The invention relates to an injector head for atomic layer deposition on a surface of a substrate. The invention further relates to an apparatus comprising such an injector head.
Atomic layer deposition is known as a method for (repeated) depositing of a monolayer of target material. Atomic layer deposition differs from for example chemical vapour deposition in that atomic layer deposition takes at least two process steps. Atomic layer deposition has the advantage of enabling a good layer thickness control.
A first one of these process steps comprises application of a precursor gas on the substrate surface. To this end, known injector heads are provided with a deposition space having a precursor supply. The supply is arranged for providing a precursor gas flow from the precursor supply via the deposition space to a precursor drain. In this way a deposition space is formed that in use is bounded by the injector head and the substrate surface.
A second one of these process steps comprises reaction of the precursor material in order to form the monolayer of target material. To this end a further deposition space is provided in the injector head having a reactant supply. The further deposition space is in use separated from precursor gas by a flow barrier and can be arranged for providing at least one of a reactant gas, a plasma, laser-generated radiation, and ultraviolet radiation for reacting the precursor after deposition of the precursor gas on at least part of the substrate surface.
In order to provide for the flow barrier, barrier gas flow may be injected between the injector head and the substrate surface. The known injection head further comprises a connection unit connectable to a respective plurality of gas supply sources and drain collectors thus providing access for respective gases via said connection unit, to a respective precursor deposition space, reactant deposition space and flow barrier.
WO 2012/105831 of the same inventor herein incorporated by reference describes an atomic layer deposition apparatus and a specific injector head arrangement. For such arrangements manufacturability is a challenge in view of the relatively high friction factor that is needed in order to provide a homogenous gas flow of the various process gases. This homogeneity is important in order to carry out a robust atomic layer deposition process. At the same time it is also important that the design is compact, since a larger number of injector heads can significantly enhance the throughput of the system.
WO2008/085474 discloses an apparatus for deposition of atom layers. A deposition head is provided by a stack of platelets, which, in view of the large number of platelets and the complicated flow paths can be problematic. A challenge exist to provide an injector head that is manufacturable and provides for the necessary homogeneity of the flow of process gasses.
Accordingly, it is an object, according to an aspect of the invention, to provide an apparatus and method for atomic layer deposition with improved homogeneity of the process gases, wherein a reliable and stable slit width is provided and a compact design can be provided.
Accordingly, an injector head is provided for atomic layer deposition on a substrate, comprising a plurality of monolithic bars coupled to a connection unit. The bars have side walls with a spacer profile, respectively stacked against side walls of a neighbouring bar to form a plurality of stacked bars. The bars comprise slots extending over a length of the bar in communication with a respective slot in the manifold. A flow path is defined through the bar with a relatively low friction factor to form a respective precursor drain; reactant drain or barrier gas drain. The spacer profiles define slits extending between adjacent bars in communication with a respective slot in the manifold. A further flow path is formed along the bar with a relatively high friction factor, to form a respective precursor gas supply; reactant gas supply or flow barrier. By the slotted bar design, at the same time accurately formed slits can be formed while ensuring mechanical integrity by the monolithic bar design. This significantly enhances manufacturability and facilitates compliance to design specification.
The invention will now be described, in a non-limiting way, with reference to the accompanying drawings, in which:
Unless stated otherwise, the same reference numbers refer to like components throughout the drawings.
The precursor and reactant supplies 4, 40 are preferably designed without substantial flow restrictions to allow for plasma deposition. Thus, towards a substrate surface 5, plasma flow is unhindered by any flow restrictions.
In this embodiment, a precursor gas is circulated in the deposition space 2 by a flow alongside the substrate surface 5. The gas flow is provided from the precursor supply 4 via the deposition space to the precursor drain 6. In use the deposition space 2 is bounded by the injector head 1 and the substrate surface 5. Gas bearings 7 are provided with a bearing gas injector 8 arranged adjacent the deposition space, for injecting a bearing gas between the injector head 1 and the substrate surface 5, the bearing gas thus forming a gas-bearing while confining the injected precursor gas to the deposition space 2. The precursor drain 6 may additionally function to drain bearing gas preventing flow of bearing gas into the deposition space 2, 3.
While in the embodiment each gas bearing 7 is shown to be dimensioned as a gas bearing, in principle, this is not necessary; for example, a flow barrier separating the deposition spaces 2, 3 need not be dimensioned as a gas bearing as long as an effective flow barrier is provided. Typically, a flow barrier may have a gap height that is larger than a gap height wherein a gas bearing is effective. In practical examples, the gas bearing operates in gap height ranges from 5 um-100 um; wherein a flow barrier may still be effective above such values, for example, until 500 um. Also, gas bearings 7 may only be effective as flow barrier (or gas bearing for that matter) in the presence of substrate 9; while flow barriers may or may not be designed to be active irrespective of the presence of substrate 9. Importantly, flow of active materials between deposition spaces 2, 3 is prevented by flow barriers at any time to avoid contamination. These flow barriers may or may not be designed as gas bearings 7.
While
A support part 10 may provided that provides a carrier less support for substrate 9 along a conveying plane which may be seen as the centre line of substrate 9. The support part 10 is arranged opposite the injector head and is constructed to provide a gas bearing pressure arrangement that balances the injector head gas-bearing 7 in the conveying plane. Although less then perfect symmetrical arrangements may be feasible to provide the effect, preferably, the balancing is provided by having an identical flow arrangement in the support part as is provided by the injector head 1. Thus, preferably, each flow ejecting nozzle of the support part 10 is symmetrically positioned towards a corresponding nozzle of the injector head 1. In this way, the substrate can be held supportless, that is, without a mechanical support, by said gas bearing pressure arrangement in between the injector head 1 and the support part 10. More in general, a variation in position, along the conveying plane, of flow arrangements in the injector head 1 and in the support part 10, that is smaller than 0.5 mm, in particular smaller than 0.2 mm, may still be regarded as an identical flow arrangement. In the example, by absence of any mechanical support, a risk of contamination of such support is prevented which is very effective in securing optimal working height of the injector head 1 relative to the substrate 9. In addition, less down time of the system is necessary for cleaning purposes. Furthermore, importantly, by absence of a mechanical support, a heat capacity of the system can be reduced, resulting in faster heating response of substrates to production temperatures, which may significantly increase production throughput and reduce power consumption.
In this respect, the deposition space defines a deposition space height D2 relative to a substrate surface; and wherein the gas bearing 7, functioning as flow barrier, comprises a flow restricting surface 11 facing a substrate surface 5, defining, relative to a substrate, a gap distance D1 which is smaller than the deposition space height D2. The deposition space is provided with a precursor supply 4 and a precursor drain 6. Said supply and drain may be arranged for providing a precursor gas flow from the precursor supply via the deposition space to the precursor drain. In use, the deposition space is bounded by the injector head 1 and the substrate surface. The deposition space may be formed by a cavity 29, having a depth D2−D1, in which the supply and drain end and/or begin. Thus, more in general, the cavity is defined in the deposition head 1 and is, in use, facing the substrate 9. By having the cavity 29 facing the substrate, it is understood that the substrate is substantially forming a closure for the cavity, so that a closed environment is formed for supplying the precursor gas. In addition, the substrate may be provided such that various adjacent parts of the substrate or even adjacent substrates or other parts may be forming such closure. The apparatus may be arranged for draining the precursor gas by means of the precursor drain 6 of the deposition head 1 from the cavity for substantially preventing precursor gas to escape from the cavity. It may be clear that the bearing supply may be positioned at a distance from the cavity. The cavity may enable to apply process conditions in the cavity that are different from process conditions in the gas-bearing layer. Preferably, the precursor supply 4 and/or the precursor drain 6 are positioned in the cavity.
The depth D2−D1 of the cavity 29 may be defined as a local increase in distance between the substrate 9 and an output face of the injector head provided with the bearing gas injector 8 and the precursor supply. The depth D2 minus D1 may be in a range from 10 to 500 micrometers, more preferably in a range from 10 to 100 micrometers.
The flow restricting surface 11 may be formed by projecting portions 110 including bearing gas injector 8. The gas-bearing layer in use is for example formed between the surface 5 and the flow restricting surface 11. A distance C1 between the precursor drains 30 may typically be in a range from 1 to 10 millimeter, which is also a typical width of the deposition space 2, 3. A typical thickness of the gas-bearing layer, indicated by D1, may be in a range from 3 to 15 micrometer. To accommodate for various surface flatness qualities, however, the bearing gap may larger than 15 micrometer, for example, extended to larger dimensions, for example, up to 70 micrometer. A typical width C2 of the projecting portion 110 may be in a range from 1 to 30 millimeter. A typical thickness D2 of the deposition space 2 out of the plane of the substrate 9 may be in a range from 3 to 300 micrometer.
This enables more efficient process settings. As a result, for example, a volumetric precursor flow rate injected from the supply 4 into the deposition space 2 can be higher than a volumetric flow rate of the bearing gas in the gas-bearing layer, while a pressure needed for the injecting of the precursor gas can be smaller than a pressure needed for injecting the bearing gas in the gas-bearing layer. It will thus be appreciated that the thickness D1 of the gas-bearing layer 7 may in general be less than a thickness D2 of the deposition space 2, measured in a plane out of the substrate surface.
At a typical flow rate of 5·10−4-2·10−3 m3/s per meter channel width and a typical distance of L=5 mm, e.g. being equal to a distance from the precursor supply to the precursor drain, the channel thickness Dc, e.g. the thickness D2 of the deposition space 2, should preferably be larger than 25-40 μm. However, the gas-bearing functionality preferably requires much smaller distances from the precursor injector head to the substrate, typically of the order of 5 μm, in order to meet the important demands with respect to stiffness and gas separation and in order to minimize the amount of bearing gas required. The thickness D2 in the deposition space 2 being 5 μm however, with the above-mentioned process conditions, may lead to unacceptably high pressure drops of ˜20 bar. Thus, a design of the apparatus with different thicknesses for the gas-bearing layer (i.e. the thickness D1) and deposition space (i.e. the thickness D2) is preferably required. For flat substrates, e.g. wafers—or wafers containing large amounts of low aspect ratio (i.e. shallow) trenches 8 having an aspect ratio A (trench depth divided by trench width)≦10—the process speed depends on the precursor flow rate (in kg/s): the higher the precursor flow rate, the shorter the saturation time.
For wafers containing large amounts of high aspect ratio (i.e. deep narrow) trenches of A≧50, the process speed may depend on the precursor flow rate and on the precursor partial pressure. In both cases, the process speed may be substantially independent of the total pressure in the deposition space 2. Although the process speed may be (almost) independent of total pressure in the deposition space 2, a total pressure in the deposition space 2 close to atmospheric pressure may be beneficial for several reasons:
The lower limit of the gas velocity vg in the deposition space 2 may be determined by the substrate traverse speed vs: in general, in order to prevent asymmetrical flow behaviour in the deposition space 2, the following condition should preferably be satisfied:
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This condition provides a preferred upper limit of the thickness D, D2 of the reaction space 3. By meeting at least one, and preferably all, of the requirements mentioned above, an ALD deposition system is obtained for fast continuous ALD on flat wafers and for wafers containing large amounts of high aspect ratio trenches.
Accordingly, in use, the total gas pressure in the deposition space 2 may be different from a total gas pressure in the additional deposition space 3. The total gas pressure in the deposition space 2 and/or the total gas pressure in the additional deposition space 3 may be in a range from 0.2 to 3 bar, for example 0.5 bar or 2 bar or even as low as 10 mBar, in particular, in a range of 0.01 bar to 3 bar. Such pressure values may be chosen based on properties of the precursor, for example a volatility of the precursor. In addition, the apparatus may be arranged for balancing the bearing gas pressure and the total gas pressure in the deposition space, in order to minimize flow of precursor gas out of the deposition space.
In the shown embodiment the conveying system is provided with pairs of gas inlets 181 and outlets 182 facing the conveying plane and providing a flow 183 along the conveying plane from the outlet 182 towards the inlet 181. For clarity reasons only one pair is referenced in the figure. A gas flow control system is arranged to provide a gas bearing pressure and a gas flow 183 along the conveying plane, to provide movement of the substrate 9 along the conveying plane along a center line through the working zone 16 by controlling the gas flow.
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The slits 161 thus defining a flow path along the bar 160 with a relatively high friction factor, to form a respective precursor gas supply; reactant gas supply or flow barrier. A typical slit width may be 40-200 micron, more particularly 50-125 micron. This provides a significant pressure drop in the supplies depositing the reaction gases and/or barrier gases near the substrate surface, providing excellent homogeneity in gas distribution, flow barrier and/or gas bearing functionality.
Stack assembly may be provided by shoulders 166 coupling to previously described shoulder pieces; and by pulling rods provided in through holes 67. These may be provided in selected elevations 69, or in side elevations 68 surrounding the through hole 67. These elevations may have polygon shape, in particular with a symmetry axis in the direction of flow. Other assembly techniques may be provided such as gluing, welding clamping etc.
It is one of the inventive insights, that the exhaust channels do not need a high friction factor, and therefore may be machined with relatively wide slot dimensions. Accordingly, a slot may have a slot width of 200-1000 micrometer. It is another inventive insight that the exhaust slots may be drilled with a channel width that may increase (to accommodate drilling equipment) in the direction from the deposition face 164, as long as the slot width is properly dimensioned near the exhaust 162 in the deposition space 2.
Accordingly, large elongated holes 162 are made in the centre of elongated bars 160. The centrally arranged relatively large machined slots do not deteriorate the stiffness of the bars 160, allowing accurate machining of the bars for precise definition of the slits 161.
It is noted that the friction factor F is inversely proportional to a slit channel length l, slit length L, and a cube of slit gap width d, according to the equality F˜1/l*L*d̂3. Since the side wall can be accurately dimensioned over the entire height of the bar 160, forming the length of the slit channel the flow homogeneity can be increased considerably. By selectively designed orifice areas in a sealing foil (not shown) that may be provided between the manifold block 170 and the slotted bars 160, a flow profile may be adjusted for the exhaust slots 162 and supply slits 161, in order to further balance a flow profile between the various channels.
While many slotted designs may be provided, preferably, the facing side 164 of the bars 160 has a contour 163 profiled to form deposition spaces 2. While
Opposite walls 165, 165′ of the bar 160 may have a similar profiled design, wherein the lower wall side 165′ ends in the recessed part 2 forming a supply slit in a deposition space for process gas injection. The spacer profile may in this way define a slit width of 10-250 micrometer.
Opposite to the lower wall 165′ the higher wall side 165 ends in contour 163. The contour 163 has a face side defining, relative to the substrate, gap distance smaller than the deposition space height to form the barrier gas injector, in the example formed by barrier gas injected along side wall 165. The spacer profiles on the profiled wall 165 are formed by interspaced elevations 69 provided on a planar bottom wall.
To further optimize the flow profile a distribution groove 72 may be provided below the elevations 69 seen in the direction of flow P. The groove may extend along a length of the side wall, substantially parallel to the face side, i.e. in a crossing direction relative to the flow P. The groove 72 may be provided adjacent the elevations 69 and may have a depth optimized to the flow, for example, about 150-200 micron and may be strip shaped to provide flow distribution over the elongation of the slit.
Preferably the groove has a widening part 73 adjacent the elevation further optimizing the flow profile. The groove may define a groove width of 1000-2500 micron and wherein the widening may be 100-500 micron.
Many profiled designs may provide for a gas flow with increased friction factor, in particular, a patterned profiling of microburls, semi-porous channel design, or interspaced elevations having polygon shape, in particular with a symmetry axis in the direction of flow. Depending on the design, the spacers themselves may introduce inhomogeneity in the gas flow through the slit. Preferably, the elevations 69 have a flow guide contour arranged to homogenize a gas flow below the interspaced elevations seen in the direction of flow.
Equally all kinematic inversions are considered inherently disclosed and to be within the scope of the present invention. The use of expressions like: “preferably”, “in particular”, “typically”, etc. is not intended to limit the invention. The indefinite article “a” or “an” does not exclude a plurality. For example, an apparatus in an embodiment according to the invention may be provided with a plurality of the injector heads. It may further be clear that the terms ‘relative motion’ and ‘relative movement’ are used interchangeably. Aspects of disclosed embodiment may be suitably combined with other embodiments and are deemed disclosed. Features which are not specifically or explicitly described or claimed may be additionally included in the structure according to the present invention without deviating from its scope.
Number | Date | Country | Kind |
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2010893 | May 2013 | NL | national |
Filing Document | Filing Date | Country | Kind |
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PCT/NL2014/050346 | 5/30/2014 | WO | 00 |