CN1603744A - Micro gyro based on composite magnetic suspension bearing - Google Patents
Micro gyro based on composite magnetic suspension bearing Download PDFInfo
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- CN1603744A CN1603744A CN 200410067569 CN200410067569A CN1603744A CN 1603744 A CN1603744 A CN 1603744A CN 200410067569 CN200410067569 CN 200410067569 CN 200410067569 A CN200410067569 A CN 200410067569A CN 1603744 A CN1603744 A CN 1603744A
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- suspension bearing
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Abstract
It is a composite magnetic suspension axis gyroscope in the micro system field which adopts single rotor and upper and down stator structure, wherein, the rotor is formed by rotor upper magnetic steel, rotor down magnetic steel and rotor base; the upper and down stators are formed by upper and down stators base. The passive suspension axis inner ring is fixed on the outer cycle of the rotation axis and its outer ring is fixed on the inner side of the limited spherical surface; the gem balls are fixed on both sides of the rotation axis and contacts with the limited spherical surface; the limited spherical surface is fixed with the stator.
Description
Technical field
What the present invention relates to is a kind of micro gyro, and particularly a kind of micro gyro based on composite magnetic suspension bearing is used for the micro-system field.
Background technology
Magnetic suspension bearing can be divided into active bearings and passive bearing, also is called electromagnetic suspension bearing and permanent-magnet suspension bearing.At present it has and does not have the machinery contact based on the gyro general using of magnetic suspension bearing, and little friction does not have wearing and tearing, and the long-life, high rotating speed such as need not to lubricate at advantage, and electromagnetic suspension bearing has the ACTIVE CONTROL ability, can effectively suppress the unbalance vibration of rotating shaft.These are used all is to utilize it to replace traditional bearing to realize gyroscopic effect.In addition, also there is the research of magnetic suspension rotor gyro at present, mainly utilizes electromagnetic action to realize the suspension and the rotation of rotor.This gyro is owing to the coupling of its rotating magnetic field and suspension magnetic is difficult to realize High Accuracy Control.
Find by prior art documents, Chinese patent application number is: 03141542.3, name is called: the little gyro in magnetic suspension rotor orientation, this patent readme is " promoted the scope of application of the little gyro of magnetic suspension rotor; adopt the sandwich structure of rotor supports post, double-sided stator, be can vertically disposed suspension system ".Mutual inductance between this patent utilization stator and the aluminum rotor realizes that the integral body of rotor suspends and rotation.Utilized the advantage of electromagnetic suspension to overcome gravity.But when adopting this structure, the degree of freedom of the turning axle of rotor on radial direction can't accurate be controlled, and its asynchronous rotation mode torque fluctuations is big, is difficult to realize high speed rotating.
Summary of the invention
The objective of the invention is to overcome deficiency of the prior art, the characteristics of utilizing driven suspension and initiatively suspending, gyroscopic inertia according to gyro self, a kind of micro gyro based on composite magnetic suspension bearing is provided, little electromagnetic machine and Gyroscope Design is as a whole, rotor makes its rigidity by the control bearing satisfy the different demands of gyro when starting with high speed rotating, for manufacturing and designing of the little gyro of high precision provides a kind of new method as the rotor of gyro.
The present invention is achieved by the following technical solutions, the present invention includes: the upper limit sphere, go up jewel ball, rotating shaft, go up ring in the driven suspension bearing, go up the driven suspension bearing outer shroud, go up the stator substrate, go up the stator planar coil, rotor upper magnetic steel, rotor substrate, rotor lower magnetic steel, stator planar coil, stator substrate down, driven suspension bearing outer shroud, ring, lowerside stone ball and lower limit sphere in the driven suspension bearing down down down.The present invention adopts single rotor and upper and lower stator structure; Rotor upper magnetic steel, rotor lower magnetic steel, rotor substrate constitute little gyrorotor; Up and down the stator planar coil, constitute little gyro stator jointly in the stator substrate up and down, rotor is positioned at the centre of upper and lower stator; Magnet steel is positioned at the both sides of rotor substrate about its rotor, is fastenedly connected by center pit and rotating shaft, and the stator planar coil is produced in the stator substrate up and down up and down.The center pit of upper and lower stator is passed in rotating shaft; Up and down driven suspension bearing by ring in the driven suspension bearing up and down and up and down the driven suspension bearing outer shroud forms, encircle in the driven suspension bearing up and down and be fixed in the cylindrical of rotating shaft, the driven suspension bearing outer shroud is fixed on the inboard of spacing sphere up and down; Passive magnetic suspension bearing support rotor and rotating shaft are suspended in the middle of the upper and lower stator it; Initiatively suspension bearing is made of lower magnetic steel on stator planar coil and the rotor up and down; The jewel ball is fixed in the both sides of rotating shaft, contacts with spacing sphere; Spacing sphere and stator are fixed together.
Initiatively suspension bearing (electromagnetic suspension bearing), driven suspension bearing (permanent-magnet suspension bearing) are formed composite magnetic suspension bearing, and the magnetic of driven suspension bearing outer shroud inboard is identical with the magnetic in the ring outside in it; Initiatively suspension bearing does not then need independent coil; Thereby reduce the complicacy of system architecture, the complicacy of being convenient to realize microminiaturization simultaneously and reducing control.Initiatively the suspending power of suspension bearing passes to the opposite high frequency sinusoidal current generation of phase place by two coils in symmetry.Rigidity by control active suspension bearing, when the starting of rotation rigid body, increase the rigidity of whole composite bearing, and when its high speed rotating, utilize gyroscopic intertia to make the rotation rigid body reduce to the bearing rigidity requirement, by reducing or remove initiatively suspending power and give the degree of freedom of rotation rigid body, thereby form gyro in certain limit.
The restriction of axial freedom is realized by jewel ball and spacing sphere.The jewel ball is positioned at the two ends of rotating shaft, and two spacing spheres are two parts of same spheroid, and its centre of sphere is the rotation center of rotor.The jewel spheroid is used for reducing friction, and when the spheroid of same radius guaranteed that then skew takes place rotor, its rotation center remained unchanged.
Change by detecting the angle that capacitance variations between stator and the rotor detects the rotation rigid body, and apply moment by the active suspension bearing and will rotate rigid body and reset the closed-loop control of realization system.
The present invention has substantive distinguishing features and marked improvement, by the design of composite magnetic suspension bearing, makes micro electromagnet driver have gyroscopic effect when high speed rotating, is one with microdrive and little Gyroscope Design.For the design of little gyro provides a kind of new method.On the basis of driven suspension, utilize the may command performance that initiatively suspends and the gyroscopic inertia of gyro, in the process of high speed rotating, change the rigidity of composite bearing in the starting of gyro, the different requirements when satisfying its different running status.Simultaneously, the active suspension bearing can also compensate because of the rotor quality that is processed to form inhomogeneous respectively, improves the precision of micro gyro.
Description of drawings
Fig. 1 structural representation of the present invention
Fig. 2 the present invention is the suspending power synoptic diagram initiatively
Fig. 3 the present invention is suspending power partial structurtes enlarged diagram initiatively
Embodiment
As shown in Figure 1 and Figure 2, the present invention includes: upper limit sphere 1, go up jewel ball 2, rotating shaft 3, go up ring 4 in the driven suspension bearing, go up driven suspension bearing outer shroud 5, go up stator substrate 6, go up stator planar coil 7, rotor upper magnetic steel 8, rotor substrate 9, rotor lower magnetic steel 10, stator planar coil 11, stator substrate 12 down, driven suspension bearing outer shroud 13, ring 14, lowerside stone ball 15 and lower limit sphere 16 in the driven suspension bearing down down down.
The present invention adopts single rotor and upper and lower stator structure, and rotor upper magnetic steel 8, rotor lower magnetic steel 10, rotor substrate 9 constitute the rotor of little gyro; Upper and lower stator planar coil 7,11, upper and lower stator substrate 6,12 constitute the upper and lower stator of little gyro.Rotor upper magnetic steel 8 and rotor lower magnetic steel 10 are positioned at the both sides of rotor substrate 9, are fastenedly connected by center pit and rotating shaft 3; Last stator planar coil 7 and following stator planar coil 11 are produced in stator substrate 6 and the following stator substrate 12 by Micrometer-Nanometer Processing Technology respectively; Rotor is positioned at the centre of upper and lower stator, and the center pit of stator is passed in rotating shaft 3; In the last driven suspension bearing ring 4 with last driven suspension bearing outer shroud 5, go up driven suspension bearing about ring 14 is formed respectively with following driven suspension bearing outer shroud 13 in the driven suspension bearing, ring 4 is fixed in the cylindrical of rotating shaft 3 in the last driven suspension bearing, and last driven suspension bearing outer shroud 5 is fixed on the inboard of upper limit sphere 1; Ring 14 is fixed in the cylindrical of rotating shaft 3 in the following driven suspension bearing, and following driven suspension bearing outer shroud 13 is fixed on the inboard of lower limit sphere 16; Passive magnetic suspension bearing support rotor and rotating shaft are suspended in the middle of two stators it; Last stator planar coil 7 constitutes up and down initiatively suspension bearing with rotor upper magnetic steel 8, following stator planar coil 11 respectively with rotor lower magnetic steel 10; Upper and lower stator planar coil 7,11 is formed by six windings, and the upper and lower magnet steel 8,10 of rotor is formed by four pairs of magnetic poles, and its control is controlled according to synchronous motor; Upper and lower jewel ball 2,15 is individually fixed in the both sides of rotating shaft, contacts with upper and lower spacing sphere 1,16; Spacing up and down sphere 1,16 and up and down stator substrate 6,12 be fixed together.
Initiatively suspension bearing (electromagnetic suspension bearing), driven suspension bearing (permanent-magnet suspension bearing) are formed composite magnetic suspension bearing.The magnetic of driven suspension bearing outer shroud 5,13 inboards is identical with the magnetic in ring 4,14 outsides in it; Initiatively suspension bearing does not then need independent coil; Thereby reduce the complicacy of system architecture, the complicacy of being convenient to realize microminiaturization simultaneously and reducing control.Initiatively the suspending power of suspension bearing passes to the opposite high frequency sinusoidal current generation of phase place by two coils in symmetry.Rigidity by control active suspension bearing, when the starting of rotation rigid body, increase the rigidity of whole composite bearing, and when its high speed rotating, utilize gyroscopic intertia to make the rotation rigid body reduce to the bearing rigidity requirement, by reducing or remove initiatively suspending power and give the degree of freedom of rotation rigid body, thereby form gyro in certain limit.
Initiatively suspension bearing passes to by the symmetric winding in upper and lower stator planar coil 7,11 that frequency is identical, amplitude is identical and 180 ° of high_frequency sine waves of phase phasic difference utilize the electromagnetic suspension principle to produce radial suspension force, and this suspending power rotates in circumference range.The suspension of its instantaneous generation is tried hard to as shown in Figure 2.The winding of one group of symmetry passes to the opposite sine-wave current of phase place, and the force direction of its generation is identical.Therefore, at this in a flash, two coils produce level and two vertical radial forces up and down, i.e. the anchorage force that initiatively suspends.
Axial displacement is limited jointly by upper and lower spacing sphere 1,16, utilizes the flexibility ratio of the low friction raising rotor of jewel ball 2, and the centre of sphere of upper and lower spacing sphere 1,16 is the rotation center of rotor.The design of sphere makes rotor still keep its rotation center when skew, improves its sensing accuracy.
Change by detecting the angle that capacitance variations between stator and the rotor detects the rotation rigid body, and apply moment by the active suspension bearing rotor is resetted, realize system's closed-loop control.
Claims (6)
1, a kind of based on the little gyro of composite magnetic suspension bearing electromagnetism, comprise: go up stator substrate (6), last stator planar coil (7), rotor substrate (9), following stator planar coil (11), following stator substrate (12), it is characterized in that, also comprise: upper limit sphere (1), last jewel ball (2), rotating shaft (3), ring (4) in the last driven suspension bearing, last driven suspension bearing outer shroud (5), rotor upper magnetic steel (8), rotor lower magnetic steel (10), following driven suspension bearing outer shroud (13), ring (14) in the following driven suspension bearing, lowerside stone ball (15) and lower limit sphere (16), adopt single rotor and last, following stator structure, rotor upper magnetic steel (8), rotor lower magnetic steel (10), rotor substrate (9) constitutes the rotor of little gyro, on, following stator planar coil (7,11) and last, following stator substrate (6,12) constitute on little gyro, following stator, rotor is positioned at the centre of two stators up and down, the center pit of stator is passed in rotating shaft (3), ring (4) is fixed in the cylindrical of rotating shaft (3) in the last driven suspension bearing, last driven suspension bearing outer shroud (5) is fixed on the inboard of upper limit sphere (1), ring (14) is fixed in the cylindrical of rotating shaft (3) in the following driven suspension bearing, following driven suspension bearing outer shroud (13) is fixed on the inboard of lower limit sphere (16), on, lowerside stone ball (2,15) be individually fixed in the both sides of rotating shaft (3), with last, lower limit sphere (1,16) contact spacing up and down sphere (1,16) with stator substrate (6 up and down, 12) be fixed together.
2, the micro gyro based on composite magnetic suspension bearing according to claim 1, it is characterized in that, rotor upper magnetic steel (8) and rotor lower magnetic steel (10) are positioned at the both sides of rotor substrate (9), be fastenedly connected by center pit and rotating shaft (3), last stator planar coil (7) and following stator planar coil (11) are produced in stator substrate (6) and the following stator substrate (12).
3, the micro gyro based on composite magnetic suspension bearing according to claim 1, it is characterized in that, bearing (3) radial rigidity is adjustable, axial displacement is by spacing sphere (1,16) and last lowerside stone ball (2,15) restriction up and down, upper and lower jewel ball (2,15) lays respectively at the two ends of rotating shaft, upper and lower spacing sphere (1,16) is two parts of same spheroid, and its centre of sphere is the rotation center of rotor.
4, the micro gyro based on composite magnetic suspension bearing according to claim 1, it is characterized in that, driven suspension bearing about encircling (4,14) up and down in the driven suspension bearing and driven suspension bearing outer shroud (5,13) being formed respectively up and down, passive magnetic suspension bearing support rotor and rotating shaft (3), it is suspended in the middle of two stators, and lower magnetic steel (8,10) constitutes up and down initiatively suspension bearing respectively on stator planar coil (7,11) and the rotor up and down.
According to claim 1 or 4 described micro gyros, it is characterized in that 5, upper and lower stator planar coil (7,11) is formed by six windings based on composite magnetic suspension bearing.
According to claim 1 or 4 described micro gyros, it is characterized in that 6, upper and lower magnet steel (8,10) is formed by four pairs of magnetic poles based on composite magnetic suspension bearing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2004100675696A CN100385202C (en) | 2004-10-28 | 2004-10-28 | Micro gyro based on composite magnetic suspension bearing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2004100675696A CN100385202C (en) | 2004-10-28 | 2004-10-28 | Micro gyro based on composite magnetic suspension bearing |
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| CN1603744A true CN1603744A (en) | 2005-04-06 |
| CN100385202C CN100385202C (en) | 2008-04-30 |
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| CNB2004100675696A Expired - Fee Related CN100385202C (en) | 2004-10-28 | 2004-10-28 | Micro gyro based on composite magnetic suspension bearing |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100398994C (en) * | 2005-07-14 | 2008-07-02 | 上海交通大学 | Flexible microgyrorotor and electromagnetic drive and dynamic tune |
| CN100419379C (en) * | 2007-04-16 | 2008-09-17 | 北京航空航天大学 | Single end support type magnetic suspension control moment gyro of single framework |
| CN100437031C (en) * | 2007-04-16 | 2008-11-26 | 北京航空航天大学 | Completely non - contacting magnetic suspension control moment gyro of single framework |
| CN101043190B (en) * | 2007-04-12 | 2010-04-14 | 上海交通大学 | Stator embedded electromagnetic suspension microsystem |
| CN101473160B (en) * | 2006-06-19 | 2011-06-15 | 卡雷尔·范德瓦尔特 | Improved gimbal |
| CN102175235A (en) * | 2011-01-21 | 2011-09-07 | 南京航空航天大学 | Spherical piezoelectric stator type gyroscope |
| CN104316038A (en) * | 2014-11-05 | 2015-01-28 | 金华中科机电研究所 | Single-shaft double-gyro stabilization system and control method thereof |
| CN104457722B (en) * | 2014-12-05 | 2017-09-26 | 浙江大学 | A kind of the single shaft double tops systems stabilisation and its control method of band control |
| CN108953895A (en) * | 2018-07-17 | 2018-12-07 | 中盟科创（深圳）科技发展有限公司 | Mechanical turntable |
| CN110146009A (en) * | 2019-05-17 | 2019-08-20 | 中国科学院上海技术物理研究所 | A kind of sandwich inductosyn structure |
| CN110748563A (en) * | 2019-09-29 | 2020-02-04 | 肇庆市衡艺实业有限公司 | Magnetic suspension device and rotary lifting mechanism thereof |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| JPH01193612A (en) * | 1988-01-28 | 1989-08-03 | Nec Home Electron Ltd | Gyroscope |
| JPH02221808A (en) * | 1989-02-22 | 1990-09-04 | Nippon Seiko Kk | Magnetic bearing gyro |
| JPH04244622A (en) * | 1991-01-29 | 1992-09-01 | Ebara Corp | Magnetic bearing device for horizontal rotary machine |
| CN1062353C (en) * | 1996-05-17 | 2001-02-21 | 北京工业大学 | Method for shortening the compass swing period of two freedom deg. swing top |
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2004
- 2004-10-28 CN CNB2004100675696A patent/CN100385202C/en not_active Expired - Fee Related
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100398994C (en) * | 2005-07-14 | 2008-07-02 | 上海交通大学 | Flexible microgyrorotor and electromagnetic drive and dynamic tune |
| CN101473160B (en) * | 2006-06-19 | 2011-06-15 | 卡雷尔·范德瓦尔特 | Improved gimbal |
| CN101043190B (en) * | 2007-04-12 | 2010-04-14 | 上海交通大学 | Stator embedded electromagnetic suspension microsystem |
| CN100419379C (en) * | 2007-04-16 | 2008-09-17 | 北京航空航天大学 | Single end support type magnetic suspension control moment gyro of single framework |
| CN100437031C (en) * | 2007-04-16 | 2008-11-26 | 北京航空航天大学 | Completely non - contacting magnetic suspension control moment gyro of single framework |
| CN102175235B (en) * | 2011-01-21 | 2012-12-12 | 南京航空航天大学 | Spherical piezoelectric stator type gyroscope |
| CN102175235A (en) * | 2011-01-21 | 2011-09-07 | 南京航空航天大学 | Spherical piezoelectric stator type gyroscope |
| CN104316038A (en) * | 2014-11-05 | 2015-01-28 | 金华中科机电研究所 | Single-shaft double-gyro stabilization system and control method thereof |
| CN104316038B (en) * | 2014-11-05 | 2017-02-01 | 衢州职业技术学院 | Single-shaft double-gyro stabilization system and control method thereof |
| CN104457722B (en) * | 2014-12-05 | 2017-09-26 | 浙江大学 | A kind of the single shaft double tops systems stabilisation and its control method of band control |
| CN108953895A (en) * | 2018-07-17 | 2018-12-07 | 中盟科创（深圳）科技发展有限公司 | Mechanical turntable |
| CN108953895B (en) * | 2018-07-17 | 2022-07-19 | 中盟科创（深圳）科技发展有限公司 | Mechanical turntable |
| CN110146009A (en) * | 2019-05-17 | 2019-08-20 | 中国科学院上海技术物理研究所 | A kind of sandwich inductosyn structure |
| CN110748563A (en) * | 2019-09-29 | 2020-02-04 | 肇庆市衡艺实业有限公司 | Magnetic suspension device and rotary lifting mechanism thereof |
| CN110748563B (en) * | 2019-09-29 | 2020-12-25 | 肇庆市衡艺实业有限公司 | Magnetic suspension device and rotary lifting mechanism thereof |
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| CN100385202C (en) | 2008-04-30 |
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Granted publication date: 20080430 Termination date: 20101028 |