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ABRT Series
Description
   

ABRT Series

ABRT-150

ABRT-200

ABRT-260

Width 146 mm 196 mm 260 mm
Tabletop Diameter 100 mm 145 mm 200 mm
Height 135 mm 165 mm 185 mm
Aperture 20 mm 30 mm 50 mm
Total Travel
360° Continuous
Motor Direct-Drive Brushless Servomotor
Stall Torque, Continuous 0.36 N-m 3.7 N-m 6.7 N-m
Peak Torque 1.4 N-m 14.6 N-m 26.6 N-m
BEMF, Line-Line, Max 10.9 Vpk/krpm 163.6 Vpk/krpm 129.8 Vpk/krpm
Continuous Current, Stall 3.8 Apk 2.7 Apk 6.2 Apk
2.7 Arms 1.9 Arms 4.4 Arms
Torque Constant 0.09 N-m/Apk 1.35 N-m/Apk 1.07 N-m/Apk
0.13 N-m/Arms 1.91 N-m/Arms 1.52 N-m/Arms
Bus Voltage Up to 320 VDC
Resolution(1) 0.267 µrad (0.055 arc sec) 0.174 µrad (0.036 arc sec) 0.133 µrad (0.027 arc sec)
Fundamental Encoder Resolution 11,840 lines/rev 18,000 lines/rev 23,600 lines/rev
Max Speed 1200 rpm 800 rpm 600 rpm
Accuracy Calibrated ±2 arc sec
Repeatability <1 arc sec
Max Load(3) Axial 20 kg 41 kg 69 kg
Radial 3 kg 6 kg 10 kg
Tilt 3.5 N-m 8 N-m 18 N-m
Axial Error Motion (Synchronous) <100 nm
Radial Error Motion (Synchronous) <150 nm
Tilt Error Motion (Synchronous) <2.4 µrad (<0.5 arc sec)
Axial Error Motion (Asynchronous) <20 nm
Radial Error Motion (Asynchronous) <20 nm
Tilt Error Motion (Asynchronous) <0.2 µrad (<0.04 arc sec)
Operating Pressure(5) 80 psig (5.5 bar) ± 5 psig (0.3 bar)
Air Consumption(6) <56.6 SLPM (<2 SCFM)
Inertia Unloaded 2300 kg-mm2 13,500 kg-mm2 46,400 kg-mm2
Total Mass 6.7 kg 14.7 kg 27.1 kg
Material Aluminum
Finish Hardcoat (62 Rockwell Hardness)
Notes:
1. Maximum resolution presumes A3200 controller using MXH500 multiplication, and accounts for controller quadrature.
2. Maximum speed based on stage capability. Maximum application velocity may be limited by system data rate and system resolution.
3. Maximum loads are mutually exclusive.
4. All error motion specifications measured at 60 rpm.
5. To protect air bearing against under-pressure, an in-line pressure switch tied to the motion controller is recommended.
6. Air supply must be clean, dry to 0° F dew point, and filtered to 0.25 µm or better. Recommend nitrogen at 99.9% purity.



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Accuracy X
For a specific point of interest in three-dimensional space, accuracy is the difference between the actual position in space and the position as measured by a measurement device. Stage accuracy is influenced by the feedback mechanism (linear encoder, rotary encoder, laser interferometer), drive mechanism (ball screw, lead screw, linear motor), and trueness of bearing ways. The measurement reference for Aerotech linear products is a laser interferometer.

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Straightness X
Straightness is a deviation from the true line of travel perpendicular to the direction of travel in the horizontal plane. For the stage assembly listed above, a straightness deviation in the travel of the X-axis stage will cause a positioning error in the Y direction. A straightness deviation in the travel of the Y-axis stage will cause a positioning error in the X direction.
Flatness X
Flatness is a deviation from the true line of travel perpendicular to the direction of travel in the vertical plane. For the stage assembly shown, a flatness deviation in the travel of the X-axis or Y-axis stage will cause a positioning error in the Z direction.
Roll X
Roll is a rotation around an axis in the horizontal plane parallel to the direction of travel. If the position of interest being measured is not located at the center of rotation, then the roll rotation will cause an Abbe error in two dimensions. For the X-axis, a roll rotation will cause an Abbe error in both the Y and Z direction.

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Pitch X
Pitch is a rotation around an axis in the horizontal plane perpendicular to the direction of travel. If the position of interest being measured is not located at the center of rotation, then the pitch rotation will cause an Abbe error in two dimensions.

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Yaw X
Yaw is a rotation around an axis in the vertical plane perpendicular to the direction of travel. If the position of interest being measured is not located at the center of rotation, then the yaw rotation will cause an Abbe error in two dimensions.

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Repeatability X
Repeatability is defined as the range of positions attained when the system is repeatedly commanded to one location under identical conditions. Uni-directional repeatability is measured by approaching the point from one direction, and ignores the effects of backlash or hysteresis within the system. Bi-directional repeatability measures the ability to return to the point from both directions. Many vendors specify repeatability as ± (resolution). This is the repeatability of any digital servo system as measured at the encoder. All of Aerotech's specifications, which include the effects of Abbe error, friction, etc. are based on actual operating conditions and usage - not on theoretical, unachievable values.
Resolution X
The smallest possible movement of a system. Also known as step size, resolution is determined by the feedback device and capabilities of the motion system. Theoretical resolution may exceed practical resolution.

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Axial Error Motion (Synchronous) X
Component of total error motion that occurs at integer multiples of rotation frequency coaxial with stage axis of rotation.
Radial Error Motion (Synchronous) X
Component of total error motion that occurs at integer multiples of rotation frequency perpendicular to the stage axis of rotation at a given axial location.
Tilt Error Motion (Synchronous) X
Component of total error motion that occurs at integer multiples of rotation frequency in an angular direction relative to the stage axis rotation. In previous specification tables published by Aerotech, the term wobble was used and is synonymous; however, wobble is no longer preferred.
Axial Error Motion (Asynchronous) X
Component of total error motion that occurs at noninteger multiples of rotation frequency coaxial with stage axis of rotation.
Radial Error Motion (Asynchronous) X
Component of total error motion that occurs at noninteger multiples of rotation frequency perpendicular to the stage axis of rotation at a given axial location.
Tilt Error Motion (Asynchronous) X
Component of total error motion that occurs at noninteger multiples of rotation frequency in an angular direction relative to the stage axis rotation.
Vacuum X
Aerotech’s vast application experience, unmatched product scope, and extensive engineering capabilities make us the partner of choice for vacuum-compatible motion systems. Since its inception, Aerotech has designed and manufactured the highest-performance motion control and positioning systems available, and our vacuum-compatible platforms are no exception.

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Cleanroom X
Aerotech has a long history of providing components and systems to the semiconductor and medical device manufacturing industries. This experience has provided extensive knowledge of how to prepare stages for cleanroom use.

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Maximum Load X
All maximum load values in the stage specification tables are based on the stage operating in a Normal Loading Condition. A Normal Loading condition results when the load is attached to the stage with the center of gravity positioned directly above the bearings.

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Orthogonality X
The condition of a surface or axis which is perpendicular (offset 90 degrees) to a second surface or axis. Orthogonality specification refers to the error from 90 degrees from which two surfaces of axes are aligned.
Accuracy X
Accuracy is defined as the difference between the commanded position and the actual position of a rotary stage. The accuracy can be influenced by the feedback device, drive mechanism (motor type), axis of rotation error motions, thermal effects (such as environmental changes), and the accuracy of mounting surfaces. Aerotech measures the accuracy of rotary tables using laser measurement techniques with ultra-precise index tables as the measurement reference. Unless specifically noted, Aerotech specifies accuracy as a peak-to-valley deviation from the nominal position.