Multi-gas distribution injector for chemical vapor deposition reactors

• US 20060021574A1
• Filed: 07/29/2005
• Published: 02/02/2006
• Est. Priority Date: 08/02/2004
• Status: Abandoned Application

• Current Assignee: Veeco Instruments Incorporated
• Original Assignee: Veeco Instruments Incorporated
• Inventors: Armour, Eric A., Kats, Mikhail, Gurary, Alex, Doppelhammer, Robert, Tompa, Gary, Kadinski, Lev
• Application Number:
  US11/192,483
• Publication Number:
  US 20060021574A1
• Time in Patent Office: Days
• US Class Current: 118/715
• CPC Class Codes: C23C 16/45565 Shower nozzles
• CPC Class Codes: C23C 16/45572 Cooled nozzles
• CPC Class Codes: C23C 16/45574 Nozzles for more than one gas

Abstract

A gas distribution injector for chemical vapor deposition reactors has precursor gas inlets disposed at spaced-apart locations on an inner surface facing downstream toward a substrate carrier, and has carrier openings disposed between the precursor gas inlets. One or more precursor gases are introduced through the precursor gas inlets, and a carrier gas substantially nonreactive with the precursor gases is introduced through the carrier gas openings. The carrier gas minimizes deposit formation on the injector. The carrier gas openings may be provided by a porous plate defining the surface or via carrier inlets interspersed between precursor inlets. The gas inlets may removable or coaxial.

Claims

1. A method of chemical vapor deposition comprising:

(a) discharging at least one precursor gas as a plurality of streams into a reaction chamber through a plurality of spaced-apart precursor inlets in a gas distribution injector so that the streams have a component of velocity in a downstream direction away from said injector towards one or more substrates disposed in said chamber, said at least one precursor gas reacting to form a reaction deposit on said one or more substrates; and

, simultaneously,

(b) discharging at least one carrier gas substantially nonreactive with said at least one precursor gases into said chamber from said injector between a plurality of adjacent ones of said precursor inlets.

2. A method as claimed in claim 1 wherein said step of discharging said at least one carrier gas includes discharging said carrier gas through a porous structure in said injector extending between adjacent ones of said precursor inlets.

3. A method as claimed in claim 1, wherein said step of discharging said at least one carrier gas includes discharging said carrier gas through a plurality of spaced apart carrier inlets in said injector disposed between adjacent ones of said precursor inlets.

4. A method as claimed in claim 1, further comprising rotating said one or more substrates within said chamber about an axis extending in said downstream direction.

5. A method as claimed in claim 4, further comprising varying the mass flow rates per unit area of at least one of said gases with radial distance from said axis.

6. A method as claimed in claim 1, wherein said step of discharging at least one precursor gas includes discharging a first precursor gas and discharging a second precursor gas reactive with said first precursor gas.

7. A method as claimed in claim 6 wherein said steps of discharging said first and second precursor gases include discharging said first precursor gas through a plurality of first precursor inlets spaced apart from one another and discharging said second precursor gas through a plurality of second precursor inlets interspersed with said first precursor inlets, and wherein said step of discharging said carrier gas includes discharging said carrier gas between said first and second precursor inlets.

8. A method as claimed in claim 6, wherein said steps of discharging said first and second precursor gases includes discharging said first precursor gas and second precursor gasses as concentric streams through at least some of said precursor inlets, each such concentric stream including a stream of the second precursor gas at least partially surrounding a stream of the first precursor gas.

9. A method as claimed in claim 6 wherein said step of discharging said at least one carrier gas includes discharging said carrier through a plurality of carrier openings including a porous screen in said injector extending between adjacent ones of said first precursor inlets and said second precursor inlets.

10. A method as claimed in claim 6 wherein said step of discharging said at least one carrier includes discharging said carrier through a plurality of carrier openings including a plurality of spaced apart carrier inlets in said injector disposed between adjacent ones of said first precursor inlets and said second precursor inlets.

11. A method as claimed in claim 6 wherein said steps of discharging a first precursor gas and discharging a second precursor gas occur at least partially non-simultaneously with one another.

12. The method as claimed in claim 6, further comprising the step of rotating said one or more substrates within said chamber about an axis extending in said downstream direction, wherein said steps of discharging a first precursor and discharging a second precursor are performed so that at least one of said first and second precursors has a mass flow rate per unit area which varies with radial distance from said axis.

13. The method of claim 1 further comprising the step of individually controlling the flow rates of at least some of said streams by means of individual flow-restricting devices associated with individual ones of at least some of said inlets.

14. A gas distribution injector for a chemical vapor deposition reactor, said injector comprising a structure defining an interior surface facing in a downstream direction and having a horizontal extent, a plurality of precursor inlets open to said interior surface at horizontally-spaced precursor inlet locations, one or more precursor gas connections and one or more precursor manifolds connecting said one or more precursor gas connections with said precursor inlets, said structure including a porous element having first and second surfaces, said second surface of said porous element defining at least a portion of said interior surface between at least some of said precursor inlet locations, said structure further defining a carrier gas manifold at least partially bounded by said first surface of said porous element and at least one carrier gas connection communicating with said carrier gas manifold.

15. An injector as claimed in claim 14 wherein said plurality of precursor inlets includes first precursor inlets open to said interior surface at first precursor inlet locations and second precursor inlets open to said interior surface at second precursor inlet locations, said one or more precursor gas connections including one or more first precursor connections and one or more second precursor connections, said one or more precursor manifolds include one or more first precursor manifolds connecting said one or more first precursor connections with said first precursor inlets and one or more second precursor manifolds connecting said second precursor connections with said second precursor inlets, at least some of said first and second precursor inlet locations being interspersed with one another over at least part of the horizontal extent of said interior surface, said porous element extending between at least some of said first and second precursor inlet locations.

16. An injector as claimed in claim 14 wherein said structure further defines one or more coolant passages, said coolant passage bounded by coolant passage walls defining a serpentine path for the coolant passage there through, said coolant passage not in fluid communication with said precursor inlets or said carrier gas manifold, said precursor inlets extending through said coolant passage walls, and said coolant passage coupled to a coolant entry port and a coolant exhaust port for communication of a coolant there through.

17. An injector as claimed in claim 16 wherein said carrier gas manifold is disposed between said porous element and said one or more coolant passages.

19. An injector as claimed in claim 15 wherein said first precursor inlets are disposed in a plurality of concentric zones on said interior surface, said one or more first precursor gas connections include a plurality of first precursor connections, said one or more first precursor manifolds including a plurality of first precursor manifolds each said first precursor manifold being connected to the first precursor inlets in one of said zones.

20. An injector as claimed in claim 19 wherein said first precursor manifolds are concentric with one another.

21. An injector as claimed in claim 19 wherein said second precursor inlets are disposed in said plurality of zones, said one or more second precursor gas connections include a plurality of second precursor connections, said one or more second precursor manifolds including a plurality of second precursor manifolds, each said second precursor manifold being connected to the second precursor inlets in one of said zones.

22. The injector as claimed in claim 14, wherein said precursor connections define individual conduits connecting each of said precursor inlets to said one or more manifolds and include individual flow restriction elements associated with at least some of said conduits.

23. The injector as claimed in claim 15, wherein said precursor connections define individual conduits connecting each of said precursor inlets to said one or more manifolds and include individual flow restriction elements associated with at least some of said conduits.

24. The injector of claim 14, wherein said individual flow restriction elements are selected from the group consisting of orifices and porous bodies.

18. An injector as claimed in claim 18 wherein said one or more coolant passages are disposed between said carrier gas manifold and said at least one precursor gas manifold.

25. An injector for a chemical vapor deposition reactor comprising structure defining an inner surface facing in a downstream direction and extending in horizontal directions transverse to said downstream direction, said structure further defining a plurality of concentric stream inlets opening through said inner surface at horizontally-spaced stream locations, each said concentric stream inlet including a first gas channel open to said inner surface at a first port and a second gas channel open to the inner surface at a second port substantially surrounding the first port, said structure further including at least one first gas manifold connected to said first gas channels, at least one second gas manifold connected to said second gas channels.

26. The injector of claim 25, further comprising a carrier gas manifold at least partially bounded by said inner surface and including a porous screen on said inner surface in said regions of said inner surface between said plurality of concentric stream inlets, said carrier gas manifold connected to said porous screen.

27. The injector of claim 25, further comprising a third gas manifold, each said concentric stream inlet including a third gas channel open to said inner surface at a third port substantially surrounding the first port, said structure further including a the third gas manifold connected to said third gas channels, wherein at least one of said first, second and third gas inlets is a carrier gas inlet and at least one of a said first, second and third gas manifolds is a carrier gas manifold.

28. An injector as claimed in claim 25 wherein said structure includes a downstream plate defining said inner surface, and a coolant chamber upstream from said downstream plate, each said concentric stream inlet including a first tube and a second tube surrounding one said first tube and in thermal communication with said coolant chamber but not in fluid communication with said coolant chamber.

29. An injector as claimed in claim 28 wherein said at least one first gas manifold includes a horizontally-extensive first gas chamber, said at least one second gas manifold includes a horizontally-extensive second gas chamber disposed downstream of said first gas chamber, said first tubes communicating with said first gas chamber and extending downstream through said second gas manifold but not in fluid communication therewith, said second tubes communicating with said second gas manifold.

30. An injector as claimed in claim 29 wherein said stream locations are arranged in a plurality of substantially concentric zones having an axis extending in said downstream direction, said structure including walls subdividing at least one of said chambers into a plurality of sub-chambers concentric with said axis, said structure further including a separate gas connection communicating with each said sub-chamber for supplying gas thereto.

31. An injector as claimed in claim 26, wherein said injector comprises first, second and third plates secured to one another to form a body with said third plate downstream of said second plate and with said second plate downstream of said first plate, wherein said first gas manifold is located upstream of said first plate, said second gas manifold is located between said first plate and said second plate, said carrier gas manifold is located between said second plate and said third plate, and said carrier gas screen is located in said third plate.

32. The injector of claim 31, wherein said structure includes a coolant chamber located in said second plate, each said first inlet including a first tube, each said second inlet including a second tube surrounding one said first tube and in thermal communication with said coolant chamber but not in fluid communication with said coolant channel.

33. A CVD reactor including an injector as claimed in claim 25, a reaction chamber and a substrate carrier mounted in said reaction chamber downstream from said injector, said carrier being rotatable about an axis extending in said downstream direction.

34. A gas distribution system for a CVD reactor, comprising:

a gas distribution injector structure defining an inner surface facing in a downstream direction and extending in horizontal directions transverse to the downstream direction, said injector structure defining a plurality of precursor inlets open to said inner surface at horizontally-spaced precursor inlet locations, said injector structure also defining a plurality of carrier gas openings open to said inner surface between said precursor inlet locations;

at least one precursor gas source connected to said precursor inlets for supplying at least one precursor gas; and

at least one carrier gas source connected to said carrier gas openings for supplying at least one carrier gas substantially nonreactive with said at least one precursor gas to said carrier openings so that said carrier gas inhibits deposits formed from said at least one precursor from depositing on said inner surface.

35. A system as claimed in claim 34 wherein said injector structure includes a porous element defining at least a portion of said inner surface and defining at least some said carrier openings.

36. A system as claimed in claim 35 wherein said porous element substantially surrounds each of said precursor inlet locations and said porous element extends between each pair of mutually-adjacent precursor inlet locations.

37. A reactor including a reactor chamber defining an interior space, an injector as claimed in claim 34 connected to said reactor chamber with said inner surface facing into the interior space and with said openings of said inlets communicating with said interior space.

38. A system as claimed in claim 34 wherein said precursor inlet locations are disposed in a first pattern and wherein said injector structure includes a plurality of carrier inlets defining said carrier openings at a plurality of horizontally-spaced carrier locations in a second pattern interspersed with said first pattern.

39. A system as claimed in claim 38 wherein said second pattern of carrier inlets are evenly distributed in the spaces between said first pattern of precursor inlets.

40. A system as claimed in claim 38, wherein the plurality of reactor inlets and the plurality of carrier inlets form a checkerboard pattern on the injector body.

41. A system as claimed in claim 34 wherein said precursor inlets are disposed on said inner surface in a plurality of zones, and wherein said at least one precursor gas source includes a plurality of precursor gas sources, the precursor inlets in different ones of said zones being connected to different ones of said precursor gas sources.

42. A system as claimed in claim 34 wherein said plurality of precursor inlets includes first precursor inlets open to said interior surface at first precursor inlet locations and second precursor inlets open to said interior surface at second precursor inlet locations, said one or more precursor gas sources including one or more first precursor gas sources connected to said first precursor inlets and one or more second precursor gas sources connected to said second precursor inlets, at least some of said first and second precursor inlet locations being interspersed with one another over at least part of the horizontal extent of said interior surface, said carrier inlet openings being disposed between at least some of said first and second precursor inlet locations.

43. A system as claimed in claim 42 wherein said first and second precursor inlets are disposed on said inner surface in a plurality of zones, and wherein said at least one first precursor gas source includes a plurality of precursor gas sources, the first precursor inlets in different ones of said zone being connected to different ones of said precursor gas sources.

44. A system as claimed in claim 34, wherein at least some of said precursor inlets are dual-port inlets, each such dual-port inlet including a first injection channel and a second injection channel extending side-by-side and a common wall separating said channels from one another, and wherein said at least one precursor source includes a first precursor source connected to said first channels and a second precursor source connected to said second channels.

45. A system as claimed in claim 34, wherein at least some of said precursor inlets are concentric inlets, each such dual-port inlet including a first injection channel and a second injection channel surrounding said first injection channel, and wherein said at least one precursor source includes a first precursor source connected to said first channels and a second precursor source connected to said second channels.

46. An injector for a chemical vapor deposition reactor comprising structure defining an inner surface facing in a downstream direction and extending in horizontal directions transverse to said downstream direction, said structure further defining at least one manifold and a plurality of inlets opening through said inner surface at horizontally-spaced inlet locations and individual conduits connecting each of said inlets to one said manifold, said structure including individual flow restriction elements associated with at least some of said conduits.

47. An injector as claimed in claim 46 wherein said structure includes one or more plates defining said manifold and at least a part of each said individual conduit, and wherein said flow restriction elements are individually detachable from said one or more plates.

48. The injector of claim 47, wherein said individual flow restriction elements include porous bodies disposed within at least some of said conduits.

49. The injector of claim 47 wherein said flow restriction elements include orifice elements disposed at said inner surface, said orifice elements defining the openings of said inlets at said inner surface.