Electric discharge laser with acoustic chirp correction

Coherent light generators – Particular active media – Gas

Reexamination Certificate

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C372S058000, C372S034000

Reexamination Certificate

active

06317447

ABSTRACT:

The present invention relates to laser discharge chambers and in particular to chambers having provisions for correction of acoustic disturbances.
BACKGROUND OF THE INVENTION
It is known that the discharge in electric discharge laser chambers can cause pressure wave disturbances that interfere with subsequent pulses. Laser chambers with provisions for minimizing these disturbances are described in U.S. Pat. No. 5,978,405 which is incorporated herein. The '405 patent is assigned to the assignee of the present invention.
FIG. 1
is a drawing of the cross section of a typical KrF excimer laser chamber. The gain region of the laser is a discharge region with a cross section of about 20 mm×4 mm shown as
34
in
FIG. 1
with a length between elongated electrodes
36
A and
36
B of about 70 cm. In the chamber laser gas is circulated by fan
38
and cooled by heat exchanger
40
. Also shown in
FIG. 1
are main insulator
42
, anode support bar
44
and preionizer rod
46
.
An important use of electric discharge lasers such as KrF excimer lasers is as light sources for integrated circuit lithography. In these applications, the lasers are line narrowed to about 0.5 pm about a desired “center-line” wavelength. The laser beam is focused by a stepper or scanner machine onto the surface of a silicon wafer on which the integrated circuits are being created. The surface is illuminated with short bursts of laser pulses at pulse rates of about 1000 Hz or greater. Very precise control of wavelength and bandwidth are required to permit the production of extremely fine integrated circuit features. The operators of most stepper and scanner machines in use today operate the laser light source at about 1000 Hz, but 2000 Hz sources are being shipped and lasers with even higher repetition rates are being developed. The typical laser gas for the KrF laser is about 99 percent neon at 3 atmospheres and at a temperature of about 45° C. At this temperature a sound wave travels about 47 cm between pulses at 1000 Hz, about 23.5 cm between pules at 2000 Hz and about 11.7 cm at 4000 Hz. Integrated circuit manufacturers desire to be able to operate their laser at any pulse rate within the operating range of the laser while maintaining beam parameters including target wavelength and bandwidth within desired specifications.
Distances between the discharge region of a typical lithography excimer laser and major reflecting surfaces within the laser chamber range from about 5 to 20 cm. Distances between reflecting surfaces in planes perpendicular to the length of the discharge region are mostly between about 5 cm to about 10 cm. Therefore, as demonstrated by a comparison of
FIG. 2A
showing distances traveled by sound with
FIG. 1
, a typical discharge created pressure wave traveling at the speed of sound in the
FIG. 1
laser operating at 1000 Hz would have to make several reflections in order to arrive back at the discharge region coincident with the next discharge. At pulse rates in the range of 2000 Hz and higher, the pressure wave traveling at the speed of sound may return to the discharge region coincident with the next pulse after only one reflection.
Wavelength Specifications For Lithography Lasers
KrF excimer lasers currently in use for integrated circuit lithography are designed for precise control of wavelength and bandwidth. Current specifications from integrated circuit makers call for control of the target wavelength to a target wavelength, such as 248,321.3 pm within a stability range of ±0.1 pm. A typical bandwidth specification may be 0.6 pm, full width half maximum and 3 pm, 95% integral.
The makers of stepper and scanner machines want to tighten these specifications and also to increase pulse repetition rate to 2000 Hz and above.
A typical method of line narrowing a lithography laser is shown in FIG.
3
. In this drawing the line narrowing module (called a “line narrowing package” or “LNP”)
7
is greatly enlarged with respect to the rest of laser system
2
. The laser beam exiting back end of laser chamber
3
is expanded with a three prism beam expander
18
, and reflected by a tuning mirror
14
on to a grating
16
disposed in the Litrow configuration. The angle at which the light illuminates and is reflected from the surface of the grating determines the selected wavelength. For example, in this prior art laser a pivot of 40 micro radians produced by stepper motor
15
will change the wavelength of the selected light by 1 pm. The three prism beam expander shown in
FIG. 3
increases the selectivity of the grating by its magnification factor which is typically about 25. A change in direction of the beam exiting the laser in the direction of the LNP can also cause a change in the wavelength selected by the grating; however, the direction change would need to be about 1 milliradian to cause a 1 pm change in the selected wavelength.
Prior art KrF excimer lasers can be operated within very tight specifications even at very high repetition rates when operating at steady state, for example, continuously at 2000 Hz. However, typical operating modes for a lithography laser light source is far from steady state continuous. In a typical mode,
170
dies on a wafer may each be illuminated with 0.15 second bursts of laser pulses at a pulse repetition rate of 2000 Hz (i.e., 300 10-mJ pulses) with a 0.15 second down time between bursts and then a 9 second down time while a new wafer is loaded onto the machine. This complete cycle would take about 1 minute and would represent a duty cycle of about 42.5 percent.
Lasers operating in burst modes at pulse repetition rates in the range of 1000 Hz or greater have displayed patterns of wavelength variation. These variations are referred to as wavelength “chirp” and to date their cause has not been known. The chirp tends to increase with increasing repetition rate.
What is needed is an electric discharge laser having provisions for minimizing acoustic disturbances at pulse rates in excess of 1000 Hz sufficiently to permit beam parameters to be maintained within desired specifications.
SUMMARY OF THE INVENTION
The present invention provides structural changes and methods for minimizing wavelength chirp in high pulse rate gas discharge lasers. Applicants have identified the major cause of wavelength chirp as pressure waves from a discharge reflecting back to the discharge region coincident with a subsequent discharge. The timing of the arrival of the pressure wave is determined by the temperature of the laser gas through which the wave is traveling. During burst mode operation, the laser gas temperature in prior art lasers changes by several degrees over periods of a few milliseconds. These changing temperatures change the location of the coincident pressure waves from pulse to pulse within the discharge region causing a variation in the pressure of the laser gas which in turn affects the index of refraction of the discharge region causing the laser beam exiting the rear of the laser to slightly change direction. This change in beam direction causes the grating in the LNP to reflect back to the discharge region light at a slightly different wavelength causing the wavelength chirp.
Two solutions to the chirp problem described in this specification is to moderate or disperse the discharge created pressure waves or to maintain the gas temperature as close as feasible to constant values (pulse-to-pulse).
In a preferred embodiment an acoustic baffle, comprised of sheet metal, preferably nickel plated aluminum, formed to produce a saw-tooth shaped surface with varying saw-teeth shapes, lining the laser chamber walls disperses the pressure waves. In this embodiment the ridges of the baffle are aligned generally with the gas flow path so that the pressure waves are dispersed in a very large number of directions other than perpendicular to the discharge direction. In another preferred embodiment the saw-teethed shaped baffle is made of perforated sheet metal so that the pressure waves are absorbed and dispersed.
In another preferred embodiment, aluminum o

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