CN103941034A - Magnetofluid composite angular velocity sensor - Google Patents

Magnetofluid composite angular velocity sensor Download PDF

Info

Publication number
CN103941034A
CN103941034A CN201410134139.5A CN201410134139A CN103941034A CN 103941034 A CN103941034 A CN 103941034A CN 201410134139 A CN201410134139 A CN 201410134139A CN 103941034 A CN103941034 A CN 103941034A
Authority
CN
China
Prior art keywords
magnetic
mfc
phase alternating
circuit
magnetic field
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201410134139.5A
Other languages
Chinese (zh)
Inventor
李醒飞
徐梦洁
梁思夏
王丽萍
张少强
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tianjin University
Original Assignee
Tianjin University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tianjin University filed Critical Tianjin University
Priority to CN201410134139.5A priority Critical patent/CN103941034A/en
Publication of CN103941034A publication Critical patent/CN103941034A/en
Pending legal-status Critical Current

Links

Abstract

The invention discloses a magnetofluid composite angular velocity sensor. A metal shell body is a cylindrical container made of soft magnetic materials and used for containing a mechanical structure and a circuit and shielding outside electromagnetic interference, and a threaded hole is formed in the bottom of the metal shell body and used for fixing the whole angular velocity sensor to a measured object. MFC are three-phase solutions composed of non-conductive base solutions, magnetic particles and non-magnetic solid particles. Permanent magnets are cylindrical and are used for providing a gradient magnetic field, and the MFC are made to generate the magnetofluid gravity suspension effect. An electromagnetic coil is wound on a 24-groove stator, the 24-groove stator and the electromagnetic coil are used for generating a rotary magnetic field, and the non-magnetic solid particles in the MFC can spin in a reversed mode. Soft magnets are used for shielding magnetic field interference generated at the cross position of the magnetic coil. A three-phase alternating current generating circuit is used for generating three-phase alternating voltages, and the three-phase alternating voltages are loaded to the electromagnetic coil through an isolation circuit to generate the rotary magnetic field. The magnetofluid composite angular velocity sensor has the advantages of being low in cost, high in linearity and high in sensitivity.

Description

A kind of magnetic fluid compound angular-rate sensor
Technical field
The present invention relates to angular-rate sensor field, relate in particular to a kind of magnetic liquid in magnetic fluid compound and angular-rate sensor of non magnetic composition spinning effect of utilizing.
Background technology
Magnetic liquid (Magnetic Fluid is called for short MF) is made up of the magnetic particle, stabilizing agent and the base fluid that are suspended in base fluid, with a kind of new function material of mobility and electro permanent magnetic dual nature.If the non magnetic solid particle (about 100-5000nm) that adds third phase to be made by different materials in magnetic fluid; and this non magnetic solid particle also has electric conductivity (metal or coated metal); magnetic fluid compound (Magnetic Fluid Composites is called for short MFC) will show the attribute of unique optics, electromagnetics and mechanical rheology aspect so.At home, the sensor taking magnetic liquid as core has just just entered the research starting stage at home, less to the research of magnetic liquid inertial sensor.
Because quality, the density of non-magnetic particle in MFC are general different from magnetic fluid, MFC generally need work under Microgravity condition.Otherwise the non magnetic solid constituent in MFC (three-phase fluid) will be deposited to the bottom of container or move on to the upper strata (unless non magnetic composition is identical with quality, the density of magnetic fluid) of liquid in containers under gradient gravity.To under earth environment, use this MFC, need to be at the additional gradient magnetic of vertical direction, magnetic fluid solution has levitation effect (producing a power upwards that is greater than conventional buoyancy) under this gradient magnetic, and non-magnetic material is wherein suspended in solution.Like this, non-magnetic material equivalence is under microgravity environment.In Microgravity, the non magnetic composition of MFC is stable without magnetic gradient, whole MFC system macroscopic view homogeneous.Like this, small additional physical field just can affect MFC liquid internal structure and attribute, makes it to occur correlation effect, shows specific optics, electromagnetics and mechanical rheological characteristics etc.
Summary of the invention
The invention provides a kind of magnetic fluid compound angular-rate sensor, the present invention utilizes magnetic liquid and the non magnetic composition spinning effect in magnetic fluid compound to propose a kind of novel angular-rate sensor, described below:
A kind of magnetic fluid compound angular-rate sensor, described magnetic fluid compound angular-rate sensor comprises: metal shell, MFC, permanent magnet, 24 groove stators, solenoid, soft magnetic bodies, and external three-phase alternating current circuit for generating,
Described metal shell is the cylindrical container that soft magnetic material forms, and for holding physical construction and circuit, and shields outside electromagnetic interference, and described metal shell bottom is provided with threaded hole, for whole angular-rate sensor is fixed on to testee;
The three-phase solution that described MFC is made up of non-conductive base fluid, magnetic particle and non magnetic solid particle;
Described permanent magnet is cylindric permanent magnet, for gradient magnetic is provided, makes described MFC produce magnetic fluid levitation effect;
Described solenoid is wrapped on described 24 groove stators, and described 24 groove stators and described solenoid, for generation of rotating magnetic field, make the non magnetic solid particle reversed spin in described MFC;
The magnetic interference that described soft magnetic bodies produces for shielding described solenoid infall;
Described three-phase alternating current circuit for generating, for generation of three-phase alternating voltage, is loaded on described solenoid and is produced rotating magnetic field by buffer circuit.
The beneficial effect of technical scheme provided by the invention is: utilize the electromagnetic attributes of magnetic fluid compound uniqueness and the New Magnetic Field Controlled fluid inertia gravity sensor of mechanical rheological characteristics to have low cost, high linearity, highly sensitive feature, change in occasion in quasistatic and low frequency inertia gravitation especially, there is high linearity and sensitivity response.
1, novel structure of the present invention, does not have solid moving-member, does not have mechanical wear, therefore has high reliability, high strength, long-life feature;
2, the present invention has low cost, high linearity, highly sensitive feature, changes in occasion especially in quasistatic and low frequency inertia gravitation, has high linearity and sensitivity response.
Brief description of the drawings
Fig. 1 is vertical view of the present invention.
Wherein: 1,2,3 and 4-screw; 5-end cap.
Fig. 2 is cut-open view A-A corresponding in Fig. 1.
Wherein: 3,4-screw; 5-end cap; 6-metal shell; 7-screw thread; 8-screw; 10-circuit platform; 11-upward wiring plate; The upper soft magnetic bodies of 12-; The upper soft magnetic bodies support of 13-; The upper permanent magnet of 14-; The upper permanent magnet support of 15-; 16-MFC; 17-24 groove stators; Permanent magnet under 18-; Soft magnetic bodies support under 19-; Soft magnetic bodies under 20-; 21-downward cabling plate; 9,22-backstay.
Fig. 3 is the schematic diagram of upper and lower wiring board of the present invention, upper and lower soft magnetic bodies support and upper and lower permanent magnet support.
Fig. 4 is the schematic diagram of 24 groove stators.
Fig. 5 is assembling decomposing schematic representation of the present invention (screw and backstay do not draw, and wherein the label of screw (23,24,25 and 26) has been marked on corresponding threaded hole).
Fig. 6 is that generation phase difference output is the electrical schematic diagram (needing to add buffer circuit between this circuit and solenoid, not shown in FIG.) of the three-phase alternating voltage of 120 °.
Fig. 7 is that three-phase 24 groove windings are wound around planimetric map.U 1and U 2the all 0 ° sinusoidal voltage of access by buffer circuit but current direction is contrary, V 1and V 2the all 120 ° sinusoidal voltages of access by buffer circuit but current direction is contrary, U 1and U 2the all 240 ° sinusoidal voltages of access by buffer circuit but current direction is contrary.Direction of current as shown in the figure.
Fig. 8 is the graph of a relation between extraneous input angular velocity f and quality factor q.Extraneous input angular velocity is taking Hz as unit.
Embodiment
For making the object, technical solutions and advantages of the present invention clearer, below embodiment of the present invention is described further in detail.
A kind of magnetic fluid compound angular-rate sensor, comprise: metal shell 6, MFC16, permanent magnet (upper permanent magnet 14 and lower permanent magnet 18), 24 groove stators 17, solenoid (not shown), soft magnetic bodies (upper soft magnetic bodies 12 and lower soft magnetic bodies 20), and external three-phase alternating current circuit for generating.
Metal shell 6, for the cylindrical container that soft magnetic material forms, for holding physical construction and the circuit of angular-rate sensor, and shields outside electromagnetic interference, and metal shell 6 bottoms are provided with threaded hole, for whole angular-rate sensor is fixed on to testee.
The three-phase solution that MFC16 is made up of non-conductive base fluid, magnetic particle and non magnetic solid particle.
Permanent magnet is cylindric permanent magnet, for gradient magnetic is provided, makes MFC16 produce magnetic fluid levitation effect, thereby non magnetic solid particle is suspended in solution equably.
Solenoid is wrapped on 24 groove stators 17, and 24 groove stators 17 and solenoid, for generation of rotating magnetic field, make the non magnetic solid particle reversed spin in MFC16.
The magnetic interference that soft magnetic bodies produces for shielding solenoid infall.
Three-phase alternating current circuit for generating is for generation of three-phase alternating voltage, is loaded into and on solenoid, produced rotating magnetic field by buffer circuit.This circuit is that those skilled in the art are in common knowledge, and the embodiment of the present invention does not repeat this.
This angular-rate sensor is the reversed spin motion of doing under the effect of rotating magnetic field by the non-magnetic material in MFC16 around z axle, and the direction of its angular momentum is also along z axle.In the time that whole angular-rate sensor has the additional angular momentum along x axle or y axle (z axle is orthogonal for x, y), the quality factor of circuit change, and within the scope of certain gyro frequency, the inverse of quality factor is linear with the additional angular velocity rotatablely moving.
Below in conjunction with the structure of detailed this angular-rate sensor of description of accompanying drawing, described below:
Fig. 1 is vertical view of the present invention.This Figure illustrates screw 1,2,3 and 4 and be along the circumferential direction uniformly distributed on end cap 5, effect is to be connected with metal shell 6.
Fig. 2 is cut-open view A-A corresponding in Fig. 1.The backstay that downward cabling plate 21 is inserted to backstay 9 and 22(fore-and-aft direction is not shown).Lower soft magnetic bodies 20 is combined to rear insertion backstay 9 and 22 with lower soft magnetic bodies support 19.24 groove stators 17 and lower permanent magnet 18 are combined to rear insertion backstay 9 and 22.And the assembly combining with backstay is put into metal shell 6.Pour into MFC16 in 24 locating slots 17 after, be coated in 24 locating slot 17 upper surfaces with glue, upper permanent magnet frame 15 and upper permanent magnet 14 are combined after rear insertion backstay 9 and 22 simultaneously, make permanent magnet frame 15 lower surfaces and 24 locating slot 17 upper surface gummeds.Upper soft magnetic bodies frame 13 and upper soft magnetic bodies 12 are combined to insertion backstay 9 and 22.Upward wiring plate 11 is inserted to backstay 9 and 22.After circuit platform 10 and circuit board etc. are combined, with unshowned screw in screw 8(and Fig. 2) be fixed on upward wiring plate 11.End cap 5 is connected by screw 1,2,3 and 4 with metal shell 6.Screw thread 7 is for whole angular-rate sensor is fixed on testee.
Fig. 3 is the schematic diagram of upper and lower wiring board of the present invention, upper and lower soft magnetic bodies support and upper and lower permanent magnet support.Groove shape in figure is used for the coil cabling that produces rotating magnetic field.Circular hole is used for inserting backstay 9 and 22.
Fig. 4 is the schematic diagram of 24 groove stators.As shown in Figure 4, groove shape is used for the coil cabling that produces rotating magnetic field, and middle circle column space is for holding MFC.Circular hole is used for inserting backstay 9 and 22.
Fig. 5 is assembling decomposing schematic representation of the present invention (screw and backstay do not draw, and wherein the label of screw has been marked on corresponding threaded hole).Install and form according to order as shown in the figure.
Fig. 6 is that generation phase difference output is the electrical schematic diagram of the three-phase alternating voltage of 120 °, is input as 50Hz sinusoidal voltage.When specific implementation, can also adopt other three-phase alternating voltage to produce circuit, the embodiment of the present invention is not restricted this.
Fig. 7 is that three-phase 24 groove windings are wound around planimetric map.U 1and U 2the all 0 ° sinusoidal voltage of access by buffer circuit but current direction is contrary, V 1and V 2the all 120 ° sinusoidal voltages of access by buffer circuit but current direction is contrary, U 1and U 2the all 240 ° sinusoidal voltages of access by buffer circuit but current direction is contrary.Direction of current as shown in the figure.
Fig. 8 is the graph of a relation between extraneous input angular velocity f and quality factor q.Extraneous input angular velocity is taking Hz as unit.
The principle of work of a kind of magnetic fluid compound angular-rate sensor of the present invention is as follows:
After being wound around in 24 locating slots 17 according to the solenoid shown in Fig. 7, when giving solenoid input phase poor while being the three-phase alternating current of 120 °, can produce the rotating magnetic field of rotating around z axle, thereby the magnetisable material in MFC solution is followed rotating magnetic field and is rotated, acting force between magnetisable material and non-magnetic material in MFC solution makes non-magnetic material produce reversed spin motion, the direction of its moment of inertia is along z axle, and z direction of principal axis as shown in Figure 2.When whole sensor has, along x axle or y axle, (z axle is orthogonal for x, y, x and y direction of principal axis are as shown in Figure 1) additional angular momentum time, the quality factor of circuit change, and within the scope of certain gyro frequency, the inverse of quality factor is linear with the additional angular velocity rotatablely moving, as shown in Figure 8.
The measuring method of brief description quality factor of circuit.The energy-storage travelling wave tube of whole circuit is equivalent to inductance L, and dissipative cell is equivalent to resistance R, records the electric current I of the voltage U at circuit two ends and the whole circuit of flowing through, and obtains U=I(LS+R), angle relationship is ∠ U=∠ I+ ∠ arctan(L ω/R).Like this, according to the value of the angle relationship of U, I and ω, just can calculate to obtain the ratio of L and R, also just obtain the quality factor of circuit.
The embodiment of the present invention to the model of each device except do specified otherwise, the model of other devices does not limit, and all can as long as can complete the device of above-mentioned functions.
It will be appreciated by those skilled in the art that accompanying drawing is the schematic diagram of a preferred embodiment, the invention described above embodiment sequence number, just to describing, does not represent the quality of embodiment.
The foregoing is only preferred embodiment of the present invention, in order to limit the present invention, within the spirit and principles in the present invention not all, any amendment of doing, be equal to replacement, improvement etc., within all should being included in protection scope of the present invention.

Claims (1)

1. a magnetic fluid compound angular-rate sensor, is characterized in that, described magnetic fluid compound angular-rate sensor comprises: metal shell, MFC, permanent magnet, 24 groove stators, solenoid, soft magnetic bodies, and external three-phase alternating current circuit for generating,
Described metal shell is the cylindrical container that soft magnetic material forms, and for holding physical construction and circuit, and shields outside electromagnetic interference, and described metal shell bottom is provided with threaded hole, for whole angular-rate sensor is fixed on to testee;
The three-phase solution that described MFC is made up of non-conductive base fluid, magnetic particle and non magnetic solid particle;
Described permanent magnet is cylindric permanent magnet, for gradient magnetic is provided, makes described MFC produce magnetic fluid levitation effect;
Described solenoid is wrapped on described 24 groove stators, and described 24 groove stators and described solenoid, for generation of rotating magnetic field, make the non magnetic solid particle reversed spin in described MFC;
The magnetic interference that described soft magnetic bodies produces for shielding described solenoid infall;
Described three-phase alternating current circuit for generating, for generation of three-phase alternating voltage, is loaded on described solenoid and is produced rotating magnetic field by buffer circuit.
CN201410134139.5A 2014-04-03 2014-04-03 Magnetofluid composite angular velocity sensor Pending CN103941034A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410134139.5A CN103941034A (en) 2014-04-03 2014-04-03 Magnetofluid composite angular velocity sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410134139.5A CN103941034A (en) 2014-04-03 2014-04-03 Magnetofluid composite angular velocity sensor

Publications (1)

Publication Number Publication Date
CN103941034A true CN103941034A (en) 2014-07-23

Family

ID=51188784

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410134139.5A Pending CN103941034A (en) 2014-04-03 2014-04-03 Magnetofluid composite angular velocity sensor

Country Status (1)

Country Link
CN (1) CN103941034A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107092756A (en) * 2017-04-26 2017-08-25 上海航天控制技术研究所 A kind of angular-rate sensor modeling method based on MHD effect
CN110208567A (en) * 2019-05-28 2019-09-06 南方科技大学 Contactless magnetic fluid rotation-speed measuring device, design method and rotating speed measurement method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103453896A (en) * 2013-09-13 2013-12-18 天津大学 Magnetic-fluid gyroscope
CN103591945A (en) * 2013-11-19 2014-02-19 天津大学 Magnetic fluid top suitable for measuring 0-1 KHz of input signals
CN203909058U (en) * 2014-04-03 2014-10-29 天津大学 Magnetofluid compound angular velocity sensor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103453896A (en) * 2013-09-13 2013-12-18 天津大学 Magnetic-fluid gyroscope
CN103591945A (en) * 2013-11-19 2014-02-19 天津大学 Magnetic fluid top suitable for measuring 0-1 KHz of input signals
CN203909058U (en) * 2014-04-03 2014-10-29 天津大学 Magnetofluid compound angular velocity sensor

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
于翔等: "一种磁流体陀螺的设计研究", 《传感技术学报》 *
唐葆霖等: "新型磁流体复合物惯性引力传感器", 《仪表技术与传感器》 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107092756A (en) * 2017-04-26 2017-08-25 上海航天控制技术研究所 A kind of angular-rate sensor modeling method based on MHD effect
CN107092756B (en) * 2017-04-26 2020-10-02 上海航天控制技术研究所 Angular velocity sensor modeling method based on magnetohydrodynamics effect
CN110208567A (en) * 2019-05-28 2019-09-06 南方科技大学 Contactless magnetic fluid rotation-speed measuring device, design method and rotating speed measurement method
CN110208567B (en) * 2019-05-28 2023-10-20 南方科技大学 Non-contact magnetic fluid rotating speed measuring device, design method and rotating speed measuring method

Similar Documents

Publication Publication Date Title
CN203909058U (en) Magnetofluid compound angular velocity sensor
Hammond Electromagnetism for engineers: an introductory course
US20100180681A1 (en) System and method for increased flux density d'arsonval mems accelerometer
US10508932B2 (en) Measuring the position of an object using eddy-currents
CN101865982B (en) Device and method for measuring ambipolar magnetic moment of spatial magnet
CN103174746A (en) Active magnetic bearing system and control circuit
Oh et al. Analysis of electromotive force characteristics and device implementation for ferrofluid based energy harvesting system
CN103941034A (en) Magnetofluid composite angular velocity sensor
CN103760616A (en) Magnetic fluid compound gravity gradiometer
Digregorio et al. Modeling and experimental characterization of an electromagnetic energy harvester for wearable and biomedical applications
CN103487224A (en) Double-magnetic-source magnetic circuit structure of permanent-magnet angle vibration table
CN105891742B (en) A method of measuring magnetic suspension system magnetic gradient
CN101216308B (en) Circular and multi-ring shaped axial magnetizing permanent magnetism antimagnetic rotor induced rotating micro gyroscope
US3089044A (en) Electromagnetic transducer device
CN104280571A (en) Electromagnetic balance type acceleration sensor
CN100483074C (en) Electromagnetic levitation static driven micro-rotation gyro
CN100489452C (en) Diamagnetic rotor electromagnetic induction driving micro-gyroscope
CN107631719A (en) A kind of obliquity sensor based on liquid metal
CN100510754C (en) Suspension type diamagnetic sensitive mass micro accelerometer
CN203673083U (en) Gravity gradient instrument of magnetofluid compound
CN207051509U (en) Axial symmetry elastic system and gravimeter
Hoon et al. The design and operation of an automated double-crank vibrating sample magnetometer
CN100565108C (en) Circle and multi-ring shaped axial and radial magnetizing permanent magnetism antimagnetic rotor charge relaxation rotating micro gyroscope
Dayton Hydrodynamic theory of magnetic fields
CN100552382C (en) Circle and multi-ring shaped axial and radial magnetizing permanent magnetism antimagnetic rotor induced rotating micro gyroscope

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20140723