-shaped folded beam 6a4, the 6th affixed U-shaped folded beam 6a3, the 7th affixed U-shaped folded beam 7a3, the first fixed pedestal 10a1 of the 8th affixed U-shaped folded beam 7a1 and inside, the second fixed pedestal 10a2, the 3rd fixed pedestal 10a3, the 4th fixed pedestal 10a4 is connected, and as shown in the figure, structure is identical for the second minor structure 1b and the first minor structure 1a simultaneously, equally by the first affixed U-shaped folded beam 6b1, the second affixed U-shaped folded beam 6b2, the 3rd affixed U-shaped folded beam 7b2, the 4th affixed U-shaped folded beam 7b4, the 5th affixed U-shaped folded beam 6b4, the 6th affixed U-shaped folded beam 6b3, the 7th affixed U-shaped folded beam 7b3, the first fixed pedestal 10b1 of the 8th affixed U-shaped folded beam 7b1 and inside, the second fixed pedestal 10b2, the 3rd fixed pedestal 10b3, the 4th fixed pedestal 10b4 is connected, and its annexation is identical with the first minor structure.The substrate using in the present embodiment is substrate of glass, also can use other base material such as silicon, polymkeric substance, all fixed pedestals are all arranged on the fixed pedestal bonding point in substrate of glass, make the physical construction part on upper strata unsettled on the glass substrate part of lower floor.
Describe as an example of the first minor structure 1a example below.The first minor structure 1a is by mass 3a, the first driving mechanism 11a1 and the second driving mechanism 11a2, the first 15a1 of testing agency and the second 15a2 of testing agency, the first affixed U-shaped folded beam 6a1, the second affixed U-shaped folded beam 6a2, the 3rd affixed U-shaped folded beam 7a2, the 4th affixed U-shaped folded beam 7a4, the 5th affixed U-shaped folded beam 6a4, the 6th affixed U-shaped folded beam 6a3, the 7th affixed U-shaped folded beam 7a3, the 8th affixed U-shaped folded beam 7a1, first drives parallel girder 8a1, second drives parallel girder 8a2, first detects parallel girder 9a1, second detects parallel girder 9a2 and the first fixed pedestal 10a1, the second fixed pedestal 10a2, the 3rd fixed pedestal 10a3, the 4th fixed pedestal 10a4 composition, the first drive area 4a1 of the first minor structure 1a, the left and right sides that the second drive area 4a2 is arranged in mass 3a, the first surveyed area 5a1, the second surveyed area 5a2 are arranged in the both sides up and down of mass 3a, the first driving mechanism 11a1 of the first drive area 4a1 drives parallel girder 8a2 to be connected with mass 3a by the first driving parallel girder 8a1, second respectively with the second driving mechanism 11a2 of the second drive area 4a2, the first 15a1 of testing agency of the first surveyed area 5a1 detects parallel girder 9a2 by the first detection parallel girder 9a1, second respectively with the second 15a2 of testing agency of the second surveyed area 5a2 and is connected with mass 3a, the first driving mechanism 11a1 is connected to the first fixed pedestal 10a1, the first driving mechanism 11a1 by the first affixed U-shaped beam 6a1 and is connected to the second fixed pedestal 10a2 by the second affixed U-shaped beam 6a2, the second 15a2 of testing agency is connected to the second fixed pedestal 10a2, the second 15a2 of testing agency by the 3rd affixed U-shaped beam 7a2 and is connected to the 3rd fixed pedestal 10a3 by the 4th affixed U-shaped beam 7a4, the second driving mechanism 11a2 by the 5th affixed U-shaped beam 6a4 be connected to the 3rd fixed pedestal 10a3, the second driving mechanism is connected to the 4th fixed pedestal 10a4 by the 6th affixed U-shaped beam 6a3, the first 15a1 of testing agency is connected to the 4th fixed pedestal 10a4, the first 15a1 of testing agency by the 7th affixed U-shaped beam 7a3 and is connected to the first fixed pedestal 10a1 by the 8th affixed U-shaped beam 7a1.
Similarly, have equally for the second minor structure 1b, the first minor structure 1b is by mass 3b, the first driving mechanism 11b1 and the second driving mechanism 11b2, the first 15b1 of testing agency and the second 15b2 of testing agency, the first affixed U-shaped folded beam 6b1, the second affixed U-shaped folded beam 6b2, the 3rd affixed U-shaped folded beam 7b2, the 4th affixed U-shaped folded beam 7b4, the 5th affixed U-shaped folded beam 6b4, the 6th affixed U-shaped folded beam 6b3, the 7th affixed U-shaped folded beam 7b3, the 8th affixed U-shaped folded beam 7b1, first drives parallel girder 8b1, second drives parallel girder 8b2, first detects parallel girder 9b1, second detects parallel girder 9b2 and the first fixed pedestal 10b1, the second fixed pedestal 10b2, the 3rd fixed pedestal 10b3, the 4th fixed pedestal 10b4 composition, the first drive area 4b1 of the first minor structure 1b, the left and right sides that the second drive area 4b2 is arranged in mass 3b, the first surveyed area 5b1, the second surveyed area 5b2 are arranged in the both sides up and down of mass 3b, the first driving mechanism 11b1 of the first drive area 4b1 drives parallel girder 8b2 to be connected with mass 3b by the first driving parallel girder 8b1, second respectively with the second driving mechanism 11b2 of the second drive area 4b2, the first 15b1 of testing agency of the first surveyed area 5b1 detects parallel girder 9b2 by the first detection parallel girder 9b1, second respectively with the second 15b2 of testing agency of the second surveyed area 5b2 and is connected with mass 3b, the first driving mechanism 11b1 is connected to the first fixed pedestal 10b1, the first driving mechanism 11b1 by the first affixed U-shaped beam 6b1 and is connected to the second fixed pedestal 10b2 by the second affixed U-shaped beam 6b2, the second 15b2 of testing agency is connected to the second fixed pedestal 10b2, the second 15b2 of testing agency by the 3rd affixed U-shaped beam 7b2 and is connected to the 3rd fixed pedestal 10b3 by the 4th affixed U-shaped beam 7b4, the second driving mechanism 11b2 by the 5th affixed U-shaped beam 6b4 be connected to the 3rd fixed pedestal 10b3, the second driving mechanism is connected to the 4th fixed pedestal 10b4 by the 6th affixed U-shaped beam 6b3, the first 15b1 of testing agency is connected to the 4th fixed pedestal 10b4, the first 15b1 of testing agency by the 7th affixed U-shaped beam 7b3 and is connected to the first fixed pedestal 10b1 by the 8th affixed U-shaped beam 7b1.
In the first minor structure 1a first drives parallel girder 8a1, second to drive parallel girder 8a2 identical, and one end is connected with mass 3a, and the other end respectively with the first driving mechanism 11a1, the second drives structure 11a2 are connected; Detection parallel girder combination first in minor structure detects parallel girder 9a1, the second detection parallel girder 9a2 is identical, and one end is connected with mass 3a, and the other end respectively with the first 15a1 of testing agency is connected with the second 15a2 of testing agency.First drives parallel girder 8a1, second to drive parallel girder 8a2 combination to detect parallel girder 9a2 combination with the first detection parallel girder 9a1, second isolates mass 3a in the motion of X-axis and Y direction.The first driving mechanism 11a1, the second driving mechanism 11a2 are limited in X-direction motion, and the first 15a1 of testing agency, the second 15a2 of testing agency in minor structure is limited in Y direction motion.
In the time of work, the first driving mechanism 11a1, the second driving mechanism 11a2 drive parallel girder 8a1, second to drive parallel girder 8a2 to drive mass 3a vibration back and forth in X-direction by first under the effect of input drive signal.Now, if there is turning rate input in Z-direction, the Coriolis force that mass 3a produces by be subject to X axis vibration in Y direction time so and produce forced vibration in the Y direction.In the time that the vibration on directions X is constant, in Y-direction, the Coriolis force of forced vibration is proportional to the input angular velocity in Z-direction, thereby can learn the input angular velocity size in Z-direction by the amplitude of the first 15a1 of testing agency, the second forced vibration of the 15a2 of testing agency measurement quality piece 3a in Y-axis.
The driving mechanism of micro-gyro as shown in Figure 2, by the first driving mechanism 11a1, the second driving mechanism 11a2, the first framework 14a1, the second framework 14a2; The first driving mechanism 11a1, the second driving mechanism 11a2 are arranged in the mass 3a left and right sides and connect by the first framework 14a1, the second framework 14a2.The first driving mechanism and the second driving mechanism are symmetrical arranged, but because two driving mechanisms will produce driving force in the same way to mass, therefore in the first driving mechanism and the second driving mechanism that arrange as shown in Figure 2, be the comb structure on right side as driving comb, the comb structure in left side regulates driving signal frequency as drive feedback broach feedback signal to the circuit that drives signal to generate, so that whole device is in optimum Working.Illustrate as an example of the first driving mechanism 11a1 example below, in the present embodiment, the first driving mechanism 11a1 comprises upper and lower two identical broach shelf structures, but also a broach shelf structure can be only set and can not affect realization of the present invention.Below take the broach shelf structure on top as example: as shown in Figure 2, each broach frame is arranged in parallel and is parallel to one side that the square at mass place approaches, be followed successively by drive feedback movable comb braces 12a1, drive feedback fixed fingers 13a1 from drawing near apart from mass, drive fixed fingers 13a2, drive movable comb braces 12a2, wherein, drive fixed fingers 13a2 to be arranged at and drive 10a7 on fixed pedestal, drive feedback fixed fingers 13a1 is arranged on drive feedback fixed pedestal 10a5.By apply the alternating voltage with direct current biasing on driving fixed fingers 13a2, adopt static type of drive to drive mass 3a to do intermittent control shaking, detect actuation movement condition feedback by drive feedback fixed fingers 13a1 and regulate driving circuit.Drive feedback movable comb braces 13a5, drive feedback fixed fingers 12a5, driving fixed fingers 12a6, driving movable comb braces 13a6, driving fixed pedestal 10a8 and the drive feedback fixed pedestal 10a6 of its middle and lower part broach shelf structure arrange equally.The drive feedback movable comb braces 12a3 of the top broach frame in the second driving mechanism 11a2, drive feedback fixed fingers 13a3, drive fixed fingers 13a4, drive movable comb braces 12a4, drive 10a11 on fixed pedestal, the drive feedback movable comb braces 12a7 of drive feedback fixed pedestal 10a9 and bottom broach frame, drive feedback fixed fingers 13a7, drive fixed fingers 13a8, drive movable comb braces 12a8, drive fixed pedestal 10a12 and drive feedback fixed pedestal 10a10 to arrange too.
The second minor structure 1b is by the first driving mechanism 11b1, the second driving mechanism 11b2, the first framework 14b1, the second framework 14b2; The first driving mechanism 11b1, the second driving mechanism 11b2 are arranged in the mass 3b left and right sides and connect by the first framework 14b1, the second framework 14b2.The first driving mechanism and the second driving mechanism are symmetrical arranged, but because two driving mechanisms will produce driving force in the same way to mass, therefore in the first driving mechanism and the second driving mechanism that arrange as shown in Figure 2, be the comb structure on right side as driving comb, the comb structure in left side regulates driving signal frequency as drive feedback broach feedback signal to the circuit that drives signal to generate, so that whole device is in optimum Working.Illustrate as an example of the first driving mechanism 11b1 example below, in the present embodiment, the first driving mechanism 11b1 comprises upper and lower two identical broach shelf structures, but also a broach shelf structure can be only set and can not affect realization of the present invention.Below take the broach shelf structure on top as example: as shown in Figure 2, each broach frame is arranged in parallel and is parallel to one side that the square at mass place approaches, be followed successively by drive feedback movable comb braces 12b1, drive feedback fixed fingers 13b1 from drawing near apart from mass, drive fixed fingers 13b2, drive movable comb braces 12b2, wherein, drive fixed fingers 13b2 to be arranged at and drive 10b7 on fixed pedestal, drive feedback fixed fingers 13b1 is arranged on drive feedback fixed pedestal 10b5.By apply the alternating voltage with direct current biasing on driving fixed fingers 13b2, adopt static type of drive to drive mass 3b to do intermittent control shaking, detect actuation movement condition feedback by drive feedback fixed fingers 13b1 and regulate driving circuit.In order to realize the anti-phase driving of two mass 3a, 3b, drive on fixed fingers 13a2 and 13b2 and apply anti-phase AC signal.Drive feedback movable comb braces 13b5, the drive feedback fixed fingers 12b5 of its middle and lower part broach shelf structure, drive fixed fingers 12b6, drive movable comb braces 13b6, drive 10b8 and drive feedback fixed pedestal 10b6 on fixed pedestal to arrange equally.The drive feedback movable comb braces 12b3 of the top broach frame in the second driving mechanism 11b2, drive feedback fixed fingers 13b3, drive fixed fingers 13b4, drive movable comb braces 12b4, drive fixed pedestal 10b11, the drive feedback movable comb braces 12b7 of drive feedback fixed pedestal 10b9 and bottom broach frame, drive feedback fixed fingers 13b7, drive fixed fingers 13b8, drive movable comb braces 12b8, drive fixed pedestal 10b12 and drive feedback fixed pedestal 10b10 to arrange too.
The testing agency of micro-gyro as shown in Figure 3, the testing agency of the first minor structure 1a is positioned at the first surveyed area 5a1 and the second surveyed area 5a2, is respectively the first 15a1 of testing agency that is positioned at the first surveyed area 5a1 and the second 15a2 of testing agency that is positioned at the second surveyed area 5a2; The first 15a1 of testing agency and the second 15a2 of testing agency are arranged in the upper and lower both sides of mass 3a.The first 15a1 of testing agency is with second the 15a2 of testing agency is same arranges, and in the present embodiment, the first 15a1 of testing agency is arranged to the identical broach shelf structure in left and right as shown in Figure 3.In the middle of reality, also one this kind broach shelf structure can be only set and not affect realization of the present invention.Wherein the broach shelf structure of left part comprises four parallel broach framves, be parallel to one side that the square at mass place approaches, from the close-by examples to those far off be followed successively by the first motion detection broach frame 16a2 apart from mass, the first fixed test broach 17a2, the second fixed test broach 17a1, the second motion detection broach frame 16a1, wherein the first fixed test broach 17a2 is arranged on the first detection comb fixed pedestal 10a15, the second fixed test broach 17a1 is arranged on the second detection comb fixed pedestal 10a13, wherein the first motion detection broach frame 16a2 matches with the first fixed test broach 17a2 and forms the first broach electric capacity, the second motion detection broach frame 16a1 matches with the second fixed test broach 17a1 and forms the second broach electric capacity, the first broach electric capacity is positioned at the side of the second broach electric capacity near mass.The broach shelf structure on right side is symmetrical arranged, and is provided with equally the first detection comb fixed pedestal 10a16 and the second detection comb fixed pedestal 10a14.Be provided with equally the first motion detection broach frame 16a3, the first fixed test broach 17a3, the second fixed test broach 17a4, the second motion detection broach frame 16a4, the first detection comb fixed pedestal 10a17 and the second detection comb fixed pedestal 10a19 of left side broach shelf structure for the second 15a2 of testing agency, the broach shelf structure on right side is symmetrical arranged, and is provided with equally the first detection comb fixed pedestal 10a18 and the second detection comb fixed pedestal 10a20.
Be positioned at the first surveyed area 5b1 and the second surveyed area 5b2 for the testing agency of the second minor structure 1b, be respectively the first 15b1 of testing agency that is positioned at the first surveyed area 5b1 and the second 15b2 of testing agency that is positioned at the second surveyed area 5b2, the first 15b1 of testing agency and the second 15b2 of testing agency are arranged in the upper and lower both sides of mass 3b.The first 15b1 of testing agency is with second the 15b2 of testing agency is same arranges, and in the present embodiment, the first 15b1 of testing agency is arranged to the identical broach shelf structure in left and right as shown in Figure 3.In the middle of reality, also one this kind broach shelf structure can be only set and not affect realization of the present invention.Wherein the broach shelf structure of left part comprises four parallel broach framves, be parallel to one side that the square at mass place approaches, from the close-by examples to those far off be followed successively by the first motion detection broach frame 16b2 apart from mass, the first fixed test broach 17b2, the second fixed test broach 17b1, the second motion detection broach frame 16b1, wherein the first fixed test broach 17b2 is arranged on the first detection comb fixed pedestal 10b15, the second fixed test broach 17b1 is arranged on the second detection comb fixed pedestal 10b13, wherein the first motion detection broach frame 16b2 matches with the first fixed test broach 17b2 and forms the first broach electric capacity, the second motion detection broach frame 16b1 matches with the second fixed test broach 17b1 and forms the second broach electric capacity, the first comb teeth part is positioned at the side of the second comb teeth part near mass.The broach shelf structure on right side is symmetrical arranged, and is provided with equally the first detection comb fixed pedestal 10b16 and the second detection comb fixed pedestal 10b14.Be provided with equally the first motion detection broach frame 16b3, the first fixed test broach 17b3, the second fixed test broach 17b4, the second motion detection broach frame 16b4, the first detection comb fixed pedestal 10b17 and the second detection comb fixed pedestal 10b19 of left side broach shelf structure for the second 15b2 of testing agency, the broach shelf structure on right side is symmetrical arranged, and is provided with equally the first detection comb fixed pedestal 10b18 and the second detection comb fixed pedestal 10b20.
Glass pedestal as shown in Figure 4, comprises signal lead and metal silicon/glass bonding point.Wherein the signal lead of the first minor structure 1a comprises public electrode lead-in wire 19a, drives input lead 20a1, drive feedback lead-in wire 21a1, detection signal go between anodal 22a1, detection signal lead-in wire negative pole 22a2, the link as shown in the figure of each lead-in wire, and public electrode lead-in wire is communicated to the first fixed pedestal 18a1; Drive input lead 20a1 to be communicated to driving fixed fingers 13a2 and the 12a6 of the first driving mechanism; Drive feedback lead-in wire 21a1 is communicated to drive feedback fixed fingers 13a1 and the 12a5 of the first driving mechanism; The detection signal anodal 22a1 that goes between is communicated to the first fixed test broach 17a2 of the first testing agency and the second fixed test broach 17a4 of the second testing agency; Detection signal lead-in wire negative pole 22a2 is communicated to the second fixed test broach 17a1 of the first testing agency and the first fixed test broach 17a3 of the second testing agency.Metal silicon/glass bonding point comprises the first fixed pedestal bonding point 18a1, the second fixed pedestal bonding point 18a2, the 3rd fixed pedestal bonding point 18a3, the 4th fixed pedestal bonding point 18a4, drive fixed pedestal bonding point 18a7, drive fixed pedestal bonding point 18a8, drive fixed pedestal bonding point 18a11, drive fixed pedestal bonding point 18a12, drive feedback fixed pedestal bonding point 18a5, drive feedback fixed pedestal bonding point 18a6, drive feedback fixed pedestal bonding point 18a9, drive feedback fixed pedestal bonding point 18a10, the second detection comb fixed pedestal bonding point 18a13, the second detection comb fixed pedestal bonding point 18a14, the first detection comb fixed pedestal bonding point 18a15, the first detection comb fixed pedestal bonding point 18a16, the first detection comb fixed pedestal bonding point 18a17, the first detection comb fixed pedestal bonding point 18a18, the second detection comb fixed pedestal bonding point 18a19, the second detection comb fixed pedestal bonding point 18a20.
The signal lead of the second minor structure 1b comprises public electrode lead-in wire 19b, drives input lead 21b1, drive feedback lead-in wire 20b1, detection signal go between anodal 22b1, detection signal lead-in wire negative pole 22b2, the link as shown in the figure of each lead-in wire, and public electrode lead-in wire is communicated to the 3rd fixed pedestal 18b3; Drive input lead 21b1 to be communicated to driving fixed fingers 13b2 and the 12b6 of the first driving mechanism; Drive feedback lead-in wire 20b1 is communicated to drive feedback fixed fingers 13b1 and the 12b5 of the first driving mechanism; The detection signal anodal 22b1 that goes between is communicated to the second fixed test broach 17b1 of the first testing agency and the first fixed test broach 17b3 of the second testing agency; Detection signal lead-in wire negative pole 22b2 is communicated to the first fixed test broach 17b2 of the first testing agency and the second fixed test broach 17b4 of the second testing agency.Metal silicon/glass bonding point comprises the first fixed pedestal bonding point 18b1, the second fixed pedestal bonding point 18b2, the 3rd fixed pedestal bonding point 18b3, the 4th fixed pedestal bonding point 18b4, drive fixed pedestal bonding point 18b7, drive fixed pedestal bonding point 18b8, drive fixed pedestal bonding point 18b11, drive fixed pedestal bonding point 18b12, drive feedback fixed pedestal bonding point 18b5, drive feedback fixed pedestal bonding point 18b6, drive feedback fixed pedestal bonding point 18b9, moving feedback fixed pedestal bonding point 18b10, the second detection comb fixed pedestal bonding point 18b13, the second detection comb fixed pedestal bonding point 18b14, the first detection comb fixed pedestal bonding point 18b15, the first detection comb fixed pedestal bonding point 18b16, the first detection comb fixed pedestal bonding point 18b17, the first detection comb fixed pedestal bonding point 18b18, the second detection comb fixed pedestal bonding point 18b19, the second detection comb fixed pedestal bonding point 18b20.
Each fixed pedestal: 10a1, 10a2, 10a3, 10a4, 10a5, 10a6, 10a7, 10a8, 10a9, 10a10, 10a11, 10a12, 10a13, 10a14, 10a15, 10a16, 10a17, 10a18, 10a19, 10a20, 10b1, 10b2, 10b3, 10b4, 10b5, 10b6, 10b7, 10b8, 10b9, 10b10, 10b11, 10b12, 10b13, 10b14, 10b15, 10b16, 10b17, 10b18, 10b19, 10b20 is corresponding keys chalaza 18a1 respectively, 18a2, 18a3, 18a4, 18a5, 18a6, 18a7, 18a8, 18a9, 18a10, 18a11, 18a12, 18a13, 18a14, 18a15, 18a16, 18a17, 18a18, 18a19, 18a20, 18b1, 18b2, 18b3, 18b4, 18b5, 18b6, 18b7, 18b8, 18b9, 18b10, 18b11, 18b12, 18b13, 18b14, 18b15, 18b16, 18b17, 18b18, 18b19, 18b20 is connected.
The two mass doublet vibration gyroscopes of the micro-full decoupling of silicon of the present invention, adopt monolateral static to drive, the working method that differential capacitor detects, on the fixed drive broach of driving mechanism, apply after the AC drive voltage with direct current biasing, produce alternation driving force, under the effect of alternation driving force, drive the first driving mechanism 11a1, the 21 driving mechanism 11a2 drives parallel girder 8a1 by first, second drives parallel girder 8a2 to drive mass 3a to do simple harmonic quantity line vibration in opposite directions along directions X, drive the first driving mechanism 11b1, the 21 driving mechanism 11b2 drives parallel girder 8b1 by first, second drives parallel girder 8b2 to drive mass 3b to do simple harmonic quantity line vibration in opposite directions along directions X, and now the first 15a1 of testing agency and the second 15a2 of testing agency, because the driving direction that is strapped in of the 8th affixed U-shaped folded beam 7a1, the 3rd affixed U-shaped beam 7a2, the 7th affixed U-shaped folded beam 7a3, the 4th affixed U-shaped folded beam 7a4 keeps static, have realized driving the decoupling zero to detecting, in the time that gyroscope has the extraneous input angle speed ω z around Z axis, according to the right-hand rule, mass 3a is subject to the effect of Corioli's acceleration in output shaft Y-axis, under the effect of Ge Shi inertial force, mass 3a does simple harmonic quantity line vibration in opposite directions along sensitive axes Y-axis, and mass 3b does contrary simple harmonic quantity line vibration along sensitive axes Y-axis with mass 3a.Detecting parallel girder 9a2 by the first detection parallel girder 9a1 and second drives the first 15a1 of testing agency and the second 15a2 of testing agency to do simple harmonic quantity line vibration in opposite directions along Y-direction, and now the first drive part 4a1, the second drive part 4a2, because the constraint that is subject to the first affixed U-shaped folded beam 6a1, the second affixed U-shaped beam 6a2, the 6th affixed U-shaped folded beam 6a3, the 5th affixed U-shaped folded beam 6a4 keeps static, have realized and have detected the decoupling zero to driving; Fixed test broach the second fixed test broach 17a1, the first fixed test broach 17a2, the first fixed test broach 17a3, the second fixed test broach 17a4 by the first 15a1 of testing agency and the second 15a2 of testing agency after electronic circuit is processed, can obtain voltage signal by this simple harmonic quantity line vibration.The principle of the second minor structure 1b is also identical.Output voltage signal is the poor of minor structure 3a and 3b output voltage signal, and the size of output voltage signal is proportional to the size of input angle speed.Compare the phase relation of output voltage signal and pumping signal by follow-up phase detector, can distinguish the direction of input angle speed.
As mentioned above, although represented and explained the present invention with reference to specific preferred embodiment, it shall not be construed as the restriction to the present invention self.Not departing under the spirit and scope of the present invention prerequisite of claims definition, can make in the form and details various variations to it.
Claims (6)
1. the two mass doublet vibration gyroscopes of the micro-full decoupling of silicon, is characterized in that, comprise pedestal, the first minor structure (1a), the second minor structure (1b) and minor structure coupling arrangement, between the first minor structure (1a) and the second minor structure (1b), connect by minor structure coupling arrangement, described the first minor structure (1a) and the second minor structure (1b) are angular velocity measurement minor structure, and described angular velocity measurement minor structure comprises mass (3a), be fixed on the first fixed pedestal (10a1) on pedestal, be fixed on the second fixed pedestal (10a2) on pedestal, be fixed on the 3rd fixed pedestal (10a3) on pedestal, be fixed on the 4th fixed pedestal (10a4) on pedestal, the first driving mechanism (11a1), the second driving mechanism (11a2), the first testing agency (15a1), the second testing agency (15a2), first drives parallel girder (8a1), second drives parallel girder (8a2), first detects parallel girder (9a1), second detects parallel girder (9a2), the first affixed U-shaped folded beam (6a1), the second affixed U-shaped folded beam (6a2), the 3rd affixed U-shaped folded beam (7a2), the 4th affixed U-shaped folded beam (7a4), the 5th affixed U-shaped folded beam (6a4), the 6th affixed U-shaped folded beam (6a3), the 7th affixed U-shaped folded beam (7a3), the 8th affixed U-shaped folded beam (7a1), the first driving mechanism (11a1) by the first affixed U-shaped beam (8a1) be connected to the first fixed pedestal (10a1), the first driving mechanism (11a1) is connected to the second fixed pedestal (10a2) by the second affixed U-shaped beam (6a2), the second testing agency (15a2) by the 3rd affixed U-shaped beam (7a2) be connected to the second fixed pedestal (10a2), the second testing agency (15a2) is connected to the 3rd fixed pedestal (10a3) by the 4th affixed U-shaped beam (7a4), the second driving mechanism (11a2) by the 5th affixed U-shaped beam (6a4) be connected to the 3rd fixed pedestal (10a3), the second driving mechanism is connected to the 4th fixed pedestal (10a4) by the 6th affixed U-shaped beam (6a3), the first testing agency (15a1) by the 7th affixed U-shaped beam (7a3) be connected to the 4th fixed pedestal (10a4), the first testing agency (15a1) is connected to the first fixed pedestal (10a1) by the 8th affixed U-shaped beam (7a1), the first driving mechanism (11a1) is arranged on a side of mass (3a), the second driving mechanism (11a2) is arranged on the relative opposite side of mass (3a), between the first driving mechanism (11a1) and mass (3a), drive parallel girder (8a1) to be connected by first, between the second driving mechanism (11a2) and mass (3a), drive parallel girder (8a2) to be connected by second, to drive this mass (3a) in upper vibration from a driving direction, the first testing agency (15a1) is arranged on a side of mass (3a), the second testing agency (15a2) is arranged on the relative opposite side of mass (3a), between the first testing agency (15a1) and mass (3a), detecting parallel girder (9a1) by first is connected, between the second testing agency (15a2) and mass (3a), detect parallel girder (9a2) by second and be connected, to detect the vibration of mass (3a) at the mass perpendicular on driving direction (3a).
2. the two mass doublet vibration gyroscopes of the micro-full decoupling of silicon according to claim 1, it is characterized in that, described minor structure coupling arrangement connects and comprises the first U-shaped folded beam (2a) and the second U-shaped folded beam (2b), the first minor structure (1a) and the second minor structure (1b) mutually against, be respectively arranged with in both next-door neighbours' the top and bottom of driving mechanism the first U-shaped folded beam (2a) with the second U-shaped folded beam (2b) to be connected the first minor structure (1a) and the second minor structure (1b).
3. the two mass doublet vibration gyroscopes of the micro-full decoupling of silicon according to claim 1, it is characterized in that, described the first fixed pedestal (10a1), the second fixed pedestal (10a2), the 3rd fixed pedestal (10a3), the 4th fixed pedestal (10a4) is arranged at respectively one foursquare four jiaos, mass (3a) is arranged at this foursquare central authorities, the first driving mechanism (11a1), the first testing agency (15a1), the second driving mechanism (11a2), the second testing agency (15a2) is arranged at respectively the outside on these square four limits, wherein the first driving mechanism (11a1) and the second driving mechanism (11a2) are arranged at the outside on relative both sides, the first testing agency (15a1) and the second testing agency (15a2) are arranged at the outside on relative other both sides.
4. the two mass doublet vibration gyroscopes of the micro-full decoupling of silicon according to claim 1, it is characterized in that, between the first driving mechanism (11a1) and the second driving mechanism (11a2), be connected with the second framework (14a2) by the first framework (14a1) respectively, described the first driving mechanism (11a1) and the second driving mechanism (11a2) are micro drives capacitor mechanism, described micro drives capacitor mechanism comprises driving movable comb braces (12a2), drive feedback movable comb braces (12a1), be arranged at the driving fixed pedestal (10a7) on pedestal, be arranged at the driving fixed fingers (13a2) that drives (10a7) on fixed pedestal, be arranged at the drive feedback fixed pedestal (10a5) on pedestal and be arranged at the drive feedback fixed fingers (13a1) on drive feedback fixed pedestal (10a5).
5. the two mass doublet vibration gyroscopes of the micro-full decoupling of silicon according to claim 4, it is characterized in that, described the first testing agency (15a1) and the second testing agency (15a2) are miniature Detection capacitance mechanism, described miniature Detection capacitance mechanism comprises the first motion detection broach frame (16a2), the second motion detection broach frame (16a1), the first detection comb fixed pedestal (10a15) and be arranged on the first fixed test broach (17a2) on the first detection comb fixed pedestal (10a15), the second detection comb fixed pedestal (10a13) and be arranged on the second fixed test broach (17a1) on the second detection comb fixed pedestal (10a13), wherein the first motion detection broach frame (16a2) matches with the first fixed test broach (17a2) and forms the first broach electric capacity, the second motion detection broach frame (16a1) matches with the second fixed test broach (17a1) and forms the second broach electric capacity, the first broach electric capacity is positioned at the side of the second broach electric capacity near mass.
6. the two mass doublet vibration gyroscopes of the micro-full decoupling of silicon according to claim 5, it is characterized in that, described angular velocity measurement minor structure is also provided with public electrode lead-in wire (19a), driving input lead (20a1), drive feedback lead-in wire (21a1), detection signal lead-in wire anodal (22a1), detection signal lead-in wire negative pole (22a2); Wherein public electrode lead-in wire is communicated to the first fixed pedestal (18a1); Drive input lead (20a1) to be communicated to the driving fixed fingers (13a2) of the first driving mechanism and (12a6); Drive feedback lead-in wire (21a1) is communicated to the drive feedback fixed fingers (13a1) of the first driving mechanism and (12a5); Detection signal lead-in wire anodal (22a1) is communicated to the first fixed test broach (17a2) of the first testing agency and the second fixed test broach (17a4) of the second testing agency; Detection signal lead-in wire negative pole (22a2) is communicated to the second fixed test broach (17a1) of the first testing agency and the first fixed test broach (17a3) of the second testing agency.
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104236535A (en) * | 2014-09-04 | 2014-12-24 | 东南大学 | Dual-mass decoupling silicon microgyroscope based on flexible connection |
CN104567849A (en) * | 2014-12-26 | 2015-04-29 | 东南大学 | Silicon micromechanical line vibrating gyroscope and bandwidth expanding method thereof |
CN104833350A (en) * | 2015-04-24 | 2015-08-12 | 东南大学 | Bionic hair sensor for being sensitive to flow velocity and accelerated velocity vectors and detection method thereof |
CN105157726A (en) * | 2015-08-06 | 2015-12-16 | 东南大学 | Device and method for inhibiting mechanical coupling error of dual-mass silicon microgyroscope |
CN105466406A (en) * | 2015-12-28 | 2016-04-06 | 南京理工大学 | Silicon micromechanical vibrating gyroscope of I-shaped structure |
WO2024087324A1 (en) * | 2022-10-28 | 2024-05-02 | 瑞声开泰科技(武汉)有限公司 | Orthogonally arranged multi-mass mems gyroscope |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201909632U (en) * | 2010-11-23 | 2011-07-27 | 东南大学 | Micro electro mechanical system (MEMS) gyroscope |
CN103245340A (en) * | 2012-02-01 | 2013-08-14 | 苏州敏芯微电子技术有限公司 | Single-chip tri-axial gyroscope |
US20130270659A1 (en) * | 2012-03-30 | 2013-10-17 | Kyoto University | Angular velocity sensor |
-
2014
- 2014-04-22 CN CN201410164249.6A patent/CN103900548B/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201909632U (en) * | 2010-11-23 | 2011-07-27 | 东南大学 | Micro electro mechanical system (MEMS) gyroscope |
CN103245340A (en) * | 2012-02-01 | 2013-08-14 | 苏州敏芯微电子技术有限公司 | Single-chip tri-axial gyroscope |
US20130270659A1 (en) * | 2012-03-30 | 2013-10-17 | Kyoto University | Angular velocity sensor |
Non-Patent Citations (1)
Title |
---|
殷勇等: "一种双质量硅微陀螺仪", 《中国惯性技术学报》 * |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104236535A (en) * | 2014-09-04 | 2014-12-24 | 东南大学 | Dual-mass decoupling silicon microgyroscope based on flexible connection |
CN104236535B (en) * | 2014-09-04 | 2017-01-18 | 东南大学 | Dual-mass decoupling silicon microgyroscope based on flexible connection |
CN104567849A (en) * | 2014-12-26 | 2015-04-29 | 东南大学 | Silicon micromechanical line vibrating gyroscope and bandwidth expanding method thereof |
CN104567849B (en) * | 2014-12-26 | 2017-08-25 | 东南大学 | A kind of silicon micro mechanical linearly coupled formula gyro and its bandwidth broadning method |
CN104833350A (en) * | 2015-04-24 | 2015-08-12 | 东南大学 | Bionic hair sensor for being sensitive to flow velocity and accelerated velocity vectors and detection method thereof |
CN105157726A (en) * | 2015-08-06 | 2015-12-16 | 东南大学 | Device and method for inhibiting mechanical coupling error of dual-mass silicon microgyroscope |
CN105466406A (en) * | 2015-12-28 | 2016-04-06 | 南京理工大学 | Silicon micromechanical vibrating gyroscope of I-shaped structure |
WO2017113911A1 (en) * | 2015-12-28 | 2017-07-06 | 南京理工大学 | Silicon-based micromechanical vibratory gyroscope with i-shaped structure |
CN105466406B (en) * | 2015-12-28 | 2019-01-18 | 南京理工大学 | The Technology of Silicon Micromechanical Vibrating Gyroscope of I-shaped structure |
US10876838B2 (en) | 2015-12-28 | 2020-12-29 | Nanjing University Of Science And Technology | Silicon-based micro-machined vibratory gyroscope with an I-shaped structure |
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