Method for diffusion limited mass transport
Abstract
Method and apparatus for continuously carrying out mass transfer reactions in a reaction chamber utilizing 15 laminar flow to provide diffusion limited transport and to provide isolation between process steps. There is provided a gaseous phase material inlet filter tube to introduce gaseous phase material in laminar flow within a reaction zone and an exhaust pressure baffle to maintain 2θ laminar flow throughout the reaction zone. Substrates may be continuously passed through a reaction zone to provide an inline system.

Term
Term ended
Expired 27 June 1989, 37.2 years ago.
- Priority and filed
- Granted
- Expired
- Today
4 claims: 1 independent, 3 dependent
- 1What is claimed is:1. A method for continuously effecting uniform vapor transport between gaseous phase material and substantially flat substrate surfaces in a process tube including at least one continuously open chamber having a longitudinal axis comprising the steps of: establishing in said continuously open chamber a first zone by providing a uniform laminar flow of a first gaseous phase material transverse to the longitudinal axis of said chamber and parallel to said substrate surfaces, said uniform laminar flow being maintained substantially throughout the length of said first zone;establishing a vapor transport zone, contiguous to said first zone, in said continuously open chamber by providing a uniform laminar flow of a second gaseous phase material parallel to and in the same direction as said first gaseous phase material, said uniform laminar flow being maintained throughout the length of said vapor transport zone, the flow rate of said second gaseous phase material being such as to prevent intermixing with said first gaseous phase material by turbulence;and passing substrates longitudinally through said first zone and said vapor transport zone in a direction perpendicular to the flow of said gaseous phase materials, said flat substrate surfaces being substantially parallel to the flow of said gaseous phase materials in order to effect substantially constant diffusion limited vapor transport between said second gaseous phase material and said substrate surfaces.
43 paragraphs in 3 sections, as filed
BRIEF DESCRIPTION OF THE DRAWINGS
The foregoing and other objects, features and advantages of the invention will be apparent from the following more particular description of a preferred embodiment of the invention, as illustrated in the accompanying drawings.
FIG. 1 is an overall isometric view of a preferred embodiment of the instant invention.
FIG. 2 is a schematic plan view of a portion of the deposition zone of the apparatus of FIG. 1.
FIG. 3 is a vertical schematic section of the deposition zone of FIG. 2 showing the velocity profile of reactant gases under ideal conditions.
FIG. 4 is a plot of deposition growth rate versus distance for diffusion limited mass transport.
FIG. 5 is a schematic overall view of the process tube of FIG. 1.
FIG. 6 is a detailed elevation of the left end, or entrance gate, of the process tube of FIG. 1.
FIG. 7 is a detailed section of the process tube of FIG. 1 taken at 7-—7.
FIG. 8 is a partial isometric sectional view showing the inside of the pre-bake and part of the deposition zone taken at 8—8 of FIG. 7, as seen from the rear of the process tube of FIG. 1.
GENERAL DESCRIPTION
Although the method and apparatus of the instant invention may generally be applicable to many vapor transport processes, only a typical reaction will be specifically referred to. The reaction that is illustratively employed to demonstrate the preferred embodiment of the instant invention is the reduction of silicon tetrachloride by hydrogen, described by the equation:
Heat
SiCh + 2Hj <=> Si + 4HC1
In actuality the reaction is more complex and depends upon reactant concentrations, temperature, pressure and reactor geometry, all of which may result in various side reactions. Since the reaction is reversible, etching and 50 other mass transport processing may also occur. It will be apparent to those skilled in the art that other vapor transport reactions may be similarly utilized. For example, the following reactions are possible: disproportionation, decomposition, condensation and gas cracking. Addi- 55 tionally, since a number of such reactions are reversible, the removal of films, or material, from substrate surfaces, as well as the deposition of material, is possible. Thus, reference to vapor deposition processes in describing the instant invention may also be considered to include any 60 heat induced chemical vapor deposition or etching process.
DETAILED DESCRIPTION
Referring now to FIG. 1, there is shown an isometric view of a preferred embodiment of the present invention, 65 generally designated 10. The process tube 10 is generally rectangular in cross section and has provided at one end an entrance gate 12 and at the other end an exit gate 14, both to be described more fully later. The central portion of the process tube 10 between the entrance and exit 70 gates comprises a continuously open chamber divided into three portions or process zones, i.e., prebake, deposition, and cooling. A number of gas inlet tubes 16-24 are provided to supply gases to the various zones. Exhaust gases leave the process tube through exhaust tubes 26 after 75
72,948 passing directly across process tube 10. Cooling water is circulated through a water jacket fed by water inlet tubes 28 and water exit tubes 30 mounted on the top and bottom of process tube 10. Substrates are mounted on car5 riers 32 which may be continuously passed through process tube 10 in a direction perpendicular and parallel to the gas flow. There is also provided a viewing port 34 for inprocess inspection of substrates as they pass through the deposition zone.
Before describing the process tube of FIG. 1 in greater detail, a brief description of the broad aspects of the operation of the process tube will be provided.
FIG. 2 schematically shows a plan view of an ideal deposition, or vapor transport, zone. In order to pass the 15 gaseous phase reactant material through the transport zone parallel to and over the flat surface of substrates 36 there is provided a fritted quartz, or sintered stainless steel, filter tube 38, preferably having a pore size of about 10 microns. The filter tube behaves exactly as the classical 20 porous plug and similarly there is no enthalpy change as the reactant gases pass through the walls of the filter tube. The reactant gases are uniformly passed into the deposition zone along the entire length of filter tube 38. Since the filter tube 38 substantially fills the entire end of 25 the deposition zone, as will be more clearly shown in reference to FIG. 8, the gases leaving the filter tube create substantially linear laminar flow throughout the entire deposition zone. Provided on the opposite side of process tube 10, after the reactant gases have passed over the 30 surface of substrate 36, there is provided an exhaust baffle 40. Exhaust baffle 40 allows for the uniform removal of gaseous reactant materials and deposition process byproducts. The exhaust baffle 40 may be, for example, a perforated steel plate or a sintered stainless steel filter 35 plate having a porosity sufficient to provide a back pressure a number of orders of magnitude greater than the longitudinal pressure drop in the exhaust plenum 42. Preferably exhaust baffle 40 is a perforated steel plate having 1 mil holes at 1000/in.<sup>2</sup>. The filter tube 38 and the exhaust 40 baffle 40 act together to provide laminar flow across the surface of substrate 36, as shown by the parallel lines in FIG. 2.
FIG. 3 shows the ideal condition of laminar flow, in a vertical plane. The velocity profile 44 is shown to illustrate how the diffusion limited transport takes place. The velocity of reactant gases parallel to substrate surfaces is zero at the substrate surfaces and progressively greater, up to a maximum velocity, through the deposition zone. Reactant material concentration is depleted from the gaseous material in close proximity to the substrate surface. This causes a net concentration unbalance and results in diffusion in the direction of the depleted area—i.e., toward the substrate surface. The substrates are heated, by means not shown, to the desired reaction temperature and as reactants diffuse toward this hot surface they pass through a temperature gradient which, at the substrate surface, is sufficient to cause the desired reaction to occur. Because the reactant gases are passed parallel to the substrate surfaces in laminar flow it is possible to maintain a substantially uniform, and controllable, deposition rate. Thus, the deposition, or other vapor phase reaction, is limited by the diffusion rate into the depleted boundary zone. Because turbulent flow is not used, no unpredictable irregularities in the flow pattern can cause irregular deposition rates at different parts of a substrate surface.
It should be noted that because some of the gaseous reactants are removed from the vapor stream as it passes over the substrate and carrier, the net concentration of the reactants will be decreased as the distance from initial deposition increases thus decreasing the diffusion or deposition rate at points further from the edge of the substrate carrier as shown in FIG. 4.
FIG. 4 is a plot of the deposition growth rate versus the distance from the initiation of deposition across the flat surface of the substrate and substrate carrier. The tion may be accomplished as shown in FIG. 5. Hydrogen gas, a carrier, supplied to both the pre-bake and cooling zones, is fed into the system through a single inlet manifold 53. Reactant gases H<sub>2</sub> and SiCl<sub>4</sub>, are added in a separate line leading to the deposition zone.
Because laminar flow is maintained in each of the three zones, there is virtually no intermixing between zones, except for a slight amount of diffusion caused by the presence of a concentration gradient between adjoining zones. The use of laminar flow allows a multiple step deposition process to be carried out in a single chamber without need for barriers or other inter-process isolation devices. As previousy referred to, other mass transport process steps may be carried out in adjacent zones without the need for physical inter-process isolation devices.
Also shown in FIG. 5 are two optional heat shields 54 and 56 which may be utilized to reduce the loss of heat radiating from heated substrates 36 without substantially effecting the laminar flow of gases through the reaction zone. The heat shields may, for example, be sheets of perforated 0.060 inch thick molybdenum with approximately 10 percent open area. An economic evaluation should be made to determine to what extent laminar flow may be sacrificed in order to provide the benefit of reducing radiant heat lost by the wafers.
Having described the broader aspects of the method and apparatus of the present invention, a more detailed description of the preferred embodiment follows.
Referring again to FIG. 1 it will be recalled that the preferred embodiment of process tube 10 consists of a long rectangular tube having an entrance gate 12 and an exit gate 14. The process tube may, for example, be about 10 feet long. The entrance and exit gates are similar in construction and provide means for passing substrates into and away from the process zones. FIG. 6 shows an elevation view of entrance gate 12. The gate may be constructed of a top and bottom slotted plate, 58 and 60, which are machined such that a substrate carrier 32 will pass through the slot with a minimum clearance. An inert gas, for example, argon, is continuously fed into the gate through tube 62 which communicates with the slot in plates 58 and 60. The longitudinal location of tube 62 on top plate 58 is determined depending upon the size of the opening between the slot and the substrate carrier, the difference in pressure between the atmosphere and the inside of the process tube and the extent to which argon leakage into the process tube can be tolerated.
It is preferable that a net flow rate of argon into the process tube be about 1 liter per minute and about 2 liters per minute into the atmosphere. Depending upon the length of the entrance, or exit, gate, sufficient positive pressure should be maintained to prevent any leakage from the system.
Substrate carriers 32 may be constructed of high purity <sup>J</sup> commercially available graphite and have a longitudinal guide made of pyrolytic graphite or molybdenum which runs along the entire edge of the carrier. The carrier 32 is generally rectangular, preferably square, and must have relatively flat leading and trailing edges in order to provide a seal between carriers as they pass continuously through the process tube. Substrates are mounted on carriers 32 with their flat deposit receiving surfaces flush with the top of the carrier, in order to prevent turbulence inside the process tube. The carrier must be sufficiently larger than substrates in order to get the flat portion of the growth curve to fall on the substrate. Carriers may be fed into the process tube by any of the available feeding mechanisms of the prior art capable of presenting a continuous string of carriers to the process tube.
Referring now to FIGS. 7 and 8 which show the elements inside process tube 10, it will be seen that the process tube is divided into three separate levels. The deposition, or vapor transport, zone as previously described, being in the center.
3,672,1 maximum growth rate is reaction limited and occurs only While the concentration of the reactants remains constant. This condition Only occurs at the first point of deposition as the concentration after deposition begins will decrease, thus preventing the reaction limited rate from controlling. 5 After deposition begins, in a laminar flow system, the deposition growth rate is diffusion limited and dependent upon the velocity of the parallel flowing reactant gases moving over the substrate surface. At a selected velocity, for example 10 cm./sec., the deposition rate will be almost flat 10 a short distance away from the beginning of deposition as indicated at 41. If substrates are not mounted at the edge of the substrate carrier, but are set back as shown in FIGS. 2 and 3, the entire substrate will fall into the flat portion of the diffusion limited transport rate curve, 15 41. Unlike a turbulent system, which operates on the nearly vertical portion Of the curve, the laminar flow system is more closely controllable and thereby more easily reproducible. Since the deposition rate curve still decreases slightly with distance it is preferable to pass reactant ma- <sup>20 </sup>terials over only a single substrate in order to minimize the effects of the decreased rate. ..
It will also be seen, for the particular reaction used as an example, that if the concentration in the gaseous phase materials were less than that in the area close to the sub- <sup>25 </sup>strate surface a reversal of the diffusion limited transport would occur and etching, or removal of the material, of a substrate would be possible. For example, if HC1 were utilized as a reactant gas and the substrate surface was silicon, a reversal of the above-referred to reaction, the <sup>30 </sup>production of SiCl<sub>4</sub> and H<sub>2</sub>, would occur.
Referring now to FIG. 5, there is shown a schematic diagram of a preferred form of the invention. The drawing shows a deposition zone located generally in the center of the process tube. This zone operates exactly as de- <sup>35 </sup>scribed above in reference to FIGS, 2 and 3. As referred to previously, the deposition zone may include one or more separate mass transport process steps. However, in order to provide a controlled environment for substrate surfaces entering the deposition zone there is provided a pre-bake zone. The purpose of. the pre-bake zone is to raise the temperature of the substrate carried on substrate carrier 32 to the proper reaction temperature before they enter the deposition zone. This is achieved by a resistance heating element, not shown, located under the substrate car- 45 tiers 32 and extending for substantially the entire length Of the pre-bake and deposition zones. While the substrates are being heated, high purity hydrogen gas is admitted to the pre-bake zone through a pre-bake filter tube 52 in order to ensure that no impurities enter the deposition 50 zone and to avoid side reactions. The structure of the pre-bake zone is the same as that of the previously described deposition zone. That is, the hydrogen travels parallel to and across the wafer surfaces in laminar flow.
Located downstream from the deposition zone is a cooling zone. The zone like the pre-bake and deposition zones also contains gas in laminar flow as delivered by cooling filter tube 53. The purpose of the cooling zone is to remove any traces of SiCl<sub>4</sub> carried over from the deposition zone and to cool substrates prior to removal from the θθ process tube 10.
One of the criteria for successful operation of process tube 10 is that longitudinal flow of gaseous material cannot be permitted, as this would create mixing between the separate gases in each zone. To prevent longitudinal flow, 65 the pressure drop across each end of the process tube 10 must be the same. Since the pressure drop through the walls of the filter tubes is significantly greater than the axial pressure drop inside the tubes, the mass flow rate per unit length of filter tube is constant. And since the 70 mass flow rate through the filter tubes is only a function of pressure, the temperature being constant, the mass flow rate from the tubes will be constant for a constant inlet pressure. Other than providing an elaborate metering system for providing separate gas flows, pressure equaliza- 75
3,672,948
The transport zone is defined by the following elements. The substrate carrier 32 and guide tracks 64 form the bottom, perforated heat shields 54 and 56 the sides, and top heat shield 66 the top. The transport zone is defined longitudinally by the length of filter tube 38. 5
Mounted directly below the pre-bake zone, and running the length of the pre-bake and deposition zones, is a resistance heater strip 68 which is supported at a number of points along its length by refractory rods 70. Heater strip 68 may be made of graphite and is mounted at both ends 10 on a terminal block 72. Because the heater strip 68 expands when heated there is also provided at the entrance end (not shown) of process tube 10 a slide block containing compression springs to maintain the heater strip in an extended state. Connected to heater strip 68 at both 15 ends is an electrical terminal 74 which extends through the bottom plate of the process tube and is best illustrated in FIG. 7. Heater strip 68 is also utilized to maintain substrate surfaces at the desired transport process temperature in the transport zone. 20
In order to provide means for passing gaseous phase material parallel to the surface of the substrates and through the deposition zone there is provided, to the right of the heat shield 54, the deposition filter tube 38 which is connected to the middle gas manifold 17 through 25 the right side plate 76. Additionally, there is provided a top and bottom gas chamber partition 78 and 80 to confine the gaseous material to the proper zone.
To prevent deposition on top heat shield 66 a continuous flow of gas is maintained in contact with the heat shield 30 to maintain the temperature of heat shield 66 below the reaction temperature. The gas is provided by a top filter tube 82 mounted in side plate 76 and connected to top gas manifold 21. The gas may be hydrogen and it may be delivered from the same source as was discussed above 35 in reference to FIG. 5.
In order to prevent leakage from the deposition zone and to assist in preserving heat in the process tube, a bottom filter tube 84 is provided. Filter tube 84 is mounted directly beneath deposition filter tube 38 on right side plate <sup>48 </sup>76 and connected to bottom gas manifold 19. As the desired gas, for example argon, passes from tube 84 under guide tracks 64 it passes through heat shields 86. The gas applied to the bottom gas manifolds 16, 19, 22 may be delivered from a single supply. <sup>45</sup>
After the gases pass through the above described elements they encounter exhaust baffle 40 which functions as described above with reference to FIG. 2. The gases then leave the process tube by way of exhaust tube 26.
In order to control the temperature of the process tube 10 and to assist in removing excess heat from the deposition zone, the top and bottom of the process tube is provided with water jackets 88.
FIG. 7 also shows the detail of the viewing port 34 <sub>gg </sub>which is optional and may be constructed with materials well known in the art.
In summary, the preferred embodiment of FIGS. 1, 5, 6, 7, and 8 is designed to provide and maintain the proper conditions for diffusion limited mass transport <sub>60 </sub>as more generally described with reference to FIGS. 2, 3, and 4. In operating the process tube of the present invention, it should be realized that an initial start up period will be necessary. The heater strip should be energized and the carrier gas, hydrogen, should be applied 55 to all inlet manifolds to provide the proper heat exchange conditions. It is preferable that the process tube be filled with substrate carriers and scrap, or dummy, substrates in order that proper flow conditions may be obtained. Argon should be applied to both the entrance and exit gates to γθ prevent gases inside the process tube from escaping into the atmosphere. After the process tube has stabilized the reactant material, SiCl<sub>4</sub>, may be added to the hydrogen flow in the deposition zone in the desired proportion to carry out the deposition process. Substrates may then be continuously passed through the process tube for extended periods. Little or no deposition will be found on the internal elements of the system due to the fact that only substrates and substrate carriers will be at the proper deposition temperature.
While the invention has been particularly shown and described with reference to a preferred embodiment thereof, it will be understood by those skilled in the art that various changes in the form and details may. be made therein without departing from the spirit and scope of the invention.
Contents3
5 sheets
Sheet 1 Sheet 2 Sheet 3 Sheet 4 Sheet 5
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Priority claims1
| Document | Office | Kind | Date |
|---|---|---|---|
| 34570 | United States of America | A |
Members12
| Document | Office | Kind | |
|---|---|---|---|
| BE760041A | Belgium | A | |
| NL7018090A | Netherlands (Kingdom of the) | A | |
| DE2064470A1 | Germany | A1 | |
| FR2075030A5 | France | A5 | |
| CH520525A | Switzerland | A | |
| US3672948AThis record | United States of America | A | |
| ES386190A1 | Spain | A1 | |
| CA931025A | Canada | A | |
| GB1328390A | United Kingdom | A | |
| DE2064470B2 | Germany | B2 | |
| SE377430B | Sweden | B | |
| DE2064470C3 | Germany | C3 |
Numbers
- Application
- 345
Titles
- English
- METHOD FOR DIFFUSION LIMITED MASS TRANSPORT
Classification
- CPC, 8
- C23C16/45504
- C23C16/455
- C23C16/45519
- C23C16/54
- C30B25/14
- Y10S438/935
- Y10S438/907
- Y10S148/006
- IPC, 4
- C23C16 44
- C23C16 455
- C23C16 54
- C30B25 14