Method of forming refractory metal contact in an opening, and resulting structure

Information

  • Patent Grant
  • 6762121
  • Patent Number
    6,762,121
  • Date Filed
    Wednesday, April 4, 2001
    23 years ago
  • Date Issued
    Tuesday, July 13, 2004
    20 years ago
Abstract
A method of ensuring against deterioration of an underlying silicide layer over which a refractory material layer is deposited by physical vapor deposition (PVD) or chemical vapor deposition (CVD) is realized by first providing a continuous polysilicon layer prior to the refractory material deposition. The continuous polysilicon layer, preferably no thicker than 50 Å, serves a sacrificial purpose and prevents interaction between any fluorine that is released during the refractory material deposition step from interacting with the underlying silicide.
Description




FIELD OF THE INVENTION




This invention relates to a method of forming a refractory metal contact over a silicon substrate in a solid state structure, and to related structures. More particularly, the invention relates to a method employing a sacrificial silicon layer that serves as a nucleation layer for subsequent deposition of a refractory material to form a contact.




BACKGROUND OF THE INVENTION




Conductive metal contacts are frequently found in semiconductor devices, and typically are formed by deposition of a refractory material, such as tungsten or the like, confined by a silicon oxide layer previously deposited over a conducting substrate containing, for example, a silicide. Steps in the conventional method of forming such contacts, and the nature of a problem that sometimes arises, are best understood with reference to

FIGS. 1

,


2


,


3


and


4


(A)-(B) hereof.





FIG. 1

is a cross-sectional view of a relevant portion of the underlying structure, wherein an underlying silicide layer


100


serves as a substrate


4


with an oxide layer


102


formed thereon. The location, shape and size of the desired conductor is determined by a through opening


104


formed in the oxide layer


102


, with exposed surface


106


of the silicide serving as a bottom


106


of the opening


104


. As best seen in

FIG. 2

, a thin metallic layer


200


is then deposited at the bottom of aperture


104


to serve as a contact liner. Then, per

FIG. 3

, a thin nucleation layer


300


of a refractory material such as tungsten is formed in the presence of silane gas to cover oxide layer


102


, the sides


108


of aperture


104


, per liner


200


. This is followed, per FIG.


4


(A), by the deposition of a layer


400


containing the desired refractory material in an amount sufficient to totally cover and fill up the inside of aperture


104


and to extend over the upper surface of oxide layer


102


. Note that the nucleation layer


300


becomes, in effect, absorbed within the refractory layer


400


.




Unfortunately, when a refractory material such as tungsten is deposited from decomposition of WF


6


through the use of either physical vapor deposition (PVD) or chemical vapor deposition (CVD), particularly during a chemical vapor deposition step, some of the fluorine released from decomposition of WF


6


combines with silicon in the silicide layer


100


and a propensity to form an undesirable region


402


, as is probably best seen in the enlarged view in FIG.


4


(B).




An example of a prior patent which appears to address a similar problem is U.S. Pat. No. 5,804,499, to Dehm et al., titled “Prevention of Abnormal WSi


x


Oxidation by In-Situ Amorphous Silicon Deposition”, which suggests a process in which amorphous silicon is deposited in a thin layer on top of tungsten silicide to prevent abnormal WSi


x


oxidation during subsequent process steps. The layer of amorphous silicon as mentioned in this patent is bounded by a spacer also made of amorphous silicon. The reference does not teach the provision of a continuous layer of silicon to address the problem at issue.




The present invention seeks to address this particular problem in a simple and efficient manner.




SUMMARY OF THE INVENTION




This invention provides a method by which a refractory material may be deposited in and over an opening in a non-conducting layer over a conducting layer, employing a known PVD or CVD step, without damage to the underlying conducting layer.




The present invention also provides a structure which includes a refractory material contact formed over an opening in a non-conductive layer deposited over a conductive metal silicide layer.




Accordingly, in a first aspect of this invention, there is provided a method of filling an opening in an oxide layer, over a liner layer formed on a silicide layer underlying both the oxide layer and the liner layer, which includes the step of forming a continuous first layer of silicon on the oxide layer, a wall of the opening and the liner layer and, thereafter, forming a second layer of a refractory material on the first layer so as to cover the same and to also substantially fill the opening.




In another aspect of this invention, there is provided a multi-layer structure which includes a silicide layer having a first surface; an oxide layer formed on the first surface and having a second surface with a through opening defined in the oxide layer from the second surface to the first surface; a liner layer formed on the first surface at a bottom of the opening, a continuous silicon layer formed to extend over the second surface, the opening surface and the liner layer; and a refractory material layer formed on the silicon layer so as to substantially fill the opening.




These and other aspects, objectives and advantages of the present invention will become clearer from an understanding of the following detailed description with reference to the appended figures.











BRIEF DESCRIPTION OF THE DRAWINGS





FIGS. 1

,


2


,


3


and


4


(A)-(B) all relate to the prior art.





FIG. 1

is a cross-sectional view showing a metal silicide layer over which is formed a non-conducting oxide layer with a through aperture defined therein.





FIG. 2

is a cross-sectional view showing the structure per

FIG. 1

, with a metallic liner layer formed at a bottom surface of the aperture.





FIG. 3

is a cross-sectional view at a stage following

FIG. 2

, showing the deposition of a nucleation layer


300


of tungsten over the oxide layer, the sides of the opening formed therein, and the liner at the bottom of the opening.




FIG.


4


(A) is a cross-sectional view at a later stage in the known process, wherein a deposit of a refractory material covers the oxide layer and fills the opening above the liner, and also indicates the presence of an undesirable region that may sometimes be formed during deposition of the refractory material due to interaction with the underlying silicide.




FIG.


4


(B) is an enlarged view of a relevant portion of FIG.


4


(A), to show more clearly the undesired contamination of the underlying silicide layer at the bottom of the opening that is otherwise filled with refractory material.





FIG. 5

, per the method according to the present invention, is a cross-sectional view of the structure per

FIG. 2

with the deposit of a continuous silicon layer over the oxide layer, the sides of the opening formed therein, and the underlying liner at the bottom of the opening.





FIG. 6

is a cross-sectional view after deposition of a refractory material over the continuous silicon layer shown in FIG.


5


.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




As indicated above, the present invention is aimed at providing a method that ensures against contamination of an underlying silicide substrate by any constituent of a refractory conducting layer during its deposition into the desired structure.




Referring to the structure illustrated in cross-sectional view in

FIG. 2

, note that a silicide layer


100


, of the order of 300-800 Å in thickness and deposited on a silicon substrate


150


, typically serves as a substrate for an oxide layer


102


deposited thereon with a through opening


104


defined therein, with a liner layer


200


deposited at the bottom


106


of opening


104


in known manner. Liner layer


200


may comprise at least one of titanium, titanium nitride, tungsten, and an alloy of titanium and tungsten, and may incidentally be deposited on the oxide layer


102


. The preferred method according to this invention includes these steps of the prior art.




In the prior art, as best understood with reference to

FIG. 3

, a layer


300


of tungsten (W) deposited from WF


6


decomposition in the presence of silane was then formed as a nucleation layer.




According to the present invention, a continuous layer


500


of amorphous or polycrystalline silicon is deposited to a controlled thickness preferably by either physical vapor depositions (PVD) or by chemical vapor deposition (CVD), to extend over the oxide layer


102


and the upper surface of liner layer


200


. This is best understood with reference to FIG.


5


.




The continuous silicon layer


500


is intended to be a sacrificial layer, i.e., it is anticipated that it may chemically interact and combine with any fluorine (F) that becomes available when, for example, WF


6


is decomposed to generate a tungsten contact layer


400


. In other words, it is intended in the present invention that some of this silicon be consumed in preference to any silicon from the underlying silicide layer


100


. The deposited silicon layer


500


must be in the form of a continuous amorphous or polycrystalline silicon layer. The deposited polysilicon may be obtained by decomposition of a silane such as silane, disilane or trisilane. However, silanes containing ions such as dichlorosilane may advantageously be used and are preferred for this purpose.




The resulting structure is best understood with reference to

FIG. 6

, in which the silicide substrate


100


supports oxide layer


102


and liner


200


, and the continuous sacrificial amorphous or polycrystalline silicon layer


500


formed thereon serves as a base for the refractory layer


600


which extends over oxide layer


102


and substantially fills the opening


104


. Note that a small imperfectly filled region


502


may exist in the refractory material


600


within the volume of the substantially filled opening


104


without any deleterious effects on the resulting contact structure and its functionality.




The structure as illustrated in

FIG. 6

can then be subjected to conventional subsequent processing such as planarization of


600


,


500


and


200


.




As previously indicated, the present invention is intended to provide a satisfactory refractory layer while avoiding the known problems associated with the related prior art. It is intended, further, that the “refractory material” may be a refractory metal, e.g., tungsten, titanium, tantalum or molybdenum employed directly as a “metal”; a refractory metal employed as a constituent of a “compound” thereof, e.g., titanium nitride, tantalum nitride, etc.; or even as a constituent of an “alloy” with another metal, e.g., titanium-tungsten. With any of these available options, the provision of a continuous silicon layer as discussed above ensures against the known problem.




It is intended that the desired refractory material layer


600


be formed in known manner by either a PVD or CVD process step.




It is preferred that the continuous sacrificial silicon layer


500


be provided as an amorphous or polysilicon film of a thickness not greater than about 50 Å.




The application of the continuous sacrificial silicon layer


500


by either the PVD or the CVD process is preferably accomplished at a temperature in the range 500°-650° C., with 600° C. being particularly preferred. It should be noted that when a PVD process is employed there may be little or no deposition of the silicon on sides


108


,


108


of opening


104


.




It should also be noted that the traditional way of providing a silicon deposition is to flow the silane gas in one process chamber over the underlying structure and, subsequent to depositing the desired silicon layer, to move the wafer supporting the desired structure into another process chamber where a WF


6


environment, for example, could be provided for the subsequent step of depositing tungsten thereon. An obvious problem in doing this is that the timing and conditions required to form the proper layer of silicon to protect the wafer from the chemically active WF


6


gas has a narrow process window and is subject to control problems.




The present invention, by utilizing the silicon layer as it does, i.e., as both a sacrificial layer and a nucleation layer, advantageously eliminates the need to do this. In other words, the wafer may be maintained in a single chamber and first be exposed to the silane or dichlorosilane to obtain the desired silicon layer under controlled conditions of time, temperature and flow rate, and this may be followed by passage of WF


6


gas over the same wafer in the same chamber under appropriate process conditions of controlled temperature, pressure and flow rate. The process is readily adaptable to either physical vapor deposition or chemical vapor deposition conducted in known manner. Any adaptation to employ any refractory metal, compound or alloy, may be made in known manner. It is considered that under all circumstances such as these, the sacrificial use of the continuous polysilicon film as taught in this invention ensures against deterioration of the underlying silicide layer.




It is considered that persons of ordinary skill in the art will consider obvious modifications of the present invention, both of the method and of the structure, and all such modifications are considered to be comprehended within the present invention which is limited solely by the claims appended below:



Claims
  • 1. A method of filling an opening in an oxide layer, over a liner layer formed on a surface of a silicide substrate underlying both the oxide layer and the liner layer, the method comprising:forming a first continuous sacrificial layer comprising silicon, by either physical vapor deposition (PVD) or chemical vapor deposition (CVD) at a first temperature in the range 500° C. to 650° C. completely covering the oxide layer and the liner layer; forming a second layer, comprising a refractory material, on the first continuous sacrificial layer at a second temperature that is lower than the first temperature so as to cover the first layer and to also substantially fill the opening; and during said forming a second layer, sacrificing at least a portion of the first continuous sacrificial layer, wherein said sacrificing at least a portion of the first continuous sacrificial layer ensures against a deterioration of the silicide substrate underlying both the oxide layer and the liner layer.
  • 2. The method according to claim 1, wherein:the first continuous sacrificial layer is a continuous layer of one of amorphous or polycrystalline that has a thickness not greater than about 50 Å.
  • 3. The method according to claim 1, wherein the first temperature is approximately 600° C.
  • 4. The method according to claim 1, wherein:the refractory material contains a metal selected from a group of refractory metals consisting of titanium, tantalum, molybdenum and tungsten.
  • 5. The method according to claim 4, wherein:the refractory material comprises one of the selected metals deposited as a metal, as a component of a nitride of the metal, or as a component of an alloy of the metal.
  • 6. The method according to claim 1, wherein:the first continuous sacrificial layer sacrificially protects the underlying liner and the silicide substrate underlying both the oxide layer and the liner layer during the step of forming the second layer.
  • 7. The method according to claim 6, wherein:the first continuous sacrificial layer serves as a nucleation layer for deposition of the second layer thereon.
  • 8. The method according to claim 7, wherein:the first continuous sacrificial layer is a continuous polysilicon layer that has a thickness not greater than about 50 Å.
  • 9. The method according to claim 1 wherein:the first temperature is approximately 600° C.; and the second layer is formed at a second temperature that is lower than the first temperature.
  • 10. The method according to claim 1, wherein:the first continuous sacrificial layer is formed by a chemical vapor deposition (CVD) process and extends continuously on the oxide layer, a wall of the opening and the liner layer.
  • 11. The method according to claim 1, wherein:the liner layer comprises at least one of titanium, titanium nitride, tungsten, and an alloy of titanium and tungsten.
  • 12. The method according to claim 1 wherein said silicide substrate comprises:a first silicide layer formed on a silicon substrate.
  • 13. The method of claim 1 wherein the second layer is formed from a fluorine containing compound.
  • 14. The method of claim 13 wherein the fluorine containing compound comprises WF6.
  • 15. The method of claim 2 wherein the second layer is formed from a fluorine containing compound.
  • 16. The method of claim 15 wherein the fluorine containing compound comprises WF6.
US Referenced Citations (6)
Number Name Date Kind
5804499 Dehm et al. Sep 1998 A
5863170 Boitnott et al. Jan 1999 A
5963836 Kang et al. Oct 1999 A
6074443 Venkatesh et al. Jun 2000 A
6281118 Park Aug 2001 B1
6303480 Desai et al. Oct 2001 B1
Foreign Referenced Citations (1)
Number Date Country
WO 9900827 Jan 1999 WO