Method for transfer of a thin layer

Information

  • Patent Grant
  • 7960248
  • Patent Number
    7,960,248
  • Date Filed
    Tuesday, December 16, 2008
    16 years ago
  • Date Issued
    Tuesday, June 14, 2011
    13 years ago
Abstract
A method for transferring a thin layer from an initial substrate includes forming an assembly of the initial substrate with one face of a silicone type polymer layer, this face having been treated under an ultraviolet radiation, and processing the initial substrate to form the thin layer on the silicone type polymer layer.
Description
RELATED APPLICATIONS

The present patent document claims the benefit of priority to French Patent Application No. 07 59893, filed Dec. 17, 2007, which is incorporated herein by reference.


TECHNICAL DOMAIN AND PRIOR ART

The invention relates to the domain of thin layers, and particularly the domain of semiconducting materials.


In particular it relates to a technique for transferring a thin layer onto an easily removable host substrate, but with sufficient bonding energy between the thin layer and the substrate.


A fracture method, known under the name of Smart Cut™ is described in the article by A. J. Auberton-Hervé et al. “Why can Smart-Cut change the future of microelectronics?” that was published in International Journal of High Speed Electronics and Systems, Vol. 10, No. 1 (2000), p. 131-146.


This method is used in particular for making SOI (Silicon On Insulator) components or elements.


An SOI structure (FIG. 1C) comprises a stack composed of a support substrate 7 (for example made of silicon), a buried dielectric layer 8, for example silicon oxide or a nitride such as Si3N4 and a silicon layer 5, in which components may be located.


The buried layer 8 forms an insulation from parasite currents and charges originating from ionised particles. It thus enables good insulation of adjacent components made in the same silicon layer and a particularly significant reduction in parasite capacitances between such adjacent components, and insulation of the thin layer 5 made of semiconducting material from the subjacent support 7.



FIGS. 1A to 1C show an example implementation of a layer transfer method using the Smart Cut™ method in order to make an SOI structure. These figures are sectional views.



FIG. 1A shows a silicon substrate 1 provided with a surface oxide layer 8, during an ionic or atomic implantation step 3 of one or several gaseous species through the face 2 of this substrate. A buried layer 4 forming a weakened zone is then formed separating the substrate 1 into two parts: a thin layer 5, located between the implanted face 2 and the weakened zone 4 and the remaining part 6 of the substrate located under the weakened zone 4.



FIG. 1B shows a step in fixing the layer 5 of the substrate 1, through its face 2, onto a support substrate 7 or a stiffener. This fixing may be obtained by direct bonding (also called molecular bonding).



FIG. 1C shows the result of a step induced by a thermal and/or mechanical effect, to separate the thin layer 5 and the remaining part 6 (not shown) of the substrate 1 along the weakened zone 4. The result that can be obtained is a silicon on insulator (SOI) type of structure. As a variant, this structure could be obtained by molecular bonding of a silicon substrate (possibly oxidised on the surface) and a host substrate (also possibly covered with an oxide layer on the surface) and mechanical-chemical thinning of the silicon substrate.


These techniques are not limited to the production of a silicon on insulator substrate, but may be more generally applied to production of a “semiconductor on insulator” structure. In particular, apart from silicon, this concerns germanium, gallium nitride, silicon carbide, gallium arsenide and indium phosphate.


Substrate 7 keeps the previous two thin layers 5, 8 stacked together to create the final structure. It must be sufficiently rigid to facilitate fracture in the case of the Smart Cut process in the implantation zone 4 of the substrate 1, rather than the occurrence of blisters on the surface of the structure. Similarly, bonding between the two substrates (1,7) must be sufficiently strong to prevent any separation at this bonding interface, particularly during application of the fracture heat treatment in the case of the Smart Cut process and to enable mechanical-chemical thinning.


In most cases, the bond of the detached film 5 on its new support 7 is permanent. This is the case particularly for SOI made by previously described techniques.


But in some cases, a double transfer of the layer 5 is required. For example, it might be desirable for the free surface 5′ of the thin layer 5 to form a buried surface after the double transfer. In other words, the transfer described above with reference to FIGS. 1A-1C is then temporary, and an additional transfer step is made, the face 5′ of the layer 5 being fixed to another substrate and the substrate 7 being eliminated.


This is the case particularly for polar materials for example such as SiC or GaN. When a thin film 5 of this material is to be transferred to a second support, there is a need once again to separate this thin film from the first transfer substrate 7 (or temporary support), after having bonded it onto a new substrate through its free face 5′, or before bonding it onto this new substrate.


In order to easily separate the substrate 7, it would be useful to have a low bonding energy between this substrate and the thin layer 5. But as described previously, such energy is not always compatible with the thinning method used to obtain the thin film. Furthermore, a double transfer cannot be made using flexible supports because:

    • they are too soft and they deform during the thinning method,
    • or they are thermodeformable or thermodegradable and do not resist temperatures imposed by the fracture method without softening or degrading, and therefore they no longer retain the rigidity necessary for the method.


Furthermore, it is impossible to increase the rigidity of such flexible materials using an oxide deposited on it, because the differences in the coefficients of expansion between this material and the deposited oxide are such that the deposited oxide is stressed and ripples appear on the surface of said material, which increases the roughness and prevents bonding.


Therefore, the problem that arises is to find a host substrate that is sufficiently rigid to obtain a thin layer by thinning (mechanical-chemical or Smart Cut) of an initial substrate that can easily be removed.


SUMMARY

The invention relates to a method for bonding a substrate to be thinned onto a temporary easily removable support, but that is capable of producing the thinning method in question.


A transfer onto a host or temporary substrate takes place by bonding an initial substrate onto the host substrate and then thinning the initial substrate to obtain the required thin layer. Thinning may be mechanical-chemical thinning, or it may be the result of a fracture method like that known under the name Smart Cut™.


The invention relates to a method for transferring a thin film from an initial substrate, for example made of semiconducting material, comprising the following steps:

    • a) assembly by direct bonding of the initial substrate with a face of a silicone type polymer layer, this face having been treated under ultraviolet radiation,
    • b) thinning of the initial substrate to form the thin layer.


The invention can be used to create a thick oxide, for example between 10 μm and 20 μm thick, on the surface of the polymer, after UV treatment of the polymer. After direct bonding, this oxide creates a strong and rigid assembly between the polymer and the initial substrate compatible with the thinning step of this substrate, either using a substrate fracture technique of the Smart Cut™ type (without applying temperatures beyond the temperature at which the polymer is stable) or by mechanical and/or chemical thinning. Simultaneously, this oxide makes the polymer sufficiently rigid so that this thinning can be done.


Thinning may be done by mechanical and/or chemical polishing.


As a variant, it can be done by creating a buried fragile zone in the initial substrate before the assembly step a) by the implantation of ionic and/or atomic species delimiting the thin layer to be transferred in this initial substrate, and application of a heat and/or mechanical fracture treatment of the initial substrate along the buried fragile zone after the assembly step a).


Advantageously, the thin layer is transferred onto another substrate called the transfer substrate.


Therefore, the invention relates particularly to a method for transferring a thin layer from an initial substrate, for example made of a semiconducting material, onto a transfer substrate for example a final substrate, this method comprising the following steps:

    • a) creation of a buried fragile zone in the initial substrate by the implantation of ionic and/or atomic species, delimiting the thin layer to be transferred in this substrate,
    • b) assembly of this initial substrate with a face of a silicone type polymer layer, this face having been subjected to a treatment under ultraviolet radiation,
    • c) fracture of the initial substrate along the buried fragile zone, to leave the layer to be transferred on the silicone type polymer layer,
    • d) transfer of the layer onto the transfer substrate.


The invention also relates to a method for making a transfer of a thin layer of a first substrate to a second substrate, also called the transfer substrate, comprising:

    • a first transfer of said layer onto a temporary substrate made of silicone material treated on the surface by a UV radiation,
    • a second transfer of said layer, from the temporary substrate made of a silicone material onto the second substrate,
    • a temporary substrate peeling step.


The first transfer may take place by assembly by direct bonding of the first substrate with the face of the temporary substrate treated under UV. A thinning can then take place by mechanical and/or chemical polishing. As a variant, it may be done by creating a buried fragile zone in the first substrate by the implantation of ionic and/or atomic species, delimiting the thin layer to be transferred in this substrate, and the application of a heat and/or mechanical fracture treatment of the first substrate along the buried fragile zone.


According to the invention, regardless of the embodiment, the polymer used as a temporary or support substrate has been treated under ultraviolet radiation, which has the advantages already described above (particularly the formation of a thick oxide, which then results in a strong rigid assembly).


A temporary bonding is then made on this support or temporary substrate that can subsequently be easily separated.


Regardless of the planned embodiment, the transfer substrate or the second substrate may be made from a rigid material or from an elastic material, for example a silicone material not treated under UV.


After transferring onto the transfer substrate, or onto the second substrate, a step to peel all or some of the silicone type polymer may be done.


The peeling step of the polymer layer can induce a separation at the interface between the silicone and the silicone transformed into oxide, or in the silicone layer. In the latter case, a step could be included to chemically eliminate the residual polymer.


An additional step can be made to eliminate the part of the polymer transformed into oxide.


Advantageously, the treatment of the polymer layer or the silicone layer under ultraviolet radiation is done under an ozone atmosphere.


For example, the silicone may be polymerised PDMS. Heat treatments may be used, particularly at low temperature or at temperatures below the silicone decomposition temperature. In particular, a fracture step may be applied by a thermal effect, along a plane of weakness or in a weakened zone, at a temperature lower than the silicone decomposition temperature.


A mechanical treatment can also be used, for example by insertion of a blade or by bending or imposing a curvature for stressing, to participate firstly in the separation of the thin film bonded to the silicone, and secondly the remaining initial substrate.


Before the assembly step, a preliminary weakening annealing can be performed to limit the thermal and/or mechanical budget necessary to obtain the fracture after the assembly.


Prior to the assembly step, and possibly before the implantation step, a step may be included to deposit an oxide layer or a nitride layer on the initial substrate.


The material from which the layer to be transferred is made may be semiconducting, for example Si or Germanium or SiC or GaN.





BRIEF DESCRIPTION OF THE DRAWINGS


FIGS. 1A to 1C show a layer transfer method,



FIGS. 2A to 2F show an example of a method according to the invention,



FIG. 3 shows the chemical structure of the PDMS, a silicone type polymer that can be used in the framework of the invention.





DETAILED DESCRIPTION

We will now describe the invention in the case of a substrate or layer made of polydimethylsiloxane (PDMS) . But it can be done with any silicone type polymer, these polymers presenting a chain based on Si—O—Si—O that can be transformed into oxide under the effect of UV radiation.



FIG. 3 shows the chemical formula of PDMS. PDMS polymerises by polyaddition, in other words by a chain reaction with combination of monomer, the reaction taking place by means of a cross-linking agent. The reaction between the polymer and the cross-linking agent occurs under the action of a catalyst (contained in the cross-linking agent) and heat or the drying time, in accordance with the following scheme:




embedded image


This polymerisation method does not generate any derivatives (water, releases of gases, etc.), which makes the polymer compatible with the microelectronics. The catalyst is disinhibited under the action of heat. Thus, the PDMS can be polymerised at different temperatures from ambient temperature up to 150° C. The polymerisation time is longer when the temperature is lower. For example, the polymerisation time at 150° C. is 15 minutes, whereas at ambient temperature it is 7 days. PDMS can be deposited on the surface of the material in a layer several millimeters thick and is therefore easily manipulated.


The presence of covalent bonds between silicon and oxygen results in silicones having a higher decomposition temperature than other polymers. Thus, PDMS remains stable at between −50° C. and 250° C.


PDMS is naturally hydrophobic after polymerisation (a contact angle θ greater than 90° can be measured) due to its CH3 terminations


In order to make hydrophilic bonding, which is required in the case of the required transfer layer, an attempt will be made to bond the two surfaces with (OH) terminations.


PDMS has the special feature that it becomes hydrophilic on the surface under the influence of the different treatments, such as a plasma treatment or a UV/Ozone treatment.



FIG. 2A shows a substrate 20 made from this PDMS polymer material. A UV treatment 22 is applied to this substrate (for example under an ozone atmosphere), which in particular changes the hydrophobic properties of PDMS into hydrophilic properties. Silicone reacts to form free radicals under the effect of UV radiation and form SiOx bonds as illustrated below:




embedded image


Therefore, an oxide film 25 is formed on the surface of the substrate 20 (FIG. 2B) . The thickness of this SiOX film 25 can reach 10 μm or even 20 μm depending on the exposure time. This layer or this film 25 is rigid, while the material subjacent to this layer keeps the flexible properties of the initial polymer.


It will be noted that this layer or this film 25 is the result of a transformation of the polymer, and not the production of a deposit on the polymer. This thus avoids all problems related to the difference between coefficients of thermal expansion of the polymer and an oxide layer, when the oxide layer is simply deposited on the polymer.


As indicated above, other treatments of the polymer can be applied to obtain a hydrophilic layer 25. This is the case of a treatment by an oxygen plasma. Such a plasma treatment can cause the appearance of Si—OH groups that are substituted for Si—CH3 groups on the surface of the PDMS. This modification of the PDMS structure takes place over a thickness that can be as much as 130 to 160 nm and which makes it particularly hydrophilic (angle of contact less than 3°). Furthermore, for a treatment applied with oxygen plasma, the reaction is faster than under UV (20 s to reach an angle of 3° under a plasma compared with 60 min in the case of a treatment under UV) . But this plasma treatment is not permanent and the hydrophilic nature of the surface changes after 45 min. Therefore, treatment under UV has the advantage that it makes the surface hydrophilic more permanently than treatment under oxygen plasma. Finally, an AFM analysis of the polymer surface after plasma treatment shows the presence of ripples, such that this surface is rough and prevents hydrophilic bonding.


Unlike plasma treatment, exposure to UV enables a more durable transformation than a plasma treatment, does not create these ripples on the surface, and therefore does not create any roughness.


A measurement made on the surface of a PDMS substrate 25 shows that its roughness is:

    • 1) 17.8 nm after plasma treatment,
    • 2) while it is 0.57 nm after treatment under UV, therefore equivalent to the roughness after polymerisation.


Bonding can then be done on the polymer substrate 25 to which the UV treatment mentioned above had been applied.


As mentioned above, the superficial portion 25 of the substrate 20 is rigid. Therefore, a stiffener (the oxide layer) is obtained on the surface of the polymer after the treatment has been applied, which is favourable for a subsequent thinning method, for example to produce a Smart Cut™ type method.


Nevertheless, it is important to emphasize that the PDMS substrate 20 maintains some elasticity due to its non-oxidized part.


Furthermore, a substrate 1 can be implanted or have been implanted as explained above with reference to FIG. 1A. For example, it may be a semiconducting substrate of Silicon or Germanium or GaN, or SiC or even LTO (LiTaO3) . Such a substrate may for example be implanted with a hydrogen beam at doses of between 5×1016 at/cm3 and a few 1017 at/cm3 for example 5×1017 at/cm3 or 1018 at/cm3, and with an energy of the order of 50 keV to 200 keV, for example between 70 keV to 180 keV.


Advantageously, a thin layer 8 of oxide (or nitride, for example SiON), that is a few nm thick for example 5 nm to about 1 μm, will have been deposited before implantation. This oxide will make polishing possible if the roughness of the semiconducting surface 1 is high, or prepare the surface for bonding with preparations such as the plasma treatment or mechanical-chemical polishing or a wet treatment, these treatments having the purpose of leaving the surface hydrophilic.


A weakening heat treatment is possible at this stage, the thermal budget of this step not introducing any blister on the surface of the substrate, which would prevent any subsequent bonding.


The surface of the PDMS substrate 20, treated as explained above, and the surface 2 of an implanted semiconducting substrate 1 of the type shown in FIG. 1A (possibly provided with a layer 8 as explained above) can then be brought into contact (FIG. 2C). Bonding is of the direct bonding or molecular bonding type, a bonding technique that is described particularly by Q. Y. Tong in “Silicon Wafer Bonding Technology for VLSI and MEMS applications”, edited by S. S. Iyer and A. J. Auberton—Hervé, 2002, INSPEC, London, Chapter 1, pages 1-20.


A solidarisation annealing of the bonding can then be applied, for example at between 100° C. and 200° C. The duration of this annealing is between a few minutes and a few hours. This annealing is done with a thermal budget, and therefore at a temperature and for a duration such that it does not cause any blistering or cleavage conditions in the semiconductor 1.


The next step can be annealing of the fracture, for example between 200° C. and 250° C., assisted or not assisted by mechanical treatment (insertion of the blade, and/or bending or imposing a curvature of semiconductor 1 for stressing, etc.). The PDMS remains stable within this temperature range. The result is then a thin semiconducting layer 5 on the surface of the PDMS substrate 20 (FIG. 2D).


As a variant, the thin layer 5 may be obtained by a mechanical-chemical thinning step of the non-implanted substrate 1 after assembly with the surface hardened polymer layer, instead of by implantation/fracture as described above.


Regardless of the method used, the layer 5 can then be transferred and bonded onto a support 30 (FIG. 2E), by a hydrophilic or hydrophobic type of molecular bonding. This support 30 may be a final support.


The next step can then be peeling of the polymer substrate 20 (FIG. 2F). The high elasticity of the PDMS substrate 20 (that it retained in its part not transformed into oxide) will enable this retraction operation by peeling. This peeling is easier if the substrate 20 is thick. For example, a thickness of a few mm, for example between 1 mm and 3mm or 3 mm, enables manual retraction.


During this retraction by peeling operation, the rupture can take place at the interface between the non-transformed polymer and the polymer transformed into oxide, in which case it is an adhesive rupture.


Or the rupture may take place within the polymer 20, in its non-transformed part, and it is then a cohesive rupture. In this case, the remainder of the layer 20 of non-transformed polymer can then be removed chemically, for example by means of a Tetra-n-butylammonium fluoride solution, 1M solution in Tetrahydrofuran (TBAF). This solution dissolves the PDMS. The etching rate of this solution is estimated at 3 μm/min.


The polymer layer 25 transformed into an oxide can also be eliminated in turn, for example by an HF treatment or selective etching.


The substrate 30 may itself have some stiffness. In this case, this substrate may be a final substrate.


As a variant, this substrate 30 can also have some flexibility, for example to enable stress relaxation in the transferred layer or film 5; in this case, it is not a final substrate. In particular, it may be a silicone substrate, for example also made of PDMS but not treated under UV.


In one example embodiment, the PDMS used is Sylgard 184 made by Dow Corning. It is composed of a monomer and a thermal primer.


The primer is mixed in the proportion 1:10. The mix generates air bubbles that are removed by placing the mix under a vacuum (10−1 bars) . The polymer can then be conditioned for 2 h before the beginning of polymerisation. The mix is then poured into moulds and polymerised at ambient temperature to prevent stresses that could develop during cooling after polymerisation at high temperature, due to its high coefficient of thermal expansion.


The result obtained is then a PDMS support 20 with a thickness between a few μm and a few mm, for example between firstly 1 μm or 5 μm or 10 μm, and secondly 1 mm or 5 mm or 10 mm. This support can be left bonded on the plate that was used as a mould or it can be separated from this plate.


The PDMS support is then treated under UV (advantageously under an ambient atmosphere, the UV radiation then transforming oxygen in the air into ozone: this treatment is referred to as UV/Ozone). The next step is to transform the surface of the PDMS substrate 20 into an oxide over a thickness of between 1 μm and 15 μm, for a treatment duration of between 20 or 30 minutes and 120 minutes. The result is then a PDMS support with a surface stiffened by a transformation, which results in a high oxide thickness.


The semiconducting substrate 1 for which a thin layer 5 is to be transferred (FIG. 1A) is implanted with gaseous species 3 such as hydrogen and/or helium that enable production of the “Smart Cut™” method.


Example implantations, energies and doses have already been given above.


Advantageously, implantation conditions are chosen that enable cleavage at a temperature below 250° C., the PDMS decomposition temperature, for example as can be done by co-implantations of hydrogen and helium ions at the doses mentioned above.


Preferably, a fairly deep implantation will be made in the material to add the stiffness of the layer to the stiffness of the oxide created to facilitate the cleavage.


Advantageously, the material 1 can be implanted as described above and pre-weakened by applying preliminary annealing to it, to obtain cleavage at a temperature of below 250° C. This annealing leads to the creation of a fragile zone, but cleavage is not initiated.


Bonding can then be done between the PDMS treated surface 20 and the semiconducting surface 1 or the layer 8 deposited on this surface, and then the substrate 1 can then be thinned, in this case by fracture by means of a heat treatment (that may or may not be assisted by a mechanical treatment). The thin layer obtained can then be transferred onto a final substrate, the PDMS layer being eliminated by peeling.

Claims
  • 1. A preparation method for the transfer of a thin layer from an initial substrate, the method comprising the following steps: a) treating one face of a silicone type polymer layer by ultraviolet radiation, to transform the surface of the polymer into an oxide layer,b) directly bonding the initial substrate with the surface of the polymer layer, andc) processing the initial substrate to form the thin layer on the silicone type polymer layer.
  • 2. The method according to claim 1, wherein processing the initial substrate comprises mechanical or chemical polishing, or both.
  • 3. The method according to claim 1, further comprising creating a buried fragile zone in the initial substrate before step a), by implanting ionic or atomic species, or both, thereby delimiting the thin layer in the initial substrate, and wherein processing the initial substrate comprises applying a heat or mechanical fracture treatment, or both, to the initial substrate along the buried fragile zone.
  • 4. The method according to claim 3, wherein applying the fracture treatment comprises applying a thermal treatment at a temperature below the silicone decomposition temperature.
  • 5. The method according to claim 3 further comprising applying a weakening preliminary annealing before step b).
  • 6. A method for transferring a thin layer comprising a preparation method according to claim 1, and further comprising a transferring the thin layer onto a transfer substrate.
  • 7. The method according to claim 6, wherein the transfer substrate comprises a silicone material.
  • 8. The method according to claim 6, further comprising a step of peeling the silicone type polymer layer after transferring the thin layer onto the transfer substrate.
  • 9. The method according to claim 8, wherein the peeling induces a separation at interface between the silicone type polymer layer and the oxide layer.
  • 10. The method according to claim 9, wherein the peeling induces a separation in the silicone type polymer layer.
  • 11. The method according to claim 10, further comprising a step of chemically eliminating residual silicone.
  • 12. The method according to claim 9, further comprising eliminating remaining portions of the oxide layer.
  • 13. The method according to claim 1, wherein the silicone type polymer layer comprises polydimethylsiloxane (PDMS).
  • 14. The method according to claim 1, wherein treating by ultraviolet radiation comprises treating under an ozone atmosphere.
  • 15. The method according to claim 1 further comprising applying a mechanical treatment to participate firstly in the separation of the thin layer bonded to the silicone type polymer layer, and secondly the remaining initial substrate.
  • 16. The method according to claim 15, wherein applying the mechanical treatment comprises inserting a blade or a curve for stressing.
  • 17. The method according to claim 1 further comprising a step of depositing an oxide layer or a nitride layer on the initial substrate before step a).
  • 18. The method according to claim 1, wherein the thin layer comprises a semiconducting material.
  • 19. The method according to the claim 18, wherein the thin layer comprises Si, Germanium, SiC, or GaN.
Priority Claims (1)
Number Date Country Kind
07 59893 Dec 2007 FR national
US Referenced Citations (192)
Number Name Date Kind
3901423 Hillberry et al. Aug 1975 A
3915757 Engel Oct 1975 A
3957107 Altoz et al. May 1976 A
3993909 Drews et al. Nov 1976 A
4006340 Gorinas Feb 1977 A
4028149 Deines et al. Jun 1977 A
4039416 White Aug 1977 A
4074139 Pankove Feb 1978 A
4107350 Berg et al. Aug 1978 A
4108751 King Aug 1978 A
4121334 Wallis Oct 1978 A
4170662 Weiss et al. Oct 1979 A
4179324 Kirkpatrick Dec 1979 A
4244348 Wilkes Jan 1981 A
4252837 Auton Feb 1981 A
4254590 Eisele et al. Mar 1981 A
4274004 Kanai Jun 1981 A
4324631 White et al. Apr 1982 A
4346123 Kaufmann Aug 1982 A
4361600 Brown Nov 1982 A
4368083 Bruel et al. Jan 1983 A
4412868 Brown et al. Nov 1983 A
4452644 Bruel et al. Jun 1984 A
4468309 White Aug 1984 A
4471003 Cann Sep 1984 A
4486247 Ecer et al. Dec 1984 A
4490190 Speri Dec 1984 A
4500563 Ellenberger et al. Feb 1985 A
4508056 Bruel et al. Apr 1985 A
4536657 Bruel Aug 1985 A
4539050 Kramler et al. Sep 1985 A
4542863 Larson Sep 1985 A
4566403 Fournier Jan 1986 A
4567505 Pease Jan 1986 A
4568563 Jackson et al. Feb 1986 A
4585945 Bruel et al. Apr 1986 A
4630093 Yamaguchi et al. Dec 1986 A
4684535 Heinecke et al. Aug 1987 A
4704302 Bruel et al. Nov 1987 A
4717683 Parrillo et al. Jan 1988 A
4764394 Conrad Aug 1988 A
4837172 Mizuno et al. Jun 1989 A
4846928 Dolins et al. Jul 1989 A
4847792 Barna et al. Jul 1989 A
4853250 Boulos et al. Aug 1989 A
4887005 Rough et al. Dec 1989 A
4894709 Phillips et al. Jan 1990 A
4904610 Shyr Feb 1990 A
4920396 Shinohara et al. Apr 1990 A
4929566 Beitman May 1990 A
4931405 Kamijo et al. Jun 1990 A
4948458 Ogle Aug 1990 A
4952273 Popov Aug 1990 A
4956698 Wang Sep 1990 A
4960073 Suzuki et al. Oct 1990 A
4975126 Margail et al. Dec 1990 A
4982090 Wittmaack Jan 1991 A
4996077 Moslehi et al. Feb 1991 A
5013681 Godbey et al. May 1991 A
5015353 Hubler et al. May 1991 A
5034343 Rouse et al. Jul 1991 A
5036023 Dautremont-Smith et al. Jul 1991 A
5110748 Sarma May 1992 A
5120666 Gotou Jun 1992 A
5138422 Fujii et al. Aug 1992 A
5198371 Li Mar 1993 A
5200805 Parsons et al. Apr 1993 A
5232870 Ito et al. Aug 1993 A
5234535 Beyer et al. Aug 1993 A
5242863 Xiang-Zheng et al. Sep 1993 A
5250446 Osawa et al. Oct 1993 A
5256581 Foerstner et al. Oct 1993 A
5259247 Bantien Nov 1993 A
5300788 Fan et al. Apr 1994 A
5310446 Konishi et al. May 1994 A
5400458 Rambosek Mar 1995 A
5405802 Yamagata et al. Apr 1995 A
5413951 Ohori et al. May 1995 A
5494835 Bruel Feb 1996 A
5524339 Gorowitz et al. Jun 1996 A
5559043 Bruel Sep 1996 A
5567654 Beilstein, Jr. et al. Oct 1996 A
5611316 Oshima et al. Mar 1997 A
5618739 Takahashi et al. Apr 1997 A
5622896 Knotter et al. Apr 1997 A
5633174 Li May 1997 A
5661333 Bruel et al. Aug 1997 A
5714395 Bruel Feb 1998 A
5804086 Bruel Sep 1998 A
5811348 Matsushita et al. Sep 1998 A
5817368 Hashimoto Oct 1998 A
5854123 Sato et al. Dec 1998 A
5863830 Bruel et al. Jan 1999 A
5863832 Doyle et al. Jan 1999 A
5877070 Goesele et al. Mar 1999 A
5882987 Srikrishnan Mar 1999 A
5897331 Sopori Apr 1999 A
5909627 Egloff Jun 1999 A
5920764 Hanson et al. Jul 1999 A
5953622 Lee et al. Sep 1999 A
5966620 Sakaguchi et al. Oct 1999 A
5981400 Lo Nov 1999 A
5985412 Gösele Nov 1999 A
5993677 Biasse et al. Nov 1999 A
5994207 Henley et al. Nov 1999 A
6010591 Gösele Jan 2000 A
6013563 Henley et al. Jan 2000 A
6013954 Hamajima Jan 2000 A
6020252 Aspar et al. Feb 2000 A
6033974 Henley et al. Mar 2000 A
6048411 Henley et al. Apr 2000 A
6054363 Sakaguchi et al. Apr 2000 A
6054370 Doyle Apr 2000 A
6057212 Chan et al. May 2000 A
6071795 Cheung et al. Jun 2000 A
6096433 Kikuchi et al. Aug 2000 A
6103597 Aspar et al. Aug 2000 A
6103599 Henley et al. Aug 2000 A
6118181 Merchant et al. Sep 2000 A
6127199 Inoue Oct 2000 A
6146979 Henley et al. Nov 2000 A
6150239 Goesele et al. Nov 2000 A
6159323 Joly et al. Dec 2000 A
6190998 Bruel et al. Feb 2001 B1
6198159 Hosoma et al. Mar 2001 B1
6200878 Yamagata et al. Mar 2001 B1
6204079 Aspar et al. Mar 2001 B1
6225190 Bruel et al. May 2001 B1
6225192 Aspar et al. May 2001 B1
6271101 Fukunaga Aug 2001 B1
6294478 Shkaguchi et al. Sep 2001 B1
6303468 Aspar et al. Oct 2001 B1
6316333 Bruel et al. Nov 2001 B1
6323108 Kub et al. Nov 2001 B1
6323109 Okonogi Nov 2001 B1
6346458 Bower Feb 2002 B1
6362077 Aspar et al. Mar 2002 B1
6362082 Doyle et al. Mar 2002 B1
6417075 Haberger et al. Jul 2002 B1
6429094 Maleville et al. Aug 2002 B1
6513564 Bryan et al. Feb 2003 B2
6534380 Yamauchi et al. Mar 2003 B1
6593212 Kub et al. Jul 2003 B1
6596569 Bao et al. Jul 2003 B1
6607969 Kub et al. Aug 2003 B1
6632082 Smith Oct 2003 B1
6645831 Shaheen et al. Nov 2003 B1
6645833 Brendel Nov 2003 B2
6653207 Ohya et al. Nov 2003 B2
6727549 Doyle Apr 2004 B1
6756285 Moriceau et al. Jun 2004 B1
6756286 Moriceau et al. Jun 2004 B1
6764936 Daneman et al. Jul 2004 B2
6770507 Abe et al. Aug 2004 B2
6774010 Chu et al. Aug 2004 B2
6902987 Tong et al. Jun 2005 B1
6946365 Aspar et al. Sep 2005 B2
6947365 Lai et al. Sep 2005 B2
6974759 Moriceau et al. Dec 2005 B2
7029548 Aspar et al. Apr 2006 B2
7052978 Shaheen et al. May 2006 B2
7476596 Lieber et al. Jan 2009 B2
7521292 Rogers et al. Apr 2009 B2
20010007367 Ohkubo Jul 2001 A1
20010007789 Aspar et al. Jul 2001 A1
20020025604 Tiwari Feb 2002 A1
20020083387 Miner et al. Jun 2002 A1
20020145489 Cornett et al. Oct 2002 A1
20020153563 Ogura Oct 2002 A1
20020185684 Campbell et al. Dec 2002 A1
20030077885 Aspar et al. Apr 2003 A1
20030108715 Roberds et al. Jun 2003 A1
20030119279 Enquist Jun 2003 A1
20030134489 Schwarzenbach et al. Jul 2003 A1
20030162367 Roche Aug 2003 A1
20030199105 Kub et al. Oct 2003 A1
20040009649 Kub et al. Jan 2004 A1
20040029358 Park et al. Feb 2004 A1
20040126708 Jing et al. Jul 2004 A1
20040144487 Martinez et al. Jul 2004 A1
20040171232 Cayrefoureq et al. Sep 2004 A1
20040209441 Maleville et al. Oct 2004 A1
20040222500 Aspar et al. Nov 2004 A1
20050029224 Aspar et al. Feb 2005 A1
20050042842 Lei et al. Feb 2005 A1
20050122845 Lizzi Jun 2005 A1
20060240275 Gadkaree Oct 2006 A1
20070020895 Moriceau et al. Jan 2007 A1
20070202660 Moriceau et al. Aug 2007 A1
20070259528 Moriceau et al. Nov 2007 A1
20080020547 Kostrzewa et al. Jan 2008 A1
20080271835 Di Cioccio et al. Nov 2008 A1
Foreign Referenced Citations (84)
Number Date Country
0 355 913 Feb 1990 EP
0 410 679 Jan 1991 EP
0 504 714 Sep 1992 EP
0 533 551 Mar 1993 EP
0 293 049 Sep 1993 EP
0 660 140 Jun 1995 EP
0 665 588 Aug 1995 EP
0 703 609 Mar 1996 EP
0 754 953 Jan 1997 EP
0 793 263 Sep 1997 EP
0 801 419 Oct 1997 EP
0 807 970 Nov 1997 EP
0 849 788 Jun 1998 EP
0 889 509 Jan 1999 EP
0 898 307 Feb 1999 EP
0 917 193 May 1999 EP
0 938 129 Aug 1999 EP
0 902 843 Mar 2000 EP
0 989 593 Mar 2000 EP
0 994 503 Apr 2000 EP
1 050 901 Nov 2000 EP
1 059 663 Dec 2000 EP
0 717 437 Apr 2002 EP
0 786 801 Jun 2003 EP
0 767 486 Jan 2004 EP
0 925 888 Nov 2004 EP
1 014 452 May 2006 EP
2 671 472 Jul 1992 FR
2 681 472 Mar 1993 FR
2 558 263 Jul 1995 FR
2 725 074 Mar 1996 FR
95 08882 Jun 1996 FR
2 736 934 Jan 1997 FR
2 748 850 Nov 1997 FR
2 748 851 Nov 1997 FR
2 758 907 Jul 1998 FR
2 767 416 Feb 1999 FR
2 767 604 Feb 1999 FR
2 771 852 Jun 1999 FR
2 773 261 Jul 1999 FR
2 774 510 Aug 1999 FR
2 781 925 Feb 2000 FR
2 796 491 Jan 2001 FR
2 797 347 Feb 2001 FR
2 809 867 Dec 2001 FR
2 819 099 Jul 2002 FR
2 855 910 Jun 2003 FR
2 847 075 May 2004 FR
2 861 497 Apr 2005 FR
2 895 562 Dec 2005 FR
2 211 991 Jul 1989 GB
53-104156 Sep 1978 JP
58 31519 Feb 1983 JP
59-54217 Mar 1984 JP
62265717 Nov 1987 JP
101004013 Jan 1989 JP
08017777 Jan 1990 JP
4199504 Jul 1992 JP
07-254690 Oct 1995 JP
7-302889 Nov 1995 JP
8133878 May 1996 JP
09-213594 Aug 1997 JP
09-307719 Nov 1997 JP
10163166 Jun 1998 JP
10233352 Sep 1998 JP
11045862 Feb 1999 JP
11074208 Mar 1999 JP
11087668 Mar 1999 JP
11-145436 May 1999 JP
11317577 Nov 1999 JP
128757 Jun 2000 RU
WO 9520824 Aug 1995 WO
WO 9908316 Feb 1999 WO
WO 9935674 Jul 1999 WO
WO 9939378 Aug 1999 WO
WO 0048238 Aug 2000 WO
WO 0063965 Oct 2000 WO
WO 0111930 Feb 2001 WO
WO 0143168 Jun 2001 WO
WO 0205344 Jan 2002 WO
WO 0247156 Jun 2002 WO
WO 02083387 Oct 2002 WO
WO 03013815 Feb 2003 WO
WO 2004044976 May 2004 WO
Related Publications (1)
Number Date Country
20090156016 A1 Jun 2009 US