1. Field of the Invention
The present invention is directed to a method and system for fabricating low defect-density oxides, and more particularly to a method and system for fabricating oxides using at least one of a pulsed RF energy source and a pulsed process gas source.
2. Discussion of the Background
Significant attention has been given to methods of forming the gate dielectric layer used in MOSFETs. Both oxidation of semiconductors and deposition of dielectric layers on the surface have heretofore been used. Thin silicon dioxide films have been formed by various methods such as thermal oxidation, low pressure chemical vapor deposition, photo-activated chemical vapor deposition, plasma enhanced chemical vapor deposition, and plasma oxidation. The most successful approach for gate oxide growth so far has been thermal oxidation of silicon at elevated temperatures (e.g., in excess of 900° C.). High temperature thermal oxidation of silicon provides a thin layer of low defect density silicon dioxide as well as a good silicon/oxide interface.
One critical property of the gate oxide layer, regardless of the way it is fabricated, is that it must have high dielectric strength, or in another words, very low defect density. Dielectric strength is directly, but inversely, related to the defect density inside the dielectric layer. Defects in the gate oxide can be formed because of numerous reasons (e.g., particulates, defects that originally resided at the silicon surface, surface contamination, and atoms arriving at the reaction front not having enough energy to move into full density location sites). Assuming the process starts with a perfect silicon surface and free of particulates and contaminants, the defect density of the resulting silicon dioxide is very much dependent upon the energies of the atoms arriving at the reaction surface. This is true for both oxidation and deposition processes.
As the ULSI technologies advance, the requirements for precise dopant distribution become extremely stringent. Processes requiring high temperature operation (e.g., at least 900° C.) for a substantial length of time (e.g., at least 5 minutes) may cause dopant re-distribution and, therefore, they should be minimized wherever possible. As a result, approaches that perform oxidation or annealing at temperatures lower than 800° C. or for a period of time shorter than a few minutes become very attractive.
Growing silicon dioxide with the assistance of a plasma discharge provides a method of fabricating silicon dioxide at temperatures as low as 300° C. Plasma assisted growth of oxides can be further classified as either: (1) plasma oxidation or (2) plasma enhanced chemical vapor deposition.
U.S. Pat. No. 4,232,057 (hereinafter “the '057 patent”) describes a method of growing oxide films on silicon utilizing plasma oxidation. The process employs oxygen at a flow rate of 0.7–10 sccm utilizing a relatively high RF power. The substrate is held at a temperature between 300°–800° C. and about 20 cm away from the plasma source, as shown in
U.S. Pat. No. 5,412,246 describes a method for growing thin oxides as gate dielectric layers using plasma discharge and an ozone/oxygen gas mixture. The ozone is generated in an ozone generator separated from the RF plasma reactor. Using the stand-alone ozone generator eliminates the need for high RF power in the oxidation chamber that may result in poor oxide quality. The use of RF power is optional as ozone itself can provide chemically active oxygen species for oxidation. Low RF power is used to enhance the oxide growth rate and to improve film quality and thickness uniformity. The low power RF (<200 watt/cm) can reexcite or redistribute the ozone. A supplemental rapid thermal oxidation at temperatures of 700°–800° C. in the presence of ozone may be introduced after the plasma oxidation as a follow-up. The dielectric strength of the resulting oxide, as shown in
U.S. Pat. No. 4,776,925 describes producing silicon oxide or nitride thin films using low energy ion beam bombardment. As shown in
A similar concept of using atomic oxygen to react with a silicon surface at elevated temperatures without plasma discharge has also been studied. U.S. Pat. Nos. 4,474,829, 4,409,260, and 5,738,909 generally use either ozone or UV radiation excited oxygen or oxygen-containing precursors to create the atomic oxygen. A high substrate temperature or an RTP process is needed in order to obtain gate-quality oxide.
Plasma enhanced chemical vapor deposition has been used to fabricate relatively thick silicon dioxide or silicon nitride layers (e.g., often >1000 A), primarily because of its high deposition rate (>3000 A/minute) and low process temperature (<500° C.). The atoms or molecules arriving at the surface in a conventional PECVD system do not have enough energy and time to diffuse into a low energy position. Therefore, the dielectric films generated generally have a high defect density and a low electric breakdown field.
Plasma oxidation and plasma enhanced chemical vapor deposition have been used to produce silicon oxide as dielectric layers. As described above, these plasma enhanced processes have the advantage of fabricating silicon oxide at low temperatures (e.g., below 800° C.). However, gate-quality films of less than 100 A produced by plasma oxidation or PECVD have not been achieved without utilizing other supplemental processes such as rapid thermal oxidation. Although oxygen ion beams have been used to produce thin oxide films as gate dielectrics, the use of relatively high-energy ion beams has the disadvantages of low throughput, possible surface damage and sputtering contamination.
It is an object of the present invention to provide a method and system for fabricating low defect density oxides. Such oxides find use as, but are not limited to, gate dielectric materials in Metal-Oxide-Semiconductor Field Effect Transistors (MOSFETs) because the resulting thin films have high dielectric strengths that are conducive to good gate dielectric layers.
This object and other advantages of the present invention are addressed by a method and system for pulsing at least one of an RF power and a process gas flow rate during formation of those oxides.
A more complete appreciation of the invention and many of the attendant advantages thereof will be readily obtained as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings, wherein:
Reference will now be made to the drawings, wherein like reference numerals designate identical or corresponding parts throughout the several views.
One chamber for use in the system of
Such source plasma generating apparatuses include a longitudinally split, metallic shield disposed within a helical coil and disposed around an internal plasma region. The plasma and coil are separated by an insulating wall. The metallic shield prevents a significant part of the electric field from being coupled to the plasma capacitively, while allowing the RF power coupled to the plasma inductively.
As it is not very effective to couple RF power to the plasma inductively, it is difficult to use purely inductive coupling to initiate plasmas in many cases. On the contrary, RF power can be very effectively coupled to the plasma capacitively. This makes the capacitive coupling useful in initiating plasmas. The disadvantage of capacitive coupling is that it generally causes large and uncontrollable plasma potentials. These high plasma potentials lead to sputtering of chamber walls and high-energy ions. Sputtering of the chamber wall results in contamination, and high-energy ion bombardment results in damage of the substrate surface.
The slits in the metallic shield are designed to optimize the relative percentage of capacitively and inductively coupled RF power. Its width, length and relative position to the coil are particularly important as it directly affects the plasma property and process performance. To avoid difficulty in initiating plasmas but at the same time keeping the plasma potential low, the total area of the slit should be above 0.2%, but less than 5% or tunable in-situ to minimize ions with excess energy.
Within such a chamber, the substrate is processed. When starting with a clean silicon surface, the fabrication of a low defect density thin oxide film can be realized through increasing the mobility of the atoms or molecules arriving at the surface so that they can move to a low energy (or full density) position. Increasingly surface mobility is generally achieved by a combination of three techniques: 1) increasing surface temperature; 2) ion bombardment; and 3) chemical vapor molecule aided mobility.
The substrate to be processed is heated to a temperature between 500°–800° C. An exemplary multi-zone resistance heater is described in PCT Application No. PCT/US00/25503, referenced above. The heater preferably utilizes fast heat delivery while maintaining a high uniformity (e.g., less than ±3° C.). Such a heater also uses a separate RF power supply to achieve a small level of negative bias on the substrate. The small bias level is used to provide the acceleration energy for the ion flux in order to achieve the surface temperature necessary for promoting the growth of the low defect density oxide film. The bias level on the wafer can be tuned through changing the RF power applied on the supporting chuck. A further example of such a chuck is illustrated in
It is well known that increasing temperature can reduce the defect density of the thin oxide film. In conventional furnace oxidation, high quality silicon dioxide is grown at a substrate temperature between 1000°–1100° C. In order to grow the same or better quality silicon oxide film at a much lower substrate temperature (e.g., 500°–800° C.), the surface temperature where the oxidation or deposition process takes place should be increased through methods other than substrate heating. One method to increase the effective surface temperature is to bombard the surface with energetic particles such as ions from the plasma. As some of the deposition or reaction species coming from the plasma are ions, those ions can effectively provide the energy required for the reaction and the movement of the atoms/molecules.
An estimation of the correlation between surface atom/molecule temperature rise and plasma flux is provided in Table 1. A simple approximation is that the surface temperature is about 200° C. higher for every 1 eV (electron volt) per adatom. Table 1 summarizes a calculation, for silicon deposition, of apparent surface temperatures for given plasma density, bias voltage and deposition rate.
The apparent surface temperature increases dramatically with either ion energy or ion density or both. When the plasma density is about 1.4×1010/cm3 and deposition rate is about 0.5 μm/min (which is close to the condition of a conventional PECVD system), the energy of the arriving ions only gives 90° C. increase in surface temperature. To produce sufficient surface temperature, the arriving species should carry high-energy flux. High-energy ion flux can be realized by either high ion energy or high ion flux or both. As high energy ions may result in surface damage due to strong sputtering effect, plasma sources having high density but low ion energy, such as the referenced ESRF source, are preferred. With a plasma source density of 1.4×1012 and a deposition rate of 3 μm/min, the increase of surface temperature is 1500° C. If the deposition rate is lower, the surface temperature could be even higher.
At high plasma density the surface atom/molecule can reach an equivalent temperature of much higher than the melting point of the material being grown. More particularly, the surface atom/molecule temperature can reach much higher than 1610° C. in the case of SiO2 growth. This phenomenon enables the material growth to be carried out very differently than in a conventional thermal growth process for which the growth temperature is much lower (e.g., 900°–1100° C.). The achieved high surface temperature enables the arriving atoms/molecules to react and move quickly to a low energy location, minimizing defect density in the growing film. Thus, by controlling the source plasma one can control the reaction rate or deposition rate.
A gas injection system can be used to inject the gas mixture into the deposition chamber. A pumping system is used to keep the reaction chamber under vacuum and achieve low gas residence time inside the chamber (e.g., less than 1 millisecond). The residence time for the processing region is generally estimated from the ratio of the processing region volume (Liters) to the pumping speed (Liters/sec) at the processing region. Therefore, it is preferable to to minimize the processing region volume and maximize the pumping speed at the processing region to achieve a low residence time. For instance, a vacuum system equipped with a 3300 l/sec turbo-molecular pump (e.g. Mitsubishi FT3300W) can be designed with sufficient flow conductance (i.e. 10,300 L/sec) to permit the delivery of 75% of the pump inlet pumping speed to the processing region. Hence, for a cylindrical processing region of diameter 25.4 cm and height 5 cm, a residence time of approximately 1 msec can be achieved. Such a gas injection and pumping system help to achieve the process conditions required for low defect-density film deposition. In the case of plasma enhanced chemical vapor deposition, chemical molecules containing silicon are required as precursors. The gas molecules of silicon-containing precursor arriving at the substrate surface should be only partially dissociated and able to diffuse and react with oxygen atoms/ions to form silicon dioxide at a low energy position.
To grow a layer of thin silicon dioxide, a silicon wafer is first cleaned in a series of chemical solutions such as NH3OH/H2O2/H2O, HCl/H202/H20, H2SO4/H2O2/H2O to remove metallic as well as organic contamination that may exist on the wafer surface. A short dip in a HF/H2O solution is also performed to remove the surface native oxide layer. The wafer is then transferred into a load-lock chamber as shown in
The wafer is heated to a processing temperature of 500°–800° C. and then processed. After the oxidation or deposition process is completed, the wafer is transferred out to a cooling chamber to cool down before returning to the unloading cassette.
The gases used in the oxidation process can be one of the following; (i) pure oxygen, (ii) a mixture of oxygen and inert gases, (iii) a mixture of oxygen and ozone, (iv) a mixture of oxygen, ozone and inert gases, and (v) other oxygen-containing gases. The gases used in the deposition process can be a mixture of oxygen-containing gases such as O2, NO, or N2O, etc., and a silicon-containing precursor such as SiCl4, or SiCl2H2, or TEOS (tetraethylorthosilicate), etc. Inert gases may also be added in the deposition gas mixture.
Turning now to the actual processing of the substrate within the chamber, after stabilization of the process gas flow and pressure, the chuck is then heated rapidly to a temperature of 500°–800° C. and RF power is applied. When RF is applied to the source plasma, the oxide growth rate will be a function of the magnitude (and duty cycle in pulsed mode). Accurate oxide thickness control, which is extremely critical for gate dielectric application, can be realized using this phenomenon. Given a fixed magnitude, the oxide thickness can be controlled by the pulse duty cycle and the total number of pulses applied. The same mechanism can be applied with pulsed process gas delivery.
According to a first embodiment illustrated in
The first source of RF power is applied on the coil to generate the source plasma having a density in the range of 1×1012–5×1013 ions/cm3. The second source of RF power is simultaneously applied to the substrate chuck to provide a small level (e.g., −5 volts–−50 volts) of negative self-bias on the wafer. As a very thin layer (10–30 Angstroms) of lower quality native oxide may grow during the initial gas flow and pressure stabilization step, a short step (e.g., 5–20 seconds) with a slightly higher level of chuck RF power should be used to achieve a negative self-bias level of between −15 volts and −50 volts. This slightly higher level of bias produces higher energy ions that can effectively sputter away the thin native oxide. However, careful process optimization is necessary to avoid any excess sputtering of the silicon surface. The power of the 2nd RF is lowered after the initial sputtering step to maintain a negative bias level of between −5 volts and −15 volts. This low bias level will provide the necessary energy (temperature) for the surface atoms/molecules while preventing the surface from sputtering damage.
An alternate embodiment, shown in
As the 1st RF source is operated in continuous mode, the plasma will stay on throughout process. The oxidation or deposition starts and stops following the cycling of the process gas flow. There is no film growth during the off cycle of the process gases where only inert gases are introduced into the chamber. A fast pumping system prevents the gas transition (from process to inert or vice versa) from affecting the film growth. The 2nd RF source (coupled to the chuck) is turned off during the process gas off cycle to minimize the inert gas ions from bombarding the grown film. In this mode, the thickness of the oxide is related to the number of cycles applied. An exemplary apparatus for pulsed gas and pulsed RF processing, including the gas injection design and the RF system design, is described in the International application PCT/US00/21667 entitled “Pulsed plasma processing method and apparatus”, and it is, therefore, incorporated herein by reference in its entirety.
In yet another alternate embodiment shown in
Obviously, numerous modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood that, within the scope of the appended claims, the invention may be practiced otherwise than as specifically described herein.
The present application is the National Stage of International Application No. PCT/US01/42925, filed Nov. 7, 2001, which claims the benefit of U.S. Provisional Application No. 60/246,113 filed on Nov. 7, 2000. The present invention is related to U.S. application Ser. No. 10/088,504 filed Sep. 17, 2002 and U.S. application Ser. No. 10/204,448 filed Sep. 3, 2002. The contents of those applications are incorporated herein by reference in their entirety.
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/US01/51502 | 11/7/2001 | WO | 00 | 5/2/2003 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO02/075801 | 9/26/2002 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
4232057 | Ray et al. | Nov 1980 | A |
4409260 | Pastor et al. | Oct 1983 | A |
4474829 | Peters | Oct 1984 | A |
4776925 | Fossum et al. | Oct 1988 | A |
4918031 | Flamm et al. | Apr 1990 | A |
5122483 | Sakai et al. | Jun 1992 | A |
5234529 | Johnson | Aug 1993 | A |
5405492 | Moslehi | Apr 1995 | A |
5412246 | Dobuzinsky et al. | May 1995 | A |
5738909 | Thakur et al. | Apr 1998 | A |
5935373 | Koshimizu | Aug 1999 | A |
6043608 | Samukawa et al. | Mar 2000 | A |
6051113 | Moslehi | Apr 2000 | A |
6051503 | Bhardwaj et al. | Apr 2000 | A |
6101972 | Bluck et al. | Aug 2000 | A |
6155198 | Danek et al. | Dec 2000 | A |
6167834 | Wang et al. | Jan 2001 | B1 |
6174450 | Patrick et al. | Jan 2001 | B1 |
6187682 | Denning et al. | Feb 2001 | B1 |
6187685 | Hopkins et al. | Feb 2001 | B1 |
6200651 | Roche et al. | Mar 2001 | B1 |
6256434 | Matuschek et al. | Jul 2001 | B1 |
6258735 | Xia et al. | Jul 2001 | B1 |
6331494 | Olson et al. | Dec 2001 | B1 |
6410462 | Yang et al. | Jun 2002 | B1 |
6413583 | Moghadam et al. | Jul 2002 | B1 |
6461483 | Gopalraja et al. | Oct 2002 | B1 |
6475353 | Lantsman | Nov 2002 | B1 |
6482476 | Liu | Nov 2002 | B1 |
6541367 | Mandal | Apr 2003 | B1 |
6562715 | Chen et al. | May 2003 | B1 |
6709715 | Lang et al. | Mar 2004 | B1 |
20020132473 | Chiang et al. | Sep 2002 | A1 |
20020171994 | Grimard et al. | Nov 2002 | A1 |
20030049931 | Byun et al. | Mar 2003 | A1 |
Number | Date | Country | |
---|---|---|---|
20040214451 A1 | Oct 2004 | US |
Number | Date | Country | |
---|---|---|---|
60246113 | Nov 2000 | US |