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Description  |
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BACKGROUND OF THE INVENTION
(1) Field of the Invention
The invention relates to a method of planarizing an integrated circuit
device, and more particularly, to a method of planarizing a submicron
integrated circuit device using spin-on-glass wherein the spin-on-glass
layer is thermally cured and then ion implanted to improve the outgassing
characteristics of the layer.
(2) Description of the Prior Art
In conventional planarization of the metallurgy-dielectric layers of an
integrated circuit, a metal is deposited and patterned by conventional
lithography and etching techniques. Then the dielectric layer, which is
typically silicon oxide material, is formed thereover. The dielectric
layer may now be etched back to planarize the metallurgy-dielectric
layers. There are basic problems in the choice of thickness of the
dielectric layer. The problems occur particularly where there are
substantially different heights on the surfaces of the integrated circuit,
particularly in the formation of memory word lines and the like in memory
products. For example, in the areas where contact is planned to be made to
the patterned metal, it is desired to have a thick dielectric layer to
keep planarity, but the thick dielectric will cause voids in other areas.
Alternatively, if a thin dielectric layer is used, there is lost planarity
in the contact area and etchback encroachment of the metal pattern, but
there will not be a void problem in other surface areas of the integrated
circuit. There is not a good solution for this planarity versus void
surface problem in the art.
The spin-on-glass materials have been used for planarization of integrated
circuits. The material to be applied is thoroughly mixed in a suitable
solvent. The spin-on-glass material suspended in the vehicle or solvent is
deposited onto the semiconductor wafer surface and uniformly spread
thereover by the action of spinning the wafer. The material fills the
indentations in the integrated circuit wafer surface, that is
planarization. Most of the vehicle or solvent is driven off by a low
temperature baking step often followed by vacuum degassing. Other coatings
of the spin-on-glass material are applied, baked and vacuum degassed until
the desired spin-on-glass layer is formed.
The final step in the making of the spin-on-glass layer is curing. Curing
is a high temperature heating step to cause the breakdown of the silicate
or siloxane material to a silicon dioxide like cross linked material.
In the conventional sandwich process, a conformal oxide is first deposited
followed by a coating of spin-on-glass material. This is cured at about
425.degree. C. to become a silicon dioxide layer with some other
materials, such as organics depending upon the particular spin-on-glass
material that is used. The final oxide of the sandwich is deposited.
In general, there are two kinds of spin-on-glass planarization. One uses
etchback and the other does not use etchback. The etchback process uses an
etching back step to remove the spin-on-glass layer which will exist in
the via holes. Its advantage is to protect the via hole from moisture or
other gases absorbed in the cured spin-on-glass which may damage the via
stepcoverage or metallurgy. The disadvantages for this etchback process
are (1) this process needs an extra etchback step and (2) it is difficult
to keep the etching selectivity of spin-on-glass to silicon oxide so that
there could be produced a poorer planarization that expected. With the
non-etchback process, it is easy to cause a poisoned via. During the
deposition of the metallurgy, moisture and other gases can be released
from the spin-on-glass layer in its sidewall regions to react with the
metallurgy to cause the so-called poisoned via. This will cause poor metal
stepcoverage or even an metallurgy and electrical open in the via.
A number of patents have addressed these and other problems in
spin-on-glass planarization. U.S. Pat. No. 5,003,062 to Yen involves a
sandwich process in which the spin-on-glass material can be either
silicate or siloxane. A vacuum degassing step is used. In U.S. Pat. No.
4,775,550 to Chu et al, the first insulating layer is very thick, on the
order of 8000 to 10,000 Angstroms. This thickness causes voids in the
submicron area. The aforementioned patent to Chu et al as well as U.S.
Pat. Nos. 4,676,867 to Elkins et al and 4,885,262 to Ting et al each show
spin-on-glass etchback processes with use of a sandwich dielectric.
The Joe H. K. Leong U.S. Pat. No. 5,192,697 describes an alternative curing
method to that of the thermal curing method. His method involves the use
of ion implantation to cause heating within the spin-on-glass layer to
cause curing of the layer. "Modification Effects in Ion-Implanted
SiO.sub.2 Spin on Glass" by N. Moriya et al in J. Electrochem, Soc. Vol,
No 5 May 1993, pp 1442-1449 describes the physical effects caused by ion
implanting into silicate and siloxane spin-on-glass layers formed on
silicon wafers.
SUMMARY OF THE INVENTION
Another object of the present invention is to provide a method of
planarizing an integrated circuit which does not result in the metallurgy
problem of poisoned via.
A principal object of the present invention is to provide an effective and
very manufacturable method of planarizing a submicron integrated circuit
using spin-on-glass that does not use an etchback step and still does not
have the poisoned via problem.
Yet another object of the present invention is to provide a method of
planarizing an integrated circuit which does not result in voids between
devices due to poisoned via problems.
In accordance with the objects of this invention a new method of
planarizing an integrated circuit is achieved. The dielectric layers
between the conductive layers of an integrated circuit are formed and
planarized via A first silicon oxide layer is deposited over the metal
layer. This is covered with a spin-on-glass layer. This layer is dried by
baking. The spin-on-glass layer is now fully cured. The cured
spin-on-glass layer is now ion implanted under the conditions of between
about 1E15 to 1E17 atoms/cm.sup.2 and energy between about 50 to 100 KEV.
A silicon oxide layer is deposited thereover. Via openings are now made
through the silicon oxide layers and the spin-on-glass layer and filled
with metal. This results in excellent planarity with no poisoned via
problems. Most importantly, this method can be used for submicron
technologies having conductor lines which are spaced from one another by
submicron feature size and can be processed without the use of an
etch-back process for the cured spin on and glass layer.
BRIEF DESCRIPTION OF THE DRAWINGS
In the accompanying drawings forming a material part of this description,
there is shown:
FIG. 1 shows the method for forming the spin-on-glass intermetal dielectric
having the reduced outgasing problem of the invention.
FIGS. 2 through 4 schematically illustrate in cross-sectional
representation one preferred embodiment of this invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring now to FIG. 1 there is shown the process outline of the formation
of the intermetal dielectric layer according to the present invention. The
intermetal dielectric layer can be formed between the contact metallurgy
and the first level metallurgy, between the first level and second level
metallurgies or between successive metal layers for an integrated circuit
as will be understood in the art. The spin-on-glass planarization process
is useful at all levels. The process begins by depositing a layer of
silicon oxide over the conductive layer, such as a metal or a highly doped
polysilicon layer as give in step 6. The spin-on-glass layer is deposited
as given by step 8 by the usual spinning method.
Both siloxane and silicate spin-on-glass materials may be used in this
method, but the siloxane type is preferred. The layer includes a vehicle
or solvent which needs to be removed by a low temperature drying or baking
step. This step is performed preferably by hot plate bake by moving the
wafer through hot plate heating sequentially, at temperatures of
80.degree. C., 150.degree. C., and 200.degree. C.
In step 10, the spin-on-glass is cured by a thermal process which includes
a nitrogen atmosphere curing at 425.degree. C. for about 40 or more
minutes. In step 12, the critical ion implantation process is used, is not
fully understood, but it is believed the process result that the
spin-on-glass structure with its --OH, --CH.sub.3 bonds are broken or
reduced in many ways. The film density of the spin-on-glass layer
increases and the quality of the layer will be very similar to that of
chemical vacuum deposited silicon oxide in the sense that it does not have
the problem of moisture absorption. Further the spin-on-glass layer will
be stable and without moisture evolving in the sidewall region of the via
holes. The last step 14 is to deposit the top silicon oxide layer over the
spin-in-glass layer.
Referring now more particularly to FIGS. 2 through 4, there is shown a
process which uses the FIG. 1 described intermetal dielectric layer in a
metal oxide field effect transistor integrated circuit. FIG. 2 is an
illustration of a partially completed, single N channel metal oxide field
effect transistor (MOSFET). The first series of steps involve the
formation of the dielectric isolation regions for isolating semiconductor
surface regions from other such regions in the semiconductor substrate 20.
The semiconductor substrate is preferably composed of silicon having a
(100) crystallographic orientation. In an effort to simplify the
description and the drawings the dielectric isolation between devices has
been only partially shown and will not be described in detail, because
they are conventional. For example, one method is described by E. Kooi in
his U.S. Pat. No. 3,970,486 wherein certain selected surface portions of a
silicon semiconductor substrate is masked against oxidation, and then the
exposed unmasked surface is oxidized to grow a thermal oxide which in
effect sinks into the silicon surface at the unmasked areas. The masked
silicon remains as a mesa surrounded by the sunken silicon dioxide or
Field OXide pattern, FOX 18. Then semiconductor devices can be provided in
the silicon mesas according to the following processes.
The surface of the silicon substrate 20 is thermally oxidized to form the
desired gate oxide 21 thickness. The preferred thickness is between about
70 to 200 Angstroms. The polysilicon layer 22 is blanket deposited by
LPCVD (Low Pressure Chemical Vapor Deposition) method to a conventional
thickness. The polysilicon layer 22 is ion implanted with phosphorous or
arsenic ions by conventional methods and dosages to render the polysilicon
layer conductive or doped with phosphorus oxychloride at a temperature
about 900.degree. C. The surface of the layer is either thermally oxidized
or a chemical vapor deposition process to form silicon oxide layer 23. The
layers 21, 22 and 23 are patterned by conventional lithography and
anisotropic etching techniques as are conventional in the art to provide a
desired pattern of gate electrodes and structure on the FOX 18 surfaces or
elsewhere as seen in FIG. 2.
The source/drain structure of the MOS FET may now be formed by conventional
methods. FIG. 2 shows an N channel MOSFET integrated circuit device
wherein the substrate or well is doped as P-. However, it is well
understood by those skilled in the art that a P channel FET integrated
circuit device could also be formed by simply substituting opposite
polarities to those given for the N channel embodiment. Also, a CMOS FET
could in a similar way be formed by making both N channel and P channel
devices upon the same substrate.
FIG. 2, for example shows the device regions, typically source/drain
regions 24 in the substrate as of N+ dopants. The N+ regions may be formed
by ion implantation as is well known in the art.
A passivation or insulating layer 26 is now formed over the surfaces of the
patterns. This layer may be composed of multilayers such as a thin layer
of silicon oxide and a much thicker layer of borophosphosilicate glass,
phosphosilicate glass or similar insulating layer. The operational
thicknesses of these layers are between about 1000 to 2000 Angstroms for
the oxide layer and between about 5000 to 6000 or more Angstroms for the
glasseous layer. These layers are typically deposited by chemical vapor
deposition in low pressure or atmospheric pressure, or in a plasma
enhanced reactive chamber.
The contact windows are openings are formed through the insulating
structure to the source/drain regions 24. Conventional lithography and
etching techniques are used to form this pattern of openings.
The first metallurgy contact layer 30 is now deposited over the surface of
the structure and within the pattern of contact openings. The metallurgy
is preferably Al/Si/Cu W-Ti (Aluminum/Silicon/Copper Tungsten-Titanium)
barrier having a thickness of between about 5K to 7K Angstroms. However,
other possible metallurgy include Aluminum-Silicon, dual-doped
polysilicon, Titanium Silicide, Titanium:Tungsten, Titanium Nitride and
Chemical Vapor Deposition Tungsten and polycides. The metallurgy may be
deposited by dc magnetron sputtering. The metallurgy is now patterned into
the desired conductive lines by conventional lithography and etching
techniques to form the pattern of metal layer 30 in FIG. 2.
Referring now more particularly to FIG. 3, the usual first dielectric
silicon oxide layer 32 of the spin-on-glass sandwich planarization
structure is now formed by PECVD (plasma enhanced chemical vapor
deposition) process above the first metallurgy pattern 30. It is typically
in the range of between about 2000 to 5000 Angstroms in thickness. This is
followed by the creation of the spin-on-glass layer 34. The spin-on-glass
material suspended in the vehicle or solvent is deposited onto the
semiconductor wafer surface and uniformly spread thereover by the action
of spinning the wafer. The material fills the indentations in the
integrated circuit wafer surface, that is planarization. Most of the
vehicle or solvent is driven off by a low temperature baking step.
Typically, successive hot plate baking at 0.degree. C., 150.degree. C. and
200.degree. C. for one minute at each hot plate step. Typically, a double
coat of the spin-on-glass material is applied. The material can be either
silicate or siloxane. However, siloxane is preferred. Each coat is 500 to
1500 Angstroms thick for a total thickness of 1000 to 3000 Angstroms.
After the spin-on-glass (SOG) layer has been completed, the layer 34 is
cured by the thermal curing method. The method improves curing of the
layer at about 425.degree. C. in a nitrogen atmosphere for 40 or more
minutes.
The Ion implantation is done preferably within an ion implantation chamber.
The wafer or wafers are set upon a pedestal within the chamber. The wafer
temperature at maintained between about 25.degree. to 100.degree. C. Ions,
preferably phosphorus (P31) or arsenic (As.sup.75) are implanted into the
thermally cured spin-on-glass layer 34 at a preferred dose of between 1E15
and 1E17 ions/cm.sup.2 and energy of 50 to 100 KeV for a thickness of
about 1500 Angstroms of Siloxane type material, such as Allied Signal III
which is a siloxane type SOG. Note that more than 1E17 up to 1E18 for
example, could be used, but of course it takes more machine time. The
preferred implant time is between about 10 to 30 minutes under these
conditions, depending upon dosage so if 1E18 is used, the time could be
about 60 minutes. Since the implantation is done within a vacuum chamber,
the gases trapped within the wafer are pulled out by the vacuum. The
action of the ions moving through the spin-on-glass layer causes the
decrease of moisture absorption into the resulting SOG layer. We believe
that the effect of the ion under these process conditions is to break or
rearrange the bonds, for example --OH, --CH.sub.3 and the like which are
radicals which absorb the moisture in an untreated SOG layer. FIG. 5 shows
this effect. FTIR (fast time infrared) microscopy for OH moisture
absorption rate at 3380 cm.sup.-1 for P.sub.31 ion implant is about 0.013.
However, without ion implant the moisture absorption rate is about 0.04.
FIG. 4 illustrates the deposition of a second layer of silicon dioxide 36.
This second layer should be deposited as soon as possible after the ion
implantation treating step to cap the spin-on-glass layer from the
atmosphere. Openings are made through the spin-on-glass sandwich 32, 34,
36 using conventional lithography and etching techniques. Contact is made
to the first metal layer 30 by a second metal layer 46 which is deposited
into the opening. The metal layer 46 is patterned by conventional
lithography and etching techniques to complete construction of the desired
FET structure shown in this FIG. 4. It is of course understood by those
skilled in the art that further layers of spin-on-glass sandwich can be
formed to allow further metallurgy to be applied over the structure.
EXAMPLES 1-3
Siloxane (Allied Signal III) spin-on-glass layers of uniform thicknesses
were deposited on three wafers. Each of these wafers having the
spin-on-glass layer thereon were hot plate baked for one minute duration
at temperatures of 80.degree. C., 150.degree. C. and 200.degree. C. The
spin-on-glass layer was cured by loading the wafers into a vacuum furnace
at 250.degree. C. and the furnace was ramped up to 425.degree. C. in 12
minutes and stabilized for 35 minutes. Curing was done in a nitrogen
atmosphere for 40 minutes and then the wafers were removed from the
furnace after the furnace was returned to atmospheric pressure. After cool
down to room temperature, the wafers were treated or not treated by ion
implantation under vacuum conditions and between 25.degree. C. and
100.degree. C. as given in the following:
______________________________________
Example Ion KEV Dosage
Time
______________________________________
1 No I/I -- -- --
2 BF.sub.2
80 2E15 30 minutes
3 P.sub.31
50 2E15 30 minutes
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EXAMPLES 4-8
Siloxane spin-on-glass layers of uniform thickness were deposited on
separate wafers having a PECVD silicon oxide layer, baked, cured and
cooled as described in Examples 1-3, above. The wafers with spin-on-glass
layers were etch-back to leave the curved spin-on-glass only within
indentations of surface or not etch-back and treated or not treated by ion
implantation as given in the Following:
______________________________________
Via
Etch- Yield Resistivity
Example
back Ion KEV Dosage
% ohm/via
______________________________________
4 No P.sub.31
50 1E16 84.2 0.319
5 No P.sub.31
50 1E16 86.8 0.319
6 No As.sup.75
80 5E15 85.7 0.301
7 No No -- -- 73.2 0.334
8 Yes No -- -- 87.1 0.306
______________________________________
The results show that spin-on-glass with ion implantation treatment
improves the yield % and via resistivity of the spin-on-glass without the
requirement of an extra etch-back step as seen in the Examples. The
spin-on-glass without the etch-back and without ion implantation treatment
(Example 7) is not as good as seen by yield % and via resistivity. The
Examples 4, 5 and 6 show the advantage of not using etch-back and using
ion implantation treatment after spin-on-glass curing.
EXAMPLES 9-13
Those Examples were made according to the process described with regard to
Examples 4-8 with the addition of a PECVD silicon oxide layer deposited
over the cured and treated by ion implantation or not treated as indicated
as follows:
______________________________________
Example
Etch-back Ion KEV Dosage Yield
______________________________________
9 No P.sub.31
50 1E15 87.1
10 No P.sub.31
80 1E15 88.2
11 Yes -- -- -- 86.4
12 No P.sub.31
50 2E15 88.0
13 No As.sup.75
80 1E15 87.0
______________________________________
The Examples which used the ion implantation treatment of cured
spin-on-glass which had not been etch-back and had a PECVD silicon oxide
capping layer formed thereover had as good a yield as the spin-on-glass
etch-back Example 11 which was not treated by ion implantation.
While the invention has been particularly shown and described with
reference to the preferred embodiments thereof, it will be understood by
those skilled in the art that various changes in form and details may be
made without departing from the spirit and scope of the invention.
* * * * *
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Description  |
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