Source: http://www.google.com/patents/US20030111013?dq=6,460,050
Timestamp: 2015-01-26 05:34:31
Document Index: 758384403

Matched Legal Cases: ['arts 41', 'art 41', 'art 42', 'arts 41', 'arts 41', 'art 41', 'arts 41', 'arts 41', 'arts 41', 'art 41', 'arts 41', 'arts 41', 'arts 41']

Patent US20030111013 - Method for the deposition of silicon germanium layers - Google PatentsSearch Images Maps Play YouTube News Gmail Drive More »Sign inAdvanced Patent SearchPatentsA vertical chemical vapor deposition (CVD) apparatus and methods for the deposition of compound films, such as silicon germanium films, are provided. In a preferred embodiment, the apparatus comprises a process chamber, wherein the process chamber is elongated in a first generally vertical direction;...http://www.google.com/patents/US20030111013?utm_source=gb-gplus-sharePatent US20030111013 - Method for the deposition of silicon germanium layersAdvanced Patent SearchPublication numberUS20030111013 A1Publication typeApplicationApplication numberUS 10/313,089Publication dateJun 19, 2003Filing dateDec 5, 2002Priority dateDec 19, 2001Publication number10313089, 313089, US 2003/0111013 A1, US 2003/111013 A1, US 20030111013 A1, US 20030111013A1, US 2003111013 A1, US 2003111013A1, US-A1-20030111013, US-A1-2003111013, US2003/0111013A1, US2003/111013A1, US20030111013 A1, US20030111013A1, US2003111013 A1, US2003111013A1InventorsTheodorus Oosterlaken, Peter ZagwijnOriginal AssigneeOosterlaken Theodorus Gerardus Maria, Zagwijn Peter MarcExport CitationBiBTeX, EndNote, RefManReferenced by (35), Classifications (15), Legal Events (1) External Links: USPTO, USPTO Assignment, EspacenetMethod for the deposition of silicon germanium layersUS 20030111013 A1Abstract A vertical chemical vapor deposition (CVD) apparatus and methods for the deposition of compound films, such as silicon germanium films, are provided. In a preferred embodiment, the apparatus comprises a process chamber, wherein the process chamber is elongated in a first generally vertical direction; a boat to support a plurality of wafers, wherein individual wafers comprising the plurality of wafers are oriented substantially horizontally, stacked substantially vertically and spaced apart vertically; and a gas injector inside the process chamber, wherein the gas injector extends in a second generally vertical direction over about the height of the boat and comprises a plurality of gas injection holes, wherein the plurality of gas injection holes extends over about the height of the gas injector, and wherein the gas injector has a feed end connected to a source of a silicon-containing gas and a source of a germanium-containing gas. The aggregate cross-section of the holes is relatively large to prevent reactions inside the gas injector and the horizontal cross-section of gas conduction channels inside the gas injector is relatively large to facilitate distribution of the precursor source gases over the height of the boat. Images(11) Claims(70)
BRIEF DESCRIPTION OF THE FIGURES [0014]FIG. 1a is a schematic cross-sectional top view of a tube-shaped process chamber in accordance with preferred embodiments of the present invention; [0015]FIG. 1b is a schematic cross-sectional side view of the tube-shaped process chamber of FIG. 1a, illustrating generalized dimensions of the process chamber; [0016]FIG. 2 is a schematic cross-sectional side view of an elongated furnace with a gas injector, constructed in accordance with preferred embodiments of the present invention; [0017]FIG. 3 is a perspective view of the process chamber of FIG. 2, as viewed from the bottom of the process chamber; [0018]FIG. 4 is a schematic front view of a gas injector in accordance with one illustrative embodiment of the present invention; [0019]FIG. 5 is a perspective view of the gas injector of FIG. 4; [0020]FIG. 6 is a horizontal cross-sectional view of the gas injector of FIG. 4; [0021]FIG. 7 is an exploded side view of a tubular process chamber with a liner and a gas injector in accordance with preferred embodiments of the present invention; [0022]FIG. 8 is a thickness-position and Ge-concentration-position plot showing the results of a chemical vapor deposition of a silicon germanium layer performed in accordance with a prior art batch process; and [0023]FIG. 9 shows the results of a chemical vapor deposition of a silicon germanium layer performed in accordance with the present invention.
DETAILED DESCRIPTION OF THE INVENTION [0024] An increasingly important consideration in batch processing is the ability to obtain a uniform film thickness across both the surface of individual wafers and across the surfaces of different wafers in a batch of wafers; that is, ideally, not only should a deposited film on a particular wafer be uniform from location to location on one wafer, but the films deposited on different wafers in a single batch of wafers should also be uniform from wafer to wafer. Current practice typically employs low pressures for batch processing, so that efficient gas transport throughout the furnace can be achieved by process gas diffusion, which in turn encourages uniform film deposition over each wafer. Over the vertical height of the process chamber, however, going from the source gas inlet end of the chamber to the exhaust end of the chamber, depletion of process gases can occur. Thus, the concentrations of precursors can decrease with increasing distance from the gas inlet. Where the inlet is at the bottom of a process chamber, the concentrations of process gases decrease along the vertical axis of the furnace, resulting in different deposition rates at different heights in the furnace. Traditionally, this has been addressed by grading the temperature along the axis to compensate for the depletion effect. [0025] In addition to the general difficulties associated with the depletion effect, the deposition of certain films is particularly problematic because the high reactivity of certain precursors used in the deposition exacerbate variations between the various wafers in a batch. Such problematic films include compound films, which comprise at least two elements in a certain ratio. In addition to thickness non-uniformity, differences in the deposition rates of the precursors can cause compositional non-uniformity between films deposited on different wafers. [0026] Examples of such problematic films are silicon germanium alloy films. (see J. Holleman, A. E. T. Kuiper and J. F. Verweij, J. Electrochem. Soc., Vol. 140, No. 6, June 1993, pp.1717-1722). Silicon germanium films are typically deposited using a germanium source gas and a silicon source gas. One factor contributing to non-uniformity problems, however, is that the germanium source gas increases the reactivity of the silicon source gas, which exacerbates the problem of precursor depletion at wafer locations farther from a gas inlet. A second factor is that the reaction rate of the germanium source gas is much higher than the reaction rate of the silicon source gas, causing faster depletion of the germanium source gas. This results in substantial variations in the germanium deposition rate at different locations inside commonly used process chambers, resulting in substantial variations in the germanium content of silicon germanium films deposited on different wafers. The combination of these two factors makes current batch processing methods unsuitable for practical use in forming silicon germanium alloy films. [0027] As noted above, one method to compensate for differences in precursor concentrations has been to apply a temperature gradient over the height of the tube to alter the deposition rate at different points in the reaction chamber. However, this approach introduces new problems as large differences in temperature are undesirable because they can cause differences in the properties of deposited films. [0028] Another currently employed strategy for improving deposited film uniformity on wafers at different positions in the process chamber is the use of a localized source gas injector configured to inject source gas into the process chamber at various locations where wafers are positioned. In this way, the depletion of gas at different positions in the tube is compensated for by the addition of fresh unreacted gas. An example of a furnace with such a localized injector is described in U.S. Pat. No. 5,902,102. [0029] This strategy, however, is not universally applicable since it is best applied to depositing particular types of films using precursors having particular properties. For example, a film that can be deposited using such a localized injector is polycrystalline silicon, deposited using silane (SiH4). The polycrystalline silicon may later be doped with phosphorus using phosphine (PH3). For a phosphorus doped film, however, both SiH4 and PH3 are typically mixed together prior to feeding the source gases to an injector. This is possible because PH3 does not react with SiH4 and even inhibits the decomposition of SiH4. Another example of a film that can be deposited using such a localized injector is a low temperature oxide, using SiH4 and O2 as source gases. In this case, the two source gases are mutually highly reactive and are thus preferably supplied via separate injectors into the furnace tube. However, at the deposition temperatures used for low temperature oxide, 450� C. for example, the individual gases are quite stable and decomposition of the gases inside the injectors is not an issue. [0030] Injectors are not considered suitable for the deposition of silicon germanium alloy films, however, because of the high reactivity of the precursors, especially inside the injector itself. A major perceived obstacle has been that the pressure inside the injector (which in essence are tubes with restrictive apertures) will be so high that uncontrollable reactions may occur inside the injector, leaving little process gas left over for the deposition of films onto the wafer substrates. In addition, as discussed above, large differences in reaction rates between silicon-containing and germanium-containing precursors continue to make it difficult to achieve a uniform film composition over different wafers in a particular batch. [0031] Conceptual Model [0032] Given the limitations of current strategies, while the present teachings are not limited by theory, the benefits of the present invention can be conceptualized and understood by the theoretical model presented below. [0033] The theoretical model describes a reaction system for a binary film. For ease of description, the deposition of silicon germanium alloy films using SiH4 and GeH4 will be taken as an example. It will be appreciated, however, that the model is generally applicable to the deposition of other compound films. [0034] Reference will now be made to the Figures, wherein like numerals refer to like parts throughout. With reference to FIGS. 1a and 1 b, a horizontal cross-section of a control volume 20 around wafers 21 that have been loaded into the batch process chamber 26 is assumed to have the shape of a ring. The wafers occupy an area made out by their perimeter 22. The control volume 20 is the space between an internal radius R1 equal to the radius of perimeter 22 and an external radius R2 equal to the radius of the inner wall 24 of the process chamber 26 and having a height dz, as shown in FIG. 1b. The wafers are held in a so-called boat (not shown), with individual wafers oriented horizontally and held stacked and spaced apart vertically above and below one another. The boat extends in the z-direction where z increases from the bottom of the process chamber towards the top of the process chamber, up to where the exhaust end of the chamber is located. [0035] The concentration of silane in the control volume 20 at a height z is given by ρSiH4 (z) and the concentration of germane is given by ρGeH4(z). The amount of silane and germanium that will accumulate in the control volume as a function of time is given by: π � ( R 2 2 - R 1 2 ) � dz  ρ SiH 4 ∂  ( z ) ∂ t = φ SiH 4 1 + φ SiH 4 2 + φ SiH 4 3 + φ SiH 4 4 ( 1 ) π � ( R 2 2 - R 1 2 ) � dz  ρ GeH 4 ∂  ( z ) ∂ t = φ GeH 4 1 + φ GeH 4 2 + φ GeH 4 3 + φ GeH 4 4 ( 2 ) [0036] wherein the four terms on the right-hand side of each equation are the amount of the gas supplied to and removed from the control volume. Negative values indicate removal from the process chamber, while positive values indicate supply of gases into the process chamber. The expressions on the right hand side are written out below. φ SiH 4 1 = π � ( R 2 2 - R 1 2 ) � v  ( z ) � ρ SiH 4  ( z ) ( 3 ) φ SiH 4 2 = v s � ρ SiH 4 i � 2   π � R 2 � dz ( 4 ) φ SiH 4 3 = - π � ( R 2 2 - R 1 2 ) � v  ( z + dz ) � ρ SiH 4  ( z + dz ) ( 5 ) φ SiH 4 4 = - 2   π � R 1 2 � ( K 1 � ( ρ SiH 4  ( z ) ) α1 + K 2 � ( ρ SiH 4  ( z ) ) α2 � ( ρ GeH 4  ( z ) ) α3 ) � dz p ( 6 ) [0037] Equation (3) gives the inflow of silane through the bottom plane of a horizontal cross-section of the control volume 20 at height z and with a velocity ν(z). Equation (4) gives the injection of silane through the outer circumference of the control volume 20, which outer circumference is defined by the inner wall 24. For simplicity, it is assumed that there is a injection of silane over the complete outer circumference of the cylindrical volume 20, with the injected silane having a gas injection velocity νs and a density ρi SiH4. Equation (5) gives the outflow of silane through the top plane of a horizontal cross-section of the control volume 20 at height z+dz (FIG. 1b). Equation (6) gives the consumption of the silane by decomposition and deposition of a film on the surfaces of wafers 21, where the total surface area of a wafer (two surfaces) is 2πR1 2 and the pitch of a wafer in the boat is p. The constants K1 and K2 are rate constants that account for the possible temperature dependence of the decomposition reaction through thermal activation. The parameters α1, α2, and α3 are the reaction order constants for the decomposition reaction. [0038] Below, similar equations are written out for germane, equation (2): φ GeH 4 1 = π � ( R 2 2 - R 1 2 ) � v  ( z ) � ρ GeH 4  ( z ) ( 7 ) φ GeH 4 2 = v s � ρ GeH 4 i � 2   π � R 2 � dz ( 8 ) φ GeH 4 3 = - π � ( R 2 2 - R 1 2 ) � v  ( z + dz ) � ρ GeH 4  ( z + dz ) ( 9 ) φ GeH 4 4 = - 2   π � R 1 2 � ( K 3 � ( ρ GeH 4  ( z ) ) α 4 + K 4 � ( ρ GeH 4  ( z ) ) α 5 � ( ρ SiH 4  ( z ) ) α 6 ) � dz p ( 10 ) [0039] wherein ρi GeH4(z) is the germane density of the injected gas. In equation (10) the constants K3 and K4 are rate constants that account for the possible temperature dependence of the decomposition reaction. The parameters α4, α5, and α6 are rate constants for the decomposition reaction. It will be appreciated that both equations (6) and (10) allow for the possibility that the decomposition rate of a species is influenced by a second species. [0040] Preferably, during deposition of a film, a steady state is achieved, so that the rate of precursor entry into the reaction chamber is equal to the rate of precursor deposition. In such a case there is no change of the concentration of the precursor gases as a function of time. As a result, the left hand expressions for both equations (1) and (2) are zero. Therefore, the sum of the equations (3), (4), (5), (6), and the sum of the equations (7), (8), (9), (10) should both be equal to 0. [0041] To verify this result, as a first step in the calculation of the sum of equations (3), (4), (5), and (6), the Taylor expansion of equation (5) can be written out as follows: φ SiH 4 3 = - π � ( R 2 2 - R 1 2 ) �  ( v  ( z ) � ρ SiH 4  ( z ) + v  ( z ) � d   ρ SiH 4  ( z ) dz � dz + dv  ( z ) dz �  ρ SiH 4  ( z ) � dz + O  ( dz 2 ) ) ( 11 ) [0042] The first term is opposite to equation (3), and therefore will cancel out when equations (3) and (5) are added. In addition, the term (dZ)2 can be ignored due to the coefficient of 0. Therefore, summing (3) and (5) yields: φ SiH 4 1 + φ SiH 4 3 = - π � ( R 2 2 - R 1 2 ) � ( v  ( z ) � d   ρ SiH 4  ( z ) dz � dz + dv  ( z ) dz �  ρ SiH 4  ( z ) � dz ) ( 12 ) [0043] The value for the gas velocity ν(z) can be calculated from the gas injection velocity νs over the injection surface 2πR2�z: v  ( z ) = 2 � π � R 2 � ( v s + C  ( z ) ) π � ( R 2 2 - R 1 2 ) � z ( 13 ) [0044] wherein C is a term that depends only on the conversion rate of the precursor gas and takes into account the generation and/or annihilation of gas through chemical reactions, e.g. the thermal decomposition of one SiH4 molecule can result in the formation of two H2 molecules. [0045] Notably, when the deposition rate in the reactor is constant over the height of the reactor, which is the theoretical objective of the preferred embodiments then the term C does not depend on z. As such, ν(z) will increase linearly as a function of z. Consequently, in the case where all the precursor gas entering the process chamber is homogeneously distributed, e.g., by using a gas injector as described herein below, ν(z) will be proportional to z. [0046] On the basis of this assumption, the set of differential equations can be written out and solved. After solving the equation, it is possible to argue that the assumption that C is constant is indeed reasonable, as discussed below. Combining equations (13), (12), (11), (4), (6), in equation (1) and simultaneously dividing by 2πdz yields the following: 0 = v s � ρ SiH 4 i � R 2 - R 1 2 p � f  ( ρ SiH 4  ( z ) , ρ GeH 4  ( z ) )  - 2 � π � R 2 � ( v s + C ) � ( z � d   ρ SiH 4  ( z ) dz + ρ SiH 4  ( z ) ) ( 14 ) [0047] A similar expression can be found for the germane concentration: 0 = v s � ρ GeH 4 i � R 2 - R 1 2 p � g  ( ρ GeH 4  ( z ) , ρ SiH 4  ( z ) )  - 2 � π � R 2 � ( v s + C ) � ( z � d   ρ GeH 4  ( z ) dz + ρ GeH 4  ( z ) ) ( 15 ) [0048] This set of differential equations has a solution when both ρSiH4(z) and ρGeH4(z) are independent of z. In this case, functions f and g are also independent of z and, as a consequence, the following results can be obtained: ρ SiH 4  ( z ) = v s � ρ SiH 4 i � R 2 - R 1 2 p � f  ( ρ SiH 4  ( z ) , ρ GeH 4  ( z ) ) 2 � π � R 2 � ( v s + C ) ( 16 ) ρ GeH 4  ( z ) = v s � ρ GeH 4 i � R 2 - R 1 2 p � g  ( ρ GeH 4  ( z ) , ρ SiH 4  ( z ) ) 2 � π � R 2 � ( v s + C ) ( 17 ) [0049] The solutions exist when the density of the species and the conversion rate of the reactants are constant over the height of the reactor. Notably, the reaction rate equation does not have to fulfill any condition other than the following: if the parameters ρSiH4(z) and ρGeH4(z) do not vary as a function of z, then the value of the reaction rate does not vary as a function of z. [0050] As noted above, the outcome of this modeling has general applicability to depositions of compound films other than silicon germanium films. In fact, precursors for other binary films may be readily substituted for the silane and germane discussed above. As such, the model indicates that each binary film can be grown with a constant deposition rate and constant film composition over the height of the process chamber 26, using a separate precursor source gas for each element constituting the binary film, by injecting the two precursor source gases into the reaction chamber 26 in a constant ratio and substantially homogeneously distributed over the height of the reactor. According to the above-described theoretical model, such an injection of precursor gas can result in a homogeneous film over the height of the boat even in cases of substantially different reaction rates for the different source gases. [0051] Process Chamber and Gas Injector [0052] A schematic cross-sectional side-view of an elongated furnace with a gas injector, in accordance with preferred embodiments of the present invention, is shown in FIG. 2. The process chamber 26 is preferably surrounded by a heating element (not shown). A liner 28, delimiting the outer perimeter of the reaction space 29, is preferably provided inside the process chamber 26. Preferably, at the bottom of the process chamber 26, a wafer load 50 may enter and exit the process chamber 26 by a door 30. Precursor source gas is injected through a gas injector 40, preferably via a gas feed conduit 44. The gas injector 40 is provided with a pattern of holes 48, preferably extending substantially over the height of the wafer load 50. Note that, because gases are first introduced into the reaction space 29 from the holes 48 of the gas injector 40, the interior of gas delivery devices, such as the gas injector 40, through which gases travel is not part of the reaction space 29 and is, in a sense, outside of the reaction space 29. Consequently, the reaction space 29 comprises the interior volume of the process chamber 26, excluding the volume occupied by gas delivery devices such as the gas injector 40. Note also that, while illustrated and described in the context of a vertical furnace, the injectors described herein can also be employed with horizontal furnace designs. [0053] In a preferred embodiment, inside the process chamber 26, gas is flowed in a generally upward direction 52 and then removed from the reaction space 29 via the exhaust space 54 between the process chamber 26 and the liner 28, where gas flows in a downward direction 56 to the exhaust 58, which is connected to a pump (not shown). The gas injector 40 preferably distributes process gases inside the process chamber 26 over the entire height of the reaction space 29. The gas injector 40 itself acts as a restriction on the flow of gas, such that the holes 48 that are closer to the conduit 44 tend to inject more gas into the reaction space than those holes 48 that are farther from the conduit 44. Preferably, this tendency for differences in gas flows through the holes 48 can be compensated to an extent by reducing the distance between the holes 48 (i.e., increasing the density of the holes 48) as they are located farther away from the conduit 44. In other embodiments, the size of individual holes making up the holes 48 can increase with increasing distance from the conduit 44, or both the size of the holes 48 can increase and also the distance between the holes 48 can decrease with increasing distance from the conduit 44. Advantageously, however, the preferred embodiments are illustrated with holes 48 of constant size so as to minimize the surface area of the sides of the gas injector 40 containing the holes 48. [0054] In one preferred embodiment, for depositing silicon germanium, the gas injector design advantageously prevents undesired and uncontrollable reactions inside the gas injector. Preferably, as described in more detail below, this is achieved by providing holes 48 in the gas injector 40 such that the total area of the opening of the holes 38 is sufficiently large to allow the pressure inside the gas injector 40 to be kept relatively low, in comparison to the pressures inside the localized injectors described earlier. Reducing the pressure inside the gas injector will result in a reduction of the reaction rate of precursors, since reaction rates typically increase with increasing pressure. An additional advantage of having relatively low pressure inside the gas injector 40 is that gas tends to expand at low pressures, so that the precursor source gases inside the gas injector 40 will expand out and through the gas injector 40. In such a case, for a given constant flow of source gas, the residence times of the source gases inside the gas injector 40 will be reduced relative to another case where similar gases in the injector 40 are at a higher pressure. Because of the combination of these advantages, in particular preferred embodiments, the decomposition of source gases can be substantially eliminated. [0055] A disadvantage, however, of low pressure inside the gas injector 40 is that the conduction of gases through the gas injector 40 is decreased. This can lead to a poor distribution of gas over the height of the gas injector 40, causing differences in the flow of precursor source gas out of the holes 48 over the height of the gas injector 40; that is, the majority of precursor source gas may flow out of the holes 48 near the gas conduit 44 end of the gas injector 40. [0056] To facilitate the flow of precursor source gas inside and along the height of the gas injector 40, the gas injector 40 is preferably provided with a large inner cross-sectional area. In addition, in one preferred embodiment, in order to better accommodate the preferred gas injector 40 inside the reaction space 29, the wall of the process chamber 26 delimiting the reaction space 29 is provided with an outwardly extending bulge 25 to accommodate the gas injector 40, as shown in FIG. 3. FIG. 3 is a perspective-view of the process chamber 26 of FIG. 2, showing the liner 23 and the gas injector 40 mounted in the liner 23, as viewed from the bottom of the process chamber 26. The gas injector 40 is accommodated in the bulge 25 in the liner 23. A second bulge 22 is also preferably provided in the liner 23 to accommodate a thermocouple (not shown) for measurement of the temperature inside the reaction space 29. By accommodating the gas injector 40 and the thermocouple in the bulge 25 and second bulge 22, respectively, that extend outwardly into the space between the liner 23 and inner wall 24, the reaction space 29 can be kept substantially cylindrical. Thus, the side of the gas injector 40 facing the center of the reaction space 29 is preferably substantially flush with an imaginary circular circumference of the reaction space 29. Such a substantially cylindrical reaction space 29 is advantageous for the uniformity of the gas flow and the film deposition process. In addition, as illustrated in FIG. 3, the sides 25 a of the bulge 25 preferably slope gradually to meet the side 25 b of the bulge 25, allowing space at the sides to the gas injector 40 for precursor gas to be emitted in the directions 65 and 68 (FIG. 6). [0057] The gas injector 40 in accordance with one illustrative embodiment of the present invention is shown in FIG. 4. The gas injector 40 preferably comprises two gas injector parts 41, and 42, each preferably provided with separate gas feed conduit connections 45 and 46, respectively. Part 41 injects gas into the lower volume of the reaction space 29 and part 42 injects gas into the upper volume of the reaction space 29. The parts 41 and 42 are connected by linkages 49 and 51. It will be appreciated, however, that the gas injector 40 may comprise more or fewer parts than the two parts 41 and 42. [0058] The gas injector 40 is provided with a pattern of holes 48 substantially extending over the height 60 (FIG. 2) of the wafer load 50 (FIG. 2). The total cross section of the holes is preferably at least about 30 mm2. The diameter of each of holes 48 is preferably about 1 mm or more, more preferably between about 2.5 mm and 3.5 mm, and most preferably about 3 mm. In the illustrative embodiment shown in FIG. 4, the gas injector 40 has 40 holes total. Consequently, with an average diameter of 3 mm per hole, the total cross-sectional area of the holes 48 is 40�3 mm�3 mm�π/4=282 mm2. More generally, the total cross-sectional area of the holes 48 is preferably about 30 mm2 or more, and more preferably between about 196 mm2 and 385 mm2. [0059] In addition, each part 41 and 42 of the gas injector 40 has an inner cross-sectional area 64 and 62 (FIG. 6), respectively, which are the cross-sectional areas in each of parts 41 and 42 available for the conduction of source gases through the gas injector 40. Preferably, each of inner cross-sectional areas 64 and 62 are at least about 100 mm2. In the illustrative embodiment, the cross-sectional area of each of the parts 41, 42 of the gas injector 40 can be about 11 mm�30 mm=330 mm2. More generally, the cross-sectional area of each of the parts 41, 42 is between about 140 mm2 and 600 mm2, more preferably between about 225 mm2 and 455 mm2, and most preferably between about 290 mm2 and 372 mm2. At its top end, the gas injector 40 can be provided with a hook 53 (FIGS. 3, 4 and 5), to secure the top end of the gas injector 40 to the hook support 53 (FIG. 3). It will be appreciated that the gas injector 40 may be secured by other means suitable for mounting it inside the process chamber 26. [0060] Reference will now be made to FIGS. 4-7, identical parts are indicated with identical reference numerals throughout. A perspective view of the gas injector 40 is presented in FIG. 5. A horizontal cross-section of the gas injector 40 is shown in FIG. 6. The cross-section is taken through the lower end of the gas injector 40 and straight through a pair of injection holes 48 provided in gas injector part 41, for injecting the gas in the lower end of the process chamber 26. Preferably, in each gas injector part, the holes 48 are provided in pairs, at the same height. In addition, the two holes 48 preferably inject the precursor gas in two directions 66 and 68, the directions 66 and 68 forming an angle 70 of about 90 degrees, to improve the radial uniformity. Moreover, as shown, the tubes comprising the gas injector 40 preferably have an oblong shape, as viewed in horizontal cross-section. Preferably, the longer dimension of the oblong shape faces the center of the process chamber 26, i.e., the side of the oblong shape with the longer dimension is perpendicular to a imaginary line extending radially from the center of the process chamber 26. [0061]FIG. 7 shows the placement of the gas injector 40 in the process chamber 26, according to preferred embodiments of the present invention. The process chamber 26 is preferably provided at its bottom end with a flange 12. The liner 23 is preferably placed inside the process chamber 26. Preferably, the gas injector 40 is placed inside the liner 23. [0062] In a preferred embodiment, two precursor source gases, providing the two constituting elements of a binary film, are mixed in the gas supply system (not shown) prior to entering the gas injector 40 via feed conduit connections 45 and 46 (FIGS. 4 and 5). Pre-mixing the precursor gases in the gas supply system is one way to ensure a homogeneous composition of injected gas over the height of the boat. However, pre-mixing is not essential. In another embodiment, the two precursor source gases can each be injected via their own separate gas injectors 40 (not shown), so that they are first mixed after being injected into the reaction space 29. Consequently, it will be appreciated that more than one gas injector 40 may be located inside the process chamber 26. [0063] Advantageously, the use of two gas injector parts 41 and 42 allows for further tuning possibilities. For example, when a gas of substantially the same composition is supplied to both parts of the gas injector 40, via separate source gas supplies and gas feed conduit connections 45 and 46, the flows supplied to the different gas injector parts can be chosen differently to fine-tune the gas flow into the reaction space 29. This will improve uniformity in the deposition rates of precursors over the height 60 of the wafer load 50 (FIG. 2). It is also possible to supply gases of different compositions to the two parts 41 and 42 of the gas injector 40 to fine-tune, over the height 60 of the wafer load 50, the composition of a deposited binary film. However, as indicated by the theoretical model discussed above, the compositions of the injected precursor source gases fed into gas injector parts 41 and 42 are more preferably the same for both parts. EXAMPLES [0064] Depositions of silicon germanium films were carried out and the results were analyzed. In a first experiment the deposition was carried out without a gas injector 40, by a system according to the prior art. Silane and germane were fed to a vertically elongated process chamber. The process chamber was configured to accommodate a load of wafers with a diameter up to 200 mm. The diameter of the wafers actually used, however, was 150 mm. All the precursor source gases were injected from one point, at the bottom end of the reaction space. The silane flow was 200 sccm, the germane flow was 15 sccm, the temperature was 460� C., the pressure was 1000 mTorr, and the deposition time was 92 minutes. [0065] The results in terms of film thickness and composition were determined and are presented in FIG. 8. The horizontal axis indicates the location of the wafers in the boat. Boat slot 1 was at the top of the boat and boat slot 140 was at the bottom of the boat. The general direction of the gas flow is as indicated in FIG. 8. A pronounced variation in both film thickness and film composition can be observed, due to depletion of source gas, particularly depletion of germane. The variation in film thickness (indicated by the plot with circles), calculated by taking the difference between the maximum and minimum film thicknesses and dividing by two times the average [(Max−Min)/(2�AVG)], is about +/−15%. For the germanium concentration (indicated by the plot with squares) the variation was about +/−6%. [0066] In a second experiment the deposition was carried out using the methods and apparatus of the preferred embodiment. Silane and germane were pre-mixed and injected into the reaction space together via a gas injector 40 (FIG. 4), as described above. The silane flow was 480 sccm, the germane flow was 60 sccm, the temperature was 490� C., the pressure was 200 mTorr and the deposition time was 60 minutes. [0067] The results are shown in FIG. 9. Relative to the results of the prior art process shown in FIG. 8, a much more uniform film thickness profile and germanium concentration over the boat was achieved. In this case, the variation in film thicknesses thickness (indicated by the plot with circles) is only about �1.1% and the variation in germanium concentration (indicated by the plot with squares) is about �1.5%. [0068] Advantageously, in addition to improved uniformity in thickness and composition, another advantage was achieved. It has been observed that the growth of polycrystalline silicon germanium layers on silicon oxide is difficult because nucleation of the film on the oxide layer is very difficult and this difficulty prevents deposition of the film in a large process window. This problem has been overcome by depositing a seeding layer, typically of pure silicon, on top of the silicon oxide before deposition of the silicon germanium layer. However, using the apparatus and methods of the present invention, the problems with nucleation were substantially eliminated and smooth silicon germanium films were deposited directly on silicon oxide, using a mixture of source gases wherein the ratio of germanium atoms to germanium plus silicon atoms is 1 to 20 or higher. Desirably, omitting the seeding layer simplifies the fabrication of integrated circuits. [0069] Although, for ease of discussion, silane (SiH4) and germane (GeH4) have been identified as precursor source gases, the use of other precursor source gases is also contemplated. For example, other silicon sources include, but are not limited to, mono-, di-, tri- or tetrachlorosilane (SiH(1−x)Clx, x=1-4), or disilane (Si2H6) or trisilane (Si3H8). Similarly, other germanium sources can include, but are not limited to, mono-, di-, tri- or tetrachlorogermane (GeH(1−x)Clx, x=1-4), digermane (Ge2H6) or trigermane (Ge3H8). It will be appreciated that, using these other source gases, process conditions should be optimized. Moreover, the precursor source gases need not be strictly composed of two precursor sources. It is possible to add dopants to the silicon germanium film. For example, boron can be added through the addition of a boron-containing source gas such as diborane (B2H6) or boron chloride (BCl3). [0070] Moreover, it will be appreciated that the present invention has applicability to depositing compound films other than silicon germanium films. In particular, the present invention may advantageously be applied to the deposition of other compound layers having precursors with highly reactive chemistries, especially precursors that cannot be used in conjunction with the localized injectors of the prior art. An example of other compound films includes arsenic doped films, using TEOS (Si(�OC2H5)4) and TEAS (AsO(�OC2H5)3) as precursor source gases. The present teachings may also be applied to the deposition of undoped silicon oxide films, using TEOS (Si(�OC2H5)4) as a source gas. Strong height-dependent variations in deposition rate can still occur with this process. In such a case, a boat with a variable pitch, according to U.S. Pat. No. 6,240,875 B1, owned by the assignee of the present application, may be used. In conjunction with the variable pitch boat, injecting TEOS through a gas injector as described in the present disclosure appeared to result in excellent deposited film uniformities. The present invention may also be applied to the deposition of high temperature oxides using silane and N2O or dichlorosilane (DCS) and N2O. In addition, deposition of silicon nitride films using dichlorosilane (DCS) and ammonia or using bis-(tertiary-butyl amino) silane and ammonia can favorably be carried out in accordance with the preferred embodiments. It will be appreciated, however, that the foregoing examples are illustrative only and not exhaustive. [0071] Consequently, although this invention has been described on the basis of particular preferred embodiments, modifications of the invention are possible and are within the spirit and scope of this disclosure. This disclosure is intended to cover modifications, adaptations or variations of the invention which make use of its general principles. Furthermore, the invention was described in the context of semiconductor manufacturing processes, but those of skill in the art will recognize that it may be adapted for use in various industries. For example, adaptation and use in applications such as chemical production is possible. 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layerUS8663736Jan 7, 2010Mar 4, 2014Soulbrain Sigma-Aldrich Ltd.Germanium complexes with amidine derivative ligand and process for preparing the sameUS20080178914 *Jan 25, 2008Jul 31, 2008Tokyo Electron LimitedSubstrate processing apparatusDE102004004858A1 *Jan 30, 2004Aug 18, 2005Infineon Technologies AgImplements for simultaneously coating number of wafers during semiconductor manufacture by deposition from gas phase, i.e. chemical vapour deposition (CVD), or compressing chemical vapour deposition (LPCVD) as well as gas injectorEP1641031A2 *May 31, 2005Mar 29, 2006Asm International N.V.Deposition of TiN films in a batch reactorEP2474643A1Jan 11, 2011Jul 11, 2012ImecMethod for direct deposition of a germanium layer* Cited by examinerClassifications U.S. Classification118/724, 118/715International ClassificationC23C16/44, C23C16/22, C23C16/455Cooperative ClassificationC23C16/455, C23C16/45512, C23C16/22, C23C16/45502, C23C16/45578European ClassificationC23C16/455K14, C23C16/455, C23C16/455A, C23C16/22, C23C16/455BLegal EventsDateCodeEventDescriptionDec 5, 2002ASAssignmentOwner name: ASM INTERNATIONAL N.V., NETHERLANDSFree format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:OOSTERLAKEN, THEODORUS GERARDUS MARIA;ZAGWIJN, PETER MARC;REEL/FRAME:013556/0714Effective date: 20021115RotateOriginal ImageGoogle Home - Sitemap - USPTO Bulk Downloads - Privacy Policy - Terms of Service - About Google Patents - Send FeedbackData provided by IFI CLAIMS Patent Services