WO2009017586A1 - Thermal distortion compensation for laser mirrors - Google Patents
Thermal distortion compensation for laser mirrors Download PDFInfo
- Publication number
- WO2009017586A1 WO2009017586A1 PCT/US2008/008446 US2008008446W WO2009017586A1 WO 2009017586 A1 WO2009017586 A1 WO 2009017586A1 US 2008008446 W US2008008446 W US 2008008446W WO 2009017586 A1 WO2009017586 A1 WO 2009017586A1
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- WIPO (PCT)
- Prior art keywords
- mirror
- mirror element
- assembly
- recited
- flange
- Prior art date
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- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 23
- 229910052802 copper Inorganic materials 0.000 claims abstract description 23
- 239000010949 copper Substances 0.000 claims abstract description 23
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 18
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 18
- 229910001220 stainless steel Inorganic materials 0.000 claims abstract description 15
- 239000010935 stainless steel Substances 0.000 claims abstract description 15
- 229910052751 metal Inorganic materials 0.000 claims description 11
- 239000002184 metal Substances 0.000 claims description 11
- 239000007769 metal material Substances 0.000 claims description 10
- 230000003993 interaction Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 28
- 238000010438 heat treatment Methods 0.000 abstract description 10
- 239000000463 material Substances 0.000 description 18
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 16
- 238000013459 approach Methods 0.000 description 10
- 238000013461 design Methods 0.000 description 10
- 229910002092 carbon dioxide Inorganic materials 0.000 description 9
- 230000008859 change Effects 0.000 description 6
- 230000008878 coupling Effects 0.000 description 5
- 238000010168 coupling process Methods 0.000 description 5
- 238000005859 coupling reaction Methods 0.000 description 5
- 230000006872 improvement Effects 0.000 description 5
- 230000003287 optical effect Effects 0.000 description 5
- 238000000576 coating method Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000004458 analytical method Methods 0.000 description 3
- 239000002826 coolant Substances 0.000 description 3
- 230000005855 radiation Effects 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 239000001569 carbon dioxide Substances 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000008030 elimination Effects 0.000 description 2
- 238000003379 elimination reaction Methods 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- SBIBMFFZSBJNJF-UHFFFAOYSA-N selenium;zinc Chemical compound [Se]=[Zn] SBIBMFFZSBJNJF-UHFFFAOYSA-N 0.000 description 2
- 230000003044 adaptive effect Effects 0.000 description 1
- 238000010420 art technique Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 230000001010 compromised effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000001351 cycling effect Effects 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 239000012780 transparent material Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES 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
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/02—Constructional details
- H01S3/03—Constructional details of gas laser discharge tubes
- H01S3/034—Optical devices within, or forming part of, the tube, e.g. windows, mirrors
- H01S3/0346—Protection of windows or mirrors against deleterious effects
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
- G02B7/18—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
- G02B7/181—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors with means for compensating for changes in temperature or for controlling the temperature; thermal stabilisation
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES 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
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/02—Constructional details
- H01S3/04—Arrangements for thermal management
- H01S3/0401—Arrangements for thermal management of optical elements being part of laser resonator, e.g. windows, mirrors, lenses
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES 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
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/05—Construction or shape of optical resonators; Accommodation of active medium therein; Shape of active medium
- H01S3/08—Construction or shape of optical resonators or components thereof
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
- G02B7/18—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
- G02B7/182—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
Definitions
- This invention relates to high power carbon dioxide slab lasers. More specifically, the invention relates to a design of a mirror system which reduces thermal distortion and improves pointing stability.
- the subject invention relates to high power diffusion cooled carbon dioxide slab lasers.
- An example of such a laser can be found in commonly owned U.S. Patent No. 5,140,606 incorporated herein by reference.
- These lasers include a pair of rectangular metal electrodes mounted within a sealed housing containing the laser gas. The electrodes are spaced closely together to define a slab shaped discharge region. RF power is used to excite the gas to generate laser light.
- the positive branch unstable resonator designs are about an order of magnitude more difficult to align than the negative branch designs but the designs are much less sensitive to output beam pointing variations as a function of changes in the curvature of the resonators mirrors with temperature changes.
- the negative branch resonators are easier to align but their beam pointing variations are much more sensitive to mirror curvature changes with temperature.
- the variation in the mirror curvature with temperature causes the pointing of the output laser beam to vary.
- the large changes in the lasers beam pointing stability with changes in mirror curvature with temperature needs to be solved. This is especially true as the discharge length becomes shorter and the width increases.
- the output coupling mirror and the return mirror have concave surfaces
- the mirrors normally extend over the entire width of the parallel facing electrodes that are separated by a small gap in the vertical dimension except at the output coupling side Direct thermal heating of the mirror's reflecting surface by the laser beam occurs because the high reflecting thin films deposited on the mirror's surface have a very small but finite absorption which heats the surface of the mirror The heat from this reflecting surface propagates through the thickness of the mirror, thereby, establishing a temperature gradient between the front and back surfaces of the mirror
- the back of the mirror Since the back of the mirror is normally attached to a massive mechanical housing holding the mirror, the back of the mirror is usually cooler then the front surface, thus maintaining a temperature gradient between the front and back surfaces
- This temperature gradient increases with laser power and causes a distortion or warping of the mirror's surface thereby disturbing the optical resonator's geometry resulting in undesirable changes in the laser' s output beam performance such as in beam profile shapes and in pointing variations
- the warping causes the concave mirror surface (the side towards the laser discharge) to become more convex Changes in output beam parameters in response to changes in operating conditions of the laser, such as RF power input to the discharge, pulse repetition frequency, duty cycle, etc , cause changes m the mirror thermal gradient and such changes are not desirable in industrial laser systems
- the elimination or reduction of these laser mirror thermal distortion effects is highly desirable and is the focus of this disclosure It is important to note that this invention has broader applications then to only reducing the pointing variations of an unstable laser resonator output beam For example, it can have relevance to reducing
- a temperature gradient across the thickness of the mirror causes bending of the mirrors. Since the back of the mirror is cooler than the reflecting surface of the mirror, the mirror becomes less concave due to the fact that the front surface expands more the back surface. We have found that a few degrees temperature gradient can make the laser's output beam deflect by an unacceptable amount.
- the bimetallic effect between the mirror material (usually copper) and the large mirror holder pate-form (usually made of aluminum) also changes the radius of curvature due to bending caused by the two materials having different thermal coefficient of expansion. It is important to note that the thermal coefficient of expansion of aluminum is larger than for copper. In this case, the bimetallic effect causes the concave mirror to become more concave.
- U.S. Patent No. 5,020,895 describes using an adaptive optics technique to compensate for the thermal deformation of the mirrors.
- This approach involved the use of active electronic feedback circuitry coupled with a sensor and an actuator, such as a piezoelectric or a regulative liquid or gas pressure chamber, to provide a force to counteract the radius of curvature arising from the thermal effects on the mirror.
- This approach adds undesirable complexity and cost of the laser.
- Another prior art technique was to use active electronic feedback circuitry coupled with a temperature sensor and a heating element to heat the back of the resonator's mirror to establish an appropriate temperature distribution to counteract the change in the radius of curvature (see U.S. Patent No.
- U.S. Patent No. 4,287,421 discloses a transparent mirror material having reflective coatings pre-selected to allow a small amount of laser radiation to propagate through the coatings and the mirror material, to be in turn, absorbed by a coating on the back side of the mirror.
- the reflection and absorption parameters are selected so that radiation A- absorbed by the absorbing coating is sufficient to heat up the back side of the mirror to compensate for the temperature gradient between the front and back of the mirror.
- the limitation of this approach is the requirement for a transparent material for the mirror. Consequently, it is not useful with copper mirrors which we believe are more resistive to damage than either Si or ZnSe mirrors.
- the end header assemblies of the laser housing are defined by a flange upon which is mounted a mirror support.
- An elongated mirror element is mounted to the support.
- the mirror element is formed from metal and includes a curved portion on the front surface thereof defining one of the reflecting surfaces of the resonator.
- the front surface further includes at least one and preferably two planar regions extending parallel to the curved portion of the mirror. These planar regions can be stepped down from the curved portion.
- metal strips are mounted onto the planar portions of the mirror element. These strips are formed from a material that has a lower coefficient of thermal expansion than the metal material of the mirror element.
- the mirror element is made of copper and the strips are made of stainless steel.
- the mirror and strips will exhibit the bimetallic effect.
- the bimetallic effect tends to cause the concave mirror to become more concave.
- the differential heating tends to causes the mirror to become less concave.
- one or more metal strips are mounted on the back of the mirror element.
- the coefficient of thermal expansion of the strips are selected to be greater than the coefficient of thermal expansion of the mirror element to counter the effects of the thermal gradient induced by heating the front surface of the mirror.
- Figure 1 is a perspective view of a header and mirror mount and mirror of the prior art showing the side facing the laser discharge.
- Figure 2 a perspective view of the prior art header showing the side outside the laser chamber.
- Figure 3A is an exploded perspective view of a header and mirror assembly formed in accordance with the subject invention.
- Figure 3B is an assembled perspective view of the header of Figure 3 A.
- Figure 4A is an exploded perspective view of a header and mirror assembly formed in accordance with the subject invention to be used on the output coupler side of the discharge.
- Figure 4B is an assembled perspective view of the header of Figure 4A.
- Figure 5 is a graph illustrating the improvement in pointing stability based on use of the subject invention in a test laser.
- Figure 6A is an exploded perspective view of a header and mirror assembly formed in accordance with a second embodiment of the subject invention.
- Figure 6B is an assembled perspective view of the header of Figure 6A.
- Figures 1 and 2 illustrate the header assembly 10 we have used in our experimental lasers for mounting a curved mirror forming a part of a negative branch unstable resonator of a CO 2 slab laser.
- the header assembly includes an aluminum flange 12 which is bolted onto the main housing to hermetically seals the laser tube housing chamber containing the electrodes, the CO2 gas mixture of CO2:N2.H e :Xe, and the resonators mirrors.
- An O-ring 14 provides the hermetical seal.
- a copper mirror 16 is mounted onto an aluminum mirror base 18 which in turn is connected to raised inside surface 20 of the aluminum flange.
- the mirror 16 includes an elongated, highly polished concave region 22 which defines the reflecting surface of the mirror
- a pair of planar surfaces 26 are located on either side of the curved surface.
- the planar surfaces are stepped down from the curved surface so that the mirror has essentially a T-shape in cross-section.
- the mounting of the copper mirror to the large aluminum base leads to a large bimetallic effect because of the large difference in thermal expansion coefficients of the materials. This bimetallic effect causes a large change in the curvature of the mirror that results in variations in the pointing direction of the laser beam with temperature.
- the raised surface 20 of the flange has a two axis angular position adjustable post
- This tiltable post 28 includes recessed front surfaces which maintain a hermetical seal by being an integral part of the end flange assembly by means of a thin web left during the machining process that connects the end of the adjustable post with the aluminum flange material (see U.S Patent No. 5,140,606 cited above).
- the four screws 32 illustrated in Figure 2 are used to adjust the o ⁇ entation of the mirror in two angular axis to align the laser's resonator cavity.
- This mirror assembly structure shown in Figures 1 and 2 was used to form a negative branch hybrid unstable waveguide resonator for a 400 to 500W CCh slab laser.
- the width of the electrodes were 3.780 inches.
- the radius of curvatures for the mirrors were approximately 0.6m. (Further details of this test laser can be found in U.S Provisional Application Serial No. 60/962,555, filed July 30, 2007 incorporated herein by reference.)
- This prior art mirror assembly structure provided a laser output beam pointing variation of 400 to 800 microradians after the laser was turned on.
- This beam pointing variation is not acceptable in most laser mate ⁇ al process working applications. It was determined by both analytical and experimental investigations that the pointing variation caused by changes in the cavity's length with temperature was approximately 30 microradians per degree C. This laser beam deflection caused by changes in the cavity's length with temperature was minor in comparison with the three thermal effects causing changes in the mirror's radius of curvature mentioned earlier; namely, temperature gradient between the mirrors front and back surfaces; the thermal expansion of the copper changing the mirror's curvature and the bimetallic effect with temperature changes between aluminum and copper.
- the largest contribution to the beam pointing variations with temperature was due to the bimetallic effect between the large aluminum base plate and the copper mirror mounted on the base plate.
- the laser beam deflection due to the bimetallic effects between copper and aluminum in the assembly shown in Figure 1 was found to be approximately 220 microradians per degree C.
- the bimetallic effect can be made to compensate for the changes in beam deflection caused by the changes in mirror radius of curvature by the changes in thermal gradient of the mirrors and by the thermal expansion between the copper and the aluminum.
- Figures 3A and 3B illustrate a preferred approach for reducing variations in pointing due to heating of the mirrors. As discussed below, there were two significant changes made to the design of Figures 1 and 2. First, the large aluminum base 18 was eliminated. Second, a pair of stainless steel strips 40 are attached to the planar surfaces 26 of the mirror 16. The stainless steel strips function to limit the warping of the mirror due to differential heating.
- the strips 40 were formed 17-4PH stainless steel.
- Each of the stainless steel strips is attached to the copper T-shaped mirror by retaining screws 44 and held in place by hex nuts 46.
- the T-shaped mirror and stainless steel strips assembly is attached to the raised surface 20 by two mounting screws (not show).
- a dowel pin 48 is used to align the mirror with the two threaded mounting holes.
- the raised surface 20 is connected to the two axis, angular adjustable post as seen in Figure 2.
- the post is used to adjust the mirror external to the hermetically sealed laser tube housing chamber.
- the thickness and length of the stainless steel strips are selected based on the dimensions of the T-shaped copper mirror and originally adjusted by analyses and experimentation until the desired amount of thermal compensation is obtained over a desired temperature range.
- Stainless steel strips have been discussed in this disclosure but other materials are also possible candidates without detracting from the invention. The only requirement is that the coefficient of thermal expansion of the strips be less than that of the material forming the mirror. In this way, the bimetallic effect can compensate for the warping created by differential heating of the mirror.
- Figures 4A and 4B are illustrations similar to Figures 3A and 3B but show the output coupler side of the laser. The major difference is the addition of output port 50 through which the laser beam exits the laser tube housing.
- a holder 52 is provided for carrying an output window (not shown) formed from materials such as a ZnSe or Si.
- the window holder 52 is designed to maintain the hermetical seal. It should be noted that the length of the mirror 26 is shorter for the output side due to the need of providing an output beam coupling port for the resonator.
- the amount of output coupling from the negative branch hybrid unstable waveguide resonator is determined by the magnification of the resonator as is well known in the art.
- An alternate and preferred approach for holding the two bimetallic materials together is to bond the two materials together by either a soldering, or brazing technique instead of using the mechanical compression technique discussed above.
- the bonding approach initially requires more development efforts than the mechanical compression approach, but it can offer more long term stability especially after the laser tube housing undergoes temperature cycling experienced in bake-out during the manufacturing cycle.
- Figure 5 is a graph illustrating some beam pointing variation data from two lasers, one with and the other without bimetallic thermal compensation.
- the curves labeled A correspond to a laser having the prior art construction of Figures 1 and 2.
- the curves labeled B correspond to a laser design in accordance with Figures 3 and 4.
- Figure 5 shows temperature variations of the laser's mirrors over time as varied by a temperature controlled coolant applied to the mirrors.
- Figure 5 also shows the beam pointing variation of the unstable resonator (UR) with time that corresponds to the mirror temperature variation at that time by the coolant. Both lasers had the same output power of 400W and were as described above.
- the prior art laser is turned on and its mirror temperature starts to rise from 22°C to approximately 29°C in approximately 1000 seconds (curve Al). This time is the normal laser start-up temperature rise time for the laser mirrors.
- the angular position of the output beam of the prior art laser (curve A2) changed by approximately 1200 microradians (i.e., from 6300 to 7500 microradians).
- the mirror temperature of the prior art laser was raised by the controlled coolant so that at approximately 1500 seconds later (i.e., time ⁇ 2500 seconds), the laser mirror temperature was approximately 4O 0 C.
- the laser beam position was approximately 9500 microradians for a change in position by 2000 microradians.
- the mirror temperature was dropped to approximately 25 0 C which caused the beam's pointing position to drop to approximately 6100 microradians (i.e., a change in angular position of approximately 3,400 microradians). This behavior is certainly not acceptable for most material working applications.
- the laser formed in accordance with the subject invention (which was equal to the prior art laser in terms of power output), was turned on and then its mirror starts to rise in temperature from 22 0 C to approximately 32°C a little past 1000 seconds later (curve Bl).
- the angular position of the output beam dropped from 6300 microradians to approximately 6100 microradians (curve B2) i.e., a change of only approximately 100 microradians. This represents over an order of magnitude improvement.
- the pointing stability shown in Figure 5 is acceptable for most material processing applications.
- a comparison of the prior art laser deflection behavior with that of a laser formed in accordance with the subject invention clearly indicates the improvement obtained with the bimetallic thermal compensation of the unstable resonator mirrors.
- the pointing stability at start up has been reduced from about one milliradians to about 100 microradians.
- Figures 6A and 6B illustrate an alternative approach.
- the embodiment of Figures 6A and 6B is the same as the embodiment of Figures 3A and 3B except that the strips 4OA for controlling mirror warping are positioned on the rear surface of mirror element 16 instead of on the front surface.
- the coefficient of thermal expansion of the strips 4OA should be greater than the coefficient of thermal expansion of the mirror element. In this manner, the bimetallic effect will tend to make the mirror more concave while the thermal gradient tends to make the mirror less concave.
- the two effects can be balanced so that the pointing stability can be improved.
- the width of mirror element 16 (vertical dimension of Figure 6A) is larger than as shown in Figure 3A to permit a pair of strips 4OA to be mounted on the rear surface of the mirror element while providing clearance of the center mount 48.
- the strips can be formed from aluminum.
- the prior art design included a large aluminum block 18 ( Figure 1) mounted to the rear surface of the mirror element. This large block produced a large and uncontrolled bimetallic effect.
- the dimensions of the strips can be selected to balance the thermal gradient effect and improve performance.
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1001076.7A GB2463614B (en) | 2007-07-31 | 2008-07-10 | Thermal distortion compensation for laser mirrors |
DE112008002013T DE112008002013T5 (en) | 2007-07-31 | 2008-07-10 | Compensation of thermal distortion for laser mirrors |
CN2008801019099A CN101803131B (en) | 2007-07-31 | 2008-07-10 | Thermal distortion compensation for laser mirrors |
JP2010519190A JP5419297B2 (en) | 2007-07-31 | 2008-07-10 | Compensation for thermal deformation in laser mirrors |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US96274007P | 2007-07-31 | 2007-07-31 | |
US60/962,740 | 2007-07-31 | ||
US12/168,376 US7664159B2 (en) | 2007-07-31 | 2008-07-07 | Thermal distortion compensation for laser mirrors |
US12/168,376 | 2008-07-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2009017586A1 true WO2009017586A1 (en) | 2009-02-05 |
Family
ID=39712649
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2008/008446 WO2009017586A1 (en) | 2007-07-31 | 2008-07-10 | Thermal distortion compensation for laser mirrors |
Country Status (6)
Country | Link |
---|---|
US (2) | US7664159B2 (en) |
JP (1) | JP5419297B2 (en) |
CN (1) | CN101803131B (en) |
DE (1) | DE112008002013T5 (en) |
GB (1) | GB2463614B (en) |
WO (1) | WO2009017586A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7664159B2 (en) * | 2007-07-31 | 2010-02-16 | Coherent, Inc. | Thermal distortion compensation for laser mirrors |
US7889775B2 (en) | 2009-01-07 | 2011-02-15 | Coherent, Inc. | Particle damage protection for high power CO2 slab laser mirrors |
US8201954B2 (en) * | 2009-01-08 | 2012-06-19 | Coherent, Inc. | Compensation for transient heating of laser mirrors |
CN102263361B (en) * | 2011-06-22 | 2012-08-15 | 华中科技大学 | Laser reflection cavity mirror assembly |
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US7265814B2 (en) * | 2003-05-14 | 2007-09-04 | Canon Kabushiki Kaisha | Mirror holding method and optical apparatus |
US7260134B2 (en) * | 2004-02-06 | 2007-08-21 | Coherent, Inc. | Dielectric coupled CO2 slab laser |
US7263116B2 (en) * | 2004-08-05 | 2007-08-28 | Coherent, Inc. | Dielectric coupled CO2 slab laser |
JP4817702B2 (en) * | 2005-04-14 | 2011-11-16 | キヤノン株式会社 | Optical apparatus and exposure apparatus provided with the same |
US7756182B2 (en) * | 2007-03-28 | 2010-07-13 | Coherent, Inc. | RF excited CO2 slab laser tube housing and electrodes cooling |
US7664159B2 (en) * | 2007-07-31 | 2010-02-16 | Coherent, Inc. | Thermal distortion compensation for laser mirrors |
-
2008
- 2008-07-07 US US12/168,376 patent/US7664159B2/en not_active Expired - Fee Related
- 2008-07-10 JP JP2010519190A patent/JP5419297B2/en not_active Expired - Fee Related
- 2008-07-10 WO PCT/US2008/008446 patent/WO2009017586A1/en active Application Filing
- 2008-07-10 GB GB1001076.7A patent/GB2463614B/en not_active Expired - Fee Related
- 2008-07-10 DE DE112008002013T patent/DE112008002013T5/en not_active Withdrawn
- 2008-07-10 CN CN2008801019099A patent/CN101803131B/en not_active Expired - Fee Related
-
2009
- 2009-12-31 US US12/651,023 patent/US7965757B2/en active Active
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US3564452A (en) * | 1965-08-23 | 1971-02-16 | Spectra Physics | Laser with stable resonator |
US3609589A (en) * | 1968-09-03 | 1971-09-28 | Perkin Elmer Corp | Mirror for resisting thermally induced warp |
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SU1597834A1 (en) * | 1988-11-05 | 1990-10-07 | Ленинградский Институт Точной Механики И Оптики | Device for focusing high-power optical radiation |
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Also Published As
Publication number | Publication date |
---|---|
GB2463614A (en) | 2010-03-24 |
GB201001076D0 (en) | 2010-03-10 |
CN101803131A (en) | 2010-08-11 |
GB2463614B (en) | 2011-12-21 |
US7664159B2 (en) | 2010-02-16 |
JP2010535418A (en) | 2010-11-18 |
JP5419297B2 (en) | 2014-02-19 |
US20100103974A1 (en) | 2010-04-29 |
CN101803131B (en) | 2012-01-25 |
US20090034577A1 (en) | 2009-02-05 |
US7965757B2 (en) | 2011-06-21 |
DE112008002013T5 (en) | 2010-06-17 |
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