WO2008130474A1 - Extendable electrode for gas discharge laser - Google Patents

Extendable electrode for gas discharge laser Download PDF

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Publication number
WO2008130474A1
WO2008130474A1 PCT/US2008/003890 US2008003890W WO2008130474A1 WO 2008130474 A1 WO2008130474 A1 WO 2008130474A1 US 2008003890 W US2008003890 W US 2008003890W WO 2008130474 A1 WO2008130474 A1 WO 2008130474A1
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WO
WIPO (PCT)
Prior art keywords
electrode
recited
housing
laser
actuator
Prior art date
Application number
PCT/US2008/003890
Other languages
French (fr)
Inventor
Richard L. Sandstrom
Tae H. Chung
Richard C. Ujazdowski
Original Assignee
Cymer, Inc. (A Nevada Corporation)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Cymer, Inc. (A Nevada Corporation) filed Critical Cymer, Inc. (A Nevada Corporation)
Priority to EP08742239.0A priority Critical patent/EP2137796B1/en
Priority to JP2010504036A priority patent/JP5680403B2/en
Priority to KR1020097022448A priority patent/KR101430516B1/en
Publication of WO2008130474A1 publication Critical patent/WO2008130474A1/en

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/02Constructional details
    • H01S3/03Constructional details of gas laser discharge tubes
    • H01S3/038Electrodes, e.g. special shape, configuration or composition
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/09Processes or apparatus for excitation, e.g. pumping
    • H01S3/097Processes or apparatus for excitation, e.g. pumping by gas discharge of a gas laser
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/09Processes or apparatus for excitation, e.g. pumping
    • H01S3/097Processes or apparatus for excitation, e.g. pumping by gas discharge of a gas laser
    • H01S3/09705Processes or apparatus for excitation, e.g. pumping by gas discharge of a gas laser with particular means for stabilising the discharge
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/09Processes or apparatus for excitation, e.g. pumping
    • H01S3/097Processes or apparatus for excitation, e.g. pumping by gas discharge of a gas laser
    • H01S3/0971Processes or apparatus for excitation, e.g. pumping by gas discharge of a gas laser transversely excited
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/02Constructional details
    • H01S3/03Constructional details of gas laser discharge tubes
    • H01S3/038Electrodes, e.g. special shape, configuration or composition
    • H01S3/0381Anodes or particular adaptations thereof
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/14Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range characterised by the material used as the active medium
    • H01S3/22Gases
    • H01S3/223Gases the active gas being polyatomic, i.e. containing two or more atoms
    • H01S3/225Gases the active gas being polyatomic, i.e. containing two or more atoms comprising an excimer or exciplex
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/23Arrangements of two or more lasers not provided for in groups H01S3/02 - H01S3/22, e.g. tandem arrangements of separate active media
    • H01S3/2366Arrangements of two or more lasers not provided for in groups H01S3/02 - H01S3/22, e.g. tandem arrangements of separate active media comprising a gas as the active medium

Definitions

  • the present application relates generally to gas discharge laser systems.
  • the present application is particularly, but not exclusively useful as an extendable electrode system for a transverse discharge gas laser.
  • Electrode erosion in high-pressure transverse discharge lasers is usually the mechanism that limits their operational lifetime.
  • the erosion of one or both of the electrodes is typically caused by the combined attack of fast ions and electrons from the current discharge.
  • the inter-electrode spacing increases to the point where the operational characteristics of the laser are so severely affected that laser operation must be stopped.
  • the gain generator must then be refurbished with new electrodes in order to re-establish the correct electrode spacing.
  • Japanese Patent Application JP06- 029592 filed on June, 10, 1991 and titled “Discharge-Pumped Laser” discloses a scheme "to regulate an interval between electrodes in accordance with consumption of a discharge part of the electrode and to always hold a discharging width constant by providing moving means for at least one of discharge electrode pair toward the other electrode.”
  • Japanese Patent Application JP06-029592 filed on June, 10, 1991 and titled “Discharge-Pumped Laser” discloses a scheme "to regulate an interval between electrodes in accordance with consumption of a discharge part of the electrode and to always hold a discharging width constant by providing moving means for at least one of discharge electrode pair toward the other electrode.”
  • Modern transverse discharge lasers are now designed to produce a relatively high power output (having both a relatively high pulse energy and high pulse repetition rate) with relatively tight specifications on beam properties such as bandwidth and pulse-to-pulse energy stability, to name just a few.
  • modern transverse discharge lasers typically include complex, highly engineered discharge chambers.
  • a relatively low impedance, low inductance current path geometry is typically provided in the chamber to conduct the extremely high peak currents that are generated by an electrical drive circuit to the electrodes.
  • the chamber may need to provide suitable heat transfer paths, for example, to prevent component overheating, and in particular, electrode overheating.
  • the chamber may need to provide suitable gas flow paths to reduce gas flow turbulence and ensure that a fresh quantity of laser gas is positioned between the electrodes prior to the initiation of the next discharge.
  • the chamber may need to provide suitable component geometries which prevent or minimize the impact of reflected acoustic waves which can reach the discharge area and adversely affect properties of the output laser beam such as bandwidth, divergence, etc.
  • Electrode extension can be performed to increase the chamber life, increase laser performance over the life of the chamber, or both.
  • the inter-electrode spacing may be adjusted to maintain a specific target gap distance between the electrodes or to optimize a specific parameter of the laser output beam such as bandwidth, pulse-to-pulse energy stability, beam size, etc.
  • control of the inter-electrode spacing may be effectuated in several different ways.
  • the inter-electrode spacing may be visually observed and the observation used to move one or both of the electrodes. For example, a technician may manually instruct a laser system controller via keypad or graphic user interface to signal an actuator, which in turn, produces the desired inter-electrode spacing adjustment.
  • the inter-electrode spacing may be adjusted using a feedback loop.
  • a controller may be provided to monitor a device parameter and generate a control signal indicative of the parameter.
  • an actuator may be operably coupled with one or both of the electrodes, the actuator responsive to the control signal to move one or both of the electrodes and adjust the inter-electrode spacing.
  • the parameter may be provided to the controller by an on-board measuring instrument or other laser component as described below.
  • the parameter can include, but is not necessarily limited to wavelength, bandwidth, pulse-to-pulse energy stability, beam size, accumulated pulse count, average historical duty cycle, a measured relationship between discharge voltage and pulse energy, or combinations thereof.
  • a controller may be programmed to scan the inter-electrode spacing over a pre-determined spacing range. During the scan, a measuring instrument or other laser component may provide one or more parameter inputs to the controller allowing the controller to determine a relationship between the parameter and the inter-electrode spacing. From the relationship, the controller may deduce an optimum inter-electrode spacing and thereafter adjust the inter- electrode spacing accordingly.
  • a first elongated rigid member having sawtooth ramp structure and a second elongated rigid member having complimentary sawtooth ramp structure are provided.
  • the ramp structures are aligned longitudinally and placed in contact with each other.
  • the first rigid member may be attached to an electrode and the second rigid member attached to an actuator such that movement of the actuator translates the second rigid member in the direction of member elongation.
  • longitudinal movement of the second rigid member causes a movement of the first rigid member (and the attached electrode) in a direction normal to the direction of member elongation.
  • Other electrode movement mechanisms are disclosed in further detail below including a cam-operated mechanism and a screw-operated mechanism.
  • a conductive, flexible member may be provided for electrically shielding moving parts and / or contact surfaces of the mechanism from the fields generated during an electrode discharge.
  • the flexible member may extend from a first flexible member edge that is attached to one of the electrodes for movement therewith to a second flexible member edge that is held fixed relative to the housing.
  • the flexible member may be formed with one or more convolutions that are aligned parallel to the direction of electrode elongation to impart flexibility to the member.
  • the second edge of the flexible member may be electrically connected to a plurality of so-called "current tines" which provide a low impedance path from the moveable electrode to a pulse power supply.
  • Fig. 1 shows a simplified, perspective, partially exploded view of a transverse discharge gas laser
  • Fig. 2 shows a simplified schematic view of a multi-stage laser system
  • Figs. 3A-D each schematically show a pair of electrodes viewed as seen along line 3A-3A in Fig. 1 with Fig. 3A showing the electrodes in their initial positions prior to erosion, Fig. 3 B showing the electrodes after erosion, Fig. 3 C showing the electrodes after erosion and after one of the electrodes has been moved to adjust the inter-electrode spacing and Fig. 3D showing the case where one electrode is moved into the initial electrode gap to accommodate erosion of the other electrode;
  • Figs. 4A-G show the components of a mechanism that may be coupled to an electrode to produce an actuator-driven, electrode movement
  • Figs. 4 A and 4B schematically show a pair of electrodes viewed as seen along line 3A-3A in Fig. 1 with Fig. 4A showing the electrode in a retracted state relative to the electrode support bar and Fig. 4B showing the electrode in an extended state relative to the electrode support bar
  • Figs. 4C and 4D show perspective, simplified views of a rigid sawtooth structure and a complementary rigid sawtooth structure, respectively
  • Figs. 4E and 4F show a moveable electrode viewed as seen along line 4E ⁇ 4E in Fig. 1 with Fig.
  • Fig. 4E showing the electrode in a retracted state relative to the electrode support bar and Fig. 4F showing the electrode in an extended state relative to the electrode support bar; and Fig. 4G shows a linkage including a push rod and pivoting lever for establishing a mechanical path between an actuator and a rigid sawtooth structure;
  • Fig. 5 shows a perspective view of a moveable electrode assembly illustrating a flexible conductive member electrically connecting the moveable electrode to a plurality of current return times
  • Figs. 6A and 6B show the components of another mechanism having a camshaft that may be coupled to an electrode to produce an actuator-driven, electrode movement, where Figs. 6A and 6B schematically show a pair of electrodes viewed as seen along line 3A-3A in Fig. 1 with Fig. 6A showing the electrode in a retracted state relative to the electrode support bar and Fig. 6B showing the electrode in an extended state relative to the electrode support bar; Figs. 7A-E show the components of drive screw mechanisms that may be coupled to an electrode to produce an actuator-driven, electrode movement, where Figs. 7A and 7B schematically show a pair of electrodes viewed as seen along line 3A-3A in Fig. 1 with Fig.
  • FIG. 7A showing the electrode in a retracted state relative to the electrode support bar and Fig. 7B showing the electrode in an extended state relative to the electrode support bar;
  • Figs. 7C-7E show a moveable electrode viewed as seen along line 4E-4E in Fig. 1 with Fig. 7C showing a mechanism having a single drive screw, Fig. 7D showing a mechanism having two drive screws, and Fig. 7E showing a mechanism having a three drive screws;
  • Figs. 8A and 8B show the components of a device having moveable flow guides to accommodate extension of electrodes having non-parallel sidewalls, where Figs. 8 A and 8B schematically show a pair of electrodes viewed as seen along line 3A-3A in Fig. 1 with Fig. 8A showing the electrode in a retracted state relative to the electrode support bar and Fig. 8B showing the electrode in an extended state relative to the electrode support bar; and
  • Fig. 9 shows a moveable electrode viewed as seen along line 4E-4E in Fig. 1 having an electrode end contour to accommodate electrode extension.
  • the device 20 may be a KrF excimer laser, an XeF excimer laser, an XeCl excimer laser, an ArF excimer laser, a molecular fluorine laser or any other type of transverse discharge gas laser known in the pertinent.
  • the device 20 may include a two-part chamber housing 22a,b being formed of a chamber wall that may be made of a conductive, corrosion resistant material, e.g., nickel-plated aluminum.
  • a conductive, corrosion resistant material e.g., nickel-plated aluminum.
  • window assemblies 24a,b may be provided at each end of the chamber housing 22a,b to allow light to enter, exit and pass through the chamber housing 22a,b along a common beam path.
  • the hollow chamber housing 22a,b and window assemblies 24a,b may surround a volume which holds a laserable gas medium under pressure together with other components suitable to create a discharge in the medium.
  • these other components may include, for example, a pair of discharge electrodes (not shown in Fig. 1), a fan to circulate the gas (not shown in Fig. 1), heat exchangers to cool the gas (not shown in Fig. 1), etc.
  • the chamber housing 22a,b may also be formed with a number of sealed inlets/outlets (not shown in Fig. 1), to allow gas to be introduced/extracted from the chamber, to allow conductors 26 to deliver an excitation voltage to the electrodes, etc.
  • the device 20 may also include a beam reverser 28 and outcoupler 30 cooperatively arranged to form an optical cavity.
  • the beam reverser 28 may be as simple as a flat, fully reflective mirror or as complex as a grating-based line-narrowing unit.
  • a moveable electrode is not limited to the stable, standing wave cavity alluded to above. Instead, a transverse discharge gas laser chamber having one or more moveable electrodes may be employed within other optical arrangements such as a one-pass amplifier, multi-pass amplifier, traveling wave amplifier such as a ring amplifier, unstable cavities, etc.
  • the device 20 may also include a pulse power system
  • Fig. 1 further illustrates that during operation of the device 20, a laser beam 34 is created which exits the optical cavity via the outcoupler 30.
  • Fig. 2 shows a multi-stage gas discharge laser device, generally designated 20' to illustrate that the inter-electrode spacing may be independently (or in some cases dependently) adjusted in one, both or all of the laser device chambers of a multi-stage device.
  • the first stage may be either a power oscillator, PO or a master oscillator, MO.
  • an oscillator is referred to as an MO if more than about a third of the total laser output power is produced in the initial oscillation cavity and is referred to as a PO if less than about a third of the total output power is produced in the initial oscillation cavity.
  • Subsequent stage(s) may be, for example, a one-pass power amplifier, a multi-pass power amplifier, a power oscillator or a traveling wave amplifier such as a ring amplifier.
  • a multistage device may include some or all of the components shown in Fig. 2, depending on the configuration.
  • the components shown in Fig. 2 include a beam reverser 28', first stage chamber 50, first stage outcoupler 30', turning optics 52a,b, incoupler 54, second stage chamber 56 and second stage outcoupler 58.
  • FIGs. 3A-D illustrate how electrode dimensional changes associated with erosion can affect the inter-electrode spacing and how the movement of one electrode relative to the other may re-establish a more desirable inter-electrode spacing.
  • Fig. 3A shows the initial electrode positions (prior to erosion) with electrode 60 spaced from electrode 62 to establish an initial inter- electrode spacing 64.
  • Fig. 3B illustrates the electrodes 60, 62 after significant electrode erosion has occurred resulting in inter-electrode spacing 66 (note initial inter-electrode spacing 64 is shown for reference purposes).
  • Fig. 3C illustrates the electrodes 60, 62 after significant electrode erosion has occurred (Fig.
  • Fig. 3D illustrates that the electrode 62 may be moved to a position where its discharge surface extends into the initial electrode gap (illustrated by the dotted lines) to accommodate erosion of electrode 60.
  • Figs. 3A-D illustrate the case of asymmetric electrode erosion.
  • electrode 62 has eroded about 10 times more than electrode 60.
  • movement of electrode 62 may be sufficient by itself (movement of electrode 60 may not be required) to provide the desired inter- electrode spacing correction.
  • This type of asymmetric electrode wear is common in certain types of transverse discharge gas lasers such as some high-power, high repetition rate, excimer lasers where the anode (the electrode electrically connected to the housing) typically erodes at a rate much greater than the cathode.
  • 3A-D illustrate asymmetric electrode erosion
  • one or both of the electrodes may be moved to provide an inter-electrode spacing correction for a device which experiences symmetric electrode wear.
  • the electrodes may be moved to set a desired inter- electrode spacing and / or may be used to move the discharge region relative to the other optics and apertures in the system.
  • the electrode movement system may be used as an alignment tool to adjust the beam footprint relative to one or more system apertures / optics.
  • the control of the inter-electrode spacing may be effectuated in several different ways.
  • the inter-electrode spacing may be visually observed, for example by looking through one of the windows 24a,b, and the observation used to move one or both of the electrodes.
  • a technician may use the observation to instruct a laser system controller 70 via keypad or graphic user interface (or any other controller input device known in the art) to signal an actuator 72, which in turn, may drive a mechanism (see description below) to produce the desired inter- electrode spacing adjustment.
  • a linkage 74 may pass through the wall of the chamber housing 22a,b, and a flexible bellows 76 (or other suitable arrangement known in the pertinent art) may be provided to prevent laser gas from exiting the chamber housing 22a,b.
  • portions (memory, processor, etc) or all of the controller 70 may be integral with (e.g. shared) or separate from a main laser system controller which controls other laser functions such as discharge voltage, timing, shutter activation, etc.
  • the inter-electrode spacing may be adjusted based on a monitored device parameter.
  • the device 20 may monitor one or more device parameters such as accumulated pulse count, average historical duty cycle, wavelength, gas pressure, running voltage, bandwidth, pulse-to-pulse energy stability (sometimes referred to as sigma), beam size, or a measured relationship between discharge voltage and pulse energy.
  • the device parameter(s) may be selected to predict the extent of electrode erosion (pulse count, average historical duty cycle, etc.) and / or may be selected to tune the laser device to produce an output beam having a desired characteristic (bandwidth, pulse-to-pulse energy stability, etc.).
  • one or more of these device parameters may be monitored by measuring a property of the output laser beam 34 using a measuring instrument 78.
  • a control signal indicative of the device parameter may then be output from the instrument 78 and transmitted to the controller 70, which in turn, provides a signal to the actuator 72.
  • Some device parameters, such as accumulated pulse count, average historical duty cycle, etc, may be provided to the controller 70 or generated within the controller 70 without the use of a measuring instrument. Thus, in at least some implementations envisioned herein, a measuring instrument 78 may not be required.
  • more than one parameter i.e., a plurality of device parameters
  • a controller may be programmed to scan the inter-electrode spacing over a pre-determined spacing range.
  • the inter- electrode spacing may be adjusted either continuously or incrementally while the laser is operating and outputting laser pulses.
  • a measuring instrument or other laser component may provide one or more parameter inputs to the controller allowing the controller to determine a relationship between the parameter(s) and the inter-electrode spacing. From the relationship, the controller may then deduce an optimum inter-electrode spacing and thereafter adjust the inter- electrode spacing accordingly.
  • Figs. 4A-E show the components of a first mechanism that may be coupled to an electrode 80 to produce an actuator-driven, electrode movement.
  • a first elongated rigid member 82 having sawtooth ramp structure and a second elongated rigid member 84 having complimentary sawtooth ramp structure are disposed within a channel formed in an electrode support bar 86, as shown in Fig. 4A (which shows the electrode 80 in a fully retracted position) and 4B (which shows the electrode 80 in a fully extended position).
  • the electrode support bar 86 is typically elongated, like the electrode and is affixed at its ends to the wall of the housing 22a,b (see Fig. 1). Perspective views of elongated rigid members 82 and 84 are shown in Figs.
  • elongated rigid member 82 is formed with a plurality of inclined, parallel surfaces, (of which surfaces 88a-c have been labeled) and an opposed flat surface 90.
  • elongated rigid member 82 is formed with a plurality of complementary, inclined, parallel surfaces, of which surfaces 92a-c have been labeled) and an opposed flat surface 94 which includes a raised flat portion 96 onto which the electrode 80 may be affixed (see Fig. 4A and 4E).
  • Fig. 4C illustrates a rigid member 82 having about 20 inclined surfaces for a 30cm electrode, it is to be appreciated that more than 20 and as few as one inclined surface may be used.
  • the rigid members 82 For the mechanism, as best seen in Figs. 4E and 4F, the rigid members 82,
  • each inclined surface 88a-c of rigid member 82 is placed into sliding contact with a corresponding inclined surface 92a-c of rigid member 84.
  • spring assemblies 100a,b may be employed to maintain a preselected contact pressure between the inclined surfaces 88a-c of rigid member 82 and inclined surfaces 92a-c of rigid member 84.
  • Figs. 4E and 4F illustrate the movement of electrode 80 in response to a movement of the elongated member 82 relative to the electrode support bar 86 with Fig. 4E showing the electrode 80 in a fully retracted position and 4F showing the electrode 80 in an extended position. Comparing Fig. 4E with 4F, it can be seen that a movement of elongated rigid member 82 relative to the electrode support bar 86 in the direction of arrow 102 will result in a movement of the electrode 80 and elongated rigid member 84 in the direction of arrow 104.
  • Fig. 4G shows a mechanism linkage which includes a substantially straight push rod 106 and an L-shaped pivoting lever 108 for establishing a mechanical path between the actuator 72 and rigid sawtooth structure 82.
  • movement of the push rod 106 in the direction of arrow 110 will cause the rigid sawtooth structure 82 to move in the direction of arrow 102 (arrow 102 also shown in Fig. 4F).
  • This in turn will cause a movement of the electrode 80 in the direction of arrow 104 as shown in Fig. 4F.
  • the rigid member 82 is disposed in a similarly sized channel formed in the support bar 86 and as such is laterally constrained therein (see Fig. 4A).
  • Fig. 4G further shows that the actuator 72 may be affixed to the wall of the chamber housing 22a and operable attached to a first end 112 of the push rod 106.
  • Push rod 106 then extends through an opening in the wall of the chamber housing 22a to a second push rod end 114 which is disposed inside the chamber.
  • Flexible bellows 76 may be provided to maintain gas pressure within the chamber while allowing translation of the push rod 106.
  • second push rod end 114 may be pivotally attached, for example using a pin / cotter key arrangement (or any similarly functioning arrangement known in the art), to the L-shaped lever 108, which in turn is pivotally attached near its midsection to the electrode support bar 86 at pivot point 116.
  • End 118 of lever 108 may be pivotally attached to rigid member 82, as shown.
  • a simpler design may be employed in which the push rod is aligned parallel to the rigid member and attached directly thereto, however, use of the L- shaped lever 108 allows for motion amplification / de-amplification depending on the relative lengths of the lever arms.
  • the actuator may be replace by a drive screw (not shown) or similar component allowing for manual adjustment of the inter-electrode spacing.
  • Another alternative to the push rod / lever system is to use a pulley / cable system to move the rigid member 82 within channel. For this alternative, the member 82 may be biased away from the pulley using a spring attached to the support bar.
  • a conductive, flexible member 120 may be provided for electrically shielding some or all of the inter- electrode spacing mechanism components and / or electrically connecting the electrode 80 to the current return tines 122a-c and / or constraining the electrode 80 and rigid member 84 from longitudinal movement (i.e., movement in the direction of arrow 98 in Fig. 4E) and / or to provide a thermally conductive path allowing heat to flow from the electrode to the support bar.
  • contacting surfaces of the electrode spacing mechanism may arc, and in extreme cases weld together, if unshielded in the presence of the electric fields generated by discharge.
  • the flexible member 120 may have a first flexible member edge 124 that is attached to electrode 80 and / or rigid member 84 for movement therewith (note: for the embodiment shown, the edge 124 is clamped between electrode 80 and rigid member 84).
  • the flexible member 120 is made of a conductive metal such as copper or brass allowing the flexible member 120 to conduct heat and / or electricity from the electrode 80 to the support bar 86 / current return tines 122a-c.
  • Figs. 4A and 5 also show that the flexible member 120 may have a second edge 126 that is attached to the support bar 86 and thus, may be held fixed relative to the housing 22a (see Fig. 1).
  • Fig. 4A further illustrates that the edge 126 of the flexible member 120 may be electrically connected to the current return tines 122 establishing an electrical path from the electrode 80 to the tines 122.
  • the current tines provide a relatively low impedance path from the flexible member 120 to a pulse power system 32 (shown in Fig. 1).
  • the flexible member 120 may be formed with one or more convolutions 128a-c, e.g. bends, that are aligned parallel to the direction of electrode elongation (i.e. the direction of arrow 98 in Fig. 4E) to impart flexibility to the member.
  • the flexible member 120 may be described as having a planar, corrugated shape.
  • the flexible member 120 may function to electrically shield some or all of the inter-electrode spacing mechanism components and / or electrically connect the electrode 80 to the current return tines 122a-c and / or constrain the electrode 80 and rigid member 84 from longitudinal movement.
  • a flexible member 120 may be designed to achieve all of these functions, it is to be appreciated that some applications may not require all three functions. For example, for some discharge power levels, shielding may not be required.
  • one or more of the three functions may be performed by another component.
  • longitudinal constraint of the electrode 80 may be performed in a different manner allowing a flexible member 120 which lacks the strength necessary to constrain the electrode 80.
  • Other arrangements may be provided which perform one or more of the functions described above including a member whose flexibility is derived from its thickness, a plurality of spaced apart flexible members and tines having one or more convolutions.
  • inter-electrode spacing can be adjusted without moving the electrode support bar 86 relative to the other laser components, e.g., fan, housing, etc.). This allows a close tolerance between the support bar 86 and other structures to be maintained. For example, in some applications, a close tolerance between the support bar 86 and a fan (not shown) may be maintained allowing the fan to run more efficiently.
  • a substantial heat transfer path is provided between the electrode 80 and the support bar 86.
  • the relatively large contact area between the rigid member 82 and rigid member 84 and the relatively large contact area between the rigid members 82, 84 and the support bar cooperate to provide a substantial heat transfer path. For some applications, this path may be useful in preventing overheating of the electrode 80.
  • Another feature of the structural arrangement shown in Figs. 4A-G and 5 is that it maintains a relatively good parallelism between electrodes over the range of electrode movements.
  • Figs. 6A and 6B show an alternative mechanism in which a camshaft 150 may be rotated about a rotation axis 152 (which may be generally parallel to the direction of electrode elongation) to provide electrode extension with Fig. 6A showing the electrode 154 in a fully retracted position and 6B showing the electrode 154 in an extended position.
  • the camshaft 150 may be in direct contact with the electrode 154 (with or without a thermally conductive rigid member establishing a heat path from the electrode 154 to the support bar 158) or, as shown, a thermally conductive rigid member 156 may be interposed between the electrode 154 and camshaft 150 and used to conduct heat from the electrode 154 to the support bar 158.
  • a thermally conductive rigid member 156 may be interposed between the electrode 154 and camshaft 150 and used to conduct heat from the electrode 154 to the support bar 158.
  • a flexible member 160 (as described above may be used to electrically shield some or all of the inter-electrode spacing mechanism components and / or electrical connect the electrode 154 to the current return tines 162 and / or provide a heat conduction path from the electrode 154 to the support bar 158.
  • the camshaft 150 may be rotated manually or by an energized actuator and may be controlled by any of the techniques / structural arrangements described above.
  • Fig. 7A-7E show alternative mechanisms which include one or more drive screws 170 to provide electrode extension with Fig. 7A showing the electrode 172 in a fully retracted position and 7B showing the electrode 172 in an extended position.
  • the drive screw(s) 170 may be in direct contact with the electrode 172 (with or without a thermally conductive rigid member establishing a heat path from the electrode 172 to the support bar 174) or, as shown, a thermally conductive rigid member 176 may be interposed between the electrode 172 and drive screw(s) 170 and used to conduct heat from the electrode 172 to the support bar 174.
  • a flexible member 178 (as described above may be used to electrically shield some or all of the inter-electrode spacing mechanism components and / or electrical connect the electrode 172 to the current return tines 180 and / or provide a heat conduction path from the electrode 172 to the support bar 174.
  • the drive screw(s) 170 may extend through the wall 182 and be threaded through a prepared hole (i.e., drilled, reamed and tapped) in the support bar 174.
  • a prepared hole may be provided in the wall 182 or some other structure or a nut (not shown) may be affixed to the wall 182 or support bar 174.
  • a flexible bellows as described above may be employed at the wall 182 to prevent gas leakage from the chamber.
  • each drive screw 170 may be rotated manually (from outside the chamber) or by an energized actuator 184 (shown with dashed lines to indicate an optional component) and may be controlled using one or more of the techniques / structural arrangements described above.
  • Springs 186a,b may be provided to bias the electrode 172 relative to the support bar 174 as shown in Fig. 7C.
  • Fig. 7D illustrates a mechanism having two drive screws 170a,b that are spaced apart along the length of the electrode 172' with each drive screw 170a, 170b independently rotatable manually (from outside the chamber) or by energized actuators 184a', 184b', respectively (shown with dashed lines to indicate an optional component).
  • Fig. 7E illustrates a mechanism having three drive screws 170c,d,e that are spaced apart along the length of the electrode 172" with each drive screw 170c,d,e independently rotatable manually (from outside the chamber) or by energized actuators 184c',d',e', respectively (shown with dashed lines to indicate an optional component).
  • each of the drive screws may be independently adjusted to adjust inter-electrode parallelism and / or inter-electrode spacing. Specifically, the drive screws may be independently adjusted until the electrode 172" is parallel to the other electrode in the discharge pair (dotted lines in Fig. 7D showing an unaligned electrode and solid lines showing an electrode after alignment into parallel with another electrode).
  • each of the drive screws 170 may be independently adjusted to adjust electrode parallelism (as described above) and / or electrode curvature and / or inter-electrode spacing. Specifically, the drive screws may be independently adjusted until the electrode 172" has a desired curvature such as straight or having a curvature matching the other electrode (dotted lines in Fig. 7D showing a non-desired curvature and solid lines showing an electrode after a curvature adjustment).
  • Figs. 8A and 8B show an electrode 200 having a tapered construction (in a plane normal to the direction of electrode elongation) in which the electrode width, 'w', decreases gradually from the electrode base 202 to the initial discharge surface 204.
  • Other electrode designs can include an hourglass shape (not shown) in which the electrode width decreases from the base to a minimum and increases thereafter to the initial discharge surface.
  • FIG. 8 A and 8B also show that flow guides 206a,b, which may be made of an insulating ceramic material may be disposed surrounding the electrode 200 on each side to control the flow of gas over the tip of the electrode 200 and prevent the discharge from striking metal structures adjacent to the electrode 200.
  • these guides may be affixed to the support bar and may remain stationary with respect thereto. Comparing Fig. 4A to 4B, it can be seen that extension of the electrode 80 with parallel sidewalls does not affect the spacing between the electrode sidewalls and stationary flow guides 206a', 206b'.
  • electrode extension may affect the spacing between the electrode sidewalls and stationary flow guides 206a,b.
  • Fig. 8A and 8B illustrate an arrangement in which the flow guides 206a,b are moveable attached to the support bar 208 allowing the flow guides 206a,b to move apart (in the direction of arrows 210a,b from one another as the electrode 200 is extended (in the direction of arrow 212).
  • each flow guide 206a,b is form with a surface 214 that contacts the electrode 200 and is inclined at an angle relative to the direction of electrode movement (arrow 212)
  • one or more springs may be provided to bias each flow guide 206a,b toward the electrode 200.
  • Fig. 9 shows a pair of electrodes 218, 220 and illustrates an end contour for a moveable electrode 220.
  • electrode 218 is formed with a relatively flat portion 222 where discharge is desired and begins to curve away from the discharge region at point 224.
  • Electrode 220 is shown with the solid line indicating its initial electrode shape and the dashed line indicating it end-of-life shape.
  • the electrode 220 is initially formed with a relatively flat portion 226 where discharge is desired, a curved transition section 228 and a second flat section 230.
  • the flat section 230 may be spaced at a distance 'df from the electrode base 232, the beginning-of-life flat section 226 may be spaced at a distance 'd 2 ' from the electrode base 232, and the end-of-life flat section 234 may be spaced at a distance 'd 3 ' from the electrode base 232, with d 2 > di > d 3 .
  • d 2 - d 3 may be about 3mm.
  • One feature of the arrangement shown is that it confines the discharge to a selected discharge region (ending near point 224) over the life of the electrode 220.

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Abstract

Disclosed herein are systems and methods for extending one or both of the discharge electrodes in a transverse discharge gas laser chamber in which one or both the electrodes are subject to a dimensional change due to erosion. Electrode extension can be performed to increase the chamber life, increase laser performance over the life of the chamber, or both. Operationally, the inter-electrode spacing may be adjusted to maintain a specific target gap distance between the electrodes or to optimize a specific parameter of the laser output beam such as bandwidth, pulse-to-pulse energy stability, beam size, etc.

Description

Extendable Electrode for Gas Discharge Laser
Richard Sandstrom
Tae H. Chung Richard C. Ujazdowski
The present application claims priority to U.S. Serial No. 11/787,463, filed on April 16, 2007, entitled Extendable Electrode for Gas Discharge Laser, which is a continuation-in-part application of co-pending, co-owned U.S. Serial No.
10/854,614 filed May 25, 2004 (attorney docket number 1999-0013-15) which is continuation of U.S. Serial No.10/056,619, filed January 23, 2002, (attorney docket number 1999-0013-01) now patent number 6,801,560, which issued on October 5, 2004, which is a continuation-in-part of U.S. Serial No. 09/768,753, which issued on July 2, 2002 as U.S. Patent No. 6,414,979 (attorney docket number 2001-0001-
01) the entire contents of each of which are hereby incorporated by reference herein.
The present application is related to U.S. Serial No. 09/590,961, which issued on October 15, 2002 as U.S. Patent No. 6,466,602 (attorney docket number 1998-0060-01), the entire contents of which are hereby incorporated by reference herein.
FIELD
The present application relates generally to gas discharge laser systems. The present application is particularly, but not exclusively useful as an extendable electrode system for a transverse discharge gas laser.
BACKGROUND
Electrode erosion in high-pressure transverse discharge lasers is usually the mechanism that limits their operational lifetime. The erosion of one or both of the electrodes is typically caused by the combined attack of fast ions and electrons from the current discharge. As the electrodes wear, the inter-electrode spacing increases to the point where the operational characteristics of the laser are so severely affected that laser operation must be stopped. The gain generator must then be refurbished with new electrodes in order to re-establish the correct electrode spacing.
In an attempt to increase laser lifetime, Japanese Patent Application JP06- 029592 filed on June, 10, 1991 and titled "Discharge-Pumped Laser" discloses a scheme "to regulate an interval between electrodes in accordance with consumption of a discharge part of the electrode and to always hold a discharging width constant by providing moving means for at least one of discharge electrode pair toward the other electrode." However, to applicant's knowledge, such a relatively simplistic system has yet to be successfully commercialized. Since 1991 when Japanese Patent Application JP06-029592 was filed, gas discharge lasers have evolved substantially. Modern transverse discharge lasers are now designed to produce a relatively high power output (having both a relatively high pulse energy and high pulse repetition rate) with relatively tight specifications on beam properties such as bandwidth and pulse-to-pulse energy stability, to name just a few. To achieve this performance, modern transverse discharge lasers typically include complex, highly engineered discharge chambers. For example, a relatively low impedance, low inductance current path geometry is typically provided in the chamber to conduct the extremely high peak currents that are generated by an electrical drive circuit to the electrodes. Also, the chamber may need to provide suitable heat transfer paths, for example, to prevent component overheating, and in particular, electrode overheating. In addition to heat transfer paths, the chamber may need to provide suitable gas flow paths to reduce gas flow turbulence and ensure that a fresh quantity of laser gas is positioned between the electrodes prior to the initiation of the next discharge. Concurrent with the above- described engineering constraints, the chamber may need to provide suitable component geometries which prevent or minimize the impact of reflected acoustic waves which can reach the discharge area and adversely affect properties of the output laser beam such as bandwidth, divergence, etc.
With the above considerations in mind, Applicants disclose an extendable electrode system for a gas discharge laser. SUMMARY
Disclosed herein are systems and methods for extending one or both of the discharge electrodes in a transverse discharge laser chamber in which the electrodes are subject to a dimensional change due to erosion. Electrode extension can be performed to increase the chamber life, increase laser performance over the life of the chamber, or both. Operationally, the inter-electrode spacing may be adjusted to maintain a specific target gap distance between the electrodes or to optimize a specific parameter of the laser output beam such as bandwidth, pulse-to-pulse energy stability, beam size, etc. As disclosed herein, control of the inter-electrode spacing may be effectuated in several different ways. In one implementation, the inter-electrode spacing may be visually observed and the observation used to move one or both of the electrodes. For example, a technician may manually instruct a laser system controller via keypad or graphic user interface to signal an actuator, which in turn, produces the desired inter-electrode spacing adjustment.
In another implementation, the inter-electrode spacing may be adjusted using a feedback loop. For example, a controller may be provided to monitor a device parameter and generate a control signal indicative of the parameter. For use with the controller, an actuator may be operably coupled with one or both of the electrodes, the actuator responsive to the control signal to move one or both of the electrodes and adjust the inter-electrode spacing. For this implementation, the parameter may be provided to the controller by an on-board measuring instrument or other laser component as described below. The parameter can include, but is not necessarily limited to wavelength, bandwidth, pulse-to-pulse energy stability, beam size, accumulated pulse count, average historical duty cycle, a measured relationship between discharge voltage and pulse energy, or combinations thereof.
In a particular implementation, a controller may be programmed to scan the inter-electrode spacing over a pre-determined spacing range. During the scan, a measuring instrument or other laser component may provide one or more parameter inputs to the controller allowing the controller to determine a relationship between the parameter and the inter-electrode spacing. From the relationship, the controller may deduce an optimum inter-electrode spacing and thereafter adjust the inter- electrode spacing accordingly.
Several mechanisms capable of being coupled to an electrode to produce an actuator-driven, electrode movement are disclosed herein. In one mechanism, a first elongated rigid member having sawtooth ramp structure and a second elongated rigid member having complimentary sawtooth ramp structure are provided. The ramp structures are aligned longitudinally and placed in contact with each other. The first rigid member may be attached to an electrode and the second rigid member attached to an actuator such that movement of the actuator translates the second rigid member in the direction of member elongation. With this structural arrangement, longitudinal movement of the second rigid member causes a movement of the first rigid member (and the attached electrode) in a direction normal to the direction of member elongation. Other electrode movement mechanisms are disclosed in further detail below including a cam-operated mechanism and a screw-operated mechanism. For use in conjunction with one or more of the electrode movement mechanisms described above, a conductive, flexible member may be provided for electrically shielding moving parts and / or contact surfaces of the mechanism from the fields generated during an electrode discharge. For example, the flexible member may extend from a first flexible member edge that is attached to one of the electrodes for movement therewith to a second flexible member edge that is held fixed relative to the housing. In some cases, the flexible member may be formed with one or more convolutions that are aligned parallel to the direction of electrode elongation to impart flexibility to the member. In one embodiment, the second edge of the flexible member may be electrically connected to a plurality of so-called "current tines" which provide a low impedance path from the moveable electrode to a pulse power supply.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 shows a simplified, perspective, partially exploded view of a transverse discharge gas laser;
Fig. 2 shows a simplified schematic view of a multi-stage laser system; Figs. 3A-D each schematically show a pair of electrodes viewed as seen along line 3A-3A in Fig. 1 with Fig. 3A showing the electrodes in their initial positions prior to erosion, Fig. 3 B showing the electrodes after erosion, Fig. 3 C showing the electrodes after erosion and after one of the electrodes has been moved to adjust the inter-electrode spacing and Fig. 3D showing the case where one electrode is moved into the initial electrode gap to accommodate erosion of the other electrode;
Figs. 4A-G show the components of a mechanism that may be coupled to an electrode to produce an actuator-driven, electrode movement, where Figs. 4 A and 4B schematically show a pair of electrodes viewed as seen along line 3A-3A in Fig. 1 with Fig. 4A showing the electrode in a retracted state relative to the electrode support bar and Fig. 4B showing the electrode in an extended state relative to the electrode support bar; Figs. 4C and 4D show perspective, simplified views of a rigid sawtooth structure and a complementary rigid sawtooth structure, respectively; Figs. 4E and 4F show a moveable electrode viewed as seen along line 4E÷4E in Fig. 1 with Fig. 4E showing the electrode in a retracted state relative to the electrode support bar and Fig. 4F showing the electrode in an extended state relative to the electrode support bar; and Fig. 4G shows a linkage including a push rod and pivoting lever for establishing a mechanical path between an actuator and a rigid sawtooth structure;
Fig. 5 shows a perspective view of a moveable electrode assembly illustrating a flexible conductive member electrically connecting the moveable electrode to a plurality of current return times;
Figs. 6A and 6B show the components of another mechanism having a camshaft that may be coupled to an electrode to produce an actuator-driven, electrode movement, where Figs. 6A and 6B schematically show a pair of electrodes viewed as seen along line 3A-3A in Fig. 1 with Fig. 6A showing the electrode in a retracted state relative to the electrode support bar and Fig. 6B showing the electrode in an extended state relative to the electrode support bar; Figs. 7A-E show the components of drive screw mechanisms that may be coupled to an electrode to produce an actuator-driven, electrode movement, where Figs. 7A and 7B schematically show a pair of electrodes viewed as seen along line 3A-3A in Fig. 1 with Fig. 7A showing the electrode in a retracted state relative to the electrode support bar and Fig. 7B showing the electrode in an extended state relative to the electrode support bar; Figs. 7C-7E show a moveable electrode viewed as seen along line 4E-4E in Fig. 1 with Fig. 7C showing a mechanism having a single drive screw, Fig. 7D showing a mechanism having two drive screws, and Fig. 7E showing a mechanism having a three drive screws;
Figs. 8A and 8B show the components of a device having moveable flow guides to accommodate extension of electrodes having non-parallel sidewalls, where Figs. 8 A and 8B schematically show a pair of electrodes viewed as seen along line 3A-3A in Fig. 1 with Fig. 8A showing the electrode in a retracted state relative to the electrode support bar and Fig. 8B showing the electrode in an extended state relative to the electrode support bar; and
Fig. 9 shows a moveable electrode viewed as seen along line 4E-4E in Fig. 1 having an electrode end contour to accommodate electrode extension.
DESCRIPTION
Referring initially to Fig. 1 , a simplified, partially exploded view of portions of a transverse discharge gas laser device are shown and generally designated 20. For example, the device 20 may be a KrF excimer laser, an XeF excimer laser, an XeCl excimer laser, an ArF excimer laser, a molecular fluorine laser or any other type of transverse discharge gas laser known in the pertinent. As shown, the device 20 may include a two-part chamber housing 22a,b being formed of a chamber wall that may be made of a conductive, corrosion resistant material, e.g., nickel-plated aluminum. As further shown in Fig. 1 , window assemblies 24a,b may be provided at each end of the chamber housing 22a,b to allow light to enter, exit and pass through the chamber housing 22a,b along a common beam path. With this structure, the hollow chamber housing 22a,b and window assemblies 24a,b may surround a volume which holds a laserable gas medium under pressure together with other components suitable to create a discharge in the medium. These other components may include, for example, a pair of discharge electrodes (not shown in Fig. 1), a fan to circulate the gas (not shown in Fig. 1), heat exchangers to cool the gas (not shown in Fig. 1), etc. It is to be appreciated that the chamber housing 22a,b may also be formed with a number of sealed inlets/outlets (not shown in Fig. 1), to allow gas to be introduced/extracted from the chamber, to allow conductors 26 to deliver an excitation voltage to the electrodes, etc.
In addition to the chamber, Fig. 1 shows that the device 20 may also include a beam reverser 28 and outcoupler 30 cooperatively arranged to form an optical cavity. For the device 20, the beam reverser 28 may be as simple as a flat, fully reflective mirror or as complex as a grating-based line-narrowing unit. It is to be appreciated that the use of a moveable electrode is not limited to the stable, standing wave cavity alluded to above. Instead, a transverse discharge gas laser chamber having one or more moveable electrodes may be employed within other optical arrangements such as a one-pass amplifier, multi-pass amplifier, traveling wave amplifier such as a ring amplifier, unstable cavities, etc. Continuing with Fig. 1, the device 20 may also include a pulse power system
32 delivering electrical pulses to electrodes located within the chamber housing 22a,b via conductors 26. Although the description that follows will be provided with reference to a pulsed laser device, it is to be appreciated that some or all of the concepts disclosed herein may be equally applicable to continuous discharge gas laser devices which have electrodes that suffer a dimension change due to erosion or some other phenomenon. Fig. 1 further illustrates that during operation of the device 20, a laser beam 34 is created which exits the optical cavity via the outcoupler 30.
Fig. 2 shows a multi-stage gas discharge laser device, generally designated 20' to illustrate that the inter-electrode spacing may be independently (or in some cases dependently) adjusted in one, both or all of the laser device chambers of a multi-stage device. For example, the first stage may be either a power oscillator, PO or a master oscillator, MO. Typically, an oscillator is referred to as an MO if more than about a third of the total laser output power is produced in the initial oscillation cavity and is referred to as a PO if less than about a third of the total output power is produced in the initial oscillation cavity. Subsequent stage(s) may be, for example, a one-pass power amplifier, a multi-pass power amplifier, a power oscillator or a traveling wave amplifier such as a ring amplifier. It is to be appreciated that a multistage device may include some or all of the components shown in Fig. 2, depending on the configuration. The components shown in Fig. 2 include a beam reverser 28', first stage chamber 50, first stage outcoupler 30', turning optics 52a,b, incoupler 54, second stage chamber 56 and second stage outcoupler 58.
INTER-ELECTRODE SPACING ADJUSTMENT Figs. 3A-D illustrate how electrode dimensional changes associated with erosion can affect the inter-electrode spacing and how the movement of one electrode relative to the other may re-establish a more desirable inter-electrode spacing. In more detail, Fig. 3A shows the initial electrode positions (prior to erosion) with electrode 60 spaced from electrode 62 to establish an initial inter- electrode spacing 64. Fig. 3B illustrates the electrodes 60, 62 after significant electrode erosion has occurred resulting in inter-electrode spacing 66 (note initial inter-electrode spacing 64 is shown for reference purposes). Fig. 3C illustrates the electrodes 60, 62 after significant electrode erosion has occurred (Fig. 3B) and after electrode 62 has been moved in the direction of arrow 68 resulting in an inter- electrode spacing that is close to the initial inter-electrode spacing 64. Fig. 3D illustrates that the electrode 62 may be moved to a position where its discharge surface extends into the initial electrode gap (illustrated by the dotted lines) to accommodate erosion of electrode 60.
Figs. 3A-D illustrate the case of asymmetric electrode erosion. In particular, it is clear from Fig. 3 B that electrode 62 has eroded about 10 times more than electrode 60. For this case, movement of electrode 62 may be sufficient by itself (movement of electrode 60 may not be required) to provide the desired inter- electrode spacing correction. This type of asymmetric electrode wear is common in certain types of transverse discharge gas lasers such as some high-power, high repetition rate, excimer lasers where the anode (the electrode electrically connected to the housing) typically erodes at a rate much greater than the cathode. Although Figs. 3A-D illustrate asymmetric electrode erosion, it is to be appreciated that one or both of the electrodes may be moved to provide an inter-electrode spacing correction for a device which experiences symmetric electrode wear. For systems where both electrodes are moveable, the electrodes may be moved to set a desired inter- electrode spacing and / or may be used to move the discharge region relative to the other optics and apertures in the system. Thus, the electrode movement system may be used as an alignment tool to adjust the beam footprint relative to one or more system apertures / optics.
INTER-ELECTRODE SPACING CONTROL For the device 20 shown in Fig. 1, the control of the inter-electrode spacing may be effectuated in several different ways. In perhaps the simplest implementation, the inter-electrode spacing may be visually observed, for example by looking through one of the windows 24a,b, and the observation used to move one or both of the electrodes. For example, a technician may use the observation to instruct a laser system controller 70 via keypad or graphic user interface (or any other controller input device known in the art) to signal an actuator 72, which in turn, may drive a mechanism (see description below) to produce the desired inter- electrode spacing adjustment. For this purpose, a linkage 74 may pass through the wall of the chamber housing 22a,b, and a flexible bellows 76 (or other suitable arrangement known in the pertinent art) may be provided to prevent laser gas from exiting the chamber housing 22a,b. It is to be appreciated that portions (memory, processor, etc) or all of the controller 70 may be integral with (e.g. shared) or separate from a main laser system controller which controls other laser functions such as discharge voltage, timing, shutter activation, etc. In another implementation, the inter-electrode spacing may be adjusted based on a monitored device parameter. For example, the device 20 may monitor one or more device parameters such as accumulated pulse count, average historical duty cycle, wavelength, gas pressure, running voltage, bandwidth, pulse-to-pulse energy stability (sometimes referred to as sigma), beam size, or a measured relationship between discharge voltage and pulse energy. The device parameter(s) may be selected to predict the extent of electrode erosion (pulse count, average historical duty cycle, etc.) and / or may be selected to tune the laser device to produce an output beam having a desired characteristic (bandwidth, pulse-to-pulse energy stability, etc.).
As shown in Fig. 1, one or more of these device parameters may be monitored by measuring a property of the output laser beam 34 using a measuring instrument 78. A control signal indicative of the device parameter may then be output from the instrument 78 and transmitted to the controller 70, which in turn, provides a signal to the actuator 72. Some device parameters, such as accumulated pulse count, average historical duty cycle, etc, may be provided to the controller 70 or generated within the controller 70 without the use of a measuring instrument. Thus, in at least some implementations envisioned herein, a measuring instrument 78 may not be required. One the other hand, more than one parameter (i.e., a plurality of device parameters) may be communicated to, or developed within, the controller 70 for processing in an algorithm to determine an appropriate inter- electrode spacing adjustment.
In a particular implementation, a controller may be programmed to scan the inter-electrode spacing over a pre-determined spacing range. Thus, the inter- electrode spacing may be adjusted either continuously or incrementally while the laser is operating and outputting laser pulses. During the scan, a measuring instrument or other laser component may provide one or more parameter inputs to the controller allowing the controller to determine a relationship between the parameter(s) and the inter-electrode spacing. From the relationship, the controller may then deduce an optimum inter-electrode spacing and thereafter adjust the inter- electrode spacing accordingly.
INTER-ELECTRODE SPACING MECHANISMS
Figs. 4A-E show the components of a first mechanism that may be coupled to an electrode 80 to produce an actuator-driven, electrode movement. For the mechanism, a first elongated rigid member 82 having sawtooth ramp structure and a second elongated rigid member 84 having complimentary sawtooth ramp structure are disposed within a channel formed in an electrode support bar 86, as shown in Fig. 4A (which shows the electrode 80 in a fully retracted position) and 4B (which shows the electrode 80 in a fully extended position). For the device, the electrode support bar 86 is typically elongated, like the electrode and is affixed at its ends to the wall of the housing 22a,b (see Fig. 1). Perspective views of elongated rigid members 82 and 84 are shown in Figs.
4C and 4D, respectively. As seen there, elongated rigid member 82 is formed with a plurality of inclined, parallel surfaces, (of which surfaces 88a-c have been labeled) and an opposed flat surface 90. Somewhat similarly, elongated rigid member 82 is formed with a plurality of complementary, inclined, parallel surfaces, of which surfaces 92a-c have been labeled) and an opposed flat surface 94 which includes a raised flat portion 96 onto which the electrode 80 may be affixed (see Fig. 4A and 4E). Although Fig. 4C illustrates a rigid member 82 having about 20 inclined surfaces for a 30cm electrode, it is to be appreciated that more than 20 and as few as one inclined surface may be used. For the mechanism, as best seen in Figs. 4E and 4F, the rigid members 82,
84 are aligned longitudinally (i.e., each aligned parallel to the direction of electrode elongation shown by arrow 98) and placed in contact with each other. Specifically, each inclined surface 88a-c of rigid member 82 is placed into sliding contact with a corresponding inclined surface 92a-c of rigid member 84. As further shown in Fig. 4E, spring assemblies 100a,b may be employed to maintain a preselected contact pressure between the inclined surfaces 88a-c of rigid member 82 and inclined surfaces 92a-c of rigid member 84.
Figs. 4E and 4F illustrate the movement of electrode 80 in response to a movement of the elongated member 82 relative to the electrode support bar 86 with Fig. 4E showing the electrode 80 in a fully retracted position and 4F showing the electrode 80 in an extended position. Comparing Fig. 4E with 4F, it can be seen that a movement of elongated rigid member 82 relative to the electrode support bar 86 in the direction of arrow 102 will result in a movement of the electrode 80 and elongated rigid member 84 in the direction of arrow 104. Similarly, movement of elongated rigid member 82 relative to the electrode support bar 86 in the direction opposite arrow 102 will result in a movement of the electrode 80 and elongated member 84 in the direction opposite arrow 104 with the spring assemblies maintaining contact between the inclined surfaces 88a-c, 92a-c.
Fig. 4G shows a mechanism linkage which includes a substantially straight push rod 106 and an L-shaped pivoting lever 108 for establishing a mechanical path between the actuator 72 and rigid sawtooth structure 82. With this arrangement, movement of the push rod 106 in the direction of arrow 110 will cause the rigid sawtooth structure 82 to move in the direction of arrow 102 (arrow 102 also shown in Fig. 4F). This in turn will cause a movement of the electrode 80 in the direction of arrow 104 as shown in Fig. 4F. Note: the rigid member 82 is disposed in a similarly sized channel formed in the support bar 86 and as such is laterally constrained therein (see Fig. 4A).
Fig. 4G further shows that the actuator 72 may be affixed to the wall of the chamber housing 22a and operable attached to a first end 112 of the push rod 106. Push rod 106 then extends through an opening in the wall of the chamber housing 22a to a second push rod end 114 which is disposed inside the chamber. Flexible bellows 76 may be provided to maintain gas pressure within the chamber while allowing translation of the push rod 106. Also shown, second push rod end 114 may be pivotally attached, for example using a pin / cotter key arrangement (or any similarly functioning arrangement known in the art), to the L-shaped lever 108, which in turn is pivotally attached near its midsection to the electrode support bar 86 at pivot point 116. End 118 of lever 108 may be pivotally attached to rigid member 82, as shown. A simpler design may be employed in which the push rod is aligned parallel to the rigid member and attached directly thereto, however, use of the L- shaped lever 108 allows for motion amplification / de-amplification depending on the relative lengths of the lever arms. If desired, the actuator may be replace by a drive screw (not shown) or similar component allowing for manual adjustment of the inter-electrode spacing. Another alternative to the push rod / lever system is to use a pulley / cable system to move the rigid member 82 within channel. For this alternative, the member 82 may be biased away from the pulley using a spring attached to the support bar. FLEXIBLE CONDUCTIVE MEMBER
As best seen cross-referencing to Figs. 4 A and 5, a conductive, flexible member 120 may be provided for electrically shielding some or all of the inter- electrode spacing mechanism components and / or electrically connecting the electrode 80 to the current return tines 122a-c and / or constraining the electrode 80 and rigid member 84 from longitudinal movement (i.e., movement in the direction of arrow 98 in Fig. 4E) and / or to provide a thermally conductive path allowing heat to flow from the electrode to the support bar. In some applications, contacting surfaces of the electrode spacing mechanism may arc, and in extreme cases weld together, if unshielded in the presence of the electric fields generated by discharge.
As shown in Figs. 4 A and 5, the flexible member 120 may have a first flexible member edge 124 that is attached to electrode 80 and / or rigid member 84 for movement therewith (note: for the embodiment shown, the edge 124 is clamped between electrode 80 and rigid member 84). Typically, the flexible member 120 is made of a conductive metal such as copper or brass allowing the flexible member 120 to conduct heat and / or electricity from the electrode 80 to the support bar 86 / current return tines 122a-c.
Figs. 4A and 5 also show that the flexible member 120 may have a second edge 126 that is attached to the support bar 86 and thus, may be held fixed relative to the housing 22a (see Fig. 1). Fig. 4A further illustrates that the edge 126 of the flexible member 120 may be electrically connected to the current return tines 122 establishing an electrical path from the electrode 80 to the tines 122. The current tines, in turn, provide a relatively low impedance path from the flexible member 120 to a pulse power system 32 (shown in Fig. 1). For the device shown, the flexible member 120 may be formed with one or more convolutions 128a-c, e.g. bends, that are aligned parallel to the direction of electrode elongation (i.e. the direction of arrow 98 in Fig. 4E) to impart flexibility to the member. With this arrangement, the flexible member 120 may be described as having a planar, corrugated shape.
As described above, the flexible member 120 may function to electrically shield some or all of the inter-electrode spacing mechanism components and / or electrically connect the electrode 80 to the current return tines 122a-c and / or constrain the electrode 80 and rigid member 84 from longitudinal movement. Although a flexible member 120 may be designed to achieve all of these functions, it is to be appreciated that some applications may not require all three functions. For example, for some discharge power levels, shielding may not be required. Moreover, one or more of the three functions may be performed by another component. For example, longitudinal constraint of the electrode 80 may be performed in a different manner allowing a flexible member 120 which lacks the strength necessary to constrain the electrode 80. Other arrangements may be provided which perform one or more of the functions described above including a member whose flexibility is derived from its thickness, a plurality of spaced apart flexible members and tines having one or more convolutions.
One feature of the structural arrangement shown in Figs. 4A-G and 5 is that the inter-electrode spacing can be adjusted without moving the electrode support bar 86 relative to the other laser components, e.g., fan, housing, etc.). This allows a close tolerance between the support bar 86 and other structures to be maintained. For example, in some applications, a close tolerance between the support bar 86 and a fan (not shown) may be maintained allowing the fan to run more efficiently.
Another feature of the structural arrangement shown in Figs. 4A-G and 5 is that a substantial heat transfer path is provided between the electrode 80 and the support bar 86. In particular, the relatively large contact area between the rigid member 82 and rigid member 84 and the relatively large contact area between the rigid members 82, 84 and the support bar cooperate to provide a substantial heat transfer path. For some applications, this path may be useful in preventing overheating of the electrode 80. Another feature of the structural arrangement shown in Figs. 4A-G and 5 is that it maintains a relatively good parallelism between electrodes over the range of electrode movements.
Figs. 6A and 6B show an alternative mechanism in which a camshaft 150 may be rotated about a rotation axis 152 (which may be generally parallel to the direction of electrode elongation) to provide electrode extension with Fig. 6A showing the electrode 154 in a fully retracted position and 6B showing the electrode 154 in an extended position. For the mechanism, the camshaft 150 may be in direct contact with the electrode 154 (with or without a thermally conductive rigid member establishing a heat path from the electrode 154 to the support bar 158) or, as shown, a thermally conductive rigid member 156 may be interposed between the electrode 154 and camshaft 150 and used to conduct heat from the electrode 154 to the support bar 158. For the mechanism shown in Fig. 6, a flexible member 160 (as described above may be used to electrically shield some or all of the inter-electrode spacing mechanism components and / or electrical connect the electrode 154 to the current return tines 162 and / or provide a heat conduction path from the electrode 154 to the support bar 158. For the device, the camshaft 150 may be rotated manually or by an energized actuator and may be controlled by any of the techniques / structural arrangements described above.
Fig. 7A-7E show alternative mechanisms which include one or more drive screws 170 to provide electrode extension with Fig. 7A showing the electrode 172 in a fully retracted position and 7B showing the electrode 172 in an extended position. For the mechanism, the drive screw(s) 170 may be in direct contact with the electrode 172 (with or without a thermally conductive rigid member establishing a heat path from the electrode 172 to the support bar 174) or, as shown, a thermally conductive rigid member 176 may be interposed between the electrode 172 and drive screw(s) 170 and used to conduct heat from the electrode 172 to the support bar 174.
For the mechanism shown in Figs. 7A-7E, a flexible member 178 (as described above may be used to electrically shield some or all of the inter-electrode spacing mechanism components and / or electrical connect the electrode 172 to the current return tines 180 and / or provide a heat conduction path from the electrode 172 to the support bar 174. Cross-referencing Figs. 7A and 7C, it may be seen that the drive screw(s) 170 may extend through the wall 182 and be threaded through a prepared hole (i.e., drilled, reamed and tapped) in the support bar 174. Alternatively, a prepared hole may be provided in the wall 182 or some other structure or a nut (not shown) may be affixed to the wall 182 or support bar 174. A flexible bellows as described above (not shown) may be employed at the wall 182 to prevent gas leakage from the chamber. For these mechanisms, each drive screw 170 may be rotated manually (from outside the chamber) or by an energized actuator 184 (shown with dashed lines to indicate an optional component) and may be controlled using one or more of the techniques / structural arrangements described above. Springs 186a,b may be provided to bias the electrode 172 relative to the support bar 174 as shown in Fig. 7C.
Fig. 7D illustrates a mechanism having two drive screws 170a,b that are spaced apart along the length of the electrode 172' with each drive screw 170a, 170b independently rotatable manually (from outside the chamber) or by energized actuators 184a', 184b', respectively (shown with dashed lines to indicate an optional component).
Fig. 7E illustrates a mechanism having three drive screws 170c,d,e that are spaced apart along the length of the electrode 172" with each drive screw 170c,d,e independently rotatable manually (from outside the chamber) or by energized actuators 184c',d',e', respectively (shown with dashed lines to indicate an optional component).
For the mechanisms having two or more drive screw(s) 170 (Figs. 7D and 7E), each of the drive screws may be independently adjusted to adjust inter-electrode parallelism and / or inter-electrode spacing. Specifically, the drive screws may be independently adjusted until the electrode 172" is parallel to the other electrode in the discharge pair (dotted lines in Fig. 7D showing an unaligned electrode and solid lines showing an electrode after alignment into parallel with another electrode).
For mechanisms having three or more drive screw(s) 170 (Fig. 7E), each of the drive screws 170 may be independently adjusted to adjust electrode parallelism (as described above) and / or electrode curvature and / or inter-electrode spacing. Specifically, the drive screws may be independently adjusted until the electrode 172" has a desired curvature such as straight or having a curvature matching the other electrode (dotted lines in Fig. 7D showing a non-desired curvature and solid lines showing an electrode after a curvature adjustment). MOVEABLE FLOW GUIDES
Although the electrode 80 shown in Fig. 4A has substantially straight, parallel sidewalls, it is to be appreciated that other electrode shapes may be used in the devices described herein. For example, Figs. 8A and 8B show an electrode 200 having a tapered construction (in a plane normal to the direction of electrode elongation) in which the electrode width, 'w', decreases gradually from the electrode base 202 to the initial discharge surface 204. Other electrode designs can include an hourglass shape (not shown) in which the electrode width decreases from the base to a minimum and increases thereafter to the initial discharge surface. Figs. 8 A and 8B also show that flow guides 206a,b, which may be made of an insulating ceramic material may be disposed surrounding the electrode 200 on each side to control the flow of gas over the tip of the electrode 200 and prevent the discharge from striking metal structures adjacent to the electrode 200. For the case of electrodes having parallel sidewalls (Fig. 4A) these guides may be affixed to the support bar and may remain stationary with respect thereto. Comparing Fig. 4A to 4B, it can be seen that extension of the electrode 80 with parallel sidewalls does not affect the spacing between the electrode sidewalls and stationary flow guides 206a', 206b'. On the other hand, for electrodes having non-parallel sidewalls, such as electrode 200 in Fig. 8A, electrode extension may affect the spacing between the electrode sidewalls and stationary flow guides 206a,b.
Fig. 8A and 8B illustrate an arrangement in which the flow guides 206a,b are moveable attached to the support bar 208 allowing the flow guides 206a,b to move apart (in the direction of arrows 210a,b from one another as the electrode 200 is extended (in the direction of arrow 212). To effectuate this flow guide movement, each flow guide 206a,b is form with a surface 214 that contacts the electrode 200 and is inclined at an angle relative to the direction of electrode movement (arrow 212) For the arrangement shown, one or more springs (not shown) may be provided to bias each flow guide 206a,b toward the electrode 200. ELECTRODE END CONTOUR
Fig. 9 shows a pair of electrodes 218, 220 and illustrates an end contour for a moveable electrode 220. As shown, electrode 218 is formed with a relatively flat portion 222 where discharge is desired and begins to curve away from the discharge region at point 224. Electrode 220 is shown with the solid line indicating its initial electrode shape and the dashed line indicating it end-of-life shape. As shown, the electrode 220 is initially formed with a relatively flat portion 226 where discharge is desired, a curved transition section 228 and a second flat section 230. As shown, the flat section 230 may be spaced at a distance 'df from the electrode base 232, the beginning-of-life flat section 226 may be spaced at a distance 'd2' from the electrode base 232, and the end-of-life flat section 234 may be spaced at a distance 'd3' from the electrode base 232, with d2 > di > d3. In a particular embodiment, the electrode 220 is formed with
Figure imgf000019_0001
= d3 + n(d2 - d3), where n is typically in the range of about 0.25 to 0.75, placing the flat section 230 between the average height of the electrode 220 over the electrode's life. For example, d2 - d3 may be about 3mm. One feature of the arrangement shown is that it confines the discharge to a selected discharge region (ending near point 224) over the life of the electrode 220.
While the particular embodiment(s) described and illustrated in this patent application in the detail required to satisfy 35 U.S.C. §112 are fully capable of attaining one or more of the above-described purposes for, problems to be solved by, or any other reasons for or objects of the embodiment(s) above described, it is to be understood by those skilled in the art that the above-described embodiment(s) are merely exemplary, illustrative and representative of the subject matter which is broadly contemplated by the present application. Reference to an element in the following Claims in the singular is not intended to mean nor shall it mean in interpreting such Claim element "one and only one" unless explicitly so stated, but rather "one or more". All structural and functional equivalents to any of the elements of the above-described embodiment(s) that are known or later come to be known to those of ordinary skill in the art are expressly incorporated herein by reference and are intended to be encompassed by the present Claims. Any term used in the Specification and/or in the Claims and expressly given a meaning in the

Claims

Specification and/or Claims in the present Application shall have that meaning, regardless of any dictionary or other commonly used meaning for such a term. It is not intended or necessary for a device or method discussed in the Specification as an embodiment to address or solve each and every problem discussed in this Application, for it to be encompassed by the present Claims. No element, component, or method step in the present disclosure is intended to be dedicated to the public regardless of whether the element, component, or method step is explicitly recited in the Claims. No claim element in the appended Claims is to be construed under the provisions of 35 U.S. C. §112, sixth paragraph, unless the element is expressly recited using the phrase "means for" or, in the case of a method claim, the element is recited as a "step" instead of an "act".2006-0089-02 19 CLAIMSWhat is claimed is:
1. A device comprising: a housing; a first electrode disposed in the housing; a second electrode disposed in the housing and spaced from the first electrode to establish a discharge gap therebetween; a mechanism moving said second electrode relative to said first electrode to vary said gap; a conductive, flexible member having a first edge attached to the second electrode for movement therewith and a second edge held fixed relative to the housing.
2. A device as recited in claim 1 wherein said flexible member forms a shield protecting said mechanism from electromagnetic fields generated in the discharge gap.
3. A device as recited in claim 1 wherein the flexible member is formed with a plurality of convolutions between the first edge and the second edge.
4. A device as recited in claim 1 wherein the mechanism comprises a first rigid member attached to the second electrode, the first rigid member having a surface modulated with a sawtooth structure and a second rigid member having a surface modulated with a sawtooth structure.
5. A device as recited in claim 1 wherein the housing comprises a housing wall, the mechanism comprises a linkage passing through the wall and an actuator moving the linkage in response to an electrical control signal.
2006-0089-02 20
6. A device as recited in claim 5 wherein the actuator is selected from the group of actuators consisting of a piezoelectric actuator, an electrostrictive actuator, a magnetostrictive actuator, a stepper motor, a servo motor, a voice coil actuator, a linear motor and a combination thereof.
7. A device as recited in claim 1 further comprising an electrode support bar attached to said housing, said second electrode moveable relative to said support bar, the mechanism providing a heat conduction path from the second electrode to the support bar.
8. A device as recited in claim 1 further comprising a controller monitoring a device parameter and generating a control signal indicative thereof, and wherein said mechanism comprises an actuator responsive to said control signal to move the second electrode relative to the first electrode.
9. A device as recited in claim 8 wherein said device is a pulsed laser and the device parameter comprises an accumulated pulse count.
10. A device as recited in claim 1 wherein the housing comprises a housing wall formed with an opening and the mechanism comprises a linkage extending through the opening.
11. A device as recited in claim 1 further comprising a flow guide and elastic element, the flow guide disposed adjacent to said second electrode and moveable relative thereto with the elastic element operable to bias the flow guide toward the second electrode.
12. A device comprising: a housing comprising a housing wall, the housing wall formed with an opening; a first electrode disposed in the housing;
2006-0089-02 21 a second electrode disposed in the housing and spaced from the first electrode to establish a discharge gap therebetween; a controller monitoring a device parameter and generating a control signal indicative thereof; a linkage extending through the opening in the housing wall; and an actuator operably coupled with the linkage and responsive to said control signal to move the second electrode relative to the first electrode.
13. A device as recited in claim 12 wherein said device is a pulsed laser and the device parameter comprises an accumulated pulse count.
14. A device as recited in claim 12 wherein said device is a pulsed laser generating an output beam and the device parameter comprises an output beam bandwidth measurement.
15. A device as recited in claim 12 wherein said device is a pulsed laser generating an output beam and the device parameter comprises an output beam pulse energy measurement.
16. A device as recited in claim 12 wherein said device is a pulsed laser generating an output beam and the device parameter comprises an output beam pulse to pulse energy stability measurement.
17. A device as recited in claim 12 wherein said device is a pulsed laser generating an output beam and the device parameter comprises a measured relationship between discharge voltage and pulse energy.
18. A device as recited in claim 12 wherein said device is a pulsed laser generating an output beam and the device parameter comprises a beam size measurement.
2006-0089-02 22
19. A laser device comprising: a first electrode; a second electrode spaced from the first electrode; a gain medium; a power supply generating a discharge between the first and second electrode; and a motorized electrode height adjusting mechanism to accommodate erosion, the mechanism adjusting height on a real time basis to tune the laser.
20. A laser device as recited in claim 19 wherein said mechanism comprises a piezoelectric driver.
21. A laser device as recited in claim 19 wherein the laser device comprises a mechanism selected from the group of mechanisms consisting of a cam, rack and pinion, incline plane and lever arm.
2006-0089-02 23
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015140930A1 (en) * 2014-03-18 2015-09-24 ギガフォトン株式会社 Gas laser device and control method therefor

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7856044B2 (en) * 1999-05-10 2010-12-21 Cymer, Inc. Extendable electrode for gas discharge laser
TWI455239B (en) * 2008-03-14 2014-10-01 Lam Res Corp Cam lock electrode clamp
US8014432B2 (en) * 2009-03-27 2011-09-06 Cymer, Inc. Regenerative ring resonator
USRE45957E1 (en) * 2009-03-27 2016-03-29 Cymer, Llc Regenerative ring resonator
CN102761047B (en) * 2012-07-30 2013-09-25 中国科学院光电研究院 Electrode mechanism of discharge cavity of gas laser
WO2014046186A1 (en) * 2012-09-21 2014-03-27 ギガフォトン株式会社 Laser device
JP6383729B2 (en) * 2013-10-02 2018-08-29 ギガフォトン株式会社 Laser equipment
TWI490254B (en) 2013-12-31 2015-07-01 Ind Tech Res Inst Inorganic passivation coating material, method for forming the same, and inorganic passivation protective film produced therefrom
WO2016143105A1 (en) * 2015-03-11 2016-09-15 ギガフォトン株式会社 Excimer laser chamber device
US10074953B2 (en) 2015-09-30 2018-09-11 Cymer, Llc Erosion resistant electrodes for use in generating gas discharge laser
KR102593750B1 (en) * 2017-10-24 2023-10-24 사이머 엘엘씨 Method of and apparatus for extending electrode life in a laser chamber
WO2019143433A1 (en) * 2018-01-17 2019-07-25 Cymer, Llc Apparatus for tuning discharge performance in a laser chamber
CN109411996A (en) * 2018-11-29 2019-03-01 北京科益虹源光电技术有限公司 A kind of excimer laser electrode structure and excimer laser
KR102669702B1 (en) * 2019-10-11 2024-05-24 사이머 엘엘씨 Conductive member for discharge laser
KR102668769B1 (en) * 2021-08-18 2024-06-24 주식회사 아밀이엔지 Method of using electrohydraulic drug-jetting device

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3736453A (en) * 1971-01-22 1973-05-29 California Inst Of Techn Arc control in compact arc lamps
US4156828A (en) * 1977-03-18 1979-05-29 Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. Glow discharge apparatus and a method of operating same
US4240044A (en) * 1979-07-16 1980-12-16 Gte Products Corporation Pulsed laser electrode assembly
US4683364A (en) * 1984-04-18 1987-07-28 Micro Surface Technology, Inc. Electrical discharge shape forming and surface conditioning device
US5847351A (en) * 1996-03-04 1998-12-08 Denso Corporation Electrode feeding apparatus for electric-discharge machining
US20050083984A1 (en) * 2003-10-17 2005-04-21 Igor Bragin Laser system sealing
US7068697B1 (en) * 2005-09-28 2006-06-27 Cymer, Inc. Adjustable flow guide to accommodate electrode erosion in a gas discharge laser

Family Cites Families (126)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3631319A (en) * 1969-10-10 1971-12-28 Laser Systems Corp Triggered spark gap device
SU743092A1 (en) 1977-04-25 1980-06-25 Предприятие П/Я Г-4345 Gas flow-through laser
US4223279A (en) 1977-07-18 1980-09-16 Mathematical Sciences Northwest, Inc. Pulsed electric discharge laser utilizing water dielectric blumlein transmission line
JPS54154988A (en) 1978-05-29 1979-12-06 Mitsubishi Electric Corp Silent discharge type gas laser device
US4251781A (en) 1979-01-22 1981-02-17 Hughes Aircraft Company Electric discharge-excited flowing gas laser with discharge confinement shield
US4245194A (en) 1979-07-16 1981-01-13 Gte Products Corporation Compact pulsed gas transport laser
DE2952046C2 (en) 1979-12-22 1982-04-15 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5300 Bonn Method and device for generating an electrical discharge in a gas flowing at supersonic speed
JPS57192091A (en) * 1981-05-20 1982-11-26 Fujitsu Ltd Gas laser tube
CA1187971A (en) * 1982-04-13 1985-05-28 Her Majesty The Queen, In Right Of Canada, As Represented By The Minister Of National Defence Preionizing arrangement for transversely excited lasers
US4455658A (en) 1982-04-20 1984-06-19 Sutter Jr Leroy V Coupling circuit for use with a transversely excited gas laser
IT1148956B (en) 1982-06-15 1986-12-03 Selenia Industire Elettroniche PULSING GAS LASERS IN SEALED STRUCTURE
US4481634A (en) 1983-04-28 1984-11-06 The Regents Of The University Of California RF Excited metal waveguide laser
US4774714A (en) 1983-05-19 1988-09-27 Laser Science, Inc. Laser system with interchangeable modules and method for interchanging such modules
JPS607296A (en) 1983-06-24 1985-01-16 Furuno Electric Co Ltd Ultrasonic wave transceiver for underwater searching
US4573496A (en) 1984-04-18 1986-03-04 General Motors Corporation Hydraulic power steering gear and rotary valve therefor
US4686682A (en) 1984-10-09 1987-08-11 Mitsubishi Denki Kabushiki Kaisha Discharge excitation type short pulse laser device
NO853264L (en) 1984-10-15 1986-04-16 Siemens Ag TRANSVERSAL EXCITED GAS WELDING AND PROCEDURE FOR ITS OPERATION.
JPS61128583A (en) * 1984-11-28 1986-06-16 Toshiba Corp Gas laser device
US4876693A (en) 1984-12-26 1989-10-24 Hughes Aircraft Company Integrated laser head and low inductance pulse forming circuit for pulsed gas lasers
US4742527A (en) 1985-05-17 1988-05-03 Cooper Lasersonics Laser having brazed anode
US4723255A (en) 1985-05-20 1988-02-02 Northrop Corporation Extended lifetime railgap switch
US4686364A (en) * 1985-07-19 1987-08-11 Schlumberger Technology Corporation In situ determination of total carbon and evaluation of source rock therefrom
US5315611A (en) 1986-09-25 1994-05-24 The United States Of America As Represented By The United States Department Of Energy High average power magnetic modulator for metal vapor lasers
US5189678A (en) 1986-09-29 1993-02-23 The United States Of America As Represented By The United States Department Of Energy Coupling apparatus for a metal vapor laser
JPS63229789A (en) * 1987-03-19 1988-09-26 Toshiba Corp Highly repetitive pulsed laser oscillator
US4860300A (en) 1987-06-03 1989-08-22 Lambda Physik Forschungs- Und Entwicklungsgesellschaft Mb Electrode for pulsed gas lasers
US4833686A (en) 1987-06-29 1989-05-23 Hughes Aircraft Company Electrodes for transversely excited gas lasers
US4751713A (en) 1987-07-31 1988-06-14 Hughes Aircraft Company Gas laser having a piezoelectric fan
US4959840A (en) 1988-01-15 1990-09-25 Cymer Laser Technologies Compact excimer laser including an electrode mounted in insulating relationship to wall of the laser
US5048041A (en) 1988-01-15 1991-09-10 Cymer Laser Technologies Compact excimer laser
US5023884A (en) 1988-01-15 1991-06-11 Cymer Laser Technologies Compact excimer laser
US5025446A (en) 1988-04-01 1991-06-18 Laserscope Intra-cavity beam relay for optical harmonic generation
IT1231783B (en) 1989-05-12 1992-01-14 Enea LASER HEAD FOR TRANSVERSE DISCHARGE EXCITATION WITH THREE ELECTRODES
GB2233814B (en) * 1989-07-10 1994-06-22 Toshiba Kk Laser apparatus
US4953174A (en) 1989-10-23 1990-08-28 Hughes Aircraft Company Preionization electrode for pulsed gas laser
US5025445A (en) 1989-11-22 1991-06-18 Cymer Laser Technologies System for, and method of, regulating the wavelength of a light beam
DD291424A5 (en) 1989-12-29 1991-06-27 Adw Zi Fuer Optik Und Spektroskopie,De ARRANGEMENT FOR GENERATING A HOMOGENEOUS LASER BEAM PROFILE
JPH04218985A (en) 1990-07-06 1992-08-10 Mitsubishi Electric Corp Excimer laser device
US5471965A (en) 1990-12-24 1995-12-05 Kapich; Davorin D. Very high speed radial inflow hydraulic turbine
DE4113241C2 (en) 1991-04-23 1994-08-11 Lambda Physik Forschung Pulsed gas discharge laser
JPH0629592A (en) * 1991-06-10 1994-02-04 Komatsu Ltd Discharge-pumped laser
JPH0567828A (en) * 1991-09-05 1993-03-19 Nec Corp Ultraviolet pulsed gas laser with pre-discharge electrode
JPH05200450A (en) * 1992-01-22 1993-08-10 Hidaka Seiki Kk Die unit
US5557629A (en) 1992-08-28 1996-09-17 Kabushiki Kaisha Komatsu Seisakusho Laser device having an electrode with auxiliary conductor members
US5359620A (en) 1992-11-12 1994-10-25 Cymer Laser Technologies Apparatus for, and method of, maintaining a clean window in a laser
US5313481A (en) 1993-09-29 1994-05-17 The United States Of America As Represented By The United States Department Of Energy Copper laser modulator driving assembly including a magnetic compression laser
DE4335079C1 (en) 1993-10-14 1995-01-19 Lambda Physik Gmbh Electrodes in a fluorine-containing discharge unit of a pulsed gas discharge laser
JPH07142795A (en) * 1993-11-17 1995-06-02 Okuma Mach Works Ltd Laser oscillator
DE4401892C2 (en) 1994-01-24 1999-06-02 Lambda Physik Forschung Electrode for a gas discharge laser and method for forming an electrode for a gas discharge laser
US5448580A (en) 1994-07-05 1995-09-05 The United States Of America As Represented By The United States Department Of Energy Air and water cooled modulator
DE4426723A1 (en) 1994-07-22 1996-01-25 Atl Lasertechnik & Accessoires Sliding discharge preionization for gas lasers
US6109574A (en) 1996-01-05 2000-08-29 Cymer, Inc. Gas laser chamber/optics support structure
US5863017A (en) 1996-01-05 1999-01-26 Cymer, Inc. Stabilized laser platform and module interface
US5646954A (en) 1996-02-12 1997-07-08 Cymer, Inc. Maintenance strategy control system and monitoring method for gas discharge lasers
JP3874123B2 (en) 1996-03-07 2007-01-31 キヤノン株式会社 Discharge electrode, excimer laser oscillation device and stepper
US5828687A (en) * 1996-12-24 1998-10-27 Alimenterics Inc. Variable dimension optical chamber and laser incorporating the same
US5771258A (en) 1997-02-11 1998-06-23 Cymer, Inc. Aerodynamic chamber design for high pulse repetition rate excimer lasers
US6128323A (en) 1997-04-23 2000-10-03 Cymer, Inc. Reliable modular production quality narrow-band high REP rate excimer laser
US5982800A (en) 1997-04-23 1999-11-09 Cymer, Inc. Narrow band excimer laser
US6064072A (en) 1997-05-12 2000-05-16 Cymer, Inc. Plasma focus high energy photon source
US6541786B1 (en) 1997-05-12 2003-04-01 Cymer, Inc. Plasma pinch high energy with debris collector
US5763930A (en) 1997-05-12 1998-06-09 Cymer, Inc. Plasma focus high energy photon source
US6452199B1 (en) 1997-05-12 2002-09-17 Cymer, Inc. Plasma focus high energy photon source with blast shield
US6192064B1 (en) 1997-07-01 2001-02-20 Cymer, Inc. Narrow band laser with fine wavelength control
US6094448A (en) 1997-07-01 2000-07-25 Cymer, Inc. Grating assembly with bi-directional bandwidth control
US6018537A (en) 1997-07-18 2000-01-25 Cymer, Inc. Reliable, modular, production quality narrow-band high rep rate F2 laser
US5852621A (en) 1997-07-21 1998-12-22 Cymer, Inc. Pulse laser with pulse energy trimmer
US6317447B1 (en) 2000-01-25 2001-11-13 Cymer, Inc. Electric discharge laser with acoustic chirp correction
US5953360A (en) 1997-10-24 1999-09-14 Synrad, Inc. All metal electrode sealed gas laser
US5940421A (en) 1997-12-15 1999-08-17 Cymer, Inc. Current reversal prevention circuit for a pulsed gas discharge laser
US6240117B1 (en) 1998-01-30 2001-05-29 Cymer, Inc. Fluorine control system with fluorine monitor
US6151349A (en) 1998-03-04 2000-11-21 Cymer, Inc. Automatic fluorine control system
US5978406A (en) 1998-01-30 1999-11-02 Cymer, Inc. Fluorine control system for excimer lasers
US6016325A (en) 1998-04-27 2000-01-18 Cymer, Inc. Magnetic modulator voltage and temperature timing compensation circuit
US6618421B2 (en) 1998-07-18 2003-09-09 Cymer, Inc. High repetition rate gas discharge laser with precise pulse timing control
US6477193B2 (en) 1998-07-18 2002-11-05 Cymer, Inc. Extreme repetition rate gas discharge laser with improved blower motor
US6208675B1 (en) 1998-08-27 2001-03-27 Cymer, Inc. Blower assembly for a pulsed laser system incorporating ceramic bearings
US6067311A (en) 1998-09-04 2000-05-23 Cymer, Inc. Excimer laser with pulse multiplier
US6567450B2 (en) 1999-12-10 2003-05-20 Cymer, Inc. Very narrow band, two chamber, high rep rate gas discharge laser system
US6493374B1 (en) 1999-09-03 2002-12-10 Cymer, Inc. Smart laser with fast deformable grating
US6208674B1 (en) 1998-09-18 2001-03-27 Cymer, Inc. Laser chamber with fully integrated electrode feedthrough main insulator
US6212211B1 (en) 1998-10-09 2001-04-03 Cymer, Inc. Shock wave dissipating laser chamber
US6597711B2 (en) * 1998-12-04 2003-07-22 Cidra Corporation Bragg grating-based laser
US6219368B1 (en) 1999-02-12 2001-04-17 Lambda Physik Gmbh Beam delivery system for molecular fluorine (F2) laser
US6782031B1 (en) 1999-03-19 2004-08-24 Cymer, Inc. Long-pulse pulse power system for gas discharge laser
US6104735A (en) 1999-04-13 2000-08-15 Cymer, Inc. Gas discharge laser with magnetic bearings and magnetic reluctance centering for fan drive assembly
US6164116A (en) 1999-05-06 2000-12-26 Cymer, Inc. Gas module valve automated test fixture
US6556612B2 (en) 1999-05-10 2003-04-29 Cymer, Inc. Line narrowed laser with spatial filter
US6625191B2 (en) 1999-12-10 2003-09-23 Cymer, Inc. Very narrow band, two chamber, high rep rate gas discharge laser system
US7856044B2 (en) * 1999-05-10 2010-12-21 Cymer, Inc. Extendable electrode for gas discharge laser
US6549551B2 (en) 1999-09-27 2003-04-15 Cymer, Inc. Injection seeded laser with precise timing control
US6414979B2 (en) 2000-06-09 2002-07-02 Cymer, Inc. Gas discharge laser with blade-dielectric electrode
US6034978A (en) 1999-05-12 2000-03-07 Cymer, Inc. Gas discharge laser with gas temperature control
US6466602B1 (en) 2000-06-09 2002-10-15 Cymer, Inc. Gas discharge laser long life electrodes
US6972421B2 (en) 2000-06-09 2005-12-06 Cymer, Inc. Extreme ultraviolet light source
US6693939B2 (en) 2001-01-29 2004-02-17 Cymer, Inc. Laser lithography light source with beam delivery
US6576912B2 (en) 2001-01-03 2003-06-10 Hugo M. Visser Lithographic projection apparatus equipped with extreme ultraviolet window serving simultaneously as vacuum window
US7928416B2 (en) 2006-12-22 2011-04-19 Cymer, Inc. Laser produced plasma EUV light source
US7415056B2 (en) 2006-03-31 2008-08-19 Cymer, Inc. Confocal pulse stretcher
US7439530B2 (en) 2005-06-29 2008-10-21 Cymer, Inc. LPP EUV light source drive laser system
US7378673B2 (en) 2005-02-25 2008-05-27 Cymer, Inc. Source material dispenser for EUV light source
US7476886B2 (en) 2006-08-25 2009-01-13 Cymer, Inc. Source material collection unit for a laser produced plasma EUV light source
US7405416B2 (en) 2005-02-25 2008-07-29 Cymer, Inc. Method and apparatus for EUV plasma source target delivery
US7491954B2 (en) 2006-10-13 2009-02-17 Cymer, Inc. Drive laser delivery systems for EUV light source
US7598509B2 (en) 2004-11-01 2009-10-06 Cymer, Inc. Laser produced plasma EUV light source
US20050259709A1 (en) 2002-05-07 2005-11-24 Cymer, Inc. Systems and methods for implementing an interaction between a laser shaped as a line beam and a film deposited on a substrate
US20060255298A1 (en) 2005-02-25 2006-11-16 Cymer, Inc. Laser produced plasma EUV light source with pre-pulse
US7843632B2 (en) 2006-08-16 2010-11-30 Cymer, Inc. EUV optics
US7518787B2 (en) 2006-06-14 2009-04-14 Cymer, Inc. Drive laser for EUV light source
US7465946B2 (en) 2004-03-10 2008-12-16 Cymer, Inc. Alternative fuels for EUV light source
US6928093B2 (en) 2002-05-07 2005-08-09 Cymer, Inc. Long delay and high TIS pulse stretcher
US7372056B2 (en) 2005-06-29 2008-05-13 Cymer, Inc. LPP EUV plasma source material target delivery system
US6635844B2 (en) 2002-01-03 2003-10-21 United Microelectronics Corp. Apparatus for on-line cleaning a wafer chuck with laser
KR100589236B1 (en) 2002-08-15 2006-06-14 에이에스엠엘 네델란즈 비.브이. Lithographic projection apparatus and reflector assembly for use in said apparatus
US7002168B2 (en) 2002-10-15 2006-02-21 Cymer, Inc. Dense plasma focus radiation source
US6919573B2 (en) 2003-03-20 2005-07-19 Asml Holding N.V Method and apparatus for recycling gases used in a lithography tool
US7217941B2 (en) 2003-04-08 2007-05-15 Cymer, Inc. Systems and methods for deflecting plasma-generated ions to prevent the ions from reaching an internal component of an EUV light source
US7217940B2 (en) 2003-04-08 2007-05-15 Cymer, Inc. Collector for EUV light source
US7230258B2 (en) 2003-07-24 2007-06-12 Intel Corporation Plasma-based debris mitigation for extreme ultraviolet (EUV) light source
US7196342B2 (en) 2004-03-10 2007-03-27 Cymer, Inc. Systems and methods for reducing the influence of plasma-generated debris on the internal components of an EUV light source
US7087914B2 (en) 2004-03-17 2006-08-08 Cymer, Inc High repetition rate laser produced plasma EUV light source
TWM272608U (en) * 2005-02-04 2005-08-11 Hon Hai Prec Ind Co Ltd System for adjusting space distance between electrodes and arc discharge device using the same
US7868304B2 (en) 2005-02-07 2011-01-11 Asml Netherlands B.V. Method for removal of deposition on an optical element, lithographic apparatus, device manufacturing method, and device manufactured thereby
US7365349B2 (en) 2005-06-27 2008-04-29 Cymer, Inc. EUV light source collector lifetime improvements
US7394083B2 (en) 2005-07-08 2008-07-01 Cymer, Inc. Systems and methods for EUV light source metrology
US7411686B2 (en) 2006-06-14 2008-08-12 Cymer, Inc. Methods and apparatus for aligning an etalon with a photodiode array

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3736453A (en) * 1971-01-22 1973-05-29 California Inst Of Techn Arc control in compact arc lamps
US4156828A (en) * 1977-03-18 1979-05-29 Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. Glow discharge apparatus and a method of operating same
US4240044A (en) * 1979-07-16 1980-12-16 Gte Products Corporation Pulsed laser electrode assembly
US4683364A (en) * 1984-04-18 1987-07-28 Micro Surface Technology, Inc. Electrical discharge shape forming and surface conditioning device
US5847351A (en) * 1996-03-04 1998-12-08 Denso Corporation Electrode feeding apparatus for electric-discharge machining
US20050083984A1 (en) * 2003-10-17 2005-04-21 Igor Bragin Laser system sealing
US7068697B1 (en) * 2005-09-28 2006-06-27 Cymer, Inc. Adjustable flow guide to accommodate electrode erosion in a gas discharge laser

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015140930A1 (en) * 2014-03-18 2015-09-24 ギガフォトン株式会社 Gas laser device and control method therefor
US9853410B2 (en) 2014-03-18 2017-12-26 Gigaphoton Inc. Gas laser device and control method therefor

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