Upload
others
View
5
Download
0
Embed Size (px)
Citation preview
DESIGN AND FINE MOTION TEST OF A PRECISION X-THETA STAGE IN VACUUM
Gyungho Khim1, Jongyoup Shim1, and Chun-Hong Park1 1Department of Ultra Precision Machines and Systems
Korea Institute of Machinery and Materials Daejeon, South Korea
INSTRUCTIONS
Recently, precision stages in vacuum are required in many applications such as mastering processes for high density optical disc [1-2], and lithography equipments for wafer or mask. These processes rely on electron beams, which are operable in only high vacuum. In this paper, a precision X-Theta stage aimed at being used for vacuum applications, representatively electron beam mastering equipments, is developed. A brief design method and experiment result focused on fine motion using commercialized controller are introduced. DESIGN OF A X-THETA STAGE
In the mastering processes of optical disc, two degree of freedom motions, linear(X) and rotary(Theta) motions, are mainly required. The linear stage is designed using linear motion ball bearings(THK, HR2555M) while rotary stage used air bearings because rotational accuracy is more important. The HR model used for linear stage has characteristics of very low height and compact size, and easy adjustment of clearance. Coreless linear motor(Trilogy, 210-4N) and linear scale(Heidenhain, LIP481R) were also used in the linear stage. These are chosen to be vacuum-compatible. Maximum stroke is 250 mm and a scale resolution is set to 5 nm. FIGURE 1 shows a structure of the linear stage.
FIGURE 1. Structure of a linear stage
The rotary stage used a vacuum-compatible air bearings(carbon porous) for extremely high
accuracy, and a slotless direct drive motor (Aerotech, S130-39-B) to suppress unwanted motion errors caused by cogging force, and a thin type of rotary encoder(Sony, BH20) to shorten the overall height of the stage. The Turbo PMAC2 controller (Delta Tau) and linear amplifier (Varedan, LA400) are used for both stages. The commutation for motor driving is carried out using not a hall sensor but encoder signal for a better smoothing motion. The rotary encoder has a resolution of 0.162 µrad (0.03 arcsec) by means of dividing the analog sine signal using interpolator board (Delta Tau, ACC-51P) The air leakage problem from the air bearings has been solved using differential exhaust method [2-3]. Sufficient vacuum level for electron beams can be obtained using three steps of exhaust system. The first exhaust line is open to the atmosphere, and the second, third exhausts are connected outside vacuum pumps. The first exhaust line is also used as feedthroughs for a motor, encoder cables, and compressed air line as well as exhaust of air. This region is connected to outside atmosphere using bellows, and always maintains atmospheric condition. Therefore non-vacuum-compatible components can be used. This is one of the big merits. FIGURE 2 shows a structure of rotary stage.
FIGURE 2. Structure of a rotary stage
Linear motor
Linear scale
Linear motion bearing
Journal bearingThrust bearing
Direct drive motor
Rotary encoder
2nd exhaust
3rd exhaust
Compressedair in
Workpiece
1st exhaust: Feedthrough for motor & encoder cable, compressed air line
(Atmospheric condition)
Shaftd3
d2
ls3
ls2
ls1
d1
Air leak
The gap between the inside of housing and the outside of shaft in differential exhaust system is very small (5~10 µm). This small gap prevents air from leaking into the vacuum chamber. The design parameters such as diameter of exhaust lines (di), seal lengths(lsi), and pumping speeds of vacuum pumps(Si) are optimally decided using optimized method with genetic algorithm [3]. Table 1 shows design results. We can also know which type of pumps should be used for the second and third exhaust lines by means of the inlet pressures(Ppi) calculated in Table 1. VACUUM LEVEL TEST
FIGURE 3 shows the X-Theta stage installed inside the vacuum chamber. The stages were fabricated with anodized aluminum 7075. It was used because of high hardness characteristic in spite of a disadvantage in outgassing. FIGURE 4 represents a vacuum chamber and various feedthroughs for signals and flows. The vacuum chamber was installed on the anti-vibration table. FIGURE 5 demonstrates a pressure variation of a vacuum chamber obtained while the air bearing is working. Turbo molecular pump(TMP) of a 550 l/s was used for exhausting the vacuum chamber. The chamber pressure was measured with a full-range vacuum gauge (PFEIFFER Vacuum, TPG 261). The chamber pressure reached 5.1×10
-4 Pa within 29 hours of
operation without activating the air bearing. Then, the second and third exhaust pumps were operated for preparation of activating the air bearing. After 1 hour, the chamber pressure was reduced to 4.7×10
-4 Pa. Compressed air of 0.4
MPa was supplied to the air bearing. The chamber pressure suddenly increased to 5.2×10
-4 Pa, but then began to decrease slowly
to 4.3×10-4 Pa after 5 hours later. This level of
vacuum pressure is sufficient for using electron beams. Moreover, it is expected that high vacuum level less than 10
-4 Pa could be
achieved with increasing time, as shown in FIGURE 5.
FIGURE 3. X-Theta stage installed inside the vacuum chamber
FIGURE 4. Vacuum chamber
FIGURE 6 shows a pressure variation of a vacuum chamber obtained while the air bearing(rotary stage) is moving. The stage is rotated with velocities of 100, 200, and 300 rpm, and the pressures are continuously measured. The pressure rise is evaluated by means of “100 log (P/P0),” where P0 is a pressure just before moving, and P is a pressure measured during moving. The pressure increased with velocity, however, it showed only increase of 0.5 % for a velocity of 300 rpm. This amount of increase is negligible.
Rotary
stage
Linear stage
E-beam
Vacuum gauge
Feedthroughs
Exhaust line
TABLE 1. Optimal design of exhaust system
Chamber pressure (Pa)
Seal lengths of i-th exhaust lines,
lsi (mm)
Diameters of i-th exhaust lines, di (mm)
Pumping speeds of i-th vacuum pump,
Si (liter/s)
Inlet pressures of i-thvacuum pump, Ppi (Pa)
ls1 ls2 ls3 d2 d3 S1 S2 S3 Pp1 Pp2 Pp3
Optimal design
2.3�10-5 4.8 10.2 11.6 16.2 24.2 Atm. 24.5 61.9 Atm 40.7 3.8×10-3
FIGURE 5. Pressure variation while air bearing is working
FIGURE 6. Pressure variation during air bearing movement FINE MOTION TEST
Vacuum-compatible grease was firstly used as a lubricant in the linear motion bearing, however, its friction was considerably high due to a high viscosity characteristic. Instead of grease lubrication, solid lubrication was adopted. DLC (Diamond Like Carbon) coating on the linear motion bearing was carried out by sputtering deposition because the DLC coating exhibits super-low friction and high hardness, and high atomic structural stability in vacuum [4]. Capacitance sensor(ADE, 2803V, 0.5 nm resolution) and acquisition board(Dewetron, Dewe-43, 24bit resolution) were used to evaluate a fine motion and the repeatability. The displacements were measured after low pass filtering for eliminating environmental noise and electrical noise. FIGURE 7 shows a fine motion step response of 5 nm, which is the same as
scale resolution, in the linear stage. The result showed the stage exactly moved 5 nm, and better fine motion would be obtained if the higher scale resolution were used. FIGURE 8 shows the bi-directional repeatability at a point. The displacements were measured for stopping at a zero position while the stage reciprocally moved 1000 counts within the measurement range of the capacitance sensor. The result showed 2σ (σ:standard deviation) of 0.005 µm.
FIGURE 7. Fine motion step response in the linear stage
FIGURE 8. Bi-directional repeatability in the linear stage
FIGURE 9. Setup for fine motion step response in the rotary stage The fine motion step response in the rotary stage was measured using a bar installed upper table of the rotary stage, and converted to angular position, as shown in FIGURE 9. The result showed the stage exactly moved a resolution of 0.162 µrad, which is the same as encoder resolution, as shown in FIGURE 10. The bi-directional repeatability was also
0 5 10 15 20 25 30 3510
-4
10-2
100
102
104
106
27 28 29 30 31 32 33 34 35
4.2
4.5
4.8
5.1
5.4
5.7
4.3x10-4 Pa
RP On
Air Bearing On
TMP On
Pressure (Pa)
Time (hr)
3rd TMP On2nd, 3rd RP On
Air Bearing On
Pressure (10-4 Pa)
Time (hr)
0 20 40 60 80 1007.56
7.60
7.64
7.68
0 20 40 60 80 100-0.2
0.0
0.2
0.4
0.6
P
P0
Stop
Start
Rotation speed
100 rpm
200 rpm
300 rpm
Pressure (10-4 Pa)
Rotation speed
100 rpm
200 rpm
300 rpm
Time (sec)
100 log(P/P
0)
0 10 20 30 40 50 60
0
5
10
15
20
25
301 cnt/step
5 nm/cnt
Displacement (nm)
Time (s)
0 20 40 60 80 100 120-0.2
-0.1
0.0
0.1
0.22σ=0.005 µm
Time (s)
Displacement (µm)
evaluated like the method done in the linear stage. The result showed 2σ of 0.054 µrad, as shown in FIGURE 11.
FIGURE 10. Fine motion step response in the rotary stage
FIGURE 11. Bi-directional repeatability in the rotary stage SIMULTANEOUS MOTION TEST OF X-THETA STAGE
Simultaneous motion between a linear and rotary stage was evaluated. When machining optical disc, the constant linear velocity control is required. So the velocity of the rotary stage must decrease with increasing radius (that is, position of the linear stage). The simultaneous motion performance was carried out using only PMAC controller without a DSP board and advanced control scheme. The linear stage must move 320 nm while the rotary stage is moving one revolution for a 25 GB Blu-ray disk. FIGURE 12 shows the experimental result that following error is lower than ±10 nm. FIGURE 13
demonstrates the comparison between command and actual velocity. Actual velocity was calculated from position of the linear stage and velocity of the rotary stage at the moment. The result showed that actual velocity is well coincided with command velocity. CONCLUSIONS
This paper describes a design and fine motion performance of a precision X-Theta stage for vacuum applications. The linear stage(X) which is designed with solid-lubricated linear motion ball bearings showed the same step response as scale resolution(5 nm). The rotary stage
(Theta) which is equipped with vacuum-compatible porous air bearings showed a vacuum level of 10
-4 Pa, and the same step
response as encoder resolution(0.162 µrad). The following error caused by simultaneous motion of X-Theta stage showed ±10 nm.
FIGURE 12. Simultaneous motion test of X-Theta stage
FIGURE 13. Comparison between command and actual velocity REFERENCES
[1] Kojima Y, et al., High Density Mastering Using Electron Beam. Japanese Journal of Applied Physics. 1998; 37: 2137-2143.
[2] Furuki M, et al., Electron Beam Recording with a Novel Differential Pumping Head Realizing more than 50 GB/Layer Capacity Disc. Japanese Journal of Applied Physics. 2003; 43: 759-763
[3] Khim G, et al., A Vacuum-Compatible Air Bearing: Design Analysis and Optimization. Key Engineering Material. 2007; 339: 37-44.
[4] Andersson J, et al., Friction of Diamond-Like Carbon Films in Different Atmospheres. Wear. 2003; 254: 1070-1075.
0 10 20 30 40 50 60
0.0
0.3
0.6
0.9 1 cnt/step
0.162 µrad/cnt
Displacement (µrad)
Time (s)
0 10 20 30 40 50 60 70 80 90-2
-1
0
1
22σ=0.054 µrad
Time (s)
Displacement (µrad)
0 500 1000 1500 2000
0.00
0.16
0.32
0.48
0.64
0 500 1000 1500 2000-20
-10
0
10
20
Linear position (mm)
Rotary position (rev)
Following Error (nm)
0 100 200 300 400 500 600 700 800499.96
499.98
500.00
500.02
500.04
500.06
Actual velocity
Command velocity
Time (s)
Linear velocity (mm/s)