Low dielectric (low k) barrier films with oxygen doping by plasma-enhanced chemical vapor deposition (PECVD)

Information

  • Patent Grant
  • 7157384
  • Patent Number
    7,157,384
  • Date Filed
    Wednesday, December 22, 2004
    20 years ago
  • Date Issued
    Tuesday, January 2, 2007
    18 years ago
Abstract
Methods are provided for depositing a silicon carbide layer having significantly reduced current leakage. The silicon carbide layer may be a barrier layer or part of a barrier bilayer that also includes a barrier layer. Methods for depositing oxygen-doped silicon carbide barrier layers are also provided. The silicon carbide layer may be deposited by reacting a gas mixture comprising an organosilicon compound, an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, and optionally, helium in a plasma. Alternatively, the silicon carbide layer may be deposited by reacting a gas mixture comprising hydrogen or argon and an organosilicon compound in a plasma.
Description
BACKGROUND OF THE INVENTION

1. Field of the Invention


Embodiments of the present invention generally relate to the fabrication of integrated circuits. More specifically, embodiments of the present invention generally relate to processes for depositing barrier layers on a substrate and structures that include the barrier layers.


2. Description of the Related Art


Semiconductor device geometries have dramatically decreased in size since such devices were first introduced several decades ago. Since then, integrated circuits have generally followed the two year/half-size rule (often called Moore's Law), which means that the number of devices that will fit on a chip doubles every two years. Today's fabrication plants are routinely producing devices having sub-quarter micron feature sizes, and tomorrow's plants soon will be producing devices having even smaller geometries.


In order to further reduce the size of devices on integrated circuits, it has become necessary to use conductive materials having low resistivity, such as copper, and insulators having low k (dielectric constant <4.0) to reduce the capacitive coupling between adjacent metal lines.


A barrier layer is typically deposited between subsequently deposited conductive materials and low k dielectric material to prevent diffusion of byproducts such as moisture onto the conductive materials. For example, moisture that can be generated during formation of a low k insulator readily diffuses to the surface of the conductive metal and increases the resistivity of the conductive metal surface.


A barrier layer can also be used to prevent diffusion of conductive materials. Low k dielectric materials are often porous and susceptible to interlayer diffusion of conductive materials, such as copper, which can result in the formation of short-circuits and device failure. A barrier layer is typically used in copper damascene structures to reduce or prevent interlayer diffusion.


Attempts have been made to deposit silicon carbide barrier layers by plasma enhanced chemical vapor deposition. However, silicon carbide barrier layers typically have had undesirable characteristics, such as unacceptable current leakage, and film instability, such as upon exposure to air. Silicon carbide layers doped with oxygen or nitrogen have shown some improvements in the areas of current leakage, compressive stress, and film stability. However, the nitrogen in nitrogen-doped silicon carbide layers can poison photoresist layers deposited on a substrate. The gases used to incorporate oxygen in oxygen-doped silicon carbide layers can oxidize underlying metal features on which the oxygen-doped silicon carbide layer is deposited.


Therefore, there remains a need for methods of depositing silicon carbide and oxygen-doped silicon carbide barrier layers with good chemical and mechanical properties.


SUMMARY OF THE INVENTION

Aspects of the invention generally provide methods for depositing a silicon carbide glue layer on a substrate, wherein the glue layer has improved current leakage without doping with oxygen or nitrogen. In one aspect, the invention provides a method for processing a substrate, including reacting a gas mixture comprising a carbon and silicon-containing compound and a member selected from the group of hydrogen, argon, and an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, such as ethylene, in a plasma and depositing a silicon carbide glue layer on the substrate. The gas mixture may also include helium.


In another aspect of the invention, a method is provided for depositing a barrier bilayer on a substrate, including reacting a gas mixture comprising an organosilicon compound, and a member selected from the group of hydrogen, argon, and an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, such as ethylene, in a plasma and depositing a silicon carbide glue layer on the substrate, reacting a second gas mixture in a plasma, and depositing an oxygen-containing silicon carbide barrier layer on the silicon carbide glue layer. In one embodiment, the oxygen-containing silicon carbide barrier layer may be deposited from a gas mixture comprising an organosilicon compound and an oxygen-containing gas having the formula CxHyOz, with X being from 0 to 2, Y being from 0 to 2, and Z being from 1 to 3, wherein X+Y is at least 1 and X+Y+Z is 3 or less. In another embodiment, the oxygen-containing silicon carbide barrier layer may be deposited from a second gas mixture comprising an organosilicon compound and an oxygen-containing compound having the general formula




embedded image



Optionally, the substrate may be pre-treated with a hydrogen plasma before the silicon carbide glue layer is deposited.


In another aspect of the invention, a method is provided for depositing a barrier bilayer on a substrate, including depositing a SiN or SiCN layer on the substrate, reacting a gas mixture in a plasma, and depositing an oxygen-containing silicon carbide barrier layer on the SiN or SiCN layer. The oxygen-containing silicon carbide barrier layer may be used as a cap layer on a SiN or SiCN layer. The oxygen-containing silicon carbide barrier layer may be deposited from a gas mixture comprising an organosilicon compound and an oxygen-containing gas having the formula CxHyOz, with X being from 0 to 2, Y being from 0 to 2, and Z being from 1 to 3, wherein X+Y is at least 1 and X+Y+Z is 3 or less. Optionally, the substrate may be pre-treated with a hydrogen plasma before the silicon carbide glue layer is deposited.


In yet another aspect, a method is provided for depositing a silicon carbide hard mask on a substrate, including reacting a gas mixture comprising an organosilicon compound and a member selected from the group of hydrogen, argon, and an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, such as ethylene, in a plasma and optionally depositing a second hard mask on the silicon carbide hard mask.





BRIEF DESCRIPTION OF THE DRAWINGS

So that the manner in which the above recited features of the present invention can be understood in detail, a more particular description of the invention, briefly summarized above, may be had by reference to embodiments, some of which are illustrated in the appended drawings. It is to be noted, however, that the appended drawings illustrate only typical embodiments of this invention and are therefore not to be considered limiting of its scope, for the invention may admit to other equally effective embodiments.



FIG. 1 is a cross-sectional view of a PRODUCER® chamber.



FIG. 2 is a cross-sectional view showing a device of an embodiment of the invention comprising a silicon carbide glue layer.



FIG. 3 is a cross-sectional view showing a device of an embodiment of the invention comprising a silicon carbide hard mask.





DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

Silicon Carbide Glue Layers


Aspects of the invention provide methods for depositing an oxygen-doped silicon carbide layer on a substrate. The oxygen-doped silicon carbide layer may be a layer that is underneath or below a photoresist layer on a substrate. The oxygen-doped silicon carbide layer may be a layer that is deposited on a silicon carbide glue layer, a SiN layer, or a SiCN layer.


Aspects of the invention provide methods for depositing a silicon carbide glue layer or a silicon carbide hard mask on a substrate. As defined herein, a “silicon carbide glue layer” or a “silicon carbide hard mask” is a silicon carbide layer having reduced current leakage in comparison to conventional silicon carbide layers that do not contain oxygen or nitrogen. The silicon carbide layers described herein have significant and unexpected improvements in current leakage.


The silicon carbide glue layer may serve as a complete barrier layer itself, or the silicon carbide glue layer may be part of a barrier bilayer that includes a barrier layer in addition to the silicon carbide glue layer. The silicon carbide glue layer may be deposited on the substrate from a gas mixture comprising an organosilicon compound. The organosilicon compound may have the formula SiHa(CH3)b(C2H5)c(C6H5)d, wherein a is 0 to 2, b is 0 to 4, c is 0 to 4. Alternatively, the organosilicon compound may have the general formula




embedded image



Alternatively, the organosilicon compound may have the general formula




embedded image



Preferably, the gas mixture does not include oxygen, nitrogen, or compounds with silicon-silicon bonds. Preferably, the gas mixture comprises trimethylsilane (TMS). The silicon carbide glue layer may be deposited on a surface of the substrate comprising part of a dielectric layer and part of a metal line disposed in the dielectric layer. The silicon carbide glue layers described herein are typically low k (k<4) layers.


In any of the embodiments or aspects described herein, the organosilicon compound used in the gas mixture to deposit the silicon carbide glue layer can be dimethylsilane, trimethylsilane, diethylsilane, diethylmethylsilane, disilanomethane, bis(methylsilano)methane, 1,2-disilanoethane, 1,2-bis(methylsilano)ethane, 2,2-disilanopropane, 1,3,5-trisilano-2,4,6-trimethylene, diphenylsilane, dimethylphenylsilane, diphenylmethylsilane, phenylmethylsilane, or combinations thereof.


In any of the embodiments or aspects described herein, a substrate upon which a silicon carbide glue layer described herein is deposited may be pre-treated with a hydrogen plasma. The pre-treatment with a hydrogen plasma may remove metal oxides, such as copper oxide, from the substrate surface. It was found that substrates including copper and pre-treated with a hydrogen plasma had a higher reflectivity than substrates including copper and pre-treated with an ammonia plasma. It is believed that the improved reflectivity is a result of removal of copper oxide from the substrate. The pre-treatment may be performed in the same chamber in which the silicon carbide glue layer is deposited. Hydrogen gas may be flowed into the chamber at a flow rate between about 300 sccm and about 1000 sccm. The substrate temperature may be between about 200° C. and about 400° C. The hydrogen gas may be reacted in the chamber at a pressure of between about 3 Torr and about 7 Torr. A RF power of between about 100 watts and about 600 watts may be applied in the chamber. The spacing between the gas distributor in the chamber and the substrate may be between about 200 mils and about 600 mils.


Methods of forming the silicon carbide glue layers described herein are preferably performed in a processing chamber adapted to deposit organosilican material while applying RF power. For example, a PRODUCER® chemical vapor deposition chamber, commercially available from Applied Materials, Inc., of Santa Clara, Calif. may be used. An example of a PRODUCER® Chamber is described in U.S. Pat. No. 5,555,681, which is incorporated by reference herein. A brief description of a PRODUCER® Chamber will be given with respect to FIG. 1.



FIG. 1 shows a cross sectional view of a chamber 100. The chamber 100 has processing regions 618 and 620. A heater pedestal 628 is movably disposed in each processing region 618, 620 by a stem 626 which extends through the bottom of the chamber body 612 where it is connected to a drive system 603. Each of the processing regions 618, 620 also preferably include a gas distribution assembly 608 disposed through the chamber lid 604 to deliver gases into the processing regions 618, 620. The gas distribution assembly 608 of each processing region also includes a gas inlet passage 640 which delivers gas into a shower head assembly 642.


The flow rates described herein for introducing gases into a plasma processing chamber are given with respect to the total processing area in a PRODUCER® chamber, i.e., both processing regions. Thus, the flow rates into each processing region of the PRODUCER® chamber are approximately half of the flow rates described herein.


In one aspect, a silicon carbide glue layer may be deposited on a substrate by reacting a gas mixture comprising an organosilicon compound, and an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, such as ethylene, and optionally, helium, in a plasma provided in a plasma processing chamber. Preferably, the organosilicon compound is trimethylsilane, and the aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond is ethylene (C2H4). A silicon carbide glue layer may be deposited in one embodiment by introducing into a plasma processing chamber an organosilicon compound at a flow rate between about 50 and about 300 sccm, and an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, at a flow rate between about 50 and about 500 sccm, such as between about 100 and about 500 sccm, and optionally, helium at a flow rate between about 0 and about 1000 sccm. Preferably, helium is introduced into the chamber at a flow rate of less than about 400 sccm. The gas mixture may be reacted in a plasma processing chamber at a pressure of between about 2 Torr and about 10 Torr, such as between about 2 and about 5 Torr. The substrate temperature may be between about 200° C. and about 400° C., such as between about 300° C. and about 400° C. A RF power of between about 100 watts and about 700 watts, such as between about 300 watts and about 700 watts, or between about 100 watts and about 600 watts, may be applied in a plasma processing chamber for processing 300 mm substrates. A RF power of between about 100 watts and about 700 watts, such as between about 100 watts and about 600 watts, may be applied in a plasma processing chamber for processing 200 mm substrates. The RF power can be provided at a high frequency such as between about 13 and about 14 MHz, such as 13.56 MHz. The gas mixture may be introduced into the chamber by a gas distributor that may be positioned between about 300 mils and about 500 mils from the substrate surface.


In another aspect, a silicon carbide glue layer may be deposited on a substrate by reacting a gas mixture comprising an organosilicon compound and a gas selected from the group of hydrogen and argon in a plasma provided in a plasma processing chamber. Preferably, the organosilicon compound is trimethylsilane. In one embodiment, a silicon carbide glue layer may be deposited by introducing into a plasma processing chamber an organosilicon compound at a flow rate between about 50 and about 350 sccm and hydrogen at a flow rate between about 100 and about 500 sccm. The gas mixture may be reacted in a plasma processing chamber at a pressure of between about 3 Torr and about 12 Torr. The substrate temperature may be between about 200° C. and about 400° C. A RF power of between about 200 watts and about 700 watts, preferably between about 300 watts and about 700 watts, may be applied in a plasma processing chamber for processing 300 mm substrates. A RF power of between about 200 watts and about 700 watts may be applied in a plasma processing chamber for processing 200 mm substrates. The RF power can be provided at a high frequency such as between about 13 and about 14 MHz, such as 13.56 MHz. In another embodiment, a silicon carbide glue layer may be deposited by introducing into a plasma processing chamber an organosilicon compound at a flow rate between about 50 and about 350 sccm and argon at a flow rate between about 100 and about 500 sccm. The gas mixture may be reacted in a plasma processing chamber. at a pressure of between about 3 Torr and about 12 Torr. The substrate temperature may be between about 200° C. and about 400° C. A RF power of between about 200 watts and about 700 wafts, preferably between about 300 watts and about 700 watts, may be applied in a plasma processing chamber for processing 300 mm substrates. A RF power of between about 200 watts and about 700 watts may be applied in a plasma processing chamber for processing 200 mm substrates. The RF power can be provided at a high frequency such as between about 13 and about 14 MHz.


Barrier Bilayers with Silicon Carbide Glue Layers


In another aspect, a barrier bilayer may be deposited on a substrate by first depositing a silicon carbide glue layer by reacting a gas mixture comprising an organosilicon compound, and an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, such as ethylene, and optionally, helium, in a plasma provided in plasma processing chamber, and then depositing a barrier layer on the substrate. Preferably, the organosilicon compound is trimethylsilane. In one example, the silicon carbide glue layer may be about 80 Å thick, and the barrier layer may be about 420 Å thick, resulting in a 500 Å barrier bilayer. A silicon carbide glue layer may be deposited in one embodiment by introducing into a plasma processing chamber an organosilicon compound at a flow rate between about 50 and about 300 sccm, an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, such as ethylene, at a flow rate between about 50 and about 500 sccm, such as between about 100 and about 500 sccm, and optionally, helium at a flow rate between about 0 and about 1000 sccm. Preferably, helium is introduced into the chamber at a flow rate of less than about 400 sccm. The gas mixture may be reacted in a plasma processing chamber at a pressure of between about 2 Torr and about 10 Torr, such as between about 2 and about 5 Torr. The substrate temperature may be between about 200° C. and about 400° C., such as between about 300° C. and about 400° C. A RF power of between about 100 watts and about 700 watts, such as between about 300 watts and about 700 watts, or between about 100 watts and about 600 watts may be applied in a plasma processing chamber for processing 300 mm substrates. A RF power of between about 200 watts and about 700 watts may be applied in a plasma processing chamber for processing 200 mm substrates. The RF power can be provided at a high frequency such as between about 13 and about 14 MHz, such as about 13.56 MHz. The gas mixture may be introduced into the chamber by a gas distributor that may be positioned between about 300 mils and out 500 mils from the substrate surface.


In another aspect, a barrier bilayer may be deposited on a substrate by first depositing a silicon carbide glue layer by reacting a gas mixture comprising an organosilicon compound and a gas selected from the group of hydrogen and argon in a plasma provided in a plasma processing chamber, and then depositing a barrier layer on the substrate. Preferably, the organosilicon compound is trimethylsilane. In one example, the silicon carbide glue layer may be about 80 Å thick, and the barrier layer may be about 420 Å thick, resulting in a 500 Å barrier bilayer. In one embodiment, a silicon carbide glue layer may be deposited by introducing into a plasma processing chamber an organosilicon compound at a flow rate between about 50 and about 350 sccm and hydrogen at a flow rate between about 100 and about 500 sccm. The gas mixture may be reacted in a plasma processing chamber at a pressure of between about 3 Torr and about 12 Torr. The substrate temperature may be between about 200° C. and about 400° C. A RF power of between about 200 watts and about 700 watts, preferably between about 300 watts and about 700 watts, may be applied in a plasma processing chamber for processing 300 mm substrates. A RF power of between about 200 watts and about 700 watts may be applied in a plasma processing chamber for processing 200 mm substrates. The RF power can be provided at a high frequency such as between about 13 and about 14 MHz, such as about 13.56 MHz. In another embodiment, a silicon carbide glue layer may be deposited by introducing into a plasma processing chamber an organosilicon compound at a flow rate between about 50 and about 350 sccm and argon at a flow rate between about 100 and about 500 sccm. The gas mixture may be reacted in a plasma processing chamber at a pressure of between about watts 3 Torr and about 12 Torr. The substrate temperature may be between about 200° C. and about 400° C. A RF power of between about 200 watts and about 700 watts, preferably between about 300 watts and about 700 watts, may be applied in a plasma processing chamber for processing 300 mm substrates. A RF power of between about 200 watts and about 700 watts may be applied in a plasma processing chamber for processing 200 mm substrates. The RF power can be provided at a high frequency such as between about 13 and about 14 MHz, such as about 13.56 MHz.


While a preferred thickness of the silicon carbide glue layers described herein in barrier bilayers is about 80 Å, other thickness of the silicon carbide glue layers may be used. For example, a silicon carbide layer of between about 50 Å and about 100 Å may be used. A desired thickness of the silicon carbide glue layer can be determined by exposing a substrate containing the silicon carbide glue layer over an underlying metal feature, such as copper, to a plasma containing oxygen. A change in the reflectivity of the metal indicates that the metal has been oxidized, and thus is not protected sufficiently by the glue layer. This minimum thickness of glue layer that results in substantially no change in the metal reflectivity can be selected as the desired thickness of the silicon carbide glue layer.


In embodiments in which the silicon carbide glue layer is part of a barrier bilayer that also includes a barrier layer, the barrier layer may be an oxygen-doped silicon carbide layer that contains no nitrogen or is substantially nitrogen free. The barrier layer may be deposited on the silicon carbide glue layer by reacting a gas mixture comprising an oxygen-containing compound and an organosilicon compound. The barrier layer may be deposited by reacting a gas mixture comprising an oxygen-containing organosilicon compound with an oxygen-free organosilicon compound. Suitable oxygen-free organosilicon compounds include methylsilane, dimethylsilane, trimethylsilane, ethylsilane, disilanomethane, bis(methylsilano)methane, 1,2-disilanoethane, 1,2-bis(methylsilano)ethane, 2,2-disilanopropane, and 1,3,5-trisilano-2,4,6-trimethylene. Suitable oxygen-containing organosilicon compounds include dimethyldimethoxysilane, 1,3-dimethyldisiloxane, 1,1,3,3-tetramethyldisiloxane, hexamethyldisiloxane, 1,3-bis(silanomethylene)disiloxane, bis(1-methyldisiloxanyl)methane, 2,2-bis(1-methyldisiloxanyl)propane, 1,3,5,7-tetramethylcyclotetrasiloxane, octamethylcyclotetrasiloxane, 2,4,6,8,10-pentamethylcyclopentasiloxane, 1,3,5,7-tetrasilano-2,6-dioxy-4,8-dimethylene, and hexamethylcyclotrisiloxane. The oxygen-containing compound may include carbon dioxide, CO, or water. For example, a gas mixture comprising trimethylsilane, helium, and carbon dioxide may be reacted in a plasma in a plasma processing chamber. Precursors and processing conditions for the deposition of an oxygen-doped silicon carbide layer are also described in commonly assigned U.S. patent application Ser. No. 10/196,498, filed Jul. 15, 2002, and entitled “A Method of Depositing Dielectric Materials in Damascene Applications,” which is incorporated by reference herein. However, other methods may be used to deposit the barrier layer.


In one embodiment, an oxygen-doped silicon carbide barrier layer may be deposited by supplying an organosilicon compound, such as TMS, to a plasma processing chamber at a flow rate between about 50 sccm and about 300 sccm, supplying an oxygen-containing gas, such as CO2, at a flow rate between about 100 sccm and about 800 sccm, supplying an inert gas, such as helium, at a flow rate between about 200 sccm and about 800 sccm, maintaining a substrate temperature between about 300° C. and about 400° C., maintaining a chamber pressure between about 2 Torr and about 5 Torr, a RF power of between about 200 watts and about 500 watts, and a spacing of the gas distributor of the chamber from the substrate of between about 300 mils and about 400 mils. The oxygen-containing gas generally has the formula CxHyOz, with X being from 0 to 2, Y being from 0 to 2, and Z being from 1 to 3, wherein X+Y is at least 1 and X+Y+Z is 3 or less. Thus, the oxygen-containing gas may include carbon dioxide, CO, or water. The oxygen-containing gas is typically an inorganic material. The oxygen-containing gas described herein is considered a non-oxidizing gas compared to oxygen or ozone. Oxygen-doped silicon carbide barrier layers were deposited according to the processes described herein, and the layers were analyzed. FTIR spectra (not shown) of the layers measured over two weeks were stable, suggesting that the composition of the layers is stable and that the layers do not absorb a significant amount of moisture. It was also found that the dielectric constant and the stress of the film did not change significantly one week after deposition. Secondary ion mass spectroscopy (SIMS) was performed to determine the amount of copper diffusion through the barrier layers. The amount of copper that diffused through the films decreased by 3 orders of magnitude over 200 Å, indicating that the films are effective copper barriers.


In another embodiment, an oxygen-doped silicon carbide barrier layer may be deposited as described above, except that an oxygen-containing compound having the general formula




embedded image



is used instead of an oxygen-containing gas having the general formula CxHyOz, with X being from 0 to 2, Y being from 0 to 2, and Z being from 1 to 3, wherein X+Y is at least 1 and X+Y+Z is 3 or less. In one example, an oxygen-doped silicon carbide barrier layer is deposited from a gas mixture comprising diethylmethylsilane and tetramethyldisiloxane or dimethyldimethoxysilane. In any of the embodiments described herein in which an oxygen-doped silicon carbide barrier layer is deposited using an oxygen-containing gas having the general formula CxHyOz, with X being from 0 to 2, Y being from 0 to 2, and Z being from 1 to 3, wherein X+Y is at least 1 and X+Y+Z is 3 or less, an oxygen-containing compound having the general formula




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may be used instead of the oxygen-containing gas.


It was found that increasing the amount of oxygen-containing gas or oxygen-containing compound relative to the organosilicon compound in the deposition of the oxygen-doped silicon carbide layer lowers the dielectric constant of the deposited films by increasing the number of Si—O bonds in the deposited layers. However, too much oxygen doping of the barrier layers may decrease etch selectively between the barrier layers and adjacent dielectric layers that may contain oxygen, resulting in an increased amount of copper diffusion into the barrier layers.


Table 1 shows a comparison of barrier layer properties of oxygen-doped silicon carbide layers deposited by the processes described herein and conventional oxygen-free silicon carbide layers. The oxygen-doped barrier layers typically have a lower dielectric constant and a lower current leakage than the oxygen-free barrier layers.











TABLE 1





Film Properties
Oxygen-doped SiC
Oxygen-free SiC

















Refractive index (RI)
1.75~1.80
>2.00


Dielectric constant (k)
4.0~4.2
>4.4


Leakage (A/cm2 at 2 MV/cm)
2.0~4.0 E−9
>E−8


Breakdown (MV/cm at 1 mA)
>5
>3.5


Stress (dyne/cm2)
−1.7~−2.0 E9
−3.0~−4.5 E8


Hardness (Gpa)
>8
>5


Elastic modulus (Gpa)
>50
>40


Oxygen concentration
5~15%
Not Determined









In another aspect, devices including embodiments of silicon carbide glue layers described herein are provided. FIG. 2 shows a device 300 comprising a dielectric layer 302 having a metal feature 304 formed therein. The metal feature 304 extends to a surface 306 of the dielectric layer 302. A silicon carbide silicon carbide glue layer 310 is formed on the surface of the dielectric layer 302. In one embodiment, the silicon carbide layer 310 is formed by reacting a gas mixture comprising an organosilicon compound, an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, such as ethylene, and optionally, helium, in a plasma in a plasma processing chamber and depositing a thin film on the surface 306 of the dielectric layer. In another embodiment, the silicon carbide layer 310 is formed by reacting a gas mixture comprising an organosilicon compound and a gas selected from the group of hydrogen and argon in a plasma in a plasma processing chamber and depositing a thin film on the surface 306 of the dielectric layer. In either embodiment, preferably, the organosilicon compound is trimethylsilane. The silicon carbide layer 310 may serve as a barrier layer that separates the metal feature 304 in the dielectric layer 302 from an additional layer 312, such as a dielectric layer, deposited on the silicon carbide layer 310 if an additional barrier layer is not deposited on the layer 310 before the dielectric layer 312 is deposited. The dielectric layer 312 may be a low dielectric constant material such as BLACK DIAMOND™ films, commercially available from Applied Materials, Inc., of Santa Clara, Calif. and SILK® films, available from Dow Chemical Company. The dielectric layer 312 may also comprise other low dielectric constant materials including polymer materials, such as parylene, or low k spin-on glass such as an un-doped silicon glass (USG) or fluorine-doped silicon alass (FSG).


Optionally, the device 300 may also include a barrier layer 320 on the silicon carbide layer 310. The barrier layer 320 may be an oxygen-doped silicon carbide layer. The barrier layer 320 may be formed by reacting a gas mixture comprising trimethylsilane, helium, and carbon dioxide in a plasma in a plasma processing chamber. Thus, the device comprises a barrier bilayer 330 that includes, the silicon carbide layer 310 and the barrier layer 320. The barrier bilayer 330 separates the metal feature 304 in the dielectric layer 302 from the additional layer 312 deposited on the barrier layer 320.


We have found that silicon carbide glue layers deposited according to the embodiments described herein have significantly and unexpectedly improved properties, such as leakage currents and breakdown voltages, compared to layers deposited by reacting a gas mixture of trimethylsilane and helium. An example of typical resulting properties of silicon carbide glue layers deposited from different gas mixtures is shown below in Table 2. The leakage currents of layers deposited according to embodiments described herein, i.e., a trimethylsilane and hydrogen gas mixture, a trimethylsilane, ethylene, and helium gas mixture, and a trimethylsilane and ethylene gas mixture, are typically lower than the leakage current of a layer deposited from a gas mixture of helium and trimethylsilane. The leakage current of layers deposited according to embodiments described herein may be an order of magnitude lower than the leakage current of a layer deposited from a gas mixture of trimethylsilane and helium. Leakage current typically increases with degrading barrier layer properties. The breakdown voltages of layers deposited according to embodiments described herein are typically higher than the breakdown voltage of a layer deposited from a gas mixture of trimethylsilane and helium. However, the uniformity, i.e., the uniformity of the layer surface measured by an optical test across the surface, of the layers described herein is typically not as good as the uniformity of a layer deposited from a gas mixture of trimethylsilane and helium.













TABLE 2






trimethylsilane,
trimethylsilane,
trimethylsilane,
trimethylsilane,


layer properties
helium
hydrogen
ethylene, helium
ethylene



















dielectric
4.17
3.88
3.73
3.81


constant (@ 0.1 MHz)


leakage current
6.8 × 10−9
3.1 × 10−9
2.3 × 10−9
2.0 × 10−9


@1 MV/cm in


A/cm2


leakage current
1.6 × 10−7
6.1 × 10−8
3.1 × 10−8
4.6 × 10−9


@2 MV/cm in


A/cm2


breakdown
3.7
4.3
4.5
4.1


voltage in MV/cm


uniformity (%)
1.5
5
2.5
2.7









It is believed that the layers deposited from a mixture of trimethylsilane and helium have less desirable properties than the layers deposited from a mixture of an organosilicon compound, such as trimethylsilane, and hydrogen or argon because helium may cause damage to deposited layers during the plasma deposition process. Damaged layers may be more likely to have current leakage problems. It is believed that hydrogen and argon do not result in the damage to the layers that helium may cause. For example, it is believed that hydrogen and argon do not contribute as much as helium may to the formation of the broken bonds in the deposition layer that may lead to silicon-silicon bond formation In the deposited layers. Silicon-silicon bonds are undesirable in a barrier layer because of their semiconducting properties, which can contribute to current leakage.


It is believed that the layers deposited from a mixture of an organosilicon compound, such as trimethylsilane, and helium have less desirable properties than the layers deposited from a mixture of an organosilicon compound, such as trimethylsilane, an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, such as ethylene, and optionally, helium, because it is expected that the decomposition of an organosilicon compound during the deposition process can lead to the formation of more silicon-silicon (Si—Si) bonds in a mixture of an organosilicon compound and helium than in a mixture of an aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, such as ethylene, an organosilicon compound, and optionally, helium. Silicon-silicon bonds are undesirable in a barrier layer because of their semiconducting properties, which can contribute to current leakage. It is believed that the addition of the aliphatic hydrocarbon comprising a carbon-carbon double bond or a carbon-carbon triple bond, to a mixture including an organosilicon compound contributes to the formation of Si—C—Si bonds in the deposited layer rather than Si—Si bonds.


In the embodiments described herein, the silicon carbide glue layer may be deposited from a mixture including a precursor or precursors having the formulae SiHa(CH3)b(C2H5)c(C6H5)d, wherein a is 0 to 2, b is 0 to 4, c is 0 to 4,




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Endo et al., U.S. Pat. No. 4,532,150, describes mixing ethylene with precursors containing Si—Si bonds to form silicon carbide films. It should be noted that organosilicon compounds containing Si—Si bonds are not described herein. It is believed that depositing a layer from a gas mixture comprising a precursor containing Si—Si bonds contributes to the formation of Si—Si bonds in the deposited layer, and significantly increases current leakage.


While the silicon carbide glue layers described herein have been discussed primarily as barrier layers or components of barrier bilayers, the silicon carbide glue layers described herein may also be used as hard masks. FIG. 3 shows an example of a device 350 incorporating a silicon carbide layer as a hard mask. An etch stop 332, such as silicon carbide or nitrogen-doped silicon carbide is deposited on a dielectric layer 312 that is equivalent to the dielectric layer 312 of FIG. 2. Another dielectric layer 334 is deposited on the etch stop 332. A silicon carbide hard mask layer 336 is then deposited on the dielectric layer 334. The silicon carbide hard mask layer 336 may serve as a hard mask by itself, or it may have another hard mask layer 338, such as a silicon oxide, deposited on it to form a hard mask bilayer 340. The hard mask bilayer 340 provides two layers of protection for the device during subsequent processing steps, such as chemical mechanical polishing (CMP) of the device and etching the device to form vias and trenches. Preferably, the hard mask layer 338 has sufficiently different etching properties such that the hard mask layer 338 and the silicon carbide hard mask layer 336 can be etched differently to provide different etch patterns for vias and trenches.


EXAMPLES
Example 1

A silicon carbide glue layer was deposited at a chamber pressure of 5 Torr and temperature of 350° C. from gases which were flowed into a plasma processing chamber as follows:


















trimethylsilane, at
160 sccm



ethylene, at
200 sccm



helium, at
200 sccm











The substrate was positioned 400 mil from the gas distribution showerhead and 450 watts of high frequency power at 13.56 MHz was applied to the showerhead for plasma enhanced deposition of a silicon carbide silicon carbide glue layer. The silicon carbide glue layer was deposited at a rate of about 886 Å/min, and had a dielectric constant of about 3.73, a uniformity of about 2.5%, a leakage current of about 2.32×10−9 A/cm2 at 1 MV/cm, a leakage current of about 3.06×10−8 A/cm2 at 2 MV/cm, and a breakdown voltage of about 4.47 MV/cm.


Example 2

A silicon carbide glue layer was deposited at a chamber pressure of 3 Torr and temperature of 350° C. from gases which were flowed into a plasma processing chamber as follows:


















trimethylsilane, at
150 sccm



ethylene, at
200 sccm.











The substrate was positioned 400 mil from the gas distribution showerhead and 600 watts of high frequency power at 13.56 MHz was applied to the showerhead for plasma enhanced deposition of a silicon carbide silicon carbide glue layer. The silicon carbide glue layer was deposited at a rate of about 1255 Å/min, and had a dielectric constant of about 3.81, a uniformity of about 2.7%, a leakage current of about 2.04×10−9 A/cm2 at 1 MV/cm, a leakage current of about 4.64×10−8 A/cm2 at 2 MV/cm, and a breakdown voltage of about 4.13 MV/cm.


Example 3

A silicon carbide glue layer was deposited at a chamber pressure of 9.5 Torr and temperature of 350° C. from gases which were flowed into a plasma processing chamber as follows:


















trimethylsilane, at
160 sccm



hydrogen, at
200 sccm.











The substrate was positioned 400 mil from the gas distribution showerhead and 450 watts of high frequency power at 13.56 MHz was applied to the showerhead for plasma enhanced deposition of a silicon carbide silicon carbide glue layer. The silicon carbide glue layer was deposited at a rate of about 161 Å/min, and had a dielectric constant of about 3.88, a uniformity of about 5%, a leakage current of about 3.1×10−9 A/cm2 at 1 MV/cm, a leakage current of about 6.1×10−8 A/cm2 at 2 MV/cm, and a breakdown voltage of about 4.3 MV/cm.


Example 4

A silicon carbide glue layer was deposited at a chamber pressure of 9.5 Torr and temperature of 350° C. from gases which were flowed into a plasma processing chamber as follows:


















trimethylsilane, at
160 sccm



argon, at
200 sccm.











The substrate was positioned 400 mil from the gas distribution showerhead and 450 watts of high frequency power at 13.56 MHz was applied to the showerhead for plasma enhanced deposition of a silicon carbide silicon carbide glue layer. The silicon carbide glue layer was deposited at a rate of about 713 Å/min, and a dielectric constant of about 4.0, a uniformity of about 1.9%, a leakage current of about 2.8×10−9 A/cm2 at 1 MV/cm, a leakage current of about 4.3×10−8 A/cm2 at 2 MV/cm, and a breakdown voltage of about 3.63 MV/cm.


Example 5

A barrier layer was deposited on one of the silicon carbide glue layers deposited as in Examples 1–4. The barrier layer was deposited at a chamber pressure of 3.5 torr and temperature of 350° C. from gases which were flowed into a plasma processing chamber as follows:


















trimethylsilane, at
100 sccm



helium, at
400 sccm



carbon dioxide, at
350 sccm.











The substrate was positioned 350 mil from the gas distribution showerhead and 400 watts of high frequency power at 13.56 MHz was applied to the showerhead for plasma enhanced deposition of an oxygen-doped silicon carbide barrier layer. The barrier layer was deposited at a rate of about 920 Å/min, and a dielectric constant of about 3.88, a uniformity of about 1.1%, a leakage current of about 4.2×10−10 A/cm2 at 1 MV/cm, a leakage current of about 3.6×10−9 A/cm2 at 2 MV/cm, a breakdown voltage of about 5.24 MV/cm. The compressive stress of the barrier layer was about 1.82×10−9 dyne/cm2.


Barrier Bilayers with SiN or SiCN Layers


In another aspect, a barrier bilayer may be deposited on a substrate by first depositing a SiN or SiCN layer on a substrate, and then depositing an oxygen-doped silicon carbide barrier layer on the substrate. The oxygen-doped barrier layer may be deposited by the processes described herein for depositing an oxygen-doped silicon carbide barrier that is part of a barrier bilayer that also contains a silicon carbide glue layer. The SiN or SiCN layer may be deposited using conventional techniques for SiN and SiCN deposition. Examples of processing gases and conditions that may be used to deposit SiCN layers are described in U.S. patent application Ser. No. 09/793,818, filed Feb. 23, 2001, which is incorporated by reference herein.


A device including the barrier bilayer is also provided. While FIG. 2 was described above with respect to a device including a barrier bilayer having a silicon carbide layer 310, the layer 310 may alternatively represent a SiN or SiCN layer.


One advantage of the methods and devices described herein that include barrier bilayers is that a photoresist may be deposited directly on the oxygen-doped silicon carbide layer of the barrier bilayer without subjecting the photoresist to nitrogen poisoning.


While the foregoing is directed to embodiments of the present invention, other and further embodiments of the invention may be devised without departing from the basic scope thereof, and the scope thereof is determined by the claims that follow.

Claims
  • 1. A method for processing a substrate, comprising: providing a substrate having conductive features formed in a dielectric material to a processing chamber;depositing a first barrier layer comprising silicon, carbon, and nitrogen on the substrate;depositing a second barrier layer contacting at least a portion of the first barrier layer, wherein the second barrier layer is a nitrogen free dielectric layer comprising silicon and carbon and deposited by reading a processing gas comprising a carbon and oxygen containing compound and an oxygen-free organosilicon compound.
  • 2. The method of claim 1, further comprising depositing a dielectric layer contacting the second barrier layer, wherein the dielectric layer comprises silicon, oxygen, and carbon and has a dielectric constant of about 3 or less.
  • 3. The method of claim 1, wherein the compound comprising oxygen and carbon is selected from the group of carbon dioxide, carbon monoxide, an oxygen-containing organosilicon compound, and combinations thereof.
  • 4. The method of claim 1, wherein the oxygen-free organosilicon compound has the formula SiHa(CH3)b(C6H5)c, wherein a is 0 to 3, b is 0 to 3, and c is 1 to 4.
  • 5. The method of claim 4, wherein the oxygen-free organosilicon compound comprises trimethylsilane, tetramethylsilane, or both.
  • 6. The method of claim 1, wherein the processing gas further comprises an inert gas selected from the group of helium, argon, and combinations thereof.
  • 7. The method of claim 6, wherein the processing gas comprises carbon dioxide, helium, and trimethylsilane.
  • 8. The method of claim 1, wherein the first barrier layer and the second barrier layer are deposited in situ in the same processing chamber or same processing system without breaking vacuum.
  • 9. The method of claim 1, wherein the depositing a second barrier layer contacting the first barrier layer comprises supplying trimethylsilane to a processing chamber at a flow rate between about 50 sccm and about 300 sccm, supplying carbon dioxide at a flow rate between about 100 sccm and about 800 sccm, supplying helium at a flow rate between about 200 sccm and about 800 sccm, maintaining a substrate temperature between about 300° C. and about 400° C., maintaining a chamber pressure between about 2 Torr and about 5 Torr, and applying a RF power of between about 200 watts and about 500 watts.
  • 10. The method of claim 1, further comprising: depositing a photoresist layer directly on the second barrier layer.
  • 11. A method for processing a substrate, comprising: providing the substrate to a processing chamber; anddepositing a barrier bilayer, wherein the barrier bilayer comprises: a first barrier layer comprising silicon, carbon, and nitrogen on the substrate; anda second barrier layer contacting at least a portion of the first barrier layer, wherein the second barrier layer is a nitrogen free dielectric layer comprising silicon and carbon and deposited by reacting a processing gas comprising a carbon and oxygen containing compound and an oxygen-free organosilicon compound.
  • 12. The method of claim 11, further comprising depositing a dielectric layer adjacent the second barrier layer, wherein the dielectric layer comprises silicon, oxygen, and carbon and has a dielectric constant of about 3 or less.
  • 13. The method of claim 11, wherein the compound comprising oxygen and carbon is selected from the group of carbon dioxide, carbon monoxide, an oxygen-containing organosilicon compound, and combinations thereof.
  • 14. The method of claim 11, wherein the oxygen-free organosilicon compound has the formula SiHa(CH3)b(C6H5)c, wherein a is 0 to 3, b is 0 to 3, and c is 1 to 4.
  • 15. The method of claim 14, wherein the oxygen-free organosilicon compound comprises trimethylsilane, tetramethylsilane, or both.
  • 16. The method of claim 11, wherein the processing gas further comprises an inert gas selected from the group of helium, argon, and combinations thereof.
  • 17. The method of claim 16, wherein the processing gas comprises carbon dioxide, helium, and trimethylsilane.
  • 18. The method of claim 11, wherein the first barrier layer and the second barrier layer are deposited in situ in the same processing chamber or same processing system without breaking vacuum.
  • 19. The method of claim 11, wherein the second barrier layer is deposited by supplying trimethylsilane to a processing chamber at a flow rate between about 50 sccm and about 300 sccm, supplying carbon dioxide at a flow rate between about 100 sccm and about 800 sccm, supplying helium at a flow rate between about 200 sccm and about 800 sccm, maintaining a substrate temperature between about 300° C. and about 400° C., maintaining a chamber pressure between about 2 Torr and about 5 Torr, and applying a RF power of between about 200 watts and about 500 watts.
  • 20. The method of claim 11, further comprising: depositing a photoresist layer directly on the second barrier layer.
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No. 10/247,404, filed Sep. 19, 2002, U.S. Pat. No. 6,838,393, which application claims benefit of U.S. provisional patent application Ser. No. 60/397,184, filed Jul. 19, 2002, and which application is a continuation-in-part of U.S. patent application Ser. No. 10/196,498, filed Jul. 15, 2002, now U.S. Pat. No. 6,890,850 which claims benefit of U.S. provisional patent application Ser. No. 60/340,615, filed Dec. 14, 2001, all of which are herein incorporated by reference.

US Referenced Citations (183)
Number Name Date Kind
3510369 Ernick et al. May 1970 A
4262631 Kubacki Apr 1981 A
4532150 Endo et al. Jul 1985 A
4634601 Hamakawa et al. Jan 1987 A
4649071 Tajima et al. Mar 1987 A
4759947 Hishihara et al. Jul 1988 A
4872947 Wang et al. Oct 1989 A
4894352 Lane et al. Jan 1990 A
4895734 Yoshida et al. Jan 1990 A
4951601 Maydan et al. Aug 1990 A
4981724 Hochberg et al. Jan 1991 A
5000113 Wang et al. Mar 1991 A
5000178 Griffith Mar 1991 A
5003178 Livesay Mar 1991 A
5011706 Tarhay et al. Apr 1991 A
5086014 Miyata et al. Feb 1992 A
5224441 Felts et al. Jul 1993 A
5238866 Bolz et al. Aug 1993 A
5242530 Batey et al. Sep 1993 A
5298587 Hu et al. Mar 1994 A
5298597 You et al. Mar 1994 A
5314724 Tsukune et al. May 1994 A
5360491 Carey et al. Nov 1994 A
5362526 Wang et al. Nov 1994 A
5423941 Komura et al. Jun 1995 A
5465680 Loboda Nov 1995 A
5468978 Dowben Nov 1995 A
5480300 Okoshi et al. Jan 1996 A
5494712 Hu et al. Feb 1996 A
5525550 Kato Jun 1996 A
5554570 Maeda et al. Sep 1996 A
5565084 Lee et al. Oct 1996 A
5591566 Ogawa Jan 1997 A
5593741 Ikeda Jan 1997 A
5607773 Ahlburn et al. Mar 1997 A
5618619 Petrmichl et al. Apr 1997 A
5628828 Kawamura et al. May 1997 A
5638251 Goel et al. Jun 1997 A
5641607 Ogawa et al. Jun 1997 A
5658834 Dowben Aug 1997 A
5679413 Petrmichl et al. Oct 1997 A
5691209 Liberkowski Nov 1997 A
5710067 Foote et al. Jan 1998 A
5711987 Bearinger et al. Jan 1998 A
5730792 Camilletti et al. Mar 1998 A
5741626 Jain et al. Apr 1998 A
5776235 Camilletti et al. Jul 1998 A
5780163 Camilletti et al. Jul 1998 A
5789316 Lu Aug 1998 A
5789776 Lancaster et al. Aug 1998 A
5817579 Ko et al. Oct 1998 A
5818071 Loboda et al. Oct 1998 A
5855681 Maydan et al. Jan 1999 A
5869396 Pan et al. Feb 1999 A
5876891 Takimoto et al. Mar 1999 A
5926740 Forbes et al. Jul 1999 A
5976979 Chen Nov 1999 A
5989998 Sugahara et al. Nov 1999 A
6045877 Gleason et al. Apr 2000 A
6051321 Lee et al. Apr 2000 A
6054379 Yau et al. Apr 2000 A
6057251 Goo et al. May 2000 A
6060132 Lee May 2000 A
6068884 Rose et al. May 2000 A
6071809 Zhao Jun 2000 A
6072227 Yau et al. Jun 2000 A
6080526 Yang et al. Jun 2000 A
6107192 Subrahmanyan et al. Aug 2000 A
6114259 Sukharev et al. Sep 2000 A
6124641 Matsuura Sep 2000 A
6140226 Grill et al. Oct 2000 A
6147009 Grill et al. Nov 2000 A
6153537 Bacchetta et al. Nov 2000 A
6159871 Loboda et al. Dec 2000 A
6169039 Lin et al. Jan 2001 B1
6242339 Aoi Jun 2001 B1
6242530 Konig et al. Jun 2001 B1
6287990 Cheung et al. Sep 2001 B1
6291334 Somekh Sep 2001 B1
6303523 Cheung et al. Oct 2001 B1
6312793 Grill et al. Nov 2001 B1
6316167 Angelopoulos et al. Nov 2001 B1
6331494 Olson et al. Dec 2001 B1
6340435 Bjorkman et al. Jan 2002 B1
6340628 Van Cleemput et al. Jan 2002 B1
6344693 Kawahara et al. Feb 2002 B1
6348725 Cheung et al. Feb 2002 B1
6352945 Matsuki et al. Mar 2002 B1
6548899 Ross Apr 2002 B1
6383955 Matsuki et al. May 2002 B1
6399489 M'Saad et al. Jun 2002 B1
6410462 Yang et al. Jun 2002 B1
6410463 Matsuki Jun 2002 B1
6413583 Moghadam et al. Jul 2002 B1
6429121 Hopper et al. Aug 2002 B1
6432846 Matsuki Aug 2002 B1
6436824 Chooi et al. Aug 2002 B1
6437443 Grill et al. Aug 2002 B1
6441491 Grill et al. Aug 2002 B1
6444136 Liu et al. Sep 2002 B1
6444568 Sundararajan et al. Sep 2002 B1
6455445 Matsuki et al. Sep 2002 B1
6465366 Nemani et al. Oct 2002 B1
6479110 Grill et al. Nov 2002 B1
6479409 Shioya et al. Nov 2002 B1
6486082 Cho et al. Nov 2002 B1
6489238 Tsui Dec 2002 B1
6495448 Lee Dec 2002 B1
6500773 Gaillard et al. Dec 2002 B1
6511903 Yau et al. Jan 2003 B1
6511909 Yau et al. Jan 2003 B1
6528426 Olsen et al. Mar 2003 B1
6531714 Bacchetta et al. Mar 2003 B1
6532150 Sivertsen et al. Mar 2003 B1
6537733 Campana et al. Mar 2003 B1
6537929 Cheung et al. Mar 2003 B1
6541282 Cheung et al. Apr 2003 B1
6541398 Grill et al. Apr 2003 B1
6548690 Mimoun Apr 2003 B1
6555476 Olsen et al. Apr 2003 B1
6559520 Matsuki et al. May 2003 B1
6562690 Cheung et al. May 2003 B1
6573193 Yu et al. Jun 2003 B1
6573196 Gaillard et al. Jun 2003 B1
6582777 Ross et al. Jun 2003 B1
6583048 Vincent et al. Jun 2003 B1
6583071 Weidman et al. Jun 2003 B1
6589888 Nemani et al. Jul 2003 B1
6592890 Green Jul 2003 B1
6593247 Huang et al. Jul 2003 B1
6593633 Jan et al. Jul 2003 B1
6593653 Sundararajan et al. Jul 2003 B1
6593655 Loboda et al. Jul 2003 B1
6596655 Cheung et al. Jul 2003 B1
6624053 Passemard Sep 2003 B1
6627532 Gaillard et al. Sep 2003 B1
6642157 Shioya et al. Nov 2003 B1
6649531 Cote et al. Nov 2003 B1
6656837 Xu et al. Dec 2003 B1
6660391 Rose et al. Dec 2003 B1
6660656 Cheung et al. Dec 2003 B1
6660663 Cheung et al. Dec 2003 B1
6703265 Asami et al. Mar 2004 B1
6730593 Yau et al. May 2004 B1
6734115 Cheung et al. May 2004 B1
6756323 Grill et al. Jun 2004 B1
6759327 Xia et al. Jul 2004 B1
6770573 Grill et al. Aug 2004 B1
6790789 Grill et al. Sep 2004 B1
6838393 Yim et al. Jan 2005 B1
6852651 Shioya et al. Feb 2005 B1
6875699 Lassig et al. Apr 2005 B1
6890850 Lee et al. May 2005 B1
6974766 Huang Dec 2005 B1
20010005546 Cheung et al. Jun 2001 A1
20020000670 Yau et al. Jan 2002 A1
20020045361 Cheung et al. Apr 2002 A1
20020093075 Gates et al. Jul 2002 A1
20020098714 Grill et al. Jul 2002 A1
20020111042 Yau et al. Aug 2002 A1
20020155386 Xu et al. Oct 2002 A1
20020160626 Matsuki et al. Oct 2002 A1
20020172766 Laxman et al. Nov 2002 A1
20020173172 Loboda et al. Nov 2002 A1
20020187629 Huang et al. Dec 2002 A1
20030001282 Meynen et al. Jan 2003 A1
20030003765 Gibson, Jr. et al. Jan 2003 A1
20030003768 Cho et al. Jan 2003 A1
20030008511 Tsai et al. Jan 2003 A1
20030040195 Chang et al. Feb 2003 A1
20030042605 Andideh et al. Mar 2003 A1
20030064154 Laxman et al. Apr 2003 A1
20030068881 Xia et al. Apr 2003 A1
20030085408 Yang et al. May 2003 A1
20030089988 Matsuure May 2003 A1
20030111730 Takeda et al. Jun 2003 A1
20030129827 Lee et al. Jul 2003 A1
20030139035 Yim et al. Jul 2003 A1
20030139062 Grill et al. Jul 2003 A1
20030194495 Li et al. Oct 2003 A1
20030194496 Xu et al. Oct 2003 A1
20030198742 Vrtis Oct 2003 A1
20030211244 Li et al. Nov 2003 A1
Foreign Referenced Citations (21)
Number Date Country
41 26 759 Feb 1993 DE
196 54 737 Dec 1996 DE
199 04 311 Aug 1999 DE
0 613 178 Feb 1994 EP
0 725 440 Aug 1996 EP
0 935 283 Aug 1999 EP
1 029 728 Aug 2000 EP
1 107 303 Jun 2001 EP
1 122 770 Aug 2001 EP
1 176 226 Jan 2002 EP
1 354 980 Oct 2003 EP
09-008031 Jan 1997 JP
9-237785 Jul 1997 JP
09-320075 Dec 1997 JP
09-321175 Sep 1999 JP
WO 9921706 May 1999 WO
WO 9933102 Jul 1999 WO
WO 9941423 Aug 1999 WO
WO 0019498 Apr 2000 WO
WO 0019508 Apr 2000 WO
WO 0020900 Apr 2000 WO
Related Publications (1)
Number Date Country
20050130440 A1 Jun 2005 US
Provisional Applications (2)
Number Date Country
60397184 Jul 2002 US
60340615 Dec 2001 US
Continuations (1)
Number Date Country
Parent 10247404 Sep 2002 US
Child 11021319 US
Continuation in Parts (1)
Number Date Country
Parent 10196498 Jul 2002 US
Child 10247404 US