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CN103422065B - magnetron sputtering apparatus and magnetron control method - Google Patents

magnetron sputtering apparatus and magnetron control method Download PDF

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Publication number
CN103422065B
CN103422065B CN201210152625.0A CN201210152625A CN103422065B CN 103422065 B CN103422065 B CN 103422065B CN 201210152625 A CN201210152625 A CN 201210152625A CN 103422065 B CN103422065 B CN 103422065B
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magnetron
target
gear
sputtering apparatus
unit
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CN103422065A (en
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陈春伟
夏威
李杨超
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Beijing North Microelectronics Co Ltd
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Beijing North Microelectronics Co Ltd
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Abstract

The present invention provides a kind of magnetron sputtering apparatus and magnetron control method, magnetron sputtering apparatus includes reaction chamber, target, magnetron, drive mechanism, magnetron positioning unit and control device, drive mechanism is connected with controlling device, and rotational velocity and the revolution speed of magnetron is controlled according to the control signal controlling device, magnetron positioning unit is for determining the initial position of magnetron, control device for determining the service cycle of magnetron according to initial position, and according to controlling rotational velocity and the revolution speed of drive mechanism service cycle, thus on the premise of magnetron is constant by each position number of times of target, control magnetron residence time in target unit are, to improve the etching homogeneity of target.This magnetron sputtering apparatus can improve the utilization rate of target, thus reduces the operating cost of magnetron sputtering apparatus;And the time changing target can be reduced, thus improve the utilization rate of magnetron sputtering apparatus.

Description

Magnetron sputtering apparatus and magnetron control method
Technical field
The invention belongs to plasma processing techniques field, relate to a kind of magnetron sputtering apparatus and Magnetron control method.
Background technology
Magnetron sputtering technique is to introduce magnetic field at target material surface, utilizes magnetic field to carry out restraining belt electrochondria Son, increases the collision probability of electronics and process gas, such that it is able to improve the density of plasma, And then working (machining) efficiency can be improved.Therefore magnetron sputtering process equipment is widely used in integrated Circuit and the production of thin film solar.
Fig. 1 is the structure diagram of typical magnetron sputtering process equipment.As it is shown in figure 1, magnetic Control sputtering process equipment includes reaction chamber 1, is provided with for carrying in the bottom of reaction chamber 1 The electrostatic chuck 2 of workpiece to be machined.It is provided with target 3, at target at the top of reaction chamber 1 The magnetron 6 being arranged over for improving sputter rate of 3, magnetron 6 is in drive mechanism 7 Driving under target 3 upper surface rotate.
Fig. 2 is the structure diagram of the drive mechanism for driving magnetron.As in figure 2 it is shown, Drive mechanism include rotating shaft the 20, first gear (not shown), the second gear 22, Three gear the 23, the 4th gear 24 and the first connecting plate 28, one end of rotating shaft 20 and motors (not shown) connects, and the other end and the first connecting plate 28 and the first gear connect. First gear, the second gear the 22, the 3rd gear the 23, the 4th gear 24 are fixed on the first connection On plate 28.Second gear 22 engages with the first gear, the 3rd gear 23 and the second gear 22 Engagement, the 4th gear 24 engages with the 3rd gear 23.Magnetron 6 is by the second connecting plate 25 are connected with the rotating shaft of the 4th gear 24.When motor-driven rotatable shaft 20 rotates, the first tooth Wheel, the second gear the 22, the 3rd gear 23 and the 4th gear 24 rotate centered by rotating shaft 20, Meanwhile, the first gear, the second gear the 22, the 3rd gear the 23, the 4th gear 24 are respectively Around respective central shaft rotation so that magnetron 6 while around the shaft 20 revolution with the The central shaft of four gears 24 is rotating shaft rotation, and then makes magnetron 6 at the upper surface of target 3 Scanning.
In actual use, although magnetron 6 can be by target 3 according to predetermined track Upper surface cover.But, due to the invariablenes turning speed of motor so that magnetron 6 is through number of times More region (region that i.e. magnetron 6 track is overlapping) residence time is more, thus leads Corrosion (consumption) speed causing this region target 3 is very fast, and the corrosion rate in other region is relatively And then cause the utilization rate of target 3 relatively low slowly,.
Fig. 9 is the target erosion profile when existing drive mechanism drives magnetron to run.Wherein, Abscissa is the target distance from the center to marginal position, and unit is mm;Vertical coordinate is target Etch depth, unit is mm.From fig. 9, it can be seen that near the corruption of its central region Erosion speed is very fast, and the corrosion rate near target rim region is relatively slow, and, target center The most uneven with the etch rate at edge, it is only about 53% through measuring the utilization rate of target 3.
Summary of the invention
The technical problem to be solved in the present invention is aiming in inductively coupled plasma equipment depositing Drawbacks described above, it is provided that a kind of magnetron sputtering apparatus, it is not changing the original operation of magnetron The corrosion rate that can make target in the case of track is identical, such that it is able to improve the utilization of target Rate.
Additionally, the present invention also provides for a kind of magnetron control method, it can not only cover target The whole surface of material, and magnetron can be made equal in the diverse location time of staying of target material surface Even, such that it is able to improve the utilization rate of target.
Solve above-mentioned technical problem be employed technical scheme comprise that a kind of magnetron sputtering of offer sets Standby, including driving of reaction chamber, target, magnetron, driving described magnetron rotation and revolution Motivation structure, described target is arranged on the top of described reaction chamber, and described magnetron is arranged on institute Stating the top of target, under the driving of described drive mechanism, described magnetron scans described target Surface, described drive mechanism is connected with described control device, and according to described control device Control signal controls rotational velocity and revolution speed, the described magnetron sputtering apparatus of described magnetron Also include: magnetron positioning unit and control device, wherein:
Described magnetron positioning unit, for determining the initial position of described magnetron;
Described control device, for according to described initial position, determining the operating week of magnetron Phase, and according to controlling rotational velocity and the revolution speed of described drive mechanism described service cycle, Thus on the premise of described magnetron is constant by each position number of times of target, control described magnetic Keyholed back plate is residence time in described target unit are so that described magnetron is frequently passing through The shorter residence time of target region, extend in the sparse target region of movement locus simultaneously The time of staying, to improve the etching homogeneity of target.
Wherein, described control device includes speed controlling subelement, described speed controlling subelement The revolution angular velocity and the spin velocity that make described magnetron meet formula (1) and formula respectively (2):
ω 1 = ( a r c c o s R 2 - r o 1 2 - r o 2 2 2 × r o 1 × r o 2 ) / [ t × ( 1 + 55 × 22 18 × 40 ) ] - - - ( 1 )
ω 2 = ( - 55 × 22 18 × 40 ) × { ( a r c c o s R 2 - r o 1 2 - r o 2 2 2 × r o 1 × r o 2 ) / [ t × ( 1 + 55 × 22 18 × 40 ) ] } - - - ( 2 )
In formula, ω 1 represents the revolution angular velocity of magnetron, unit: radian per second;
ω 2 represents the spin velocity of magnetron, unit: radian per second;
Ro1 represents the revolution-radius of magnetron, unit: millimeter;
Ro2 represents the rotation radius of magnetron, unit: millimeter;
R represents the distance between the center of magnetron center and magnetron motion track, Unit: millimeter.
Wherein, described drive mechanism includes motor, gear assembly, the first connecting plate and control Make the servo-driver of described motor speed, wherein:
Upper surface at described target is provided with bracing frame, and described motor is fixed on support frame as described above;
Described gear assembly includes n engaged successively along described first connecting plate length direction Gear, wherein n is the integer more than 2, and described n gear is fixed on described first and connects On plate;
Described first connecting plate and described gear assembly are positioned at outermost gear with described The output shaft of motor connects, described magnetron and the gear farthest apart from the output shaft of described motor Central shaft connect;
Under the driving of described motor, described first connecting plate drive described gear assembly and Described magnetron revolves round the sun centered by the output shaft of described motor, meanwhile, described magnetron with away from Rotation centered by the central shaft of the farthest gear of described motor output shaft;
Described servo-driver controls turning of motor according to the control signal of described control device Speed, thus control rotational velocity and the revolution speed of described magnetron.
Wherein, described gear assembly includes engaging successively the first gear, the second gear, Three gears and the 4th gear, wherein,
Described first gear is connected with the output shaft of described motor,
Described magnetron is connected with the central shaft of described 4th gear by the second connecting plate.
Wherein, described magnetron is fixed on one end of described second connecting plate, described second The other end of connecting plate is provided with the first counterweight that the weight with described magnetron matches, in order to carry The stability of high described magnetron rotation.
Wherein, described gear assembly is partial to one end setting of described first connecting plate, described The other end of the first connecting plate is provided with and described gear assembly, described magnetron and described The second counterweight that the weight sum of one counterweight matches, in order to improve the steady of described magnetron revolution Qualitative.
Wherein, described drive mechanism includes absolute value encoder, described absolute value encoder with Described servo-driver and described motor connect, in order to record described magnetron position and Rotation and the number of turns of revolution, and the position of described magnetron and the number of turns of rotation and revolution are led to Cross described servo-driver and feed back to described control device.
Wherein, described magnetron positioning unit includes signal emission element and signal receiving part, Described signal emission element is used for sending magnetron framing signal, and described signal receiving part is used for Receive the magnetron framing signal sent from described signal emission element;Wherein:
Described signal emission element is fixed on described magnetron, and described signal receiving part is solid Be scheduled on support frame as described above and with described signal emission element to arrange position relative;Or, institute Stating signal emission element to be fixed on support frame as described above, described signal receiving part is fixed on described On magnetron and with described signal emission element to arrange position relative.
Wherein, described sensor signal emission element is Magnet, and described sensor signal receives Parts are Hall switch integrated sensor.
The present invention also provides for a kind of magnetron control method, is used for improving in magnetron sputtering apparatus The etching homogeneity of target, according to the initial position of described magnetron, determines the operating of magnetron Cycle, and according to controlling rotational velocity and the revolution speed of magnetron described service cycle, in institute State magnetron by each position number of times of target constant on the premise of, change described magnetron in institute State residence time in target unit are so that described magnetron is in the target district of frequent process The shorter residence time in territory, extends when the stop of the sparse target region of movement locus simultaneously Between, to improve the etching homogeneity of target.
Wherein, revolution angular velocity and the spin velocity of described magnetron meets formula (1) respectively With formula (2):
ω 1 = ( a r c c o s R 2 - r o 1 2 - r o 2 2 2 × r o 1 × r o 2 ) / [ t × ( 1 + 55 × 22 18 × 40 ) ] - - - ( 1 )
ω 2 = ( - 55 × 22 18 × 40 ) × { ( a r c c o s R 2 - r o 1 2 - r o 2 2 2 × r o 1 × r o 2 ) / [ t × ( 1 + 55 × 22 18 × 40 ) ] } - - - ( 2 )
In formula, ω 1 represents the revolution angular velocity of magnetron, unit: radian per second;
ω 2 represents the spin velocity of magnetron, unit: radian per second;
Ro1 represents the revolution-radius of magnetron, unit: millimeter;
Ro2 represents the rotation radius of magnetron, unit: millimeter;
R represents the distance between the center of magnetron center and magnetron motion track, Unit: millimeter.
The method have the advantages that
The magnetron sputtering apparatus that the present invention provides, at magnetron by each position number of times of target On the premise of constant, make magnetron residence time in target unit are equal, i.e. at magnetic In the case of keyholed back plate movement locus is constant, controls the movement velocity of magnetron, make magnetron in-orbit Move with speed faster in the place that mark intersects, in the disjoint place of track with slower speed Motion, so that magnetron residence time in target unit are is equal, so that target exists The corrosion rate of various location is identical, and then improves the utilization rate of target, and this is possible not only to fall The operating cost of low magnetron sputtering apparatus, and the time changing target can be reduced, thus carry The utilization rate of high magnetron sputtering apparatus.
The magnetron control method that the present invention provides, at magnetron by each position of target time On the premise of number is constant, control magnetron residence time in target unit are, i.e. at magnetic In the case of keyholed back plate movement locus is constant, controls the movement velocity of magnetron, make magnetron in-orbit Move with speed faster in the place that mark intersects, in the disjoint place of track with slower speed Motion, so that it is equal to control magnetron residence time in target unit are, so that target Material is identical in the corrosion rate of various location, and then improves the utilization rate of target.
Accompanying drawing explanation
Fig. 1 is the structure diagram of typical magnetron sputtering process equipment;
Fig. 2 is the structure diagram of the drive mechanism for driving magnetron;
The structure diagram of the magnetron sputtering apparatus that Fig. 3 provides for the embodiment of the present invention;
Fig. 4 is the structure chart of embodiment of the present invention drive mechanism;
Fig. 5 is the top view of embodiment of the present invention drive mechanism;
The track of magnetron when Fig. 6 is the driving magnetron operation of embodiment of the present invention drive mechanism Figure;
The trajectory diagram of magnetron when Fig. 7 is the driving magnetron operation of existing drive mechanism;
Fig. 8 is that target erosion is bent when embodiment of the present invention drive mechanism drives magnetron to run Line;
Fig. 9 is the target erosion profile when existing drive mechanism drives magnetron to run;
Figure 10 is control device, the flow chart of drive mechanism in the present embodiment;
Figure 11 is servomotor speed curves figure within a period of motion;
Figure 12 is the movement velocity trajectory diagram that magnetron runs 5 seconds;
Figure 13 is servomotor another speed curves figure within a period of motion.
Detailed description of the invention
For making those skilled in the art be more fully understood that technical scheme, knot below Magnetron sputtering apparatus and magnetron control method that closing accompanying drawing provides the present invention are retouched in detail State.
The magnetron control method that the present embodiment provides is to hit for improving magnetron sputtering apparatus The etching homogeneity of material, this control method, according to the initial position of magnetron, determines magnetron Service cycle, and according to controlling rotational velocity and the revolution speed of magnetron this service cycle, from And on the premise of magnetron is constant by each position number of times of target, change magnetron at target Residence time in unit are.In other words, in the case of magnetron motion track is constant, Control the movement velocity of magnetron, make magnetron in the place of its track cross with speed faster Motion, in the disjoint place of track with slower speed motion, so that magnetron is at target In unit are, residence time is equal, and then improves the utilization rate of target.
Do not change due to technical scheme in prior art the period of motion of magnetron and Movement locus, therefore, uses following known variables in technical scheme:
Magnetron revolution-radius: ro1=115/25.4 unit: millimeter
Magnetron rotation radius: ro2=55/25.4 unit: millimeter
The revolution angular velocity omega 1 (unit: radian) of magnetron and spin velocity ω 2 of magnetron (unit: radian) meets following relation: ω 2=-(55 × 22) × ω 1/ (18 × 40).
Further, below equation is met:
(1) the movement locus formula of magnetron:
X=ro1 × cos (ω 1 × t)+ro2cos (ω 2 × t)
Y=ro1 × sin (ω 1 × t)+ro2 × sin (ω 2 × t)
In formula, X represents the abscissa of magnetron center point;Y represents the vertical of magnetron center point Coordinate;ω 1 represents the revolution angular velocity of magnetron, unit: radian;ω 2 represents magnetron Spin velocity, unit: radian;Ro1 represents the revolution-radius of magnetron, unit: millimeter; Ro2 represents the rotation radius of magnetron, unit: millimeter;T represents the operation time of magnetron, Unit: second.
(2)X2+Y2=R2
In formula, X represents the abscissa of magnetron center point;Y represents the vertical of magnetron center point Coordinate;R represents the radius at the physical location distance movement locus center of magnetron center point, should Value changes according to the actual motion position of magnetron.
Therefore, in technical scheme, the revolution angular velocity of magnetron and spin velocity Meet formula respectively 1. with formula 2.:
In formula, ω 1 represents the revolution angular velocity of magnetron, unit: radian per second;ω 2 represents magnetic The spin velocity of keyholed back plate, unit: radian per second;Ro1 represents the revolution-radius of magnetron, single Position: millimeter;Ro2 represents the rotation radius of magnetron, unit: millimeter;R represents magnetron Distance between the center of center and magnetron motion track, unit: millimeter.
The magnetron control method that the present embodiment provides, at magnetron by each position of target On the premise of number of times is constant, make magnetron residence time in target unit are equal, from And make target equal in the corrosion rate of various location, and then improve the utilization rate of target.Real Trampling proof, the magnetron control method utilizing the present invention to provide controls the scanning of magnetron, permissible The utilization rate of target is brought up to more than 60%.
The structure diagram of the magnetron sputtering apparatus that Fig. 3 provides for the embodiment of the present invention.Refer to Fig. 3, magnetron sputtering apparatus include reaction chamber 1, electrostatic chuck, target 3, magnetron 6, For driving the drive mechanism 7 of magnetron 6 rotation and revolution, magnetron positioning unit and control Device 13 processed, electrostatic chuck is used for carrying workpiece to be machined, and it is arranged in reaction chamber 1 Bottom.Target 3 is arranged on the top in reaction chamber 1, i.e. target 3 and electrostatic chuck Position is relative.Magnetron 6 is arranged on the top of target 3, in order to improve the sputtering speed of target 3 Rate.Magnetron positioning unit is for determining the initial position of described magnetron.Magnetron 6 with drive Motivation structure 7 connects, and the control end of drive mechanism 7 is connected with controlling device 13, drive mechanism 7 drive magnetron 6 to scan the upper surface of target 3 under the control controlling device 13.
Being also arranged above bracing frame 4 at target 3, bracing frame 4 is a closure member, bracing frame Forming a sealing space with target 3, magnetron 6 is arranged in this sealing space.Sealing Deionized water it is full of, to reduce magnetron 6 and the temperature of target 3 in space.
Fig. 4 is the structure chart of embodiment of the present invention drive mechanism.Fig. 5 is the embodiment of the present invention The top view of drive mechanism.In Figure 5, " A " represents the minimum diameter of magnetron scanning track, " B " represents the maximum gauge of magnetron scanning track, and " C " represents that gear assembly end is swept Retouch track.
See also Fig. 3, Fig. 4 and Fig. 5, drive mechanism include motor 11, gear assembly, First connecting plate 28 and the servo-driver 12 of control motor 11 rotating speed.Motor 11 with watch The input taking driver 12 connects, and controls the outfan of device 13 and servo-driver 12 Connecting, servo-driver 12 can control motor 11 according to the control signal controlling device 13 Rotating speed.
Wherein, motor 11 is fixed on bracing frame 4.
In order to ensure not change the period of motion and the movement locus of original magnetron, it is necessary first to Determine the initial position of magnetron, in the present invention, use magnetron positioning unit to determine magnetic control The initial position of pipe, the i.e. initial point of magnetron motion track.
When magnetron positioning unit drive mechanism brings into operation, magnetron positioning unit is first The magnetron original position signal transmission detected extremely is controlled device 13, so that controlling device The position of magnetron 6 can be accurately acquired, thus be more accurately controlled turning of motor 11 Speed.
In the present embodiment, gear assembly includes the arranged along the first connecting plate 28 length direction One gear (not shown), the second gear the 22, the 3rd gear 23 and the 4th gear 24, First gear, the second gear the 22, the 3rd gear 23 and the 4th gear 24 engages successively and It is connected with the first connecting plate 28 respectively.
First connecting plate the 28, first gear is connected with the output shaft of motor 11, magnetron 6 Connected by the central shaft of the second connecting plate 25 with the 4th gear 24 farthest apart from motor output shaft Connect.Under the driving of motor 11, the first gear, the second gear the 22, the 3rd gear 23 with And the 4th gear 24 rotating around respective central shaft rotation, simultaneously at the band of the first connecting plate 28 Revolve round the sun centered by the output shaft of motor 11 under Dong.At the first connecting plate 28 and the 4th gear Under the drive of 24, magnetron 6 revolve round the sun centered by the output shaft by motor 11 while with Rotation centered by the central shaft of four gears 24.Therefore, by controlling the rotating speed of motor 11, i.e. Revolution and the rotational velocity of magnetron 6 can be controlled.
In the present embodiment, magnetron 6 is arranged on one end of the second connecting plate 25, second even The other end of fishplate bar 25 is provided with the first counterweight 27 that the weight with magnetron matches, and first joins Weigh being equal in weight of the weight of 27 and magnetron 6, such that it is able to make drive mechanism even running, Improve the stability of magnetron 6 rotation, and then the service life of drive mechanism can be improved.
Further, gear assembly is partial to one end of the first connecting plate 28 and is arranged, and connects first The other end of plate 28 arranges the second counterweight 26, the weight of the second counterweight 26 and gear assembly, The weight sum coupling of magnetron 6 and the first counterweight 27.Can carry by the second counterweight 26 The stability of high magnetron 6 revolution, so that drive mechanism more even running, and then improve The service life of drive mechanism.
In the present embodiment, magnetron positioning unit is for determining the initial position of magnetron.Control The initial position that device processed determines according to magnetron positioning unit, determines the operating week of magnetron Phase, and according to controlling rotational velocity and the revolution speed of drive mechanism this service cycle.Specifically, Servo-driver controls the rotating speed of motor 11 according to the control signal controlling device, thus controls The rotational velocity of magnetron 6 and revolution speed.Control device and include speed controlling subelement and fortune Dynamic TRAJECTORY CONTROL subelement, speed controlling subelement make driving magnetron 6 revolution angular velocity and With formula 2. 1. spin velocity meet formula respectively:
In formula, ω 1 represents the revolution angular velocity of magnetron, unit: radian per second;ω 2 represents magnetic The spin velocity of keyholed back plate, unit: radian per second;Ro1 represents the revolution-radius of magnetron, single Position: millimeter;Ro2 represents the rotation radius of magnetron, unit: millimeter;R represents magnetron Distance between the center of center and magnetron motion track, unit: millimeter.
The track of magnetron when Fig. 6 is the driving magnetron operation of embodiment of the present invention drive mechanism Figure.The trajectory diagram of magnetron when Fig. 7 is the driving magnetron operation of existing drive mechanism.At Fig. 6 With in Fig. 7, the revolution-radius ro1 of magnetron is 115/25.4, the rotation radius ro2 of magnetron Being 55/25.4, the sweep time of magnetron is 5 seconds.Comparison diagram 6 and Fig. 7 it can be seen that this The tracing point ratio of inventive embodiments magnetron is more uniform, and the distribution density of tracing point is uniform.
Fig. 8 is that target erosion is bent when embodiment of the present invention drive mechanism drives magnetron to run Line.Fig. 9 is the target erosion profile when existing drive mechanism drives magnetron to run.At Fig. 8 With in Fig. 9, abscissa represents the target center distance to edge, unit: millimeter (mm); Vertical coordinate represents the degree of depth of target erosion, unit: millimeter (mm).Comparison diagram 8 and Fig. 9 can To find out, when the present embodiment drive mechanism drives magnetron, the corrosion curve of target is evenly.
In the present embodiment, position that drive mechanism also includes recording magnetron 6 and from Turn and the absolute value encoder (not shown) of the number of turns of revolution, absolute value encoder with watch Taking driver 12 and motor 11 connects, absolute value encoder is according to the rotation circle of motor 11 Number is possible not only to record the current position of magnetron 6 and rotation and the number of turns of revolution, and will The number of turns of the position of magnetron 6 and rotation and revolution feeds back to control by servo-driver 12 Device 13 processed, controls device 13 and records the current position of magnetron 6 and rotation and revolution The number of turns.So when drive mechanism is owing to the reasons such as power down are time out of service, can be by definitely Value encoder and control device 13 and record the position of magnetron 6 and rotation and the number of turns of revolution, After re-powering, drive mechanism can make magnetron 6 continue fortune according to the track before power down OK.
In the present embodiment, magnetron positioning unit includes that signal emission element 14 and signal receive Parts 15, signal emission element 14 is used for sending magnetron framing signal, signal receiving part 15 for receiving the magnetron framing signal sent from signal emission element 14.
As a kind of embodiment, since it is considered that inspection environment is in water, and magnetic control Pipe carries out revolving round the sun and adds the selection of rotation, so the present invention uses magnetic proximity sensor to carry out determining Position.As it is shown on figure 3, signal emission element 14 is fixed on magnetron 6, at magnetron 6 Arrive at movement locus outer, bracing frame 4 above it is installed signal receiving part 15 and with signal emission element 14 to arrange position relative;Connect when magnetron 6 moves to signal When receiving below parts 15, signal receiving part 15 receives signal, now transports as magnetron The initial point of dynamic track.Or, signal emission element 14 is fixed on bracing frame 4, signal Receive parts 15 be fixed on magnetron 6 and with signal emission element 14 position phase is set Right.When signal receiving part 15 receives the magnetron location letter that signal emission element 14 sends Number time, the position at now magnetron 6 place is defined as the starting point of magnetron motion track.
In the present embodiment, signal emission element 14 is Magnet, and signal receiving part 15 is suddenly You switch integrated sensor.In order to improve the precision of magnetron positioning unit, guaranteeing that Hall is opened While the switching curve of pass integrated sensor intersects with the magnetic field of Magnet, also to reduce magnetic as far as possible The intersecting area in the magnetic field of ferrum and Hall switch integrated sensor.
Servomotor of the present invention is to control to carry out its speed by PLC to turn, and Figure 11 is that servomotor exists Speed curves figure in one period of motion.Since it is desired that public affairs turn around in ensureing 1 second, In public affairs turn around, the rotation speed change of servomotor.Figure 12 is the motion that magnetron runs 5 seconds Speed trajectory figure, as shown in figure 12, after magnetron runs 5 seconds, magnetron is returned to speed Identical position is (in terms of Figure 12, although the beginning and end of magnetron motion speed is the most complete Overlap, but beginning and end is respectively positioned on the motion of extension, i.e. magnetron of movement velocity track Speed is identical), after i.e. 5 seconds, the movement velocity track of magnetron is with 5 seconds as cycle but not It is confined to 5 seconds, simply can exist as the period of motion for repeating motion with magnetron motion track In this example as a example by 5 seconds.In order to determine servomotor position of rotation, servomotor is installed Absolute value encoder, the effect of absolute encoder be exactly record position and by rotate the number of turns final Pass to PLC, the power down conservation zone being stored in PLC, and absolute value encoder record itself Data the most also will keep, even if so system runs into unexpected power down, re-power After, PLC still can guarantee that magnetron continues motion according to the track before power down.
As another embodiment, signal emission element 14 is arranged in magnetron counterweight, Magnet is installed in counterweight 6 the most in the diagram, is positioned at counterweight track outer signal installed above Receive parts 15, due to counterweight 6 and magnetron 27 in motor process straight at same all the time On line, so when counterweight 6 arrives outer, signal receiving part 15 has signal, now Magnetron 27 is in the position nearest from the target center of circle.In order to ensure precision, signal receiving part The switching curve of 15 intersects area and reduces as far as possible with the magnetic field of signal emission element 14.Same sample The control unit used in example is identical with example one with control method, such as Figure 10, but due to Now magnetron initial point signal be magnetron from the target center of circle the most nearby, magnetron motion is from there Setting in motion, so corresponding motor speed controlling curve the most just runs according to Figure 13.Watching Take and absolute value encoder is installed on the gear shaft that motor connects, be used for recording the position of servomotor It is also prevented from power down simultaneously and loses magnetron position.With in sample instance with 5 seconds as cycle, but not Being confined to 5 seconds, the principle of selection cycle is still that repeatable motion is with magnetron motion track Foundation.
Figure 10 is control device, the flow chart of drive mechanism in the present embodiment.Refer to Figure 10, Control device 13 to transmit to servo-driver 12, the control signal controlling motor 11 by watching Take driver 12 to control motor 11 and run, motor 11 drive gear assemblies and the first connecting plate 28 rotate centered by the output shaft of motor 11, and then drive magnetron 6 to scan target 3 Surface.Meanwhile, absolute value encoder by include the current position of magnetron 6 and rotation and The encoder feedback signal transmission of the number of turns of revolution is transmitted to controlling dress by servo-driver 12 Put, the position of the control current magnetron of device record 6 and rotation and the number of turns of revolution.
The present embodiment controls device and controls subelement by speed controlling subelement and movement locus Control running orbit and the speed of service of magnetron, so that magnetron is in target material surface unit are On the time of staying equal so that target is unanimous on the whole in the corrosion rate of various location, It is more than 60% through measuring the utilization rate understanding target.
It should be noted that in the present embodiment, gear assembly includes four gears, but this Invention is not limited to and this.Gear assembly can include n gear, and wherein, n is for being more than In the integer of 2.N gear is fixed on the first connecting plate 28 and engages successively, gear train In part, a gear of outermost (end) is connected with the output shaft of motor 11, magnetron 6 On the central shaft of the farthest gear of output shaft being fixed on distance motor 11.Driving of motor 11 Under Dong, magnetron 6 revolves round the sun centered by the output shaft of motor, and with distance motor output shaft Rotation centered by the central shaft of remote gear.Therefore, permissible by controlling the rotating speed of motor 11 Control magnetron 6 revolution and the speed of rotation.
The magnetron sputtering apparatus that the present embodiment provides, at magnetron by each position of target time On the premise of number is constant, makes magnetron residence time in target unit are equal, i.e. exist In the case of magnetron motion track is constant, controls the movement velocity of magnetron, make magnetron exist Move with speed faster in the place of track cross, in the disjoint place of track with slower speed Degree motion, so that magnetron residence time in target unit are is equal, so that target Identical in the corrosion rate of various location, and then the utilization rate of raising target, this is possible not only to Reduce the operating cost of magnetron sputtering apparatus, and the time changing target can be reduced, thus Improve the utilization rate of magnetron sputtering apparatus.
It is understood that the principle that is intended to be merely illustrative of the present of embodiment of above and adopt Illustrative embodiments, but the invention is not limited in this.General in this area For logical technical staff, without departing from the spirit and substance in the present invention, can make Various modification and improvement, these modification and improvement are also considered as protection scope of the present invention.

Claims (10)

1. a magnetron sputtering apparatus, it is characterised in that described magnetron sputtering apparatus includes instead Answer chamber, target, magnetron, driving described magnetron rotation and the drive mechanism of revolution, magnetic Keyholed back plate positioning unit and control device, described target is arranged on the top of described reaction chamber, institute State magnetron and be arranged on the top of described target, under the driving of described drive mechanism, described magnetic Keyholed back plate scans the surface of described target, and described drive mechanism is connected with controlling device, and according to institute State rotational velocity and the revolution speed of the control signal described magnetron of control controlling device, its In:
Described magnetron positioning unit, for determining the initial position of described magnetron;
Described control device, for according to described initial position, determining the operating week of magnetron Phase, and according to controlling rotational velocity and the revolution speed of described drive mechanism described service cycle, Thus on the premise of described magnetron is constant by each position number of times of target, control described magnetic Keyholed back plate is residence time in described target unit are so that described magnetron is frequently passing through The shorter residence time of target region, extend in the sparse target region of movement locus simultaneously The time of staying, to improve the etching homogeneity of target;
Described drive mechanism includes motor, gear assembly, the first connecting plate and controls described The servo-driver of motor speed, wherein:
Upper surface at described target is provided with bracing frame, and described motor is fixed on support frame as described above;
Described gear assembly includes n engaged successively along described first connecting plate length direction Gear, wherein n is the integer more than 2, and described n gear is fixed on described first and connects On plate;
Described first connecting plate and described gear assembly are positioned at outermost gear with described The output shaft of motor connects, described magnetron and the gear farthest apart from the output shaft of described motor Central shaft connect;
Under the driving of described motor, described first connecting plate drive described gear assembly and Described magnetron revolves round the sun centered by the output shaft of described motor, meanwhile, described magnetron with away from Rotation centered by the central shaft of the farthest gear of described motor output shaft;
Described servo-driver controls turning of motor according to the control signal of described control device Speed, thus control rotational velocity and the revolution speed of described magnetron.
Magnetron sputtering apparatus the most according to claim 1, it is characterised in that described control Device processed includes that speed controlling subelement, described speed controlling subelement make the public affairs of described magnetron Tarnsition velocity and spin velocity meet formula (1) and formula (2) respectively:
ω 1 = ( a r c c o s R 2 - r o 1 2 - r o 2 2 2 × r o 1 × r o 2 ) / [ t × ( 1 + 55 × 22 18 × 40 ) ] - - - ( 1 )
ω 2 = ( - 55 × 22 18 × 40 ) { ( a r c c o s R 2 - r o 1 2 - r o 2 2 2 × r o 1 × r o 2 ) / [ t × ( 1 + 55 × 22 18 × 40 ) ] } - - - ( 2 )
In formula, ω 1 represents the revolution angular velocity of magnetron, unit: radian per second;
ω 2 represents the spin velocity of magnetron, unit: radian per second;
Ro1 represents the revolution-radius of magnetron, unit: millimeter;
Ro2 represents the rotation radius of magnetron, unit: millimeter;
R represents the distance between the center of magnetron center and magnetron motion track, Unit: millimeter.
Magnetron sputtering apparatus the most according to claim 1, it is characterised in that described tooth Wheel assembly includes the first gear, the second gear, the 3rd gear and the 4th gear engaged successively, Wherein,
Described first gear is connected with the output shaft of described motor,
Described magnetron is connected with the central shaft of described 4th gear by the second connecting plate.
Magnetron sputtering apparatus the most according to claim 3, it is characterised in that described magnetic Keyholed back plate is fixed on one end of described second connecting plate, and the other end at described second connecting plate is provided with The first counterweight matched with the weight of described magnetron, in order to improve described magnetron rotation Stability.
Magnetron sputtering apparatus the most according to claim 4, it is characterised in that described tooth Wheel assembly is partial to one end of described first connecting plate and is arranged, at the other end of described first connecting plate It is provided with and the weight sum phase of described gear assembly, described magnetron and described first counterweight Second counterweight of coupling, in order to improve the stability of described magnetron revolution.
Magnetron sputtering apparatus the most according to claim 1, it is characterised in that described in drive Motivation structure includes absolute value encoder, described absolute value encoder and described servo-driver and Described motor connects, in order to record the position of described magnetron and rotation and the number of turns of revolution, And described servo-driver is passed through in the position of described magnetron and the number of turns of rotation and revolution Feed back to described control device.
Magnetron sputtering apparatus the most according to claim 1, it is characterised in that described magnetic Keyholed back plate positioning unit includes signal emission element and signal receiving part, described signal emission element For sending magnetron framing signal, described signal receiving part is for receiving from described signal The magnetron framing signal that emission element sends;Wherein:
Described signal emission element is fixed on described magnetron, and described signal receiving part is solid Be scheduled on support frame as described above and with described signal emission element to arrange position relative;Or, institute Stating signal emission element to be fixed on support frame as described above, described signal receiving part is fixed on described On magnetron and with described signal emission element to arrange position relative.
Magnetron sputtering apparatus the most according to claim 7, it is characterised in that described letter Number emission element is Magnet, and described signal receiving part is Hall switch integrated sensor.
9. a magnetron control method, in employing claim 1-8 described in any one Magnetron sputtering apparatus, for improving the etching homogeneity of target in magnetron sputtering apparatus, its feature It is, according to the initial position of described magnetron, determines the service cycle of magnetron, and according to Control rotational velocity and the revolution speed of magnetron described service cycle, thus at described magnetron By each position number of times of target constant on the premise of, change described magnetron at described target list The long-pending upper residence time of plane so that described magnetron is in the stop of the target region of frequent process Time shortens, and extends the time of staying in the sparse target region of movement locus simultaneously, to improve The etching homogeneity of target.
Magnetron control method the most according to claim 9, it is characterised in that institute State the revolution angular velocity of magnetron and spin velocity meet formula (1) and formula (2) respectively:
ω 1 = ( a r c c o s R 2 - r o 1 2 - r o 2 2 2 × r o 1 × r o 2 ) / [ t × ( 1 + 55 × 22 18 × 40 ) ] - - - ( 1 )
ω 2 = ( - 55 × 22 18 × 40 ) { ( a r c c o s R 2 - r o 1 2 - r o 2 2 2 × r o 1 × r o 2 ) / [ t × ( 1 + 55 × 22 18 × 40 ) ] } - - - ( 2 )
In formula, ω 1 represents the revolution angular velocity of magnetron, unit: radian per second;
ω 2 represents the spin velocity of magnetron, unit: radian per second;
Ro1 represents the revolution-radius of magnetron, unit: millimeter;
Ro2 represents the rotation radius of magnetron, unit: millimeter;
R represents the distance between the center of magnetron center and magnetron motion track, Unit: millimeter.
CN201210152625.0A 2012-05-16 2012-05-16 magnetron sputtering apparatus and magnetron control method Active CN103422065B (en)

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CN106958011B (en) * 2017-05-17 2019-02-22 赵其煜 Dynamic controls the control device and control method of sputtering target material utilization rate
CN110629173B (en) * 2018-06-25 2021-12-17 北京北方华创微电子装备有限公司 Magnetron control method, magnetron control device and magnetron sputtering equipment
CN110894590B (en) * 2018-09-13 2021-08-13 北京北方华创微电子装备有限公司 Magnetron sputtering method, control module and equipment for magnetron sputtering equipment

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050236267A1 (en) * 2004-04-27 2005-10-27 Paul Rich Methods and apparatus for controlling rotating magnetic fields
CN1890399A (en) * 2003-12-12 2007-01-03 应用材料公司 Mechanism for varying the spacing between sputter magnetron and target
CN1914351A (en) * 2004-03-24 2007-02-14 应用材料股份有限公司 Selectable dual position magnetron
CN102074446A (en) * 2010-12-08 2011-05-25 清华大学 Magnetron with adjustable compound trace

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1890399A (en) * 2003-12-12 2007-01-03 应用材料公司 Mechanism for varying the spacing between sputter magnetron and target
CN1914351A (en) * 2004-03-24 2007-02-14 应用材料股份有限公司 Selectable dual position magnetron
US20050236267A1 (en) * 2004-04-27 2005-10-27 Paul Rich Methods and apparatus for controlling rotating magnetic fields
CN102074446A (en) * 2010-12-08 2011-05-25 清华大学 Magnetron with adjustable compound trace

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