BACKGROUND OF THE INVENTION1. Field of the Invention
Embodiments of the present invention generally relate to the fabrication of integrated circuits and particularly to a method for protecting sidewalls of hard mask spacers during an etching process.
2. Description of the Related Art
Reducing the size of integrated circuits (ICs) results in improved performance, increased capacity and/or reduced cost. Each size reduction requires more sophisticated techniques to form the ICs. Photolithography is commonly used to pattern ICs on a substrate. An exemplary feature of an IC is a line of a material which may be a metal, semiconductor or insulator. Linewidth is the width of the line and the spacing is the distance between adjacent lines. Pitch is defined as the distance between a same point on two neighboring lines. The pitch is equal to the sum of the linewidth and the spacing. Due to factors such as optics and light or radiation wavelength, however, photolithography techniques have a minimum pitch below which a particular photolithographic technique may not reliably form features. Thus, the minimum pitch of a photolithographic technique can limit feature size reduction.
Self-aligned double patterning (SADP) is one method for extending the capabilities of photolithographic techniques beyond the minimum pitch. Such a method is illustrated inFIGS. 1A-1F. With reference toFIG. 1A, patternedcore features102 are formed from sacrificial structural material above adielectric layer114 on asubstrate100 using standard photo-lithography and etching techniques. The patterned features are often referred to as placeholders or cores and have linewidths and/or spacings near the optical resolution of a photolithography system using a high-resolution photomask. As shown inFIG. 1B, aconformal layer106 of hard mask material such as silicon oxide is subsequently deposited overcore features102.Hard mask spacers108 are then formed on the sides ofcore features102 by preferentially etching the hard mask material from the horizontal surfaces with an anisotropic plasma etch to open the hard mask material deposited on top of the patternedcore features102 as well as remove the hard mask material deposited at the bottom between the two sidewalls, as shown inFIG. 1C. The patternedcore features102 may then be removed, leaving behind hard mask spacers108 (FIG. 1D). At this pointhard mask spacers108 may be used as an etch mask for transferring the pattern to thedielectric layer114 to formdielectric ribs116, as shown inFIG. 1E. Thehard mask spacers108 are subsequently removed (FIG. 1F). Therefore, the density of thedielectric ribs116 is twice that of the photo-lithographically patternedcore features102, and the pitch of thedielectric ribs116 is half the pitch of the patternedcore features102.
Currently,hard mask spacers108 are formed by an atomic layer deposition (ALD) using an etchable material such as silicon oxides. These oxides are typically deposited at very low temperature (e.g., less than 200° C.). As a result, the material quality is poor, with low density and poor mechanical strength and degraded chemical resistance to subsequent etching chemistries. During the etching of the hard mask material, the spacer sidewalls, e.g., sidewalls107 (FIG. 1D) are exposed to the plasma. Due to the poor material quality of typical ALD hard mask spacers, the sidewalls are damaged and thus causing higher line edge roughness. This issue becomes serious with shrinking feature size.
Therefore, there is a need for a method of protecting the sidewalls of the hard mask spacers such that the patterning integrity is greatly improved.
SUMMARY OF THE INVENTIONEmbodiments of the present invention provide a method for protecting sidewalls of hard mask spacers during an etching process. In one embodiment, a method of forming a nitrogen-doped amorphous carbon layer on a substrate in a processing chamber is provided. The method generally includes depositing a predetermined thickness of a sacrificial dielectric layer over a substrate, forming patterned features on the substrate by removing portions of the sacrificial dielectric layer to expose an upper surface of the substrate, depositing conformally a predetermined thickness of a nitrogen-doped amorphous carbon layer on the patterned features and the exposed upper surface of the substrate, selectively removing the nitrogen-doped amorphous carbon layer from an upper surface of the patterned features and the upper surface of the substrate using an anisotropic etching process to provide the patterned features filled within sidewall spacers formed from the nitrogen-doped amorphous carbon layer, and removing the patterned features from the substrate.
In another embodiment, a method of forming a device in a processing chamber is provided. The method generally includes forming patterned features on an upper surface of a substrate, depositing conformally a predetermined thickness of a sacrificial dielectric layer on the patterned features and an exposed upper surface of the substrate, selectively removing the sacrificial dielectric layer from an upper surface of the patterned features and the exposed upper surface of the substrate to provide the patterned features filled within first sidewall spacers formed from the sacrificial dielectric layer, forming second sidewall spacers adjacent to the first sidewall spacers, the second sidewall spacers being formed from a nitrogen-doped amorphous carbon material having a carbon:nitrogen ratio of between about 0.1% nitrogen to about 4.0% nitrogen, and removing the patterned features filled within the first sidewall spacers.
In yet another embodiment, a method of forming a nitrogen-doped amorphous carbon layer on a substrate in a processing chamber is provided. The method generally includes depositing conformally a nitrogen-doped amorphous carbon layer on patterned features formed on the substrate, wherein the deposition is performed, selectively removing the nitrogen-doped amorphous carbon layer from an upper surface of the patterned features and an upper surface of the substrate using an anisotropic etching process to provide patterned features filled within sidewall spacers formed from the nitrogen-doped amorphous carbon layer, and removing the patterned features from the substrate.
BRIEF DESCRIPTION OF THE DRAWINGSSo that the manner in which the above recited features of the present invention can be understood in detail, a more particular description of the invention, briefly summarized above, may be had by reference to embodiments, some of which are illustrated in the appended drawings. It is to be noted, however, that the appended drawings illustrate only typical embodiments of this invention and are therefore not to be considered limiting of its scope, for the invention may admit to other equally effective embodiments.
FIGS. 1A-1F illustrate cross-sectional views representing a conventional double patterning process.
FIG. 2 is a flowchart depicting steps associated with an exemplary patterning process according to one embodiment of the invention.
FIGS. 3A-3E illustrate cross-sectional views of a structure formed by the steps set forth inFIG. 2.
FIG. 4 is a flowchart depicting steps associated with an exemplary patterning process according to another embodiment of the invention.
FIGS. 5A-5H illustrate cross-sectional views of a structure formed by the steps set forth inFIG. 4.
DETAILED DESCRIPTIONEmbodiments of the present invention relate to an ultra-conformal strippable spacer process. In various embodiments, an ultra-conformal carbon-based material, such as amorphous carbon, is deposited over features of sacrificial structure material patterned using a high-resolution photomask. The ultra-conformal carbon-based material serves as a protective layer during an ashing or etching process, leaving the sacrificial structure material with an upper surface exposed and sidewalls protected by the carbon-based spacers. Upon removal of the sacrificial structure material, the remaining carbon-based spacers may perform as a hardmask layer for etching the underlying layer or structure. In one example, the carbon-based material may be an undoped or a nitrogen-doped amorphous carbon material.
Embodiments of the present invention may be performed using any suitable processing chamber such as a plasma enhanced chemical vapor deposition (PECVD) chamber. The processing chamber may be incorporated into a substrate processing system. An exemplary substrate processing system that may be used to practice the invention is described in commonly assigned U.S. Pat. No. 6,364,954 issued on Apr. 2, 2002, to Salvador et. al. and is herein incorporated by reference. Examples of suitable systems include the CENTURA® systems which may use a DxZ™ processing chamber, PRECISION 5000® systems, PRODUCER™ systems, PRODUCER GT™ and the PRODUCER SE™ processing chambers which are commercially available from Applied Materials, Inc., Santa Clara, Calif. It is contemplated that other processing system, including those available from other manufacturers, may be adapted to practice the embodiments described herein.
Exemplary Fabrication Sequence Employing a-C Protective LayerFIG. 2 is a process flowchart depicting steps associated with an exemplary self-aligned double patterning process according to one embodiment of the invention.FIGS. 3A-3E illustrate cross-sectional views of a structure formed by the steps set forth inFIG. 2. It is contemplated that the self-aligned double patterning process is chosen for illustration purpose. The concept of the invention is equally applicable to other processes, single or dual patterning scheme, such as via/hole shrink process, self-aligned triple patterning (SATP) process, or self-aligned quadruple patterning (SAQP) process, etc. that may require the use of protective spacers with variable line width and spacing or protective sacrificial layer as needed in various semiconductor processes such as NAND flash application, DRAM application, or CMOS application, etc. In addition, the number or sequence of steps illustrated inFIG. 2 is not intended to limiting as to the scope of the invention described herein, since one or more steps can be added, deleted and/or reordered without deviating from the basic scope of the invention described herein.
Theprocess200 starts atbox202 by forming a sacrificialstructural layer320 on asubstrate300. The sacrificialstructural layer320 may be a silicon-based material such as silicon oxide, silicon nitride, or polysilicon. Alternatively, the sacrificialstructural layer320 may be a carbon-based material such as amorphous carbons. In cases where a carbon-based sacrificial structural layer is desired, the sacrificialstructural layer320 may be a combination of amorphous carbon and hydrogen (hydrogenated amorphous carbon film). One exemplary amorphous carbon film may be a strippable Advanced Patterning Film™ (APF) material commercially available from Applied Materials, Inc. of Santa Clara, Calif. It is contemplated that the choice of materials used for the sacrificialstructural layer320 may vary depending upon the etching/ashing rate relative to the conformal protective layer to be formed thereon. While not shown, in certain embodiments where a carbon-based sacrificial structural layer is used, one or more anti-reflective coating layers may be deposited on the carbon-based sacrificial structural layer to control the reflection of light during a lithographic patterning process. Suitable anti-reflective coating layer may include silicon dioxide, silicon oxynitride, silicon nitride, or combinations thereof. One exemplary anti-reflective coating layer may be a DARC™ material commercially available from Applied Materials, Inc. of Santa Clara, Calif.
Thesubstrate300 may have a substantiallyplanar surface323 as shown. Alternatively, thesubstrate300 may have patterned structures, a surface having trenches, holes, or vias formed therein. While thesubstrate300 is illustrated as a single body, thesubstrate300 may contain one or more materials used in forming semiconductor devices such as metal contacts, trench isolations, gates, bitlines, or any other interconnect features. In one embodiment, thesubstrate300 may include one or more metal layers, one or more dielectric materials, semiconductor material, and combinations thereof utilized to fabricate semiconductor devices. For example, thesubstrate300 may include an oxide material, a nitride material, a polysilicon material, or the like, depending upon application. In cases where a memory application is desired, thesubstrate300 may include the silicon substrate material, an oxide material, and a nitride material, with or without polysilicon sandwiched in between.
In some embodiments, thesubstrate300 may include a plurality of alternating oxide and nitride materials (i.e., oxide-nitride-oxide (ONO)), one or more oxide or nitride materials, polysilicon or amorphous silicon materials, oxides alternating with amorphous silicon, oxides alternating with polysilicon, undoped silicon alternating with doped silicon, undoped polysilicon alternating with doped polysilicon, or updoped amorphous silicon alternating with doped amorphous silicon deposited on a surface of the substrate (not shown). Thesubstrate300 may be a material or a layer stack comprising one or more of the following: crystalline silicon, silicon oxide, silicon oxynitride, silicon nitride, strained silicon, silicon germanium, tungsten, titanium nitride, doped or undoped polysilicon, doped or undoped silicon wafers and patterned or non-patterned wafers, silicon on insulator (SOI), carbon doped silicon oxides, silicon nitrides, doped silicon, germanium, gallium arsenide, glass, sapphire, low k dielectrics, and combinations thereof.
Atbox204, a resistlayer330, such as a photoresist material, is deposited on the sacrificialstructural layer320 as shown inFIG. 3A.
Atbox206, patterned features321 formed from the sacrificialstructural layer320 are produced on thesubstrate300 using standard photo-lithography and etching techniques, as shown inFIG. 3B. The patterned features may be formed from any suitable material, for example oxides, such as silicon dioxide, silicon oxynitride, or nitrides such as silicon nitride. The patterned features are sometimes referred to as placeholders, mandrels or cores and have specific linewidths and/or spacings based upon the photoresist material used. The width of the patterned features321 may be adjusted by subjecting the resistlayer330 to a trimming process. After the pattern has been transferred into the sacrificialstructural layer320, any residual photoresist and hard mask material (if used) are removed using a suitable photoresist stripping process.
Atbox208, a carbon-basedprotective layer340 is deposited conformally or substantially conformally on the patterned features321 and the exposed surfaces of thesubstrate300, as shown inFIG. 3C. The thickness of the carbon-basedprotective layer340 may be between about 5 Å and about 200 Å. In one embodiment, the carbon-based protective layer is an amorphous carbon (a-C) layer. The amorphous carbon may be undoped or doped with nitrogen. In one example, the carbon-basedprotective layer340 is a nitrogen-doped amorphous carbon layer. The nitrogen-doped amorphous carbon layer may be deposited by any suitable deposition techniques such as plasma enhanced chemical vapor deposition (PECVD) process. In one embodiment, the nitrogen-doped amorphous carbon layer may be deposited by flowing, among others, a hydrocarbon source, a nitrogen-containing gas such as N2or NH3, and a plasma-initiating gas in a PECVD chamber. In another embodiment, the nitrogen-doped amorphous carbon layer may be deposited by flowing, among others, a hydrocarbon source, such as a gas-phase hydrocarbon or a liquid-phase hydrocarbon that has been entrained in a carrier gas, a nitrogen-containing hydrocarbon source, and a plasma-initiating gas into a PECVD chamber. The hydrocarbon source may be a mixture of one or more hydrocarbon compounds. In some embodiments, the hydrocarbon source may not be required. Instead, a nitrogen-containing hydrocarbon source and a plasma-initiating gas are flowed into the PECVD chamber to form the nitrogen-doped amorphous carbon protective layer on the patterned features321 and the exposed surfaces of thesubstrate300.
The hydrocarbon compounds may be partially or completely doped derivatives of hydrocarbon compounds, including fluorine-, oxygen-, hydroxyl group-, and boron-containing derivatives of hydrocarbon compounds. Hydrocarbon compounds or derivatives thereof that may be included in the hydrocarbon source may be described by the formula CxHy, where x has a range of between 1 and 10 and y has a range of between 2 and 30. Suitable hydrocarbon compounds may include, but are not limited to, acetylene (C2H2), ethane (C2H6), propylene (C3H6), propyne (C3H4), propane (C3H8), butane (C4H10), butylene (C4H8), butyne (C4H6), vinylacetylene, phenylacetylene (C8H6), benzene, styrene, toluene, xylene, ethylbenzene, acetophenone, methyl benzoate, phenyl acetate, phenol, cresol, furan, alpha-terpinene, cymene, 1,1,3,3,-tetramethylbutylbenzene, t-butylether, t-butylethylene, methyl-methacrylate, and t-butylfurfurylether, compounds having the formula C3H2and C5H4, monofluorobenzene, difluorobenzenes, tetrafluorobenzenes, hexafluorobenzene, and the like. Additional suitable hydrocarbons may include ethylene, pentene, butadiene, isoprene, pentadiene, hexadiene, monofluoroethylene, difluoroethylenes, trifluoroethylene, tetrafluoroethylene, monochloroethylene, dichloroethylenes, trichloroethylene, tetrachloroethylene, and the like.
Nitrogen containing hydrocarbon compounds or derivatives thereof that may be included in the nitrogen containing hydrocarbon source can be described by the formula CxHyNz, where x has a range of between 1 and 12, y has a range of between 2 and 20, and z has a range of between 1 and 10. Suitable nitrogen containing hydrocarbon compounds may include one or more of the following compounds methylamine, dimethylamine, trimethylamine (TMA), triethylamine, aniline, quinoline, pyridine, acrilonitrile, and benzonitrile.
In certain embodiments, the nitrogen doped amorphous carbon deposition process may include the use of a plasma-initiating gas that is introduced into the PECVD chamber at before and/or same time as the hydrocarbon compound and a plasma is initiated to begin deposition. The plasma-initiating gas may be a high ionization potential gas including, and not limited to, helium gas, hydrogen gas, nitrogen gas, argon gas and combinations thereof. The plasma-initiating gas may also be a chemically inert gas, such as helium gas, nitrogen gas, or argon gas. Suitable ionization potentials for gases are from about 5 eV (electron potential) to 25 eV. The plasma-initiating gas may be introduced into the PECVD chamber prior to the nitrogen containing hydrocarbon source and/or the hydrocarbon source, which allows a stable plasma to be formed and reduces the chances of arcing. An inert gas used as a diluent gas or a carrier gas, such as argon, may be introduced with the plasma-initiating gas, the nitrogen containing hydrocarbon source, the hydrocarbon source, or combinations thereof. Suitable dilution gases such as helium (He), hydrogen (H2), nitrogen (N2), ammonia (NH3), or combinations thereof, among others, may be added to the gas mixture, if desired. Ar, He, and N2are used to control the density and deposition rate of the amorphous carbon layer. In some cases, the addition of H2and/or NH3can be used to control the hydrogen ratio of the amorphous carbon layer. Alternatively, dilution gases may not be used during the deposition.
In cases where the nitrogen-doped amorphous carbon is deposited using a hydrocarbon source and a nitrogen-containing gas, the nitrogen-containing gas may be introduced into the PECVD chamber at a nitrogen-containing gas to hydrocarbon source ratio of about 1:100 to about 10:1.
In various embodiments, the nitrogen doped amorphous carbon layer may be deposited at a chamber pressure of about 0.5 Torr or greater, such as from about 0.5 Torr to about 20 Torr, and in one embodiment, about 2 Torr or greater, for example, from about 2 Torr to about 12 Torr, and a substrate temperature from about 25° C. to about 800° C., such as at a temperature from about 200° C. to about 400° C. The electrode spacing between a showerhead and substrate surface when depositing the layer may be between 200 mils and 5,000 mils spacing, for example, about 500 mils spacing. In certain embodiments, where a plasma is used, the hydrocarbon source, the nitrogen doped amorphous carbon source, and the plasma-initiating gas are introduced into the PECVD chamber and a plasma is initiated to begin the deposition.
Plasma may be generated by applying RF power at a power density to substrate surface area of from about 0.01 W/cm2to about 5 W/cm2, such as from about 0.8 W/cm2to about 2.3 W/cm2, for example, about 2 W/cm2. The power application may be from about 1 Watt to about 2,000 watts, such as from about 10 W to about 100 W, for a 300 mm substrate. It is noted that the RF power can be either single frequency or dual frequency. If a single frequency power is used, the frequency power may be between about 10 KHz and about 30 MHz. If a dual-frequency RF power is used to generate the plasma, a mixed RF power may be used. The mixed RF power may provide a high frequency power in a range from about 10 MHz to about 30 MHz, for example, about 13.56 MHz, as well as a low frequency power in a range of from about 10 KHz to about 1 MHz, for example, about 350 KHz. A dual frequency RF power application is believed to provide independent control of flux and ion energy since the energy of the ions hitting the film surface influences the film density. The applied RF power and use of one or more frequencies may be varied based upon the substrate size and the equipment used. In certain embodiments, a single frequency RF power application may be used, and is typically, an application of the high frequency power as described herein.
An exemplary deposition process for processing 300 mm circular substrates may employ, among others, a plasma-initiating gas, a nitrogen containing hydrocarbon source, and a dilution gas. The deposition process may include supplying a plasma-initiating gas, such as helium and/or argon, at a flow rate from about 0 sccm to about 50,000 sccm, for example, between about 400 sccm to about 8,000 sccm, supplying a nitrogen containing hydrocarbon source, at a flow rate from about 10 sccm to about 2,000 sccm, for example, from about 500 sccm to about 1,500 sccm. In case the nitrogen containing hydrocarbon source is a liquid precursor, then the nitrogen containing hydrocarbon source flow can be between 15 mg/min and 2,000 mg/min, for example between 100 mg/min and 1,000 mg/min. A dilution gas, such as NH3, He, Ar, H2, or N2, may be supplied at a flow rate from about 0 sccm to about 5,000 sccm, for example about 500 sccm to about 1,000 sccm. The deposition process may be performed with a dual frequency RF power from about 5 W to about 1,600 W, for example between about 10 W and about 100 W, at a chamber pressure from about 0.5 Torr to about 50 Torr, for example between about 5 torr and about 15 Torr, and a substrate temperature from about 25° C. to about 650° C., for example between about 200° C. and about 400° C. This process range provides a deposition rate for a nitrogen doped amorphous carbon layer in the range of about 10 Å/min to about 30,000 Å/min. One skilled in the art, upon reading the disclosure herein, can calculate appropriate process parameters in order to produce a nitrogen doped amorphous carbon film of different deposition rates. The as-deposited nitrogen-doped amorphous carbon layer has an adjustable carbon:nitrogen ratio that ranges from about 0.1% nitrogen to about 4.0% nitrogen, such as about 1.5% to about 2%. An example of nitrogen doped amorphous carbon materials deposited by the processes described herein is provided as follows.
A nitrogen doped amorphous carbon deposition process may include providing a flow rate of helium to the processing chamber at about 200 sccm to 1,500 sccm, for example about 500 sccm, providing a flow rate of benzonitrile to the processing chamber at about 100 mg/min to about 1,000 mg/min, and providing a flow rate of ammonia to the processing chamber at about 0 sccm to about 2,000 sccm, applying a high frequency RF power (13.56 MHz) at about 30 W to 200 W (for a 200 mm wafer), maintaining a deposition temperature of about 200° C. to about 550° C., maintaining a chamber pressure of about 2 Torr to 15 Torr, with a spacing of about 100 mils to about 800 mils to produce a nitrogen doped amorphous carbon layer having a thickness of about 10 Å to about 1,000 Å.
Referring back toFIG. 2, atbox210, after the carbon-basedprotective layer340 has been deposited conformally on the patterned features321, the carbon-basedprotective layer340 is anisotropically etched (a vertical etch) to expose an upper surface of thesubstrate300 inareas311 and expose an upper surface of patternedfeatures321, resulting in patterned features321 (formed from the sacrificial structural layer320) protected by carbon-basedsidewall spacers341, as shown inFIG. 3D.
Atbox212, the patterned features321 (formed from the sacrificial structural layer320) are removed using a conventional plasma etching process or other suitable wet stripping process, leaving non-sacrificial carbon-basedsidewall spacers341 as shown inFIG. 3E. The plasma etching process may be done by introducing a fluorine-based etching chemistry into a plasma above the substrate. Due to the improved material quality and coverage, the carbon-basedsidewall spacers341 are not damaged because they have very good selectivity to the fluorine-based reactive etching chemistry or the wet strip-based chemistry. Upon removal of the patterned features321, the remaining carbon-basedsidewall spacers341 may be used as a hardmask for etching the underlying layer, layer stack, or structure. Particularly, the density of the carbon-basedsidewall spacers341 in accordance with this patterning process is twice that of the photo-lithographically patternedfeatures321, the pitch of carbon-basedsidewall spacer341 is half the pitch of the patterned features321.
FIG. 4 is a flowchart depicting steps associated with an exemplary patterning process according to another embodiment of the invention.FIGS. 5A-5H illustrate cross-sectional views of a structure formed by the steps set forth inFIG. 4. It is noted that the concept of this embodiment is equally applicable to other processes, single or dual patterning scheme, such as via/hole shrink process, back end of line (BEOL) self-aligned double patterning (SADP) process, or self-aligned quadruple patterning (SAQP) process, etc. that may require the use of protective spacers with variable line width and spacing or protective sacrificial layer as needed in various semiconductor processes such as NAND flash application, DRAM application, or CMOS application, etc.
Theprocess400 starts atbox402 by providing asubstrate500 into a processing chamber, such as a PECVD chamber. Thesubstrate500 may be one or more materials used in forming semiconductor devices including a silicon material, an oxide material, a polysilicon material, or the like, as discussed above with respect tosubstrate300 shown inFIG. 3A.
Atbox404, a non-sacrificialstructural layer520 is deposited on thesubstrate500 as shown inFIG. 5B. The non-sacrificialstructural layer520 may be a carbon-based material such as amorphous carbons. In one example, the non-sacrificialstructural layer520 is an Advanced Patterning Film™ (APF) material commercially available from Applied Materials, Inc. of Santa Clara, Calif. While not shown, in certain embodiments where a carbon-based non-sacrificial structural layer is used, one or more anti-reflective coating layers may be deposited on the carbon-based non-sacrificial structural layer to control the reflection of light during a lithographic patterning process. Suitable anti-reflective coating layer may include silicon dioxide, silicon oxynitride, silicon nitride, or combinations thereof. One exemplary anti-reflective coating layer may be a DARC™ material commercially available from Applied Materials, Inc. of Santa Clara, Calif.
Atbox406, a bottom anti-reflective coating (BARC)layer540 is deposited over thenon-sacrificial structure layer520. TheBARC layer540 may be an organic material such as polyamides and polysulfones. TheBARC layer540 is believed to reduce reflection of light during patterning of the subsequent resist layer and is also helpful for thinner resist layers because theBARC layer540 increases the total thickness of the multi-layered mask for improved etch resistance during etch of underlying layer or structure. In certain embodiments, theBARC layer540 may further include a lightabsorbing layer530 deposited between theBARC layer540 and thenon-sacrificial structure layer520 as shown inFIG. 5C, to improve photolithography performance. The lightabsorbing layer530 may be a metal layer, such as nitrides. In one example, thelight absorbing layer530 is titanium nitride.
Atbox408, a resist layer, such as a photoresist material, is then deposited on theBARC layer540. The resist layer is then patterned by a lithographic process producing a patterned resistlayer550 with a desiredetch pattern551, as shown inFIG. 5D. Theetch pattern551 is shown to have different pattern width for exemplary purpose.
Atbox410, theBARC layer540, thelight absorbing layer530, and thenon-sacrificial structure layer520 are patterned respectively using conventional photolithography and etching processes to transfer the desiredetch pattern551 into thenon-sacrificial structure layer520, leaving patternednon-sacrificial features521, as shown inFIG. 5E.
Atbox412, a first conformal layer is deposited conformally or substantially conformally on the patternednon-sacrificial features521 and the exposed surfaces of thesubstrate500. The first conformal layer may comprise a strippable material having an etching rate different from the patternedsacrificial features521. Suitable materials for the first conformal layer may include, for example, oxides such as silicon dioxide, silicon oxynitride, or nitride such as silicon nitride. The first conformal layer is then anisotropically etched to expose an upper surface of thesubstrate500 inareas511 and expose an upper surface of patternednon-sacrificial features521, resulting in patterned non-sacrificial features521 (formed from the non-sacrificial structural layer520) protected bystrippable sidewall spacers561 formed from the first conformal layer, as shown inFIG. 5F.
Atbox414, non-sacrificial carbon-basedsidewall spacers571 are then formed adjacent the patternednon-sacrificial features521 in a manner similar to thesidewall spacers561 as shown inFIG. 5G. The non-sacrificial carbon-basedsidewall spacers571 may be an amorphous carbon (a-C) undoped or doped with nitrogen formed by the processes as described above with respect toboxes208 and210. In one embodiment, the non-sacrificial carbon-basedsidewall spacers571 are nitrogen-doped amorphous carbon.
Atbox416, thestrippable sidewall spacers561, located between the patternednon-sacrificial features521 and the non-sacrificial carbon-basedsidewall spacers571, are removed using a conventional wet stripping process or other suitable process, leaving patternednon-sacrificial features521 and non-sacrificial carbon-basedsidewall spacers571 as shown inFIG. 5H. The remaining patternednon-sacrificial features521 and non-sacrificial carbon-basedsidewall spacers571 may then be used as a hardmask for etching the underlying layer, layer stack, or structure. Particularly, the density of the resulting hardmask (i.e., patternednon-sacrificial features521 and non-sacrificial carbon-based sidewall spacers571) in accordance with this patterning process is triple that of the patterned resistlayer550, the pitch of resulting hardmask (i.e., patternednon-sacrificial features521 and non-sacrificial carbon-based sidewall spacers571) is half the pitch of the patterned resistlayer550.
Carbon-based protective layers or sidewall spacers deposited in accordance with the present invention have been observed to be able to provide excellent conformality higher than 95% with an improved film uniformity of about 1.5%, high film density of about 1.25-1.60 g/cc, and a compressive film stress less than 50 MPa. Since the sidewalls of hard mask spacers are not damaged during the ashing or anisotropic plasma etching process, the line edge roughness is significantly reduced as compared to the conventional ALD grown spacers using silicon oxide materials. Therefore, the resulting hard mask spacers can provide superior etch profile and etch selectivity with little or no microloading.
While the foregoing is directed to embodiments of the present invention, other and further embodiments of the invention may be devised without departing from the basic scope thereof, and the scope thereof is determined by the claims that follow.