AOM modulation techniques employing transducers to modulate different axes
View Patent ↗Digital control of frequency and/or amplitude modulation techniques of an intracavity and/or extracavity AOM ( 60 ) facilitate substantially full extinction of a laser beam ( 90 ) to prevent unwanted laser energy from impinging a workpiece ( 80 ); facilitate laser pulse amplitude stability through closed-loop control of pulse-to-pulse laser energy; facilitate beam-positioning control including, but not limited to, closed-loop control for applications such as alignment error correction, beam walk rectification, or tertiary positioning; and facilitate employment of more than one transducer on an AOM ( 60 ) to perform any of the above-listed applications.
1. A method for enhancing beam positioning control from an AOM suited for positioning along a beam path between a laser and a workpiece having first and second transverse surface axes, the AOM having a beam entrance surface, a beam exit surface, and a first transducer that is positioned on a first transducer surface of the AOM, the first transducer surface being in a first plane that is transverse to the beam entrance surface, comprising:
generating a laser beam along a beam path that impinges a workpiece;
propagating the laser beam through the AOM positioned along the beam path;
controlling a first frequency of a first RF signal applied to the first transducer that modulates within a first transducer modulation zone that traverses the beam path to affect a first exit angle of the beam path along the first surface axis;
controlling a second frequency of a second RF signal applied to a second transducer positioned on a second transducer surface of the AOM, the second transducer surface being in a second plane that is transverse to the beam entrance surface and the first plane, the second transducer modulating in a second transducer modulation zone that is transverse to the first transducer modulation zone and traverses the beam path to affect a second exit angle of the beam path along the second surface axis; and
coordinating the first and second frequencies to deflect the beam path along the first and second surface axes to impinge the workpiece at a desired beam position at a cooperative deflection angle resulting from the first and second exit angles imparted by the first and second transducers in response to the first and second frequencies of the first and second RF signals.
2. The method of claim 1 in which the first and second transducer modulation zones are generally orthogonal.
3. The method of claim 1 in which the first and second transducer modulation zones intersect.
4. The method of claim 1 in which the first and second frequencies are different.
5. The method of claim 1 in which the beam path that impinges the workpiece comprises a first order beam path propagated from the AOM.
6. The method of claim 1 in which the beam path that impinges the workpiece comprises a zero order beam path propagated from the AOM.
7. The method of claim 1 in which the beam path impinges the AOM at an angle that is generally perpendicular to the beam entrance surface.
8. The method of claim 1 in which the beam path impinges the AOM at an entrance angle that is at or in proximity to a Bragg angle with respect to the beam entrance surface or the first transducer modulation zone.
9. The method of claim 8 in which the first and second RF signals have respective first and second amplitudes, and the first and/or second amplitude is adjusted to compensate for deviations from Bragg efficiency resulting from shifts in the first and/or second exit angles of the beam path from the Bragg angle.
10. The method of claim 1 in which a third frequency of a third RF signal is applied to a third transducer positioned on a third transducer surface of the AOM, the third transducer surface is generally transverse to the beam entrance surface, and the third transducer modulates in a third transducer modulation zone that traverses the beam path and affects the first exit angle such that the first and third RF signals cooperate to control the first exit angle.
11. The method of claim 10 in which the first and third transducer modulation zones are generally parallel.
12. The method of claim 10 in which the first and third transducer surfaces are coplanar.
13. The method of claim 10 in which the third transducer is spaced-apart and oriented at a small angle with respect to the first transducer such that the first and third transducer modulation zones are nonparallel and non-overlapping.
14. The method of claim 10 in which the first and third frequencies are different.
15. The method of claim 10 in which the first and third frequencies are the same.
16. The method of claim 11 in which the first and third frequencies are generally harmonically related.
17. The method of claim 10 in which the first and third frequencies have different phases.
18. The method of claim 11 in which the first and second frequencies are generally in phase.
19. The method of claim 10 in which the beam path impinges the AOM at an entrance angle that is at or in proximity to a Bragg angle with respect to the beam entrance surface or the first transducer modulation zone.
20. The method of claim 10 in which the first and third RF signals cooperate to control the first exit angle at a resolution beyond which either of the first or third transducers can provide independently.
21. The method of claim 10 in which the first and third RF signals cooperate to control the first exit angle to include a cooperative deflection angle range beyond deflection angle ranges that either of the first or third transducers can provide independently.
22. The method of claim 1 , further comprising:
providing slow and fast movement-controlling signals from a positioning signal processor;
controlling with a slow positioner driver a large range of relative beam-directing movement of a translation stage, generally along a translation axis in response to the slow movement-controlling signal;
controlling with the first and/or second transducers a small range of relative beam-directing movement of the AOM in response to the fast movement-controlling signal; and
effecting the large range of relative beam-directing movement between the beam path and the workpiece on the translation stage; and
effecting with the AOM the small range of relative beam-directing movement between the beam path and the workpiece to impinge the workpiece at a desired beam position.
23. The method of claim 22 , further comprising:
acquiring error information concerning differences between the beam path and the desired beam position; and
conveying the error information to the first and/or second transducers to compensate for the differences between the beam path and the desired beam position.
24. The method of claim 22 , further comprising:
acquiring off-axis information concerning differences between the beam path along a scan line and desired beam positions off-axis but parallel to the scan line; and
conveying the off-axis information to the first and/or second transducers to deflect the laser beam to impinge the desired beam positions parallel to the scan line over the workpiece.
25. An AOM control system for controlling an AOM suited to be positioned along a beam path between a laser and a workpiece, the AOM having a beam entrance surface, a beam exit surface, and a first transducer that is positioned on a first transducer surface, the first transducer surface being in a first plane that is transverse to the beam entrance surface, the first transducer being adapted to modulate within a first transducer modulation zone that traverses the beam path, comprising:
a second transducer attached to a second transducer surface that is in a second plane that is transverse to the beam entrance surface, the second transducer being adapted to modulate within a second transducer modulation zone that traverses the beam path;
a first RF driver including or in communication with a first variable frequency controller adapted to apply a first frequency of a first RF signal to the first transducer to modulate within the first transducer modulation zone to affect a first exit angle of the beam path along a first Cartesian axis; and
a second RF driver including or in communication with a second variable frequency controller to apply a second frequency of a second RF signal to the second transducer to modulate a second transducer modulation zone that is transverse to the first transducer modulation zone to affect a second exit angle of the beam path along a second Cartesian axis that is transverse to the first Cartesian axis such that a cooperative deflection angle results from application of the first and second RF signals contemporaneously.
26. The AOM control system of claim 25 in which the first and second transducer modulation zones are generally orthogonal.
27. The AOM control system of claim 25 in which the first and second transducer modulation zones intersect.
28. The AOM control system of claim 25 in which the first and second RF drivers are adapted to provide independent first and second frequencies.
29. The AOM control system of claim 25 further comprising a beam position controller to coordinate the first and second frequencies to deflect with the AOM the laser beam from the beam path to impinge the workpiece at a desired beam position resulting from the cooperative deflection angle.
30. The AOM control system of claim 25 in which the AOM is adapted to be positioned such that a first order beam is propagated along the beam path.
31. The AOM control system of claim 25 in which the AOM is adapted to be positioned such that the beam path impinges the AOM at an angle that is generally perpendicular to the beam entrance surface.
32. The AOM control system of claim 25 in which the AOM is suited for impingement by the beam path at an entrance angle that is at or in proximity to a Bragg angle with respect to the beam entrance surface or the first transducer modulation zone.
33. The AOM control system of claim 32 in which the first and second RF drivers are adapted to adjust a first amplitude of the first RF signal and a second amplitude of the second RF signal to compensate for deviations from Bragg efficiency resulting from shifts in the first and/or second exit angles of the beam path from the Bragg angle.
34. The AOM control system of claim 25 further comprising:
a third transducer, positioned on a third transducer surface that is in a third plane that is generally transverse to the beam entrance surface, for modulating within a third transducer modulation zone; and
a third RF driver to modulate a third frequency of a third RF signal applied to the third transducer to modulate within the third transducer modulation zone that traverses the beam path and affects the first exit angle such that the first and third RF signals cooperate to control the first exit angle.
35. The AOM control system of claim 34 in which the first and third transducer modulation zones are generally parallel.
36. The AOM control system of claim 34 in which the first and third transducer surfaces are coplanar.
37. The AOM control system of claim 34 in which the third transducer is spaced-apart and oriented at a small angle with respect to the first transducer such that the first and third transducer modulation zones are nonparallel and non-overlapping.
38. The AOM control system of claim 34 in which the first and third RF drivers are adapted to provide different first and third frequencies.
39. The AOM control system of claim 34 in which the AOM is suited for impingement by the beam path at an entrance angle that is at or in proximity to a Bragg angle with respect to the beam entrance surface or the first transducer modulation zone.