CN101017088A - Internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscope - Google Patents
Internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscope Download PDFInfo
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- CN101017088A CN101017088A CN 200710037893 CN200710037893A CN101017088A CN 101017088 A CN101017088 A CN 101017088A CN 200710037893 CN200710037893 CN 200710037893 CN 200710037893 A CN200710037893 A CN 200710037893A CN 101017088 A CN101017088 A CN 101017088A
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Abstract
This invention relates to one inner stable hanging ring rotor micro rotation top in micro machine system technique field, wherein, setting the stable float coil, rotation coil and sensor electrode onto base to form fix connection and base; micro rotor is floating one the base under electronic magnetic force and the ring rotor is under function of hanging coil force to get stable hanging outside rotation coil to generate rotation magnetic field; micro rotor is under rotation magnetic field to generate rotation torque for high speed rotation through sensor electrode.
Description
Technical field
What the present invention relates to is a kind of gyro of field of micro electromechanical technology, specifically is a kind of internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscope.
Background technology
In the time of two more than ten years in the past, the micro machining process of domestic and international application silicon or body Micrometer-Nanometer Processing Technology have processed little oscillation gyro of multiple structure, but little for various reasons oscillation gyro is difficult to reach the high precision of traditional gyro.The nineties in last century, people such as Shearwood have proposed a kind of electromagnetic suspension micro-rotary gyro, the electromagnetic suspension micro-rotary gyro is made up of major parts such as planar coil, induction electrode and little rotors, and wherein planar coil is divided into three kinds of suspended coil, revolving coil and ballast coils again according to its function difference.The electromagnetic suspension micro-rotary gyro relies on electromagnetic induction principle and electromagnetic force theory to be suspended and rotates, the planar coil top is placed with little rotor, suspended coil is positioned at the position at close center, near suspended coil is revolving coil, revolving coil can be divided into heterogeneous, little rotor is in the rotating magnetic field, and what be in the stator coil outermost is ballast coil, and also distributing between the stator coil has the sensing capacitance electrode.
Find that through literature search U.S. Patent number is to prior art: 5955800, name is called: suspension system (Leivitation Systems).Mentioning this system in this patent literary composition is that following components is formed: a) maximum gauge is the high conductivity body of 1500 μ m; B) suspending power generation device; C) micro device that rotor is rotated.In the little gyro of this electromagnetic suspension rotor, suspended coil, revolving coil, ballast coil are cascaded, and suspended coil is the most inboard, the revolving coil position that mediates, and ballast coil is positioned at outermost.It utilizes the electromagnetic field edge effect of ballast coil in little rotor outside, produces stable suspersion.There is following deficiency in planar coil tandem electromagnetic suspension micro-rotary gyro: 1. need the high-frequency current by two kinds of different frequencies in the tandem coil, this has increased the complicacy of control circuit; 2. stable suspersion drives electromagnetic field and rotates the driving electromagnetic field and spatially overlaps, and has therefore increased the phase mutual interference between them; 3. rotary electromagnetic field all has distribution on the entire radius length direction, but the rotary electromagnetic field of radius larger part plays the effect of the overwhelming majority.This system is 520 microns at diameter, and thickness is 12 microns rotor, and the maximum (top) speed that obtains is 1000 commentaries on classics per minutes.This rotating speed does not reach the requirement of the little gyro of high precision far away.In order to obtain high-precision gyro, need the structure of novel stator coil, thereby further improve the suspension stability and the rotation rotating speed of little rotor.
Summary of the invention
The objective of the invention is to overcome deficiency of the prior art, a kind of internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscope is provided.Adopt the coil separate type, the stable suspersion coil is placed on the position of stator near central authorities, utilize of the edge effect of ballast coil electromagnetic field, produce stable suspersion in the ring-shaped rotor inboard.Revolving coil is placed on the outermost of stator, has increased the space possessive volume and the electromagnetic force opplied moment of revolving coil electromagnetic field like this, thereby increased the rotary torsion square of little rotor.New structure can improve the rotating speed of little rotor greatly, has solved disadvantages of background technology.
The present invention is achieved by the following technical solutions, the present invention includes: little rotor, stable suspersion coil, revolving coil, sensing electrode, matrix.The stable suspersion coil is made up of stable suspersion coil outer ring, stable suspersion coil inner ring, connecting line three parts.Annexation is: stable suspersion coil inner ring, stable suspersion coil outer ring, connecting line, sensing electrode, revolving coil all are located on the matrix, formation is fixedly connected with matrix, little rotor at electromagnetic force effect low suspension above matrix, little rotor is annular, and stable suspersion coil inner ring is connected by connecting line with stable suspersion coil outer ring.
Among the present invention, adopt the coil separate type, stable suspersion coil and revolving coil separate separately, and this structure has not only weakened the interference between two kinds of coil electromagnetism fields, and the electric current in two coils can control separately, and this has reduced the design difficulty of control circuit.In structure of the present invention, little rotor is a kind of cirque structure, suspending stabilized coil is placed on the most inboard, utilizes the edge effect of the inboard electromagnetic field of annular little rotor, obtains the stable suspersion of little rotor.This structure is that revolving coil is at the outside of stator vacating space, the revolving coil sensing electrode can be placed on the outside of little rotor, this structure has increased the active area of rotary electromagnetic field, also increased simultaneously the radius of action of rotating electromagnetic power, thereby increase the rotary torsion square, and then can increase the rotating speed of little rotor.It has also increased the pole plate area of sensing electrode, can increase the accuracy of detection of sensing electrode like this.
At present, the little gyro of MEMS all is the little oscillation gyro that adopts the Corioli's acceleration effect mostly.This slightly the gyro weak point be that measuring accuracy is not high, be unable to catch up with traditional large scale gyro far away, thereby limited applying of these gyros.The interior steady suspension ring-shaped micro-rotating gyroscope that the present invention proposes places the stable suspersion coil inboard of stator, revolving coil is arranged on the outside of stator, this structure can improve the rotary torque of little rotor greatly, and then improves the rotating speed of little rotor, thereby obtains the little gyro of high-precision MEMS.The little gyro of the high precision that the present invention obtains can be generalized to the application of the little gyro of MEMS the high-precision inertial navigation system that requires of Aeronautics and Astronautics, navigation and other.
Description of drawings
Fig. 1 is a general structure synoptic diagram of the present invention;
Fig. 2 is the stable suspersion vertical view of the little gyro of the present invention;
Fig. 3 is the revolving coil of the little gyro of the present invention and the view of sensing electrode;
Fig. 4 is the space view of the little rotor of the little teetotum of the present invention.
Embodiment
Below in conjunction with accompanying drawing embodiments of the invention are elaborated: present embodiment has provided detailed embodiment and process being to implement under the prerequisite with the technical solution of the present invention, but protection scope of the present invention is not limited to following embodiment.
As shown in Figure 1, present embodiment comprises: little rotor 1, stable suspersion coil 2, revolving coil 3, sensing electrode 4, matrix 5.As shown in Figure 2, stable suspersion coil 2 is made up of stable suspersion coil outer ring 6, stable suspersion coil inner ring 7, connecting line 8 three parts.Annexation is: stable suspersion coil 2, revolving coil 3, sensing electrode 4 all are located on the matrix 5, form fixed connection with matrix 5, little rotor 1 at electromagnetic force effect low suspension above matrix 5, little rotor 1 is annular, and stable suspersion coil outer ring 6 is connected by connecting line 8 with stable suspersion coil inner ring 7.
As shown in Figure 2, on matrix 5, be distributed with stable suspersion coil outer ring 6, connecting line 8 and stable suspersion coil inner ring 7 from outside to inside, the three forms the multi-turn stable suspersion coil 2 of a sealing, and totally 4 of stable suspersion coils 2 distribute in a circumferential direction axisymmetricly.The lead-in wire of stable suspersion coil 2 adopts the buried regions fabrication techniques at bottom, draws from the bottom.Stable suspersion coil 2 sizes are determined jointly that by the size of little rotor 1 stable suspersion coil outer ring 6 diameters are bigger than the internal diameter of the little rotor 1 of annular, and stable suspersion coil inner ring 7 diameters are littler than annular little rotor 1 internal diameter.When passing through high-frequency current in stable suspersion coil 2, according to Theory of Electromagnetic Field, the little rotor 1 that is in stable suspersion coil 2 tops will be subjected to the effect of induced electricity magnetic force.The distribution of electromagnetic force that stable suspersion coil inner ring 7 electromagnetic fields induce on little rotor 1 is in the inside edge of little rotor 1, and outside being tilted to.The electromagnetic force that 6 magnetic fields, stable suspersion coil outer ring produce is positioned at little rotor 1 inside, and is close to the rotational symmetry distribution.The resultant direction of the distribution electromagnetic force that stable suspersion coil 2 produces upwards makes that little rotor 1 is suspended.When the center of little rotor 1 was in the center of matrix 5, the cross component force of distribution electromagnetic force was cancelled out each other, and made a concerted effort for straight up.When there was off-centre in little rotor 1 relative matrix 5 centers, the cross component force of electromagnetic force was no longer offset, and the side force direction of generation is pointed to rotor center, makes that little rotor 1 is not dished out, and finally obtains stable suspension.
As shown in Figure 3, be distributed with eight revolving coils 3 on the matrix 5, a sensing electrode 4 arranged, totally eight in the inside of each revolving coil 3.The sensing electrode 4 and one adjacent of the composition that are in revolving coil 3 inside detect electric capacity, this pair of electrodes that detects electric capacity and offside is formed and is detected electric capacity and form a differential capacitance, and differential capacitance can detect little rotor 1 deflection angle on this direction.Eight capacitor plates can detect the deflection angle on the both direction.
Eight revolving coils 3 can be divided into two group of four phase coil, when passing through the high frequency exchange current in revolving coil 3, current and phase difference 90 degree of adjacent windings, like this, form rotating magnetic field in space, little rotor 1 place, little rotor 1 produces high speed rotating under the effect of rotating magnetic field.The lead-in wire of each sensing electrode 4 and revolving coil 3 also is to adopt the bottom of buried regions fabrication techniques at stable suspersion coil 2, revolving coil 3 or sensing electrode 4, draws from bottom.
As shown in Figure 4, little rotor 1 is annular, the inner ring size of the little rotor 1 of annular is that it is bigger than the radius of suspending stabilized coil inner ring 6, and is littler than the radius of suspending stabilized coil outer ring 7 by both size decisions of suspending stabilized coil inner ring 6 and suspending stabilized coil outer ring 7.Little rotor 1 adopts electric conductivity preferred metal material to form.The external diameter of little rotor 1 does not wait to several thousand microns from the hundreds of micron, and thickness can be tens microns.
Claims (8)
1, a kind of internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscope, comprise: little rotor (1), stable suspersion coil (2), revolving coil (3), sensing electrode (4), matrix (5), stable suspersion coil (2) is by stable suspersion coil outer ring (6), stable suspersion coil inner ring (7), connecting line (8) three parts are formed, it is characterized in that, stable suspersion coil (2), revolving coil (3), sensing electrode (4) all is located on the matrix (5), and matrix (5) forms fixed connection, little rotor (1) is in the top of electromagnetic force effect low suspension in matrix (5), little rotor (1) is annular, and stable suspersion coil outer ring (6) is connected by connecting line (8) with stable suspersion coil inner ring (7).
2, internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscope according to claim 1, it is characterized in that, on described matrix (5), be distributed with stable suspersion coil outer ring (6), connecting line (8) and stable suspersion coil inner ring (7) from outside to inside, the three forms the multi-turn stable suspersion coil (2) of a sealing, totally 4 of stable suspersion coils (2), distribute axisymmetricly in a circumferential direction, the lead-in wire of stable suspersion coil (2) is arranged on bottom, draws from stable suspersion coil (2) bottom.
3, internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscope according to claim 1 and 2, it is characterized in that, described stable suspersion coil (2) size is determined jointly by the size of little rotor (1), stable suspersion coil outer ring (6) diameter is bigger than the internal diameter of annular little rotor (1), and stable suspersion coil inner ring (7) diameter is littler than annular little rotor (1) internal diameter.
4, according to claim 1 or 2 described internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscopes, it is characterized in that, the distribution of electromagnetic force that described stable suspersion coil inner ring (7) electromagnetic field induces on little rotor (1) is in the inside edge of little rotor (2), and outside being tilted to, the electromagnetic force that magnetic field, stable suspersion coil outer ring (6) produces is positioned at little rotor (1) inside, and being close to rotational symmetry distributes, the resultant direction of the distribution electromagnetic force that stable suspersion coil (2) produces upwards, make that little rotor (2) is suspended, when the center of little rotor (1) is in the center of matrix (5), the cross component force of distribution electromagnetic force is cancelled out each other, make a concerted effort for straight up, when there is off-centre in relative matrix (5) center of little rotor (1), the cross component force of electromagnetic force is no longer offset, the side force direction that produces is pointed to rotor center, makes that little rotor (1) is not dished out, and finally obtains stable suspension.
5, according to claim 1 or 2 described internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscopes, it is characterized in that, be distributed with eight revolving coils (3) on the described matrix (5), in the inside of each revolving coil (3) sensing electrode (4) is arranged, totally eight, be in a sensing electrode (4) of stable suspersion coil inside and adjacent one and form a detection electric capacity, this pair of electrodes that detects electric capacity and offside is formed detection electric capacity and is formed a differential capacitance, differential capacitance can detect little rotor (1) deflection angle on this direction, and eight capacitor plates can detect the deflection angle on the both direction.
6, internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscope according to claim 1, it is characterized in that, described revolving coil (3) has eight, they are divided into two group of four phase coil, when in revolving coil (3), passing through the high frequency exchange current, current and phase difference 90 degree of adjacent windings, in little rotor (1) space, place, form rotating magnetic field like this, little rotor (1) is under the effect of rotating magnetic field, produce high speed rotating, the lead-in wire of each sensing electrode (4) and revolving coil (3) is located at the lower floor at revolving coil (3) and sensing electrode (4), draws from bottom.
7, internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscope according to claim 1 is characterized in that, described stable suspersion coil (2), revolving coil (3) and sensing electrode (4) all are planar structures.
8, according to claim 1 or 7 described internal stabilized electromagnetic suspension ring-shaped micro-rotating gyroscopes, it is characterized in that on described stable suspersion coil (2), revolving coil (3) or the sensing electrode (4) one deck insulating material being arranged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2007100378937A CN100504297C (en) | 2007-03-08 | 2007-03-08 | Internal stabilized electromagnetic suspension ring-shaped rotor micro-rotating gyroscope |
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| CNB2007100378937A CN100504297C (en) | 2007-03-08 | 2007-03-08 | Internal stabilized electromagnetic suspension ring-shaped rotor micro-rotating gyroscope |
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| CN101017088A true CN101017088A (en) | 2007-08-15 |
| CN100504297C CN100504297C (en) | 2009-06-24 |
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| CNB2007100378937A Expired - Fee Related CN100504297C (en) | 2007-03-08 | 2007-03-08 | Internal stabilized electromagnetic suspension ring-shaped rotor micro-rotating gyroscope |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101839717A (en) * | 2010-03-26 | 2010-09-22 | 南京航空航天大学 | Near-field ultrasound floated-type gyroscope |
| CN103944456A (en) * | 2014-04-14 | 2014-07-23 | 清华大学 | Motor |
| CN105423995A (en) * | 2014-09-03 | 2016-03-23 | 葛幸华 | Separation type round inductosyn having new structure sensing member |
| CN108427347A (en) * | 2018-04-04 | 2018-08-21 | 肇庆学院 | A kind of control system of interior steady formula electromagnetic suspension micro mirror |
| CN109631869A (en) * | 2018-12-11 | 2019-04-16 | 西安航天精密机电研究所 | A kind of high-precision two-dimensional linear movement pick-up system |
| CN110672082A (en) * | 2019-12-06 | 2020-01-10 | 中国人民解放军国防科技大学 | Concentrated mass vibrating gyroscope based on push-up magnetic suspension platform |
| CN113063408A (en) * | 2021-03-15 | 2021-07-02 | 西安交通大学 | Ultrasonic suspended gyroscope based on planar holographic transducer |
| WO2022007089A1 (en) * | 2020-07-09 | 2022-01-13 | 瑞声声学科技(深圳)有限公司 | Mems gyroscope and electronic product |
-
2007
- 2007-03-08 CN CNB2007100378937A patent/CN100504297C/en not_active Expired - Fee Related
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101839717A (en) * | 2010-03-26 | 2010-09-22 | 南京航空航天大学 | Near-field ultrasound floated-type gyroscope |
| CN101839717B (en) * | 2010-03-26 | 2012-12-12 | 南京航空航天大学 | Near-field ultrasound floated-type gyroscope |
| CN103944456A (en) * | 2014-04-14 | 2014-07-23 | 清华大学 | Motor |
| CN103944456B (en) * | 2014-04-14 | 2016-06-08 | 清华大学 | Motor |
| CN105423995A (en) * | 2014-09-03 | 2016-03-23 | 葛幸华 | Separation type round inductosyn having new structure sensing member |
| CN105423995B (en) * | 2014-09-03 | 2018-01-16 | 葛幸华 | Separate type round induction synchrometer with new construction sensing part |
| CN108427347A (en) * | 2018-04-04 | 2018-08-21 | 肇庆学院 | A kind of control system of interior steady formula electromagnetic suspension micro mirror |
| CN108427347B (en) * | 2018-04-04 | 2023-08-15 | 肇庆学院 | Control system of internal stable electromagnetic suspension micromirror |
| CN109631869A (en) * | 2018-12-11 | 2019-04-16 | 西安航天精密机电研究所 | A kind of high-precision two-dimensional linear movement pick-up system |
| CN110672082A (en) * | 2019-12-06 | 2020-01-10 | 中国人民解放军国防科技大学 | Concentrated mass vibrating gyroscope based on push-up magnetic suspension platform |
| WO2022007089A1 (en) * | 2020-07-09 | 2022-01-13 | 瑞声声学科技(深圳)有限公司 | Mems gyroscope and electronic product |
| CN113063408A (en) * | 2021-03-15 | 2021-07-02 | 西安交通大学 | Ultrasonic suspended gyroscope based on planar holographic transducer |
| CN113063408B (en) * | 2021-03-15 | 2022-10-28 | 西安交通大学 | Ultrasonic suspended gyroscope based on planar holographic transducer |
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| CN100504297C (en) | 2009-06-24 |
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Granted publication date: 20090624 Termination date: 20120308 |