WO2022116393A1 - 磁浮重力补偿装置以及包括该装置的运动台 - Google Patents
磁浮重力补偿装置以及包括该装置的运动台 Download PDFInfo
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- 230000005484 gravity Effects 0.000 title claims abstract description 164
- 238000005339 levitation Methods 0.000 title claims abstract description 61
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L21/00—Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
- H01L21/67—Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere
- H01L21/683—Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere for supporting or gripping
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
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- H02N15/00—Holding or levitation devices using magnetic attraction or repulsion, not otherwise provided for
Definitions
- the invention relates to the field of integrated circuit equipment manufacturing, and more particularly to a constant-rigidity maglev gravity compensation device and a motion table including the device.
- the micro-movement stage is the core component, which can complete the precise positioning of the silicon wafer in the vertical three axes of Z/Rx/Ry.
- the conventional vertical three-axis micro-motion stage three actuators are usually used for a three-point layout, and then a flexible mechanism is used for vertical guidance and motion decoupling to ensure vertical performance.
- the magnetic levitation voice coil motor device proposed by U.S. patent US2009066168A1 compensates the gravity of the vertical motion module by the magnetic resistance of the magnetic levitation gravity compensation device, and compensates the force of the flexible mechanism by adjusting the amplitude and direction of the coil input current.
- the magnetic levitation coil motor not only has a complicated magnetic circuit structure, but also has a rigidity of the output magnetic levitation force close to zero, so the control algorithm must be used to achieve control accuracy.
- a gravity compensation device with a simple structure, constant stiffness in a small stroke range, and the opposite stiffness of the flexible mechanism is needed at this stage, that is, the compensation device at the zero point can output the same gravity amplitude and opposite direction as the vertical motion module. force, and the output stiffness of the compensation device is guaranteed to be constant.
- the air flotation gravity compensation device commonly used in the industry can adjust the pressure of the compressed gas in real time through a proportional valve to achieve constant stiffness gravity compensation. Performance has an impact.
- the purpose of the present invention is to provide a constant stiffness maglev gravity compensation device with simple structure and control and no hysteresis in control, so as to solve the problems existing in the above-mentioned prior art.
- maglev gravity compensation device comprising:
- first end magnet steel and a second end magnet steel are respectively located at two axial ends of the inner base magnet steel and extend in the axial direction , and the outer diameters of the first end magnet steel and the second end magnet steel gradually increase along the directions away from the two axial ends of the inner base magnet steel;
- the outer ring magnetic steel which is cylindrical, is located outside the inner base magnetic steel coaxially with the inner base magnetic steel and is radially spaced from the inner base magnetic steel.
- the magnetization direction of the first end magnet steel and the second end magnet steel is axially outward from the inner base magnet steel, and the magnetization direction of the outer magnetic ring magnet steel is The magnetic direction is radially outward.
- first end magnet and the second end magnet are mirror-symmetrical with respect to an axial bisector of the inner base magnet.
- the central axes of the inner base magnet, the first end magnet and the second end magnet coincide with each other and are rotationally symmetric about the central axis.
- the inner base magnet has axial through holes, and the first end magnet and the second end magnet have axial through holes.
- the inner base magnetic steel is cylindrical
- the first end magnetic steel is composed of multiple sections of cylindrical magnetic steel adjacent to each other in the axial direction
- the second end magnetic steel is composed of axial magnetic steels.
- the inner diameter of the multi-segment cylindrical magnets is the same, and the outer diameters are from the cylindrical magnet far from the inner base magnet to the cylindrical magnet close to the inner base magnet. The magnets decrease in turn.
- the difference between the outer diameters of adjacent cylindrical magnets in the multi-segment cylindrical magnets of the first end magnets is equal, and the axial lengths are equal;
- the difference between the outer diameters of adjacent cylindrical magnets in the multi-stage cylindrical magnets of the second end magnets is equal, and the axial lengths are equal.
- the first end magnetic steel is composed of three sections of cylindrical magnetic steel adjacent to each other in the axial direction
- the second end magnetic steel is composed of three sections of cylindrical magnetic steel adjacent to each other in the axial direction. composition.
- the outer diameter of the cylindrical magnet farthest from the inner base magnet among the first end magnet and the second end magnet is R 5
- the axial length is L 5
- the outer diameter of the inner base magnet is R 2
- the axial length of the outer ring magnet is L 1 , where R 2 /2 ⁇ R 5 ⁇ R 2 , L 1 /4 ⁇ L 5 ⁇ L 1 /2.
- the radial dimension of the axial through hole of the inner base magnetic steel is the same as the radial dimension of the axial through hole of the first end magnet steel and the second end magnet steel.
- the radial dimension of the axial through holes of the first end magnet steel and the second end magnet steel is directed from the end away from the inner base magnet towards the inner base magnet decrease.
- the included angle ⁇ between the inner peripheral surface of the axial through hole of the first end magnet steel and the second end magnet steel and the radial direction is the same as the angle ⁇ of the first end magnet steel and the radial direction.
- the relationship between the angle ⁇ between the outer peripheral surface of the second end magnet steel and the radial direction is ⁇ 135°.
- the outer magnetic ring magnetic steel is composed of a plurality of arc-shaped plates adjacent to each other in the circumferential direction.
- the inner base magnetic steel includes a diameter-reduced section, and the diameter-reduced section is located in an axial middle section of the inner base magnetic steel and has an outer diameter smaller than that of the rest.
- the axial length of the outer ring magnet is L 1
- the axial length of the end magnet is L 2
- the axial length of the inner base magnet is L 3
- the end magnet is L 3 .
- the axial movement stroke of the steel and the inner base magnetic steel relative to the outer magnetic ring magnetic steel is S
- the difference between the mechanical stroke and the effective stroke is ⁇ S
- L 3 +2L 2 -L 1 S+ ⁇ S
- the value range of ⁇ S/S is [0.1, 3.0].
- the base angle ⁇ of the end magnet steel is 60° to 88°.
- the base angle ⁇ of the end magnet steel is 75°.
- the present invention also provides a motion table, comprising a workpiece table and a base, the workpiece table is configured to be able to rotate and move vertically relative to the base, and the magnetic levitation gravity compensation device is provided below the workpiece table.
- the magnetic levitation gravity compensation device of the present invention solves the problems of complex structure, complicated control and hysteresis in control of the prior art aerodynamic constant stiffness gravity compensation device, and solves the problem that the existing gravity compensation device has zero stiffness or nonlinearity.
- the invention realizes the characteristic that the magnetic levitation output force is linear along the stroke, and the output force at the zero point can offset the vertical structure gravity.
- the invention can not only compensate the gravity of the vertical motion mechanism, but also realize constant stiffness compensation based on the linearization of the magnetic field, balance the elastic deformation reaction force of the flexible mechanism within the stroke range, reduce the load of the vertical actuator, and greatly improve the The vertical performance of the micro-movement stage.
- FIG. 1 is a schematic structural diagram of a maglev gravity compensation device according to a first embodiment of the present invention.
- FIG. 2 is a schematic longitudinal cross-sectional view of the embodiment shown in FIG. 1 .
- FIG. 3 is a schematic diagram of the magnetization direction of the magnetic steel of the embodiment shown in FIG. 1 .
- FIG. 4 is a schematic view of the size of the magnetic steel of the embodiment shown in FIG. 1 .
- FIG. 5 is an output force curve within the stroke range of the embodiment shown in FIG. 1 .
- FIG. 6 is a schematic structural diagram of a maglev gravity compensation device according to a second embodiment of the present invention.
- FIG. 7 is a schematic diagram of the size of the magnetic steel of the magnetic levitation gravity compensation device according to the third embodiment of the present invention (D 2 >D 3 ).
- FIG 8 is a schematic diagram of the size of the magnetic steel of the magnetic levitation gravity compensation device according to the third embodiment of the present invention (D 2 ⁇ D 3 ).
- FIG. 10 is a schematic diagram of the size of the magnetic steel of the magnetic levitation gravity compensation device according to the third embodiment of the present invention (R 3 >R 2 ).
- FIG. 11 is a schematic diagram of the magnetizing direction of the magnetic steel of the magnetic levitation gravity compensation device according to the fourth embodiment of the present invention.
- FIG. 13 is a schematic diagram of the structure of the magnetic levitation gravity compensation device and the magnetization direction of the magnetic steel according to the fourth embodiment of the present invention.
- FIG. 14 is a schematic diagram of a wedge-shaped hole structure of a maglev gravity compensation device according to a fifth embodiment of the present invention.
- FIG. 15 is a schematic structural diagram of a maglev gravity compensation device according to a sixth embodiment of the present invention.
- 16 is a schematic structural diagram of a stepped magnetic steel group according to a seventh embodiment of the present invention.
- 17 is a schematic diagram of the magnetization direction of the stepped magnet steel group according to the seventh embodiment of the present invention.
- FIG. 18 is a schematic view of the dimensions of the magnet steel of the stepped magnet steel group according to the seventh embodiment of the present invention.
- FIG. 19 is a schematic structural diagram of a circular truncated magnetic steel and a circular magnetic steel scheme according to an eighth embodiment of the present invention.
- FIG. 20 is a schematic diagram of the dimensions of the circular truncated magnetic steel and the circular ring magnetic steel according to the eighth embodiment of the present invention.
- Fig. 21 is the layout form of the magnetic levitation gravity compensation device in the motion table according to the present invention.
- the workpiece table can realize the rotation and vertical lifting of the silicon wafers carried on it around the Z direction.
- the workpiece table can be driven by a voice coil motor to achieve its lifting.
- a gravity compensation device such as a maglev gravity compensation device is usually provided.
- an elastic connecting piece can be arranged between the workpiece table and the base. As the workpiece table rises and falls in the vertical direction, the elastic connecting piece will generate elastic force, and the elastic force changes linearly with the stroke of the workpiece table. .
- the invention provides a magnetic levitation gravity compensation device that changes linearly with the stroke, so as to realize the compensation for the gravity of the workpiece table and the elastic force of the elastic connecting piece.
- the magnetic levitation gravity compensation device 100 includes: an inner base magnet 103 , a first end magnet 102 a and a second end magnet 102 b , and an outer magnetic ring magnet 101 .
- the inner base magnet 103 is cylindrical, and the first end magnet 102a and the second end magnet 102b are located at two axial ends of the inner base magnet 103 and extend axially downward and upward.
- the first end magnet 102a is located axially below the inner base magnet 103 and the second end magnet 102b is located axially above the inner base magnet 103 .
- the first end magnetic steel 102a and the second end magnetic steel 102b are in the shape of a truncated cone, and the outer diameters gradually increase downward and upward from the two axial ends near the inner base magnetic steel 103, respectively. big.
- the first end magnet 102a and the second end magnet 102b are each provided with an axial through hole, and the axial through hole and the axial through hole of the inner base magnet 103 have the same diameter and communicate with each other.
- the shape and size of the first end magnet 102 a and the second end magnet 102 b are the same as each other, and are mirror-symmetrical with respect to the middle radial plane of the inner base magnet 103 .
- the outer ring magnet 101 has a cylindrical shape, and is located outside the inner base magnet 103 coaxially with the inner base magnet 103 and radially spaced from the inner base magnet 103 .
- the first end magnet 102a and the second end magnet 102b are adjacent to the inner base magnet 103, but it should be understood that a certain air gap may also be provided therebetween, and the air gap is usually not greater than 1mm .
- the outer magnetic ring magnetic steel 101 is the stator magnetic steel of the gravity compensation device, and the inner base magnetic steel 103 and the first end magnetic steel 102a and the second end magnetic steel 102b are the gravity compensation device mover magnetic steel .
- the outer magnetic ring magnet 101 can also be set as the mover magnet of the gravity compensation device, and the inner base magnet 103 and the first end magnet 102a and the second end magnet 102b are the stator of the gravity compensation device. magnetic steel.
- the vertical force can be understood as the magnetic levitation force of the device, wherein when the outer magnetic ring magnetic steel 101 and the inner base magnetic steel 103 are axially centered relative to each other, it is the device zero point, Since the device needs to compensate the gravity of the workpiece table when the device is at the zero point, the amplitude of the output magnetic buoyancy must be equal to the gravity of the workpiece table, and the elastic force of the elastic connector is zero.
- the output magnetic buoyancy direction of the magnetic levitation gravity compensation device is vertically upward. Since the output force of the elastic connecting piece arranged between the workpiece table and the base changes linearly with the vertical movement of the workpiece table, only when the output magnetic levitation force of the device also changes linearly with the vertical movement of the workpiece table, and both change When the slopes are equal, the magnetic levitation gravity compensation device can fully realize the compensation effect of the gravity of the workpiece table and the elastic force of the elastic connecting piece. Based on this, the outer diameters of the first end magnetic steel 102a and the second end magnetic steel 102b in the device need to gradually increase from the ends close to the inner base magnetic steel 103 downward and upward respectively.
- FIG. 3 shows the magnetization direction of each magnetic steel in the maglev gravity compensation device 100 .
- the magnetization directions of the inner base magnet 103 and the second end magnet 102b are the same and both are axially upward, while the magnetization direction of the first end magnet 102a is axial downward, and the outer ring magnet 101 The magnetization direction is radially outward.
- the magnetization direction of the outer ring magnet 101 can also be set to be radially inward, the magnetization direction of the first end magnet 102a is axially upward, and the second end magnet 102b and the inner magnet 102b
- the magnetization directions of the base magnetic steel 103 are the same and both are axially downward.
- the outer magnetic ring magnetic steel 101 is formed by splicing 8 pieces of magnetic steel.
- the 8 segmented magnets are arc-shaped plate magnets bisected radially by a cylinder at equal angular intervals of 45°.
- the outer magnetic ring magnetic steel 101 can also be formed by splicing other number of divided magnetic steels.
- the number of divided pieces N is set to an even number, such as 2 Blocks, 4 blocks, 6 blocks, etc.
- the outer magnetic ring magnetic steel 101 is formed by splicing the divided magnetic steels to facilitate the magnetization and processing of the magnetic steels.
- the value of the pole arc coefficient a of the magnetic steel is positively related to the output stiffness of the magnetic levitation gravity compensation device, and the pole arc coefficient a of the magnetic steel is the pole arc coefficient of the magnetic steel.
- the ratio of the arc length to the polar distance, the polar arc coefficient a is preferably [0.7, 0.95].
- the outer diameter of one end of the first end magnet 102 a and the second end magnet 102 b adjacent to the inner base magnet 103 is larger than the outer diameter of the inner base magnet 103 .
- the outer diameter of one end of the first end magnet 102a and the second end magnet 102b adjacent to the inner base magnet 103 may also be equal to or smaller than the outer diameter of the inner base magnet 103, and the first end magnet
- the size of the outer diameter of the steel 102a and the second end magnetic steel 102b affects the slope of the magnetic levitation force output by the magnetic levitation gravity compensation device within the stroke range.
- FIG. 4 shows a schematic view of the size of the maglev gravity compensation device 100 .
- the axial lengths of the outer magnetic ring magnetic steel 101, the first end magnetic steel 102a, the second end magnetic steel 102b, and the inner base magnetic steel 103 are L 1 , L 2 and L 3 , respectively.
- the radius of one end of the first end magnet 102a and the second end magnet 102b adjacent to the inner base magnet 103 and the radius of the inner base magnet 103 are denoted by R 2 and R 3 respectively, the first end magnet 102a and the second end magnet 102a
- the radius of the end of the end magnet 102b away from the inner base magnet 103 is denoted by R 21
- the diameter of the axial through hole of the first end magnet 102a, the second end magnet 102b and the inner base magnet 103 is denoted by D 0
- the base angle of the first end magnet 102a and the second end magnet 102b is denoted by ⁇ .
- the relationship between the radius of one end of the first end magnetic steel 102a and the second end magnetic steel 102b adjacent to the inner base magnetic steel 103 and the radius of the inner base magnetic steel 103 depends on the compensation required by the magnetic levitation gravity compensation device at the zero point.
- the size of the weight that is, the gravity of the workpiece table. In this embodiment, preferably R 2 >R 3 .
- the axial through hole diameter D 0 is related to the stiffness of the magnetic levitation gravity compensation device.
- the first end magnetic steel 102a, the second end magnetic steel 102b and the axial through holes of the inner base magnetic steel 103 have the same size.
- the bottom angle ⁇ of the first end magnet 102a and the second end magnet 102b determines the linearity of the magnetic field, which in turn affects the stiffness of the magnetic levitation gravity compensation device.
- the value range of the base angle ⁇ is [60°, 88°].
- the base angle ⁇ can be expressed as In this embodiment, the bottom angle ⁇ of the first end magnet 102a and the second end magnet 102b is preferably 75°.
- the output force simulation curve of the maglev gravity compensation device 100 is shown in FIG. 5 .
- the horizontal axis represents the stroke of the maglev gravity compensation device
- the vertical axis represents the output force amplitude.
- the two stroke end points and the zero point and their corresponding output forces are marked in the figure.
- x is the limit displacement in one direction
- G is the gravity of the workpiece table to be compensated by a single maglev gravity compensation device.
- the design stiffness of the maglev gravity compensation device is k
- FIG. 6 shows a maglev gravity compensation device 200 according to another embodiment of the present invention.
- This embodiment is basically the same as the maglev gravity compensation device 100 , that is, the maglev gravity compensation device 200 includes: an inner base magnet 203 , a first end magnet 202 a and a second end magnet 202 b , and an outer magnetic ring magnet 201 .
- the inner base magnet 203 is cylindrical, and the first end magnet 202a and the second end magnet 202b are respectively located at two axial ends of the inner base magnet 203 and axially downward from the inner base magnet 203 and extending upwards.
- the first end magnet 202a is located axially below the inner base magnet 203 and the second end magnet 202b is located axially above the inner base magnet 203 .
- the first end magnet 202a and the second end magnet 202b are truncated cones, and the outer diameters gradually increase from the two axial ends adjacent to the inner base magnet 203 toward the direction away from the inner base magnet 203 .
- the first end magnet 202a and the second end magnet 202b are each provided with an axial through hole, and the axial through hole and the axial through hole of the inner base magnet 203 have the same diameter and communicate with each other.
- the shape and size of the first end magnet 202 a and the second end magnet 202 b are the same as each other, and are mirror-symmetrical with respect to the axial mid-section radial plane of the inner base magnet 203 .
- the outer ring magnet 201 has a cylindrical shape, and is located outside the inner base magnet 203 coaxially with the inner base magnet 203 and radially spaced from the inner base magnet 203 .
- the difference between the maglev gravity compensation device 200 and the maglev gravity compensation device 100 is that the outer magnetic ring magnetic steel 201 is composed of a radially magnetized magnetic steel.
- a maglev gravity compensation device 300 according to a third embodiment of the present invention is shown in FIGS. 7 and 8 .
- This embodiment is basically the same as the maglev gravity compensation device 100, that is, the maglev gravity compensation device 300 includes: an inner base magnet 303, a first end magnet 302a, a second end magnet 302b, and an outer magnetic ring magnet 301 .
- the inner base magnet 303 is cylindrical, and the first end magnet 302a and the second end magnet 302b are respectively located at the two axial ends of the inner magnet 303 and axially downward from the inner magnet 303 and extending upwards.
- the first end magnet 302a is located axially below the inner base magnet 303 and the second end magnet 302b is located axially above the inner base magnet 303 .
- the first end magnet 302a and the second end magnet 302b are truncated cones, and the outer diameters gradually increase from the two axial ends adjacent to the inner base magnet 303 toward the direction away from the inner base magnet 303 .
- the first end magnet 302a and the second end magnet 302b are respectively provided with axial through holes, and the axial through holes and the axial through holes of the inner base magnet 303 communicate with each other.
- the shape and size of the first end magnet 302 a and the second end magnet 302 b are the same as each other, and are mirror-symmetrical with respect to the axial mid-section radial plane of the inner base magnet 303 .
- the outer ring magnet 301 is cylindrical, and is located outside the inner base magnet 303 coaxially with the inner base magnet 303 and radially spaced from the inner base magnet 303 .
- the difference between the magnetic levitation gravity compensation device 300 and the magnetic levitation gravity compensation device 100 is that the axial through holes of the first end magnetic steel 302 a and the second end magnetic steel 302 b have different diameters from the axial through holes of the inner base magnetic steel 303 .
- the axial through hole diameter of the first end magnet 302a and the second end magnet 302b may be smaller ( FIG. 7 ) or larger ( FIG. 8 ) than the axial through hole diameter of the inner base magnet 303 .
- the diameter relationship between the axial through holes of the first end magnetic steel 302a and the second end magnetic steel 302b and the axial through hole of the inner base magnetic steel 303 is related to the installation method of the magnetic steel, and is related to the output of the magnetic levitation gravity compensation device.
- the stiffness of the force is independent of the zero point compensation gravity value.
- the gravity value compensated by the zero position of the magnetic levitation gravity compensation device is related to the magnetic field strength provided by the inner base magnetic steel 303. Under the same condition of the outer magnetic ring magnetic steel 301, the greater the magnetic field strength of the inner base magnetic steel 303, the higher the compensation at the zero position. The larger the gravity value.
- maglev gravity compensation device 400 illustrates a maglev gravity compensation device 400 according to a fourth embodiment of the present invention.
- This embodiment is basically the same as the maglev gravity compensation device 100 , that is, the maglev gravity compensation device 400 includes: an inner base magnet 403 , a first end magnet 402 a and a second end magnet 402 b , and an outer magnetic ring magnet 401 .
- the inner base magnet 403 is cylindrical, and the first end magnet 402a and the second end magnet 402b are respectively located at two axial ends of the inner base magnet 403 and axially downward from the inner base magnet 403 and extending upwards.
- the first end magnet 402a is positioned axially below the inner base magnet 403 and the second end magnet 402b is positioned axially above the inner base magnet 403 .
- the first end magnet 402a and the second end magnet 402b are truncated cones, and the outer diameters gradually increase from the two axial ends of the inner base magnet 403 toward the direction away from the inner base magnet 403 .
- the first end magnet 402a and the second end magnet 402b are each provided with an axial through hole, and the axial through hole and the axial through hole of the inner base magnet 403 communicate with each other.
- the shape and size of the first end magnet 402a and the second end magnet 402b are the same as each other, and are mirror-symmetrical with respect to the axial midpoint radial plane of the inner base magnet 403.
- the outer ring magnet 401 has a cylindrical shape, and is located outside the inner base magnet 403 coaxially with the inner base magnet 403 and radially spaced from the inner base magnet 403 .
- the outer diameter of the end of the first end magnet 102a and the second end magnet 102b adjacent to the inner base magnet 103 is smaller than the outer diameter of the inner base magnet 103, while in the magnetic levitation gravity In the compensation device 400 , the outer diameter of one end of the first end magnet 402 a and the second end magnet 402 b adjacent to the inner base magnet 403 is equal to or smaller than the outer diameter of the inner base magnet 403 .
- FIG. 11 shows a maglev gravity compensation device 500 according to a fourth embodiment of the present invention.
- This embodiment is basically the same as the maglev gravity compensation device 100, that is, the maglev gravity compensation device 500 includes: an inner base magnet 503, a first end magnet 502a and a second end magnet 502b, and an outer magnetic ring magnet 501 .
- the inner base magnet 503 is cylindrical, and the first end magnet 502a and the second end magnet 502b are respectively located at the two axial ends of the inner base magnet 503 and axially downward from the inner base magnet 503 and extending upwards.
- the first end magnet 502a is located axially below the inner base magnet 503 and the second end magnet 502b is located axially above the inner base magnet 503 .
- the first end magnet 502a and the second end magnet 502b are truncated cones, and the outer diameter gradually increases from the two axial ends adjacent to the inner base magnet 503 toward the direction away from the inner base magnet 503 .
- the first end magnet 502a and the second end magnet 502b are each provided with an axial through hole, and the axial through hole and the axial through hole of the inner base magnet 503 communicate with each other.
- the shape and size of the first end magnet 502 a and the second end magnet 502 b are the same as each other, and are mirror-symmetrical with respect to the axial mid-section radial plane of the inner base magnet 503 .
- the outer ring magnet 501 is cylindrical, and is located outside the inner base magnet 503 coaxially with the inner base magnet 503 and radially spaced from the inner base magnet 503 .
- the magnetization direction of the inner base magnet 103 is the axial direction
- the magnetization direction of the inner base magnet 503 is the same as that of the outer magnetic ring magnet 501.
- the magnetic directions are the same and both are radially outward.
- the magnetization direction of the first end magnet 502a and the second end magnet 502b can also be set to be from the end away from the inner base magnet 503 toward the inner base magnet. 503, while the magnetization directions of the inner base magnet 503 and the outer ring magnet 501 are the same and both are radially inward.
- the gravity compensation device does not need to compensate the gravity of the workpiece table at the zero point, therefore, the magnetic levitation gravity compensation device 500 can adopt the above-mentioned magnetization direction.
- the inner base magnetic steel 504 can be formed by splicing a plurality of radially magnetized segmented magnetic steels (refer to the maglev gravity compensation device 800 of the seventh embodiment).
- the inner base magnetic steel 504 can also be replaced by a cylinder 505 made of an unmagnetized high-permeability material. As shown in FIG. 13 , when the inner base magnetic steel is not magnetized, the output force stiffness of the magnetic levitation gravity compensation device will be reduced, and the high magnetic permeability material in this embodiment is preferably a permalloy.
- FIG. 12 shows the output force curve of the maglev gravity compensation device 500 .
- the horizontal axis is the stroke of the magnetic levitation gravity compensation device
- the vertical axis is the output force amplitude. It can be seen from the figure that the output force amplitude of the maglev gravity compensation device at the zero point is zero.
- the output force range of the maglev gravity compensation device can be obtained as [-F, F] .
- FIG. 14 shows a maglev gravity compensation device 600 according to a fifth embodiment of the present invention.
- This embodiment is basically the same as the maglev gravity compensation device 100 , that is, the maglev gravity compensation device 600 includes: an inner base magnetic steel 603 , a first end magnetic steel 602 a and a second end magnetic steel 602 b , and an outer magnetic ring magnetic steel 601 .
- the inner base magnet 603 is cylindrical, and the first end magnet 602a and the second end magnet 602b are located at the two axial ends of the inner base magnet 603 and are axially downward from the inner base magnet 603 and extending upwards.
- the first end magnet 602a is located axially below the inner base magnet 603 and the second end magnet 602b is located axially above the inner base magnet 603 .
- the first end magnet 602a and the second end magnet 602b are truncated cones, and the outer diameters gradually increase from the two axial ends of the inner base magnet 603 toward the direction away from the inner base magnet 603 .
- the first end magnet 602a and the second end magnet 602b are each provided with an axial through hole, and the axial through hole and the axial through hole of the inner base magnet 603 communicate with each other.
- the shape and size of the first end magnet 602 a and the second end magnet 602 b are the same as each other, and are mirror-symmetrical with respect to the middle radial plane of the inner base magnet 603 .
- the outer ring magnet 601 has a cylindrical shape, and is located outside the inner base magnet 603 coaxially with the inner base magnet 603 and radially spaced from the inner base magnet 603 .
- the difference is that in the maglev gravity compensation device 100, the diameters of the axial through holes of the first end magnet 602a and the second end magnet 602b remain constant along the axial direction, while in the maglev gravity compensation device 600, the first end The diameters of the axial through holes of the first magnetic steel 602a and the second end magnetic steel 602b gradually increase from the inner base magnetic steel to the direction away from the inner base magnetic steel, that is, the axial through holes thereof are truncated.
- the truncated through hole is more difficult to process, but by adjusting the bottom angle ⁇ of the truncated through hole of the first end magnet 602a and the second end magnet 602b and the third
- the relationship between the bottom angle ⁇ of the magnetic steel at the first end and the second end can fine-tune the output stiffness k of the magnetic levitation gravity compensation device to a certain extent.
- the relationship of ⁇ can be expressed as: (1) 60° ⁇ 88°, (2) ⁇ 135°.
- FIG. 15 shows a maglev gravity compensation device 700 according to a sixth embodiment of the present invention.
- This embodiment is basically the same as the maglev gravity compensation device 100 , that is, the maglev gravity compensation device 700 includes: an inner base magnet 703 , a first end magnet 702 a and a second end magnet 702 b , and an outer magnetic ring magnet 701 .
- the first end magnet 702a and the second end magnet 702b are located at both axial ends of the inner base magnet 703 and extend axially downward and upward from the inner base magnet 703, respectively.
- the first end magnet 702a is located axially below the inner base magnet 703 and the second end magnet 702b is located axially above the inner base magnet 703 .
- the first end magnet 702a and the second end magnet 702b are truncated cones, and the outer diameter gradually increases from the two axial ends of the inner base magnet 703 toward the direction away from the inner base magnet.
- the shape and size of the first end magnet 702 a and the second end magnet 702 b are the same as each other, and are mirror-symmetrical with respect to the middle radial plane of the inner base magnet 703 .
- the outer ring magnet 701 is cylindrical, and is located outside the inner base magnet 703 coaxially with the inner base magnet 703 and radially spaced from the inner base magnet 703 .
- the inner base magnet 703 is cylindrical
- the first end magnet 702a and the second end magnet 702b are truncated cones
- the inner base magnet 703 and the first end magnet 702a and the second end magnet 702a The end magnets 702b are not provided with axial through holes.
- This arrangement increases the difficulty of assembling the magnetic steel to a certain extent, but the outer diameters of the first end magnetic steel 702a, the second end magnetic steel 702b and the inner base magnetic steel 703 are also reduced accordingly, and the magnetic levitation gravity compensation device Under the premise that the design output stiffness k remains unchanged, the volume of the maglev gravity compensation device can be reduced to a certain extent; or the design output stiffness k of the maglev gravity compensation device can be further improved under the premise that the volume of the maglev gravity compensation device remains unchanged.
- the first end magnetic steel 702a and the second end magnetic steel 702b can also be composed of a plurality of cylindrical shafts stacked up and down to form a stepped magnetic steel.
- the steel group is formed, wherein the number of axial segments of the magnet steel in the stepped magnet steel group is N t , and the difference between the radial size and the axial size of the axially adjacent magnet steel needs to be obtained through simulation iteration according to the design requirements.
- the number of blocks N t of the axial magnets in the stepped magnet group is in the range of N t ⁇ 2, N t ⁇ Z, and the radial size difference between the adjacent magnets in the axial direction determines the magnetic levitation gravity compensation device.
- the output stiffness of the compensating device, the axial dimension value and the difference of the adjacent magnetic steel in the axial direction determine the output displacement of the compensation device.
- the number of blocks N t of the axial magnetic steel of the stepped magnetic steel group is 3, and the radial dimension difference of the adjacent magnetic steel in the axial direction is both 2.0 mm.
- FIG. 16 shows a maglev gravity compensation device 800 according to a seventh embodiment of the present invention.
- the maglev gravity compensation device 800 includes: an inner base magnet 805 , first end magnets 804 a , 803 a and 802 a , second end magnets 804 b , 803 b and 802 b , and an outer magnetic ring magnet 801 .
- the inner base magnetic steel 805 is cylindrical, and the first end magnets 804a, 803a and 802a and the second end magnets 804b, 803b and 802b are respectively located at the two axial ends of the inner base magnet 805 and sequentially from the inner
- the base magnet 805 extends axially downward and upward.
- first end magnets 804a, 803a and 802a are located axially below the inner base magnet 805 and the second end magnets 804b, 803b and 802b are located axially of the inner base magnet 805 above.
- Each of the first end magnets 804a, 803a, and 802a and each of the second end magnets 804b, 803b, and 802b are cylindrical, and the outer diameter is along the direction from the two ends of the inner base magnet 805 away from the inner base magnet. The direction of 805 increases sequentially.
- Each of the first end magnets 804a, 803a, and 802a and each of the second end magnets 804b, 803b, and 802b are provided with axial through holes, and the axial through holes are the same as the diameter of the axial through holes of the inner base magnet 805. identical and connected to each other.
- the shape and size of each of the first end magnets 804a, 803a and 802a and each of the second end magnets 804b, 803b and 802b are respectively the same as each other, and are mirror-symmetrical with respect to the axial mid-section radial plane of the inner base magnet 805 .
- the outer ring magnet 801 has a cylindrical shape and is located outside the inner base magnet 805 coaxially with the inner base magnet 805 and radially spaced from the inner base magnet 805 .
- FIG. 17 shows a schematic diagram of the magnetizing direction of the magnetic steel of the maglev gravity compensation device 800 .
- the magnetization direction of the outer ring magnet 801 is radial magnetization, while the magnetization direction of the inner base magnet 805 and the first and second end magnets is axial magnetization, wherein the first end magnets are magnetized in the axial direction.
- the magnetization direction of the magnets 804a, 803a and 802a is axial upward, while the magnetization direction of the second end magnets 804b, 803b and 802b is axial downward, and the magnetization direction of the inner base magnet 805 is Axially upward, the magnetization direction of the outer ring magnetic steel 801 is radially outward.
- the magnetization direction of the outer magnet ring magnet 801 may be radially inward, the magnetization direction of each of the first end magnets 804a, 803a and 802a is axially downward, and the magnetization direction of each of the second end magnets 804a, 803a and 802a is axially downward.
- the magnetization directions of the end magnets 804b, 803b and 802b are axially upward, and the magnetization direction of the inner base magnets 805 is axially downward.
- the magnetization direction of the outer ring magnet 801 may be axial magnetization, and the magnetization direction of the inner base magnet 805 and each of the first and second end magnets may be radial magnetization.
- FIG. 18 shows a schematic view of the size of the maglev gravity compensation device 800 according to the seventh embodiment of the present invention.
- the number of blocks N t of the axial magnetic steel of the magnetic steel group is 3.
- the axial lengths of the outer ring magnet 801, the inner base magnet 805, the first end magnets 804a, 803a and 802a and the second end magnets 804b, 803b and 802b are respectively determined by L 1 , L 5 , L 4.
- L 3 and L 2 indicate that the axial through holes of the inner base magnet 805 and the first and second end magnets are the same and are indicated by D 0 , the inner base magnet 805 and the ring magnet 802-804
- the radii of are represented by R 5 and R 4 , R 3 and R 2 respectively.
- the number of blocks N t of the axial magnetic steel of the stepped magnetic steel group is 3, and the radial dimension difference between the adjacent magnetic steels in the axial direction is both 2.0 mm.
- the design criteria for the size relationship of the magnetic steel at each end can be deduced.
- Li is the axial length of each end magnet
- the axial length of the end magnet farthest from the inner base magnet is set as L 2
- the end magnet closest to the inner base magnet has the length of L 2 .
- the axial length is set to L Nt-1 .
- the diameter R 5 and the axial length L 5 of the inner base magnet are closely related to the weight of the vertical motion mechanism of the workpiece table.
- the value range of R 5 is R 2 /2 ⁇ R 5 ⁇ R 2
- the value of L 5 The range L 1 /4 ⁇ L 5 ⁇ L 1 /2. If the weight to be compensated by the maglev gravity compensation device increases or decreases, in order to keep the output stiffness of the compensation device unchanged, it is only necessary to adjust R 5 and L 5 .
- FIG. 19 shows a maglev gravity compensation device 900 according to an eighth embodiment of the present invention.
- the magnetic levitation gravity compensation device 900 includes: an inner base magnetic steel 903 , a first end magnetic steel 902 a , a second end magnetic steel 902 b , and an outer magnetic ring magnetic steel 901 .
- the first end magnet 902a and the second end magnet 902b are respectively located at both axial ends of the inner base magnet 903 and extend axially downward and upward from the inner base magnet 903 .
- the first end magnet 902a is located axially below the inner base magnet 903 and the second end magnet 902b is located axially above the inner base magnet 903 .
- the first end magnet 902a and the second end magnet 902b are truncated cones, and the outer diameter gradually increases from the two axial ends of the inner base magnet 903 toward the direction away from the inner base magnet 903 .
- the shape and size of the first end magnet 902 a and the second end magnet 902 b are the same as each other, and are mirror-symmetrical with respect to the axial mid-section radial plane of the inner base magnet 903 .
- the outer ring magnet 901 has a cylindrical shape and is located outside the inner base magnet 903 coaxially with the inner base magnet 903 and radially spaced from the inner base magnet 903 . It should be understood that the first end magnetic steel 902a and the second end magnetic steel 902b can also be formed by a group of cylindrical magnetic steels adjoining in sequence in the axial direction.
- the axial middle section of the inner base magnetic steel 903 of the magnetic levitation gravity compensation device 900 has a diameter reduction section 904, and the axial ends of the diameter reduction section 904 are the first axial section 903a and the second axial section respectively. Segment 903b.
- the diameter of the diameter-reduced section 904 is smaller than the diameters of the first axial section 903a and the second axial section 903b.
- the magnetization directions of the first end magnetic steel 902a and the first axial segment 903a are both axially downward, while the magnetization directions of the diameter-reduced segment 904 , the second end magnet 902b and the second axial segment 903b All along the axis upwards.
- the stiffness of the magnetic levitation gravity compensation device 900 is slightly larger near the zero point, while the stiffness at the end points on both sides is unchanged, which can be applied to the working condition of the large damping force near the zero point.
- FIG. 20 shows a schematic size diagram of the maglev gravity compensation device 900 .
- the diameters of the axial through holes of the first end magnetic steel 902a and the second end magnetic steel 902b and the inner base magnetic steel 903 are equal, and both are D 0 .
- the diameter of the diameter-reduced section 904 is represented by R 4 , where R 4 ⁇ R 3 .
- the inner base magnet, the first end magnet and the second end magnet have a common central axis, and are rotationally symmetrical about the central axis, so as to ensure that the generated The magnetic force is evenly distributed along the circumference.
- the present invention also provides a motion table, the motion table includes a workpiece table and a base, and the workpiece table is arranged to be able to rotate and move vertically relative to the base.
- the workpiece table is used to carry the workpiece to be processed.
- Figure 21 shows a bottom view of a workpiece table using the maglev gravity compensation device according to the present invention.
- a concave cavity is provided under the workpiece table for accommodating the magnetic levitation gravity compensation device according to the present invention.
- the cavity below the workpiece table can be one, two, three or four.
- the figure shows a schematic diagram of the center point arrangement of a maglev gravity compensation device, two maglev gravity compensation devices arranged side by side, three maglev gravity compensation devices arranged in a regular triangle, for example, and four maglev gravity compensation devices arranged in a square. It is understood that other numbers and other arrangements of maglev gravity compensation devices may also be provided.
- the shape of the worktable using the maglev gravity compensation device is not limited to the square shown in the figure, but can be set to any shape as required. It should be understood that the vertical line where the equivalent center of gravity of the maglev gravity compensation device is located should be collinear with the vertical line where the center of gravity of the vertical motion mechanism is located.
- the magnetic levitation gravity compensation device can provide a magnetic buoyancy force that changes linearly with the stroke, that is, it can compensate the gravity of the workpiece table and the elastic force generated by the elastic connecting device with constant stiffness, and can satisfy the gravity compensation of the motion table in some cases. demand.
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Abstract
Description
Claims (18)
- 一种磁浮重力补偿装置,其特征在于,包括:内基磁钢,所述内基磁钢沿轴向延伸;第一端部磁钢和第二端部磁钢,所述第一端部磁钢和所述第二端部磁钢分别位于所述内基磁钢的两个轴向端并沿轴向延伸,且所述第一端部磁钢和第二端部磁钢的外径分别沿远离所述内基磁钢的所述两个轴向端方向逐渐增大;外磁环磁钢,所述外磁环磁钢呈筒状,与所述内基磁钢同轴地位于所述内基磁钢外且与所述内基磁钢径向间隔开。
- 根据权利要求1所述的磁浮重力补偿装置,其特征在于,所述第一端部磁钢和所述第二端部磁钢的充磁方向为从所述内基磁钢沿轴向向外,所述外磁环磁钢的充磁方向为径向向外。
- 根据权利要求1所述的磁浮重力补偿装置,其特征在于,所述第一端部磁钢和所述第二端部磁钢相对于所述内基磁钢的轴向平分面镜像对称。
- 根据权利要求1所述的磁浮重力补偿装置,其特征在于,所述内基磁钢、所述第一端部磁钢和所述第二端部磁钢中心轴线彼此重合且关于所述中心轴线旋转对称。
- 根据权利要求1所述的磁浮重力补偿装置,其特征在于,所述内基磁钢具有轴向通孔,所述第一端部磁钢和第二端部磁钢具有轴向通孔。
- 根据权利要求1所述的磁浮重力补偿装置,其特征在于,所述内基磁钢呈圆筒状,所述第一端部磁钢由沿轴向彼此邻接的多段筒状磁钢组成,所述第二端部磁钢由沿轴向彼此邻接的多段筒状磁钢组成,所述多段筒状磁钢的内径相同,而各外径从远离所述内基磁钢的筒状磁钢朝向靠近所述内基磁钢的筒状磁钢依次减小。
- 根据权利要求1或6所述的磁浮重力补偿装置,其特征在于,所述第一端部磁钢的多段筒状磁钢中各相邻筒状磁钢的外径之差相等,且轴向长度相等;以及所述第二端部磁钢的多段筒状磁钢中各相邻筒状磁钢的外径之差相等,且轴向长度相等。
- 根据权利要求6所述的磁浮重力补偿装置,其特征在于,所述第一端部磁钢由沿轴向彼此邻接的三段筒状磁钢组成,所述第二端部磁钢由沿轴向彼此邻接的三段筒状磁钢组成。
- 根据权利要求1或6所述的磁浮重力补偿装置,其特征在于,所述第一端部磁钢和所述第二端部磁钢中最远离所述内基磁钢的筒状磁钢的外径为R 5,轴向长度为L 5,内基磁钢的外径为R 2,外磁环磁钢的轴向长度为L 1,其中R 2/2≤R 5≤R 2,L 1/4≤L 5≤L 1/2。
- 根据权利要求6所述的磁浮重力补偿装置,其特征在于,所述内基磁钢的轴向通孔的径向尺寸与所述第一端部磁钢和第二端部磁钢的轴向通孔的径向尺寸相同。
- 根据权利要求6所述的磁浮重力补偿装置,其特征在于,所述第一端部磁钢和第二端部磁钢的轴向通孔的径向尺寸自远离所述内基磁钢的端部朝向所述内基磁钢减小。
- 根据权利要求11所述的磁浮重力补偿装置,其特征在于,所述第一端部磁钢和第二端部磁钢的所述轴向通孔的内周面与径向方向的夹角β与所述第一端部磁钢和第二端部磁钢的外周面与径向方向的夹角α的关系为α≤β≤135°。
- 根据权利要求1所述的磁浮重力补偿装置,其特征在于,所述外磁环磁钢由沿周向彼此邻接的多个弧形板组成。
- 根据权利要求1所述的磁浮重力补偿装置,其特征在于,所述内基磁钢包括径缩段,所述径缩段位于内基磁钢的轴向中段且外径小于其余部分的外径。
- 根据权利要求1所述的磁浮重力补偿装置,其特征在于,所述外磁环磁钢的轴向长度为L 1,端部磁钢的轴向长度为L 2,内基磁钢的轴向长度为L 3,所述端部磁钢和所述内基磁钢相对于所述外磁环磁钢沿轴向移动行程为S,则L 3+2L 2-L 1=S+ΔS,其中ΔS/S的取值范围为[0.1,3.0]。
- 根据权利要求1所述的磁浮重力补偿装置,其特征在于,所述端部磁钢的底角为α为60°至88°。
- 根据权利要求16所述的磁浮重力补偿装置,其特征在于,所述端部磁钢的底角为α为75°。
- 一种运动台,其特征在于,包括工件台和底座,所述工件台设置成能够相对于所述底座旋转和垂向移动,所述工件台下方设有根据权利要求1-16中任一项所述的磁浮重力补偿装置。
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JP2023528446A JP2023549227A (ja) | 2020-12-01 | 2021-02-10 | 磁気浮上式重力補償装置及び該装置を含む移動ステージ |
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CN113048185B (zh) * | 2021-03-09 | 2022-04-19 | 复旦大学 | 一种重力补偿器及承载装置 |
CN112994526B (zh) * | 2021-04-23 | 2022-05-24 | 上海隐冠半导体技术有限公司 | 一种磁浮重力补偿器 |
CN113471112B (zh) * | 2021-07-16 | 2024-02-20 | 上海隐冠半导体技术有限公司 | 磁浮重力补偿装置和微动台 |
CN113745138B (zh) * | 2021-09-03 | 2024-03-22 | 上海隐冠半导体技术有限公司 | 磁浮装置和微动台 |
CN117307647B (zh) * | 2023-11-27 | 2024-03-01 | 上海隐冠半导体技术有限公司 | 一种磁弹簧装置及磁弹簧设计方法 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100026431A1 (en) * | 2008-07-29 | 2010-02-04 | Thales | Magnetically suspended gyroscopic actuator device |
CN102859215A (zh) * | 2010-04-20 | 2013-01-02 | 约翰尼斯海登海恩博士股份有限公司 | 具有无源的重力补偿功能的引导装置和能垂直运动地被支承的平台 |
CN105988304A (zh) * | 2015-02-28 | 2016-10-05 | 上海微电子装备有限公司 | 一种可调磁浮力重力补偿器 |
CN112201611A (zh) * | 2020-12-01 | 2021-01-08 | 上海隐冠半导体技术有限公司 | 磁浮重力补偿装置以及包括该装置的运动台 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2596836B2 (ja) * | 1989-08-28 | 1997-04-02 | 信越化学工業株式会社 | 磁場発生装置 |
JP5808659B2 (ja) * | 2011-12-12 | 2015-11-10 | 株式会社日立メディコ | 磁気共鳴イメージング装置及びT1ρイメージング法 |
CN105281531B (zh) * | 2014-07-11 | 2018-06-01 | 上海微电子装备(集团)股份有限公司 | 具有重力补偿功能的音圈电机 |
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Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100026431A1 (en) * | 2008-07-29 | 2010-02-04 | Thales | Magnetically suspended gyroscopic actuator device |
CN102859215A (zh) * | 2010-04-20 | 2013-01-02 | 约翰尼斯海登海恩博士股份有限公司 | 具有无源的重力补偿功能的引导装置和能垂直运动地被支承的平台 |
CN105988304A (zh) * | 2015-02-28 | 2016-10-05 | 上海微电子装备有限公司 | 一种可调磁浮力重力补偿器 |
CN112201611A (zh) * | 2020-12-01 | 2021-01-08 | 上海隐冠半导体技术有限公司 | 磁浮重力补偿装置以及包括该装置的运动台 |
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