WO2002045475A2 - Protective overcoat for replicated diffraction gratings - Google Patents

Protective overcoat for replicated diffraction gratings Download PDF

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Publication number
WO2002045475A2
WO2002045475A2 PCT/US2001/046667 US0146667W WO0245475A2 WO 2002045475 A2 WO2002045475 A2 WO 2002045475A2 US 0146667 W US0146667 W US 0146667W WO 0245475 A2 WO0245475 A2 WO 0245475A2
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Prior art keywords
layer
grating
aluminum
protective layer
mgf
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Application number
PCT/US2001/046667
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French (fr)
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WO2002045475A3 (en
Inventor
Xiaojiang J. Pan
Richard G. Morton
Alexander I. Ershov
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Cymer, Inc.
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Priority claimed from US09/731,938 external-priority patent/US6529321B2/en
Application filed by Cymer, Inc. filed Critical Cymer, Inc.
Priority to EP01987291A priority Critical patent/EP1340106B1/en
Priority to DE60132355T priority patent/DE60132355T2/en
Priority to AU2002239525A priority patent/AU2002239525A1/en
Priority to JP2002547276A priority patent/JP4549019B2/en
Publication of WO2002045475A2 publication Critical patent/WO2002045475A2/en
Publication of WO2002045475A3 publication Critical patent/WO2002045475A3/en

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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/225Oblique incidence of vaporised material on substrate
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/0694Halides
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/14Metallic material, boron or silicon
    • C23C14/16Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/24Vacuum evaporation
    • G02B1/105
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B1/00Optical elements characterised by the material of which they are made; Optical coatings for optical elements
    • G02B1/10Optical coatings produced by application to, or surface treatment of, optical elements
    • G02B1/14Protective coatings, e.g. hard coatings
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B5/00Optical elements other than lenses
    • G02B5/18Diffraction gratings
    • G02B5/1847Manufacturing methods
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B5/00Optical elements other than lenses
    • G02B5/18Diffraction gratings
    • G02B5/1847Manufacturing methods
    • G02B5/1852Manufacturing methods using mechanical means, e.g. ruling with diamond tool, moulding
    • GPHYSICS
    • G03PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03FPHOTOMECHANICAL PRODUCTION OF TEXTURED OR PATTERNED SURFACES, e.g. FOR PRINTING, FOR PROCESSING OF SEMICONDUCTOR DEVICES; MATERIALS THEREFOR; ORIGINALS THEREFOR; APPARATUS SPECIALLY ADAPTED THEREFOR
    • G03F7/00Photomechanical, e.g. photolithographic, production of textured or patterned surfaces, e.g. printing surfaces; Materials therefor, e.g. comprising photoresists; Apparatus specially adapted therefor
    • G03F7/70Microphotolithographic exposure; Apparatus therefor
    • G03F7/70008Production of exposure light, i.e. light sources
    • G03F7/70025Production of exposure light, i.e. light sources by lasers
    • GPHYSICS
    • G03PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03FPHOTOMECHANICAL PRODUCTION OF TEXTURED OR PATTERNED SURFACES, e.g. FOR PRINTING, FOR PROCESSING OF SEMICONDUCTOR DEVICES; MATERIALS THEREFOR; ORIGINALS THEREFOR; APPARATUS SPECIALLY ADAPTED THEREFOR
    • G03F7/00Photomechanical, e.g. photolithographic, production of textured or patterned surfaces, e.g. printing surfaces; Materials therefor, e.g. comprising photoresists; Apparatus specially adapted therefor
    • G03F7/70Microphotolithographic exposure; Apparatus therefor
    • G03F7/70008Production of exposure light, i.e. light sources
    • G03F7/70041Production of exposure light, i.e. light sources by pulsed sources, e.g. multiplexing, pulse duration, interval control or intensity control
    • GPHYSICS
    • G03PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03FPHOTOMECHANICAL PRODUCTION OF TEXTURED OR PATTERNED SURFACES, e.g. FOR PRINTING, FOR PROCESSING OF SEMICONDUCTOR DEVICES; MATERIALS THEREFOR; ORIGINALS THEREFOR; APPARATUS SPECIALLY ADAPTED THEREFOR
    • G03F7/00Photomechanical, e.g. photolithographic, production of textured or patterned surfaces, e.g. printing surfaces; Materials therefor, e.g. comprising photoresists; Apparatus specially adapted therefor
    • G03F7/70Microphotolithographic exposure; Apparatus therefor
    • G03F7/70483Information management; Active and passive control; Testing; Wafer monitoring, e.g. pattern monitoring
    • GPHYSICS
    • G03PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03FPHOTOMECHANICAL PRODUCTION OF TEXTURED OR PATTERNED SURFACES, e.g. FOR PRINTING, FOR PROCESSING OF SEMICONDUCTOR DEVICES; MATERIALS THEREFOR; ORIGINALS THEREFOR; APPARATUS SPECIALLY ADAPTED THEREFOR
    • G03F7/00Photomechanical, e.g. photolithographic, production of textured or patterned surfaces, e.g. printing surfaces; Materials therefor, e.g. comprising photoresists; Apparatus specially adapted therefor
    • G03F7/70Microphotolithographic exposure; Apparatus therefor
    • G03F7/70483Information management; Active and passive control; Testing; Wafer monitoring, e.g. pattern monitoring
    • G03F7/7055Exposure light control in all parts of the microlithographic apparatus, e.g. pulse length control or light interruption
    • G03F7/70558Dose control, i.e. achievement of a desired dose
    • GPHYSICS
    • G03PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03FPHOTOMECHANICAL PRODUCTION OF TEXTURED OR PATTERNED SURFACES, e.g. FOR PRINTING, FOR PROCESSING OF SEMICONDUCTOR DEVICES; MATERIALS THEREFOR; ORIGINALS THEREFOR; APPARATUS SPECIALLY ADAPTED THEREFOR
    • G03F7/00Photomechanical, e.g. photolithographic, production of textured or patterned surfaces, e.g. printing surfaces; Materials therefor, e.g. comprising photoresists; Apparatus specially adapted therefor
    • G03F7/70Microphotolithographic exposure; Apparatus therefor
    • G03F7/70483Information management; Active and passive control; Testing; Wafer monitoring, e.g. pattern monitoring
    • G03F7/7055Exposure light control in all parts of the microlithographic apparatus, e.g. pulse length control or light interruption
    • G03F7/70575Wavelength control, e.g. control of bandwidth, multiple wavelength, selection of wavelength or matching of optical components to wavelength

Definitions

  • Diffraction gratings are frequently used in lasers for reflecting back into a laser's resonating cavity only a narrow range of wavelengths of light centered at one particular wavelength. Light energy at this narrow range of wavelengths resonates within the cavity and is emitted through a partially reflective mirror at the other end of the cavity. Examples of such diffraction gratings and various methods of making these diffraction gratings are described in U.S. Patent Nos. 5,080,465; 5,436,764; and 5,493,393, incorporated herein by reference.
  • a master diffraction grating is first manufactured. This master grating is then used to form many replica gratings. Each of these replica gratings may then be used as a master grating for forming other replica gratings.
  • a master grating may be formed by depositing aluminum over a substrate, such as glass.
  • a diamond tool under interferometric control may then be used to rule very closely spaced grooves in the aluminum layer.
  • the separation of the grooves is related to the wavelength of the light to be reflected by the grating and to the narrowness of the range of wavelengths it is required to reflect.
  • the diamond tool rules on the order of tens of thousands of grooves per inch.
  • the diffraction grating surface may be ten inches long and one inch wide. Creating a precision master grating by physical ruling is an extremely time consuming and expensive process.
  • replicas of the grating may be made using techniques such as are described in an article by Torbin and Wiskin in Soviet Journal of Optical Technology, Vol. 40(3) (March, 1973): 192-196.
  • a release agent such as silver, gold, copper glycerine, carnuba wax, debutyphthalate or low vapor pressure oil is coated on the surface of the master.
  • a thin (e.g., 1 micron) reflective layer, such as aluminum, is then deposited onto the release layer.
  • An uncured polyester cement (epoxy) may then be deposited on the aluminum layer, and a glass or metal substrate is then placed on top of the epoxy. After the cement is cured, the glass layer, epoxy layer, and aluminum layer are then separated from the master grating, resulting in a replica of the master grating.
  • Magnesium fluoride is a known optical coating. Coatings of this material having thicknesses of ⁇ /4 are used to reduce unwanted reflections. Also MgF 2 coatings have been shown to improve the efficiency of gratings operating at wavelengths greater than about 500 to 600nm. (See Maystre, et al, Applied Optics, Vol. 19(18) (September 15, 1980): 3099-3102. Al O 3 and SiO are also well known coating materials for ultraviolet wavelengths.
  • replicated gratings One important use of replicated gratings is to line narrow excimer lasers producing ultraviolet light at wavelengths of 248 nm and 193 nm. Applicant has discovered that prior art replica gratings suffer substantial performance degradation when subject to intense ultraviolet radiation especially at the higher energy 193nm wavelength. What is needed are replica gratings capable of long term high quality performance in intense ultraviolet radiation.
  • the present invention provides an overcoat protected diffraction grating.
  • a replica grating having a thin aluminum reflective grating surface is produced by replication of a master grating or a submaster grating.
  • the thin aluminum reflective surface may be cracked or have relatively thick grain boundaries containing oxides and hydroxides of aluminum and typically is also naturally coated with an aluminum oxide film.
  • the grating is subsequently overcoated in a vacuum chamber with one or two thin, pure, dense aluminum overcoat layers and then also in the vacuum the aluminum overcoat layer or layers are coated with one or more thin protective layers of a material transparent to ultraviolet radiation.
  • this protective layer is a single layer of MgF 2 , SiO 2 or Al 2 O 3 .
  • the layer is a layer of MgF 2 or SiO covered with a layer of Al 2 O 3 and in a third preferred embodiment the protective layer is made up of four alternating layers of MgF 2 and Al 2 O 3 or four alternating layers of SiO 2 and Al 2 O .
  • the thickness of the transparent protective layers are chosen to produce a phase shift at the proposed operating wavelengths of an integral number of 2 ⁇ .
  • the thin protective layer not only protects the aluminum from ultraviolet caused degradation but also improves the normal reflectivity of the reflecting faces of the grating.
  • the grating is especially suited for use for wavelength selection in an ArF laser operating producing an ultraviolet laser beam at a wavelength of about 193 nm.
  • the oxygen free aluminum overcoat prevents the ultraviolet light from causing damage by stimulating chemical reactions in grating materials under the aluminum grating surface or in the aluminum oxide film.
  • the protective layers prevent oxygen from getting to the aluminum.
  • FIG. 1 is a drawing of a vacuum deposition chamber.
  • FIG. 2 is a drawing of a section of a prior art replica grating.
  • FIG. 3 is a drawing of the same section as shown in FIG. 2 with an overcoat according to an embodiment of the present invention.
  • FIG. 4 is a drawing highly enlarged of a section of the section shown in FIG. 3.
  • FIG. 5 is a graph of test data showing a performance comparison of an overcoated grating with a prior art grating.
  • FIG. 6 is a graph showing unsatisfactory performance of a prior art grating overcoated with non-dense aluminum an then MgF 2 .
  • FIG. 7 shows performance data using a grating coated with a dense Al layer and MgF .
  • FIG. 8 shows a four layer protective coating designed for improved reflectivity.
  • FIGS. 9 A, B and C show reflections in phase through protective coatings.
  • FIG. 10 shows test results of MgF , SiO and Al 2 O 3 coatings in mirrors in a 193 nm UV environment.
  • FIG. 11 shows reflectance as a function of coating thickness for MgF SiO 2 and Al 2 O 3 coatings.
  • FIG. 12 is a table showing preferred protective layer thicknesses.
  • the aluminum coating deposited during the replication process is subjected to forces during the subsequent take- apart step of the replication process which tend to generate very small fractures in the aluminum coating and may also contain oxides and hydroxides of aluminum in the grain boundaries. These fractures and grain boundary regions allow small quantities of ultraviolet radiation to leak through to the underlying epoxy when the grating is put into service in an excimer laser.
  • the ultraviolet light which reaches the epoxy causes photodecomposition of the epoxy, releasing gases which cause blisters in the overlying aluminum coating. This blistering greatly increases scatter losses from the reflecting facets of the grating.
  • Applicant has been able to partially solve the problem caused by the cracks in the original aluminum layer of the replica grating by depositing another thin reflective overcoat of aluminum of about 100 nm to 200 nm on the surface of the replica after the replica has been removed from the master and cleaned.
  • the overcoating is preformed in a vacuum chamber by sputtering or evaporation.
  • This overcoat produces a major improvement in the grating performance especially when used for wavelength selection in a KrF excimer laser operating at a wavelength of about 248 nm.
  • Applicant has discovered that even with the aluminum overcoat substantial performance degradation occurred when the grating is used for wavelength selection in an ArF excimer laser operating at a wavelength of about 193nm.
  • the degradation is due to quantum photochemical and photophysical mechanisms involving high energy UV photon interaction with oxygen in the aluminum film as deposited; or at the boundary of the oxide layer which naturally forms on aluminum surfaces when those surfaces are exposed to air after the aluminum coating has been deposited on the grating. This degradation can be accentuated if the UV radiation of the aluminum surface takes place in an environment containing oxygen such as air. However, even if the space over the aluminum surface is purged with nitrogen during periods of UV illumination, reactions with oxygen in Al 2 O 3 surface films or in the grain boundary regions can degrade performance.
  • FIG. 1 describes a method of coating a grating to provide a grating suitable to long term use in high intensity ultraviolet environments.
  • FIG. 2 is a drawing of a section of the grating surface.
  • the grating substrate 40 is glass covered by an epoxy layer 42 which is about 15 microns thick which is covered by 1 micron aluminum layer 44.
  • the grooves are spaced at intervals of 11.7966 microns and are triangular shaped and about 3.5 microns deep at the deep end of each groove.
  • the 3.5 micron face of the groove makes a 11.3° angle with the normal to the face of the grating.
  • the grating When used in a Littrow configuration for wavelength selection in a laser, the grating is tilted at 11.3 degrees to the incoming beam so that the incoming beam meets the short surface at 90 degrees.
  • the 3.5 micron face is the reflective face.
  • an ArF laser operating at a wavelength of 193.38 nm twice the distance between successive short faces is exactly equivalent to 122 wavelengths of the 193.38 nm ArF light. Twice the distance between the short faces is also exactly equivalent to 95 wavelengths of KrF light at 248.35 nm. Therefore, the same grating can be used for wavelength selection of either KrF lasers or ArF lasers.
  • prior art replicated grating 2 is mounted in physical vapor deposition vacuum chamber 4 above vapor sources of aluminum metal and magnesium fluoride.
  • Aluminum is contained in an aluminum crucible 6 and magnesium fluoride is contained in a magnesium fluoride crucible 8 both of which are mounted on a rotating support 10 which may be rotated so as to provide a first coating of aluminum and a second coating of MgF 2 .
  • Vacuum pump 12 provides a vacuum pressure of 10 " torr or less, which is sufficient to assure a mean free path several times longer than the distance between the source and the grating. This provides essentially collision free atomic and molecular deposition.
  • the collision rate of background gases, such as oxygen or hydrogen, with the surface to be coated is substantially less than the arrival rate of aluminum atoms or magnesium fluoride molecules. This results in the deposition of pure, dense aluminum and magnesium fluoride on the grating surface. There is therefore very little oxygen or hydrogen present within the bulk coating materials.
  • the sources are heated with an electron beam 16 from an electron beam source 14 in the conventional manner, the beam being bent to the crucible location with a magnetic field from a magnetic source (not shown).
  • grating 2 is mounted in vacuum chamber 4 at an angle of such that the coating atoms strike the grating surface at an angle of about 50 degrees to the normal. This means that the atoms are impinging on the short surface at an angle of 29 degrees to the normal to the short surface and the long surface at an angle of about 61 degrees to the normal of that surface.
  • the coating process should continue until a dense aluminum thickness of about lOOnm is achieved.
  • the support 10 is used to rotate the MgF source in place and an overcoat of MgF of about 54 nm is placed over the aluminum coating on the short surface of the grating.
  • the thicknesses of both coatings on the long surface will be about 55% of the corresponding thickness on the short surface.
  • the result of the double coating is shown in FIGS. 3 and 4.
  • Gratings overcoated in accordance with the dense aluminum and MgF overcoat have been tested by Applicant in wavelength selecting modules on an ArF laser and compared to prior art non-densely unovercoated gratings.
  • FIG. 5 Data from the ArF experiment is shown in FIG. 5. After about 20 million pulses at 10 mJ per pulse at 193nm the prior art grating has decreased in reflectivity to about 75% of its initial value; whereas the grating overcoated in accordance with the present invention still provides a reflectivity of more than 95% of its initial value.
  • FIG. 7 presents data showing that the single coating of MgF provides excellent results up to about 2 billion pulses. However, Applicants' continued tests have shown that the gratings deteriorate rapidly after about 2 billion pulses.
  • MgF 2 coating shown in FIGS. 3 and 4 provides a tremendous lifetime improvement for the gratings in an ArF laser LNP
  • other coatings in the place of or in addition to the MgF 2 are needed to protect the grating surface from degradation beyond about 2 billion pulses.
  • substantial improvements in reflectivity can result from use of multiple coatings.
  • Pure aluminum has maximum reflection coefficient of about 92.5% at 193 nm. Although this is a sufficient reflectivity for some applications, it is sometimes desirable to increase the reflectivity even more. Higher reflectivity would not only make lasers work more efficiently, but also it will reduce percentage of laser power, which is absorbed by the grating surface. In case of aluminum surface discussed above, a maximum of 92.5% of light at 193 nm is reflected, but the rest 7.5% of light is absorbed.
  • the state-of-the-art excimer lasers may have 10-20 W of light power going onto the grating during operation. Absorbing 7.5% of this power will cause grating surface to heat up.
  • the reflectivity of the Al surface can be increased if it is overcoated with one or several layers of dielectric materials, such as MgF , Al O 3 , SiO 2 and others.
  • the aluminum surface is coated with alternating layers of high and low refractive index materials.
  • MgF 2 and SiO 2 can be used as a low refractive index materials.
  • Al O 3 is an example of high refractive index material.
  • the coating thicknesses are chosen in such a way, that reflections from each layer are all in phase with each other, so that total reflection is thus increased. Being in phase means that the phase differences of these reflection waves are the integer number of 2 ⁇ radians.
  • FIGS. 9 A, 9B and 9C show the overcoat structure for one, two and four layer overcoats. In the design of these coatings, all layers, except for the layer next to aluminum surface, have geometrical thickness of about ⁇ /4-n, where n is refractive index of layer material, and ⁇ is the wavelength. This thickness means that the light traveling through this layer twice will have a phase shift of ⁇ .
  • each transparent protective layer has a thickness corresponding to 2 ⁇ phase shift, however, if this is not easily done another preferred approach is to design all of the transparent protective layers so that the total phase shift through them is an integral number of 2 ⁇ .
  • the first layer on aluminum surface its thickness is less than ⁇ /4n in case of 2 and 4 layer designs, because phase shift is between 0 and ⁇ in the interface of this layer and Al surface.
  • the thickness of a single layer of MgF 2 in a single layer design is between ⁇ /4n and ⁇ /2n. Readers are referred to numerous optical references which explain in detail techniques for choosing these coating thicknesses to achieve maximum reflectance. Specifically, a recommended reference is Chapter 40 of Handbook of Optics, Volume I, pages 42-1 to 42-54, published by McGraw Hill with offices in New York and many other cities. The editor-in-chief is Michael Bass.
  • MgF 2 overcoat the reflectivity of the aluminum surface can be slightly increased.
  • overcoating Al with MgF layer about 50 nm thick can increase its reflectivity up to 93.2%. It is desirable to increase the reflectivity even more.
  • a multilayer overcoat can be used. This overcoat consists of alternating layers of high and low refractive index materials.
  • a two layer overcoat, having 23 nm thick MgF 2 layer as a first layer on top of Al surface, and a 26 nm thick layer of A1 2 0 3 on top of MgF 2 will boast the total reflectivity at 193 nm to about 95.5%.
  • Even higher reflectivity can be achieved using a four layer overcoat such as this:
  • This coating shown in FIG. 8 will have a total reflectivity of about 97.1%> at 193 nm.
  • Persons skilled in the art can recognize, that other high and low refractive index materials can be used.
  • this multilayer overcoat is that the total dielectric film thickness is rather small: about 48 nm in case of two layer overcoat and about 109 nm in case of four layer overcoat. Therefore, it is significantly smaller than the size of the groove which is typically somewhat larger than 3,000 nm.
  • the increase of total reflectivity from about 92.5% (uncoated Al) to 97.1% ( four layer overcoated Al) is very important, especially if this coating is used on a grating working in high average power UV laser, such as excimer lithography laser.
  • a very important feature of this invention is that the coatings are chosen to accomplish two purposes (1) protect the grating surface from ultraviolet caused degradation and (2) improve normal reflectivity from the reflecting grating faces. This improvement in reflectivity has two very important effects: (1) greater reflectivity increases the efficiency of the grating and improves laser overall performance and (2) greater reflectivity means that less light energy is absorbed to the grating surface reducing the thermal load on the grating which can cause temperature increases and resulting distortion of the surface which could in turn adversely affect performance of the grating.
  • a single coating of Al 2 O 24 nm thick may be applied over a 23 nm thick MgF 2 coating as discussed above.
  • the Al O is applied by adding an Al 2 O 3 crucible on the rotating support 10 shown in FIG. 1.
  • Al 2 O 3 is much tougher than MgF 2 . It protects the MgF from UV damage and improves reflectivity as described above.
  • FIG. 8 shows the four layer coating discussed above which is 23 nm MgF , 26 nm Al 2 O 3 , 34 nm MgF 2 and 26 nm Al 2 O 3 .
  • Coatings of SiO over the MgF 2 may be applied as described above for the Al O with similar results.
  • SiO 2 is a glass, and so less brittle than MgF 2 and, as the Al 2 O 3 , protects the MgF 2 from UV damage, extending the useful life of the grating.
  • Thin films of SiO 2 are also transparent to the UV radiation. Standard well known techniques needed to select thicknesses for optimum reflectivity performance may be used to specify thicknesses.
  • the aluminum overcoating be a pure dense coat of aluminum and that the coating is free of oxidation.
  • Merely coating the original cracked and/or non-dense coating on the prior art grating with MgF provides no substantial improvement.
  • experiments by Applicant in a 248nm environment showed poor initial performance and rapid degradation of a grating having a MgF 2 coating but with an aluminum overcoat applied at a vacuum pressure higher than 10 "5 torr, see FIG. 6. It is also important as stated above to put the MgF 2 coating on the aluminum overcoat before there is any significant oxidation of the aluminum overcoat.
  • the UV will cause chemical changes below the MgF 2 layer and distort the grating surface, thus reducing reflectivity.
  • the pure dense aluminum coating is very important at high UV levels such as those produced by excimer lasers.
  • Applicants have specified two separate dense Al layers as indicated in the examples shown in FIG. 12.
  • MgF 2 has lower refractive index than SiO 2 and Al 2 O 3 have, which makes the grating efficiency (reflectance) less sensitive to coating thickness variation.
  • MgF 2 material is excellent for 193nm transmission.
  • MgF 2 coating tends to have certain local microstructure which can leave channels for oxygen penetration. For grating protection coating, this feature of MgF 2 coating can be even worse as the grating surface is not flat. Hydroscopic properties of MgF 2 coating is another concern.
  • SiO 2 and Al 2 O 3 have different structures (hexagon instead of tetragon) and are more amorphous than MgF 2 in the coating process.
  • a coating of SiO 2 can be more uniform on the grating surface and more chemically inert to ambient environment than MgF 2 .
  • aluminum mirrors were coated with MgF 2 , SiO 2 and Al 2 O 3 and comparison tests were conducted. The test results are plotted in FIG. 10.
  • SiO showed the longest durability of coating protection.
  • the exposure laser energy was 5 mJ per pulse at 193nm.
  • the average intensity was 4.5 mJ/cm .
  • Each mirror was exposed to several hundred million pulses as the results of FIG. 1 show.
  • the testing mirrors were in room air.
  • the initial reflectance of all three mirrors was lower than 90%.
  • the relatively low initial reflectance of the Al O 3 sample is believed to have been caused by surface contamination on the mirror surface prior to coating.
  • FIG. 11 shows that the calculated Al 2 O 3 coating reflection varies somewhat (but not very much) with the thickness of a given protection coating, where, the complex of refractive index of aluminum is 0.11+2.2i at 193nm (E. Palik, Optical Constants of Solids).
  • the refractive indexes of SiO 2 and MgF 2 coating materials are shown in the figure as well.
  • the results presented in FIG. 10 show that both SiO 2 and Al 2 O 3 provided substantial additional protection as compared to MgF .
  • the preferred thicknesses are those which correspond to high reflectances in the FIG. 11 graph. For example, about 20 nm or 80 nm for SiO 2 and about 15 nm or 64 nm for Al 2 O 3 would be preferred.
  • FIG. 12 presents a matrix of recommended coatings for a grating to be used for line narrowing an ArF excimer laser.
  • the total thickness of the protective layer or layers is less than 10% of the width of the reflecting face of the grating. However, thicknesses outside these ranges may be specified. It is most important that good coatings be applied to the surface which will be exposed to the intense ultraviolet light. For the grating shown in FIGS. 2 and 3, that surface is the short, 3.5 micron surface.
  • the test results discussed above were obtained using a wavelength selecting module containing a three-prism beam expander, and a beam angle adjusting mirror along with the overcoat material diffraction grating arranged in a Littrow configuration.
  • persons skilled in the art will recognize many other applications for gratings fabricated according to the present invention. Therefore, the appended claims are to encompass within their scope all such changes and modifications as fall within the true spirit and scope of this invention.

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Abstract

An overcoat protected diffraction grating. A replica grating having a thin aluminum reflective grating surface is produced by replication of a master grating or a submaster grating. The thin aluminum reflective surface may be cracked or have relatively thick grain boundaries containing oxides and hydroxides of aluminum and typically is also naturally coated with an aluminum oxide film. The grating is subsequently overcoated in a vacuum chamber with one or two thin, pure, dense aluminum overcoat layers and then also in the vacuum the aluminum overcoat layer or layers are coated with one or more thin protective layers of a material transparent to ultraviolet radiation. In preferred embodiments this protective layer is a single layer of MgF2, S1O2 or Al2O3. In other preferred embodiments the layer is a layer of MgF2 or S1O2 covered with a layer of Al2O3 and in a third preferred embodiment the protective layer is made up of four alternating layers of MgF2 and Al2O3 or four alternating layers of S1O2 and Al2O3. Preferably, the thickness of the transparent protective layers are chosen to produce a phase shift at the proposed operating wavelengths of an integral number of 2π.

Description

PROTECTIVE OVERCOAT FOR REPLICATED DIFFRACTION GRATINGS
FIELD OF THE INVENTION
This application is a continuation-in-part application of U.S. Serial No. 09/731,938, filed December 7, 2000 which was a continuation-in-part of U.S. Serial No. 08/939,611, filed September 29, 1997 now U.S. Patent No. 6,162,495 issued December 19, 2000. This invention relates to diffraction gratings and, in particular, to techniques used for improving performance and extending the life of diffraction gratings.
BACKGROUND OF THE INVENTION
Diffraction gratings are frequently used in lasers for reflecting back into a laser's resonating cavity only a narrow range of wavelengths of light centered at one particular wavelength. Light energy at this narrow range of wavelengths resonates within the cavity and is emitted through a partially reflective mirror at the other end of the cavity. Examples of such diffraction gratings and various methods of making these diffraction gratings are described in U.S. Patent Nos. 5,080,465; 5,436,764; and 5,493,393, incorporated herein by reference.
Typically, a master diffraction grating is first manufactured. This master grating is then used to form many replica gratings. Each of these replica gratings may then be used as a master grating for forming other replica gratings.
As described in the '465 patent, a master grating may be formed by depositing aluminum over a substrate, such as glass. A diamond tool under interferometric control may then be used to rule very closely spaced grooves in the aluminum layer. The separation of the grooves is related to the wavelength of the light to be reflected by the grating and to the narrowness of the range of wavelengths it is required to reflect. In one example, the diamond tool rules on the order of tens of thousands of grooves per inch. The diffraction grating surface may be ten inches long and one inch wide. Creating a precision master grating by physical ruling is an extremely time consuming and expensive process. Once a master grating has been made, replicas of the grating may be made using techniques such as are described in an article by Torbin and Wiskin in Soviet Journal of Optical Technology, Vol. 40(3) (March, 1973): 192-196. In one such method, a release agent, such as silver, gold, copper glycerine, carnuba wax, debutyphthalate or low vapor pressure oil is coated on the surface of the master. A thin (e.g., 1 micron) reflective layer, such as aluminum, is then deposited onto the release layer. An uncured polyester cement (epoxy) may then be deposited on the aluminum layer, and a glass or metal substrate is then placed on top of the epoxy. After the cement is cured, the glass layer, epoxy layer, and aluminum layer are then separated from the master grating, resulting in a replica of the master grating.
Magnesium fluoride is a known optical coating. Coatings of this material having thicknesses of λ/4 are used to reduce unwanted reflections. Also MgF2 coatings have been shown to improve the efficiency of gratings operating at wavelengths greater than about 500 to 600nm. (See Maystre, et al, Applied Optics, Vol. 19(18) (September 15, 1980): 3099-3102. Al O3 and SiO are also well known coating materials for ultraviolet wavelengths.
One important use of replicated gratings is to line narrow excimer lasers producing ultraviolet light at wavelengths of 248 nm and 193 nm. Applicant has discovered that prior art replica gratings suffer substantial performance degradation when subject to intense ultraviolet radiation especially at the higher energy 193nm wavelength. What is needed are replica gratings capable of long term high quality performance in intense ultraviolet radiation.
SUMMARY OF THE INVENTION
The present invention provides an overcoat protected diffraction grating. A replica grating having a thin aluminum reflective grating surface is produced by replication of a master grating or a submaster grating. The thin aluminum reflective surface may be cracked or have relatively thick grain boundaries containing oxides and hydroxides of aluminum and typically is also naturally coated with an aluminum oxide film. The grating is subsequently overcoated in a vacuum chamber with one or two thin, pure, dense aluminum overcoat layers and then also in the vacuum the aluminum overcoat layer or layers are coated with one or more thin protective layers of a material transparent to ultraviolet radiation. In preferred embodiments this protective layer is a single layer of MgF2, SiO2 or Al2O3. In other preferred embodiments the layer is a layer of MgF2 or SiO covered with a layer of Al2O3 and in a third preferred embodiment the protective layer is made up of four alternating layers of MgF2 and Al2O3 or four alternating layers of SiO2 and Al2O . Preferably, the thickness of the transparent protective layers are chosen to produce a phase shift at the proposed operating wavelengths of an integral number of 2π. The thin protective layer not only protects the aluminum from ultraviolet caused degradation but also improves the normal reflectivity of the reflecting faces of the grating. The grating is especially suited for use for wavelength selection in an ArF laser operating producing an ultraviolet laser beam at a wavelength of about 193 nm. The oxygen free aluminum overcoat prevents the ultraviolet light from causing damage by stimulating chemical reactions in grating materials under the aluminum grating surface or in the aluminum oxide film. The protective layers prevent oxygen from getting to the aluminum.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a drawing of a vacuum deposition chamber.
FIG. 2 is a drawing of a section of a prior art replica grating.
FIG. 3 is a drawing of the same section as shown in FIG. 2 with an overcoat according to an embodiment of the present invention.
FIG. 4 is a drawing highly enlarged of a section of the section shown in FIG. 3.
FIG. 5 is a graph of test data showing a performance comparison of an overcoated grating with a prior art grating.
FIG. 6 is a graph showing unsatisfactory performance of a prior art grating overcoated with non-dense aluminum an then MgF2. FIG. 7 shows performance data using a grating coated with a dense Al layer and MgF .
FIG. 8 shows a four layer protective coating designed for improved reflectivity.
FIGS. 9 A, B and C show reflections in phase through protective coatings.
FIG. 10 shows test results of MgF , SiO and Al2O3 coatings in mirrors in a 193 nm UV environment.
FIG. 11 shows reflectance as a function of coating thickness for MgF SiO2 and Al2O3 coatings.
FIG. 12 is a table showing preferred protective layer thicknesses.
DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS APPLICANT'S EXPERIMENTS
Applicant has discovered that the aluminum coating deposited during the replication process, typically about 1 micron thick, is subjected to forces during the subsequent take- apart step of the replication process which tend to generate very small fractures in the aluminum coating and may also contain oxides and hydroxides of aluminum in the grain boundaries. These fractures and grain boundary regions allow small quantities of ultraviolet radiation to leak through to the underlying epoxy when the grating is put into service in an excimer laser. The ultraviolet light which reaches the epoxy causes photodecomposition of the epoxy, releasing gases which cause blisters in the overlying aluminum coating. This blistering greatly increases scatter losses from the reflecting facets of the grating. The ultraviolet light also causes bulk shrinkage of the epoxy, which distorts the original groove shape, causing a loss of reflectivity in the desired diffraction order. These effects severely limit the useful lifetime of the grating, causing unavailability of the equipment in which it is used at relatively frequent intervals. Second Aluminum Coating
Applicant has been able to partially solve the problem caused by the cracks in the original aluminum layer of the replica grating by depositing another thin reflective overcoat of aluminum of about 100 nm to 200 nm on the surface of the replica after the replica has been removed from the master and cleaned. The overcoating is preformed in a vacuum chamber by sputtering or evaporation. This overcoat produces a major improvement in the grating performance especially when used for wavelength selection in a KrF excimer laser operating at a wavelength of about 248 nm. However, Applicant has discovered that even with the aluminum overcoat substantial performance degradation occurred when the grating is used for wavelength selection in an ArF excimer laser operating at a wavelength of about 193nm.
Applicant believes the degradation is due to quantum photochemical and photophysical mechanisms involving high energy UV photon interaction with oxygen in the aluminum film as deposited; or at the boundary of the oxide layer which naturally forms on aluminum surfaces when those surfaces are exposed to air after the aluminum coating has been deposited on the grating. This degradation can be accentuated if the UV radiation of the aluminum surface takes place in an environment containing oxygen such as air. However, even if the space over the aluminum surface is purged with nitrogen during periods of UV illumination, reactions with oxygen in Al2O3 surface films or in the grain boundary regions can degrade performance.
Dense Aluminum Coating with MgF Overcoat
FIG. 1 describes a method of coating a grating to provide a grating suitable to long term use in high intensity ultraviolet environments.
Applicant has performed coating operations with a prior art grating having dimensions of about 250 mm in length, 35 mm thick and 35mm wide in order to produce gratings with substantially increased lifetime and improved performance. The grooves of this grating are spaced at about 84.77 grooves per mm. FIG. 2 is a drawing of a section of the grating surface. The grating substrate 40 is glass covered by an epoxy layer 42 which is about 15 microns thick which is covered by 1 micron aluminum layer 44. The grooves are spaced at intervals of 11.7966 microns and are triangular shaped and about 3.5 microns deep at the deep end of each groove. The 3.5 micron face of the groove makes a 11.3° angle with the normal to the face of the grating. When used in a Littrow configuration for wavelength selection in a laser, the grating is tilted at 11.3 degrees to the incoming beam so that the incoming beam meets the short surface at 90 degrees. The 3.5 micron face is the reflective face. In an ArF laser operating at a wavelength of 193.38 nm, twice the distance between successive short faces is exactly equivalent to 122 wavelengths of the 193.38 nm ArF light. Twice the distance between the short faces is also exactly equivalent to 95 wavelengths of KrF light at 248.35 nm. Therefore, the same grating can be used for wavelength selection of either KrF lasers or ArF lasers.
Referring now to FIG. 1, prior art replicated grating 2 is mounted in physical vapor deposition vacuum chamber 4 above vapor sources of aluminum metal and magnesium fluoride. Aluminum is contained in an aluminum crucible 6 and magnesium fluoride is contained in a magnesium fluoride crucible 8 both of which are mounted on a rotating support 10 which may be rotated so as to provide a first coating of aluminum and a second coating of MgF2. Vacuum pump 12 provides a vacuum pressure of 10" torr or less, which is sufficient to assure a mean free path several times longer than the distance between the source and the grating. This provides essentially collision free atomic and molecular deposition. Also, at this pressure the collision rate of background gases, such as oxygen or hydrogen, with the surface to be coated is substantially less than the arrival rate of aluminum atoms or magnesium fluoride molecules. This results in the deposition of pure, dense aluminum and magnesium fluoride on the grating surface. There is therefore very little oxygen or hydrogen present within the bulk coating materials. The sources are heated with an electron beam 16 from an electron beam source 14 in the conventional manner, the beam being bent to the crucible location with a magnetic field from a magnetic source (not shown).
To provide the secondary aluminum coating and the MgF2 overcoating, grating 2 is mounted in vacuum chamber 4 at an angle of such that the coating atoms strike the grating surface at an angle of about 50 degrees to the normal. This means that the atoms are impinging on the short surface at an angle of 29 degrees to the normal to the short surface and the long surface at an angle of about 61 degrees to the normal of that surface. The coating process should continue until a dense aluminum thickness of about lOOnm is achieved. Without breaking the vacuum in the chamber 4, the support 10 is used to rotate the MgF source in place and an overcoat of MgF of about 54 nm is placed over the aluminum coating on the short surface of the grating. The thicknesses of both coatings on the long surface will be about 55% of the corresponding thickness on the short surface. The result of the double coating is shown in FIGS. 3 and 4.
Test Results
Gratings overcoated in accordance with the dense aluminum and MgF overcoat have been tested by Applicant in wavelength selecting modules on an ArF laser and compared to prior art non-densely unovercoated gratings.
Data from the ArF experiment is shown in FIG. 5. After about 20 million pulses at 10 mJ per pulse at 193nm the prior art grating has decreased in reflectivity to about 75% of its initial value; whereas the grating overcoated in accordance with the present invention still provides a reflectivity of more than 95% of its initial value. FIG. 7 presents data showing that the single coating of MgF provides excellent results up to about 2 billion pulses. However, Applicants' continued tests have shown that the gratings deteriorate rapidly after about 2 billion pulses.
Applicants have noted that deterioration begins in the higher flux regions of the grating indicating that the deterioration after 2 billion pulses is due to accumulated UV radiation. Applicants suspect that the radiation causes tiny cracks in the MgF2 which grow over time permitting UV assisted oxidation of the underlying pure dense aluminum overcoat.
Other Coatings
Although the MgF2 coating shown in FIGS. 3 and 4 provides a tremendous lifetime improvement for the gratings in an ArF laser LNP, other coatings in the place of or in addition to the MgF2 are needed to protect the grating surface from degradation beyond about 2 billion pulses. Furthermore, Applicants have discovered that substantial improvements in reflectivity can result from use of multiple coatings.
Coating Thickness To Improve Reflectivity
Pure aluminum has maximum reflection coefficient of about 92.5% at 193 nm. Although this is a sufficient reflectivity for some applications, it is sometimes desirable to increase the reflectivity even more. Higher reflectivity would not only make lasers work more efficiently, but also it will reduce percentage of laser power, which is absorbed by the grating surface. In case of aluminum surface discussed above, a maximum of 92.5% of light at 193 nm is reflected, but the rest 7.5% of light is absorbed. The state-of-the-art excimer lasers may have 10-20 W of light power going onto the grating during operation. Absorbing 7.5% of this power will cause grating surface to heat up. That, in turn, might cause significant distortions in the properties of the laser beam, generated by these lasers, such as spectral bandwidth, divergence, and even shape and size of the laser beam. These distortions can even make those lasers not suitable for microlithography exposure and force a reduction in power, thus reducing the microlithography throughput and increasing the cost of the integrated circuits. Therefore, it is desirable to increase the reflectivity of the grating surface.
The reflectivity of the Al surface can be increased if it is overcoated with one or several layers of dielectric materials, such as MgF , Al O3, SiO2 and others. In this case, the aluminum surface is coated with alternating layers of high and low refractive index materials. As a low refractive index materials, MgF2 and SiO2 can be used. Al O3, on the other hand, is an example of high refractive index material.
Preferably, the coating thicknesses are chosen in such a way, that reflections from each layer are all in phase with each other, so that total reflection is thus increased. Being in phase means that the phase differences of these reflection waves are the integer number of 2π radians. FIGS. 9 A, 9B and 9C show the overcoat structure for one, two and four layer overcoats. In the design of these coatings, all layers, except for the layer next to aluminum surface, have geometrical thickness of about λ/4-n, where n is refractive index of layer material, and λ is the wavelength. This thickness means that the light traveling through this layer twice will have a phase shift of π. This fact and the fact that the light has an addition phase shift of π when reflecting from the interface of high and low refractive index materials, if it is coming from the high refractive index side, and a phase shift of zero, if it is coming from the low refractive index side; provides that the phase difference of all reflected waves is a whole number of 2π, that means they are all interfere constructively, thus increasing overall reflectivity.
As stated above, preferably the thickness of each transparent protective layer has a thickness corresponding to 2 π phase shift, however, if this is not easily done another preferred approach is to design all of the transparent protective layers so that the total phase shift through them is an integral number of 2 π.
As for the first layer on aluminum surface, its thickness is less than λ/4n in case of 2 and 4 layer designs, because phase shift is between 0 and π in the interface of this layer and Al surface. Similarly, the thickness of a single layer of MgF2 in a single layer design is between λ/4n and λ/2n. Readers are referred to numerous optical references which explain in detail techniques for choosing these coating thicknesses to achieve maximum reflectance. Specifically, a recommended reference is Chapter 40 of Handbook of Optics, Volume I, pages 42-1 to 42-54, published by McGraw Hill with offices in New York and many other cities. The editor-in-chief is Michael Bass.
By doing a single layer MgF2 overcoat the reflectivity of the aluminum surface can be slightly increased. For example, overcoating Al with MgF layer about 50 nm thick can increase its reflectivity up to 93.2%. It is desirable to increase the reflectivity even more. For that, a multilayer overcoat can be used. This overcoat consists of alternating layers of high and low refractive index materials. A two layer overcoat, having 23 nm thick MgF2 layer as a first layer on top of Al surface, and a 26 nm thick layer of A1203 on top of MgF2 will boast the total reflectivity at 193 nm to about 95.5%. Even higher reflectivity can be achieved using a four layer overcoat such as this:
Air
26 nm thick Al2O3
34 nm thick MgF2 26 nm thick Al2O3 23 nm thick MgF Aluminum.
This coating shown in FIG. 8 will have a total reflectivity of about 97.1%> at 193 nm. In all these coatings, MgF is used as a low refractive index material (n = 1.43), while Al O3 is used as a high refractive index material (n = 1.8). Persons skilled in the art can recognize, that other high and low refractive index materials can be used.
The advantage of this multilayer overcoat is that the total dielectric film thickness is rather small: about 48 nm in case of two layer overcoat and about 109 nm in case of four layer overcoat. Therefore, it is significantly smaller than the size of the groove which is typically somewhat larger than 3,000 nm. The increase of total reflectivity from about 92.5% (uncoated Al) to 97.1% ( four layer overcoated Al) is very important, especially if this coating is used on a grating working in high average power UV laser, such as excimer lithography laser.
The Al coating absorbs all the light which was not reflected. That means, in case of uncoated aluminum 100% - 92.5% = 7.5% of incident light is absorbed. On the other hand, in case of four layer overcoat, only 100 - 97.1% = 2.9% of incident light is absorbed. Therefore, by increasing total reflectivity from 92.5% to 97.1% we actually reduced absorption by 7.5% divided by 2.9% equals 2.59 times. Reduction of total power absorbed by the diffraction grating is very important, as it reduces all the thermal effects and thermal distortions in the properties of the laser beam caused by bulk heating of the grating, because these effects are normally proportional to the absorbed power.
Other techniques for the application of multiple layers for enhancing normal reflectivity may be utilized to increase normal reflectivity as compared to an uncoated aluminum surface. A very important feature of this invention is that the coatings are chosen to accomplish two purposes (1) protect the grating surface from ultraviolet caused degradation and (2) improve normal reflectivity from the reflecting grating faces. This improvement in reflectivity has two very important effects: (1) greater reflectivity increases the efficiency of the grating and improves laser overall performance and (2) greater reflectivity means that less light energy is absorbed to the grating surface reducing the thermal load on the grating which can cause temperature increases and resulting distortion of the surface which could in turn adversely affect performance of the grating.
MgF2 and Al2O3
A single coating of Al2O 24 nm thick may be applied over a 23 nm thick MgF2 coating as discussed above. Preferably the Al O is applied by adding an Al2O3 crucible on the rotating support 10 shown in FIG. 1. Al2O3 is much tougher than MgF2. It protects the MgF from UV damage and improves reflectivity as described above. FIG. 8 shows the four layer coating discussed above which is 23 nm MgF , 26 nm Al2O3, 34 nm MgF2 and 26 nm Al2O3.
MgF2 and Si O2
Coatings of SiO over the MgF2 may be applied as described above for the Al O with similar results. SiO2 is a glass, and so less brittle than MgF2 and, as the Al2O3, protects the MgF2 from UV damage, extending the useful life of the grating. Thin films of SiO2 are also transparent to the UV radiation. Standard well known techniques needed to select thicknesses for optimum reflectivity performance may be used to specify thicknesses.
Importance of Dense Non-Oxidized Al Overcoat
It is important that the aluminum overcoating be a pure dense coat of aluminum and that the coating is free of oxidation. Merely coating the original cracked and/or non-dense coating on the prior art grating with MgF provides no substantial improvement. In fact, experiments by Applicant in a 248nm environment showed poor initial performance and rapid degradation of a grating having a MgF2 coating but with an aluminum overcoat applied at a vacuum pressure higher than 10"5 torr, see FIG. 6. It is also important as stated above to put the MgF2 coating on the aluminum overcoat before there is any significant oxidation of the aluminum overcoat. If there is an oxide film on the aluminum, the UV will cause chemical changes below the MgF2 layer and distort the grating surface, thus reducing reflectivity. It should be noted that the requirement for a pure dense aluminum coat is not normally important when the grating is used in environments where the UV intensity is low, such as in astronomy work. The pure dense aluminum coating, however, is very important at high UV levels such as those produced by excimer lasers. In preferred embodiments Applicants have specified two separate dense Al layers as indicated in the examples shown in FIG. 12.
Comparison Tests - MgF2, SiO2, Al2O3
MgF2 has lower refractive index than SiO2 and Al2O3 have, which makes the grating efficiency (reflectance) less sensitive to coating thickness variation. MgF2 material is excellent for 193nm transmission. However, MgF2 coating tends to have certain local microstructure which can leave channels for oxygen penetration. For grating protection coating, this feature of MgF2 coating can be even worse as the grating surface is not flat. Hydroscopic properties of MgF2 coating is another concern.
Other materials, such as SiO2 and Al2O3, have different structures (hexagon instead of tetragon) and are more amorphous than MgF2 in the coating process. A coating of SiO2, for example, can be more uniform on the grating surface and more chemically inert to ambient environment than MgF2. To test the coatings in a 193 nm ultraviolet environment, aluminum mirrors were coated with MgF2, SiO2 and Al2O3 and comparison tests were conducted. The test results are plotted in FIG. 10. SiO showed the longest durability of coating protection. The exposure laser energy was 5 mJ per pulse at 193nm. The average intensity was 4.5 mJ/cm . Each mirror was exposed to several hundred million pulses as the results of FIG. 1 show. The testing mirrors were in room air. The initial reflectance of all three mirrors was lower than 90%. The relatively low initial reflectance of the Al O3 sample is believed to have been caused by surface contamination on the mirror surface prior to coating.
A little higher refractive index of SiO2 than MgF2 does not change much the insensitiveness of the grating efficiency on coating thickness. FIG. 11 shows that the calculated Al2O3 coating reflection varies somewhat (but not very much) with the thickness of a given protection coating, where, the complex of refractive index of aluminum is 0.11+2.2i at 193nm (E. Palik, Optical Constants of Solids). The refractive indexes of SiO2 and MgF2 coating materials are shown in the figure as well.
The results presented in FIG. 10 show that both SiO2 and Al2O3 provided substantial additional protection as compared to MgF . The preferred thicknesses are those which correspond to high reflectances in the FIG. 11 graph. For example, about 20 nm or 80 nm for SiO2 and about 15 nm or 64 nm for Al2O3 would be preferred.
Recommended Coatings
FIG. 12 presents a matrix of recommended coatings for a grating to be used for line narrowing an ArF excimer laser.
While particular embodiments of the present invention have been shown and described, it will be obvious to those skilled in the art that changes and modifications may be made without departing from this invention in its broader aspects. For example, persons skilled in the art will understand that methods other than vacuum evaporation could be used to produce an oxide-free, dense aluminum overcoat. Many different combinations of layers of various thicknesses could be utilized to achieve the two important objectives of this invention, i.e. surface protection and increased reflectivity. Preferred thicknesses for the aluminum coat are from about 50nm to about 200nm or two dense coats of 150nm each as shown in FIG. 12 could be used. The single MgF2 layer could be replaced with a layer of either SiO2 or Al2O3 as indicated. Also other similar coatings such as GdF3 or A1F3 could be used. Preferably, the total thickness of the protective layer or layers is less than 10% of the width of the reflecting face of the grating. However, thicknesses outside these ranges may be specified. It is most important that good coatings be applied to the surface which will be exposed to the intense ultraviolet light. For the grating shown in FIGS. 2 and 3, that surface is the short, 3.5 micron surface. The test results discussed above were obtained using a wavelength selecting module containing a three-prism beam expander, and a beam angle adjusting mirror along with the overcoat material diffraction grating arranged in a Littrow configuration. However, persons skilled in the art will recognize many other applications for gratings fabricated according to the present invention. Therefore, the appended claims are to encompass within their scope all such changes and modifications as fall within the true spirit and scope of this invention.

Claims

CLAIMS What is claimed is:
1. A process for coating a replica of a diffraction grating defining a grating surface having grooves defining reflective faces, said process comprising:
A. placing said replica in a vacuum chamber and reducing the chamber pressure to below 10"6 torr; and
B. while maintaining chamber pressure below 10" torr, depositing on said grating surface at least one overcoat reflector layer of aluminum;
C. while maintaining chamber pressure below 10"6 torr, depositing on said overcoat layer of aluminum a protective layer comprising one or more layers of material transparent to 193nm ultraviolet light;
D. installing said replica in a gas discharge laser producing laser radiation at wavelengths of about 193 nm or less than 193 mm;
2. The process of Claim 1 wherein said overcoat layer of aluminum on said reflective face is between 200nm and 50nm thick.
3. The process of Claim 1 wherein each of said reflective faces define a width and said protective layer on said reflective face has a thickness of less than 10% of said width.
4. The process of Claim 1 wherein each of said reflective faces define a width and said protective layer on said reflective face has a thickness of less than 5% of said width.
5. The process of Claim 3 wherein said protective layer on at least one set of surfaces is about 150 nm thick and said aluminum layer is about 100 nm thick.
6. The process as in Claim 1 wherein said chamber pressure is below 5 x 10"7 torr.
7. The process as in Claim 1 wherein the chamber pressure is continuously maintained below 10"6 torr during steps A, B and C.
8. The process as in Claim 7 wherein both of said depositing steps are accomplished using an electron beam sputtering technique.
9. The process as in Claim 6 wherein both of said depositing steps are accomplished using a vapor deposition technique.
10. A process as in Claim 1 wherein said material transparent to 193nm ultraviolet light material is chosen from a group consisting of MgF2, Al2O3, SiO2, CaF , A1F3 and GdF3.
11. A process as in Claim 1 wherein said protective layer comprises a single layer of MgF2.
12. A process as in Claim 1 wherein said protective layer is a single layer of SiO2.
13. A process as in Claim 1 wherein said protective layer is Al2O3.
14. A process as in Claim 1 wherein said protective layer is MgF2 about 24 nm thick.
15. A process as in Claim 1 wherein said protective layer is MgF2 about 90 nm thick.
16. A process as in Claim 1 wherein said protective layer is SiO about 20 nm thick.
17. A process as in Claim 1 wherein said protective layer is S^ about 80 nm thick.
18. A process as in Claim 1 wherein said protective layer is Al2O about 14 nm thick.
19. A process as in Claim 1 wherein said protective layer is Al2O3 about 64 nm thick.
20. A process as in Claim 1 wherein said protective layer is two layers comprising MgF2 and Al2O3.
21. A process as in Claim 1 wherein said protective layer is two layers comprising S^ and Al2O3.
22. A process as in Claim 1 wherein said protective layer is four layers comprising a first MgF2 layer, a first Al O3 layer, a second MgF layer and a second layer of Al2O3.
23. A process as in Claim 1 wherein said protective layer is four layers comprising a first S;ιθ2 layer, a first Al2O3 layer, a second S^ layer and a second Al2O3 layer.
24. A process as in Claim 1 wherein said protective layer comprises a layer of MgF2 about 24 nm thick and an Al2O layer about 26 nm thick.
25. A process as in Claim 1 wherein said protective layer comprises a first layer of MgF2 about 22 nm thick, a second layer of Al2O3 about 26 nm thick, a third layer of MgF2 about 34 nm thick and a fourth layer of Al2O3 about 26 nm thick.
26. An overcoat protected diffraction grating having a large number of parallel grooves, each groove having a reflective face, said grating comprising:
A. a rigid substrate;
B. an aluminum grating layer comprising a very large number of parallel grooves; C. an adhesive layer affixing said aluminum grating layer to said rigid substrate;
D. at lease one thin aluminum reflective overcoat layer overcoating said aluminum grating layer, said aluminum overcoat layer having a thickness of less than 200 nm on said reflective faces;
E. a protective layer comprised of one or more layers of material transparent to 193nm ultraviolet light, overcoating said aluminum overcoat layer;
wherein said protective layer or layers have a thickness or thicknesses chosen to increase normal reflectivity of said reflecting face of each groove.
27. A grating as in Claim 26 wherein said large number of parallel grooves define a cross section approximately triangular in shape.
28. A grating as in Claim 27 wherein said grooves are spaced apart by about 11.7966 microns.
29. A grating as in Claim 26 wherein said protective layer is comprised of a first layer of MgF2 about 22 nm thick, a second layer of Al O3 about 26 nm thick, a third layer of MgF2 about 35 nm thick and a fourth layer of Al2O3 about 26 nm thick.
30. A grating as in Claim 26 wherein said protective layer is configured to produce a phase shift in 193 nm ultraviolet light of an integral number of 2π.
31. A grating as in Claim 26 wherein said material transparent to 193 nm ultraviolet light is chosen from a group consisting of MgF2, Al2O3, SiO , CaF2, A1F3 and GdF3.
32. A line narrowing module for an ArF laser comprising:
A. a prism beam expander for expanding a laser beam produced by said ArF laser; B. an overcoat protected diffraction grating having a large number of parallel grooves, each groove having a reflective face, said grating comprising:
1. a rigid substrate;
2. an aluminum grating layer comprising a very large number of parallel grooves;
3. an adhesive layer affixing said aluminum grating layer to said rigid substrate;
4. at least one thin aluminum overcoat reflecting layer overcoating said aluminum grating layer, said aluminum overcoat layer having a thickness of less than 200 nm on said reflective faces;
5. a thin protective layer overcoating said aluminum overcoat layer, said protective layer being comprised of one or more layers of a material or materials chosen from a group consisting of MgF2, CaF2, A1F3, SiO2 and Al2O3;
C. a beam angle adjustment means for adjusting directions of said laser beam relative to said grating in order to select a narrow wavelength for amplification by said laser;
wherein said protective layer or layers have a thickness or thicknesses chosen to increase normal reflectivity of said reflecting face of each groove.
33. A process as in Claim 32 wherein said first protective layer is MgF2 or CaF2 and further comprising a second protective layer deposited on top of said first protective layer, said second protective layer being comprised of a material chosen from a group consisting of SiO2, Al2O3 and A1F3.
34. A line narrowing module as in Claim 32 wherein said protective layer is configured to produce a phase shift in 193 nm ultraviolet light of an integral number of 2π.
PCT/US2001/046667 2000-12-07 2001-11-07 Protective overcoat for replicated diffraction gratings WO2002045475A2 (en)

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EP01987291A EP1340106B1 (en) 2000-12-07 2001-11-07 Protective overcoat for replicated diffraction gratings
DE60132355T DE60132355T2 (en) 2000-12-07 2001-11-07 PROTECTIVE OVERLAY FOR REPLICATED LOAD GRIDS
AU2002239525A AU2002239525A1 (en) 2000-12-07 2001-11-07 Protective overcoat for replicated diffraction gratings
JP2002547276A JP4549019B2 (en) 2000-12-07 2001-11-07 Protective film for replicated diffraction gratings

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US09/731,938 2000-12-07
US09/731,938 US6529321B2 (en) 1997-09-29 2000-12-07 Protective overcoat for replicated diffraction gratings
US09/910,362 2001-07-20
US09/910,362 US6511703B2 (en) 1997-09-29 2001-07-20 Protective overcoat for replicated diffraction gratings

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DE60132355D1 (en) 2008-02-21
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JP4549019B2 (en) 2010-09-22
WO2002045475A3 (en) 2002-10-10
TW548336B (en) 2003-08-21
EP1340106A4 (en) 2006-07-05
JP2004514794A (en) 2004-05-20
EP1340106A2 (en) 2003-09-03
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US6511703B2 (en) 2003-01-28
AU2002239525A1 (en) 2002-06-18

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