The present invention relates generally to methods and structures for forming semiconductor devices with reduced contact resistance.
An integrated circuit (IC) generally includes a semiconductor substrate in which a number of device regions are formed by diffusion or ion implantation of suitable dopants. This substrate usually includes a passivating layer and an insulating layer, which are required in order to form different device regions. The total thickness of these layers is usually less than one micron. Openings through these layers (called vias or contact holes) and trenches therein allow electrical contact to be made selectively to the underlying device regions. A conducting material such as copper is used to fill these holes, which then make contact to semiconductor devices
Described herein are interconnect structures and methods of fabricating the interconnect structures. In one or more embodiments, the interconnect structure includes an interconnect dielectric having at least one contact landing within the interconnect dielectric and/or underlying the interconnect dielectric. The at least one contact landing includes a roughened upper surface, and a conductive metal in contact with the roughened upper surface of the contact landing, wherein the roughened upper surface has a surface roughness of 1 nanometer to 10 nanometer.
In one or embodiments, a method of fabricating an interconnect structure includes forming one or more openings in an interconnect dielectric, wherein the one or more openings expose at least one contact landing. An oxidative gas cluster ion beam process is then performed to the at least one contact landing, wherein oxidative gas cluster ion beam process forms an irregular oxide layer on an exposed surface of the at least one contact landing. Next, a cleaning process is performed o selectively remove the irregular oxide layer from the exposed surface of the at least one contact landing to form an irregular surface on the at least one contact landing, wherein the irregular surface has a surface roughness of 1 nanometer to 10 nanometers. The one or more openings are then filled with a conductive metal, wherein the conductive metal directly contacts the irregular surface on the at least one contact landing.
In one or more other embodiments, a method of fabricating an interconnect structure includes forming one or more openings in an interconnect dielectric, wherein the one or more openings expose at least one contact landing, and wherein the at least one contact landing has a smooth planar exposed surface. The smooth planar exposed surface of the at least one contact landing is roughened to form a roughened surface, wherein the roughened surface has a surface roughness of 1 nanometer to 10 nanometers. The one or more openings exposing the at least one contact landing are then filled with a conductive metal, wherein the conductive metal directly contacts the roughened surface on the at least one contact landing.
Additional features are realized through the techniques of the present invention. Other embodiments are described in detail herein and are considered a part of the claimed invention. For a better understanding of the invention with the features, refer to the description and to the drawings.
The subject matter which is regarded as the invention is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The forgoing features are apparent from the following detailed description taken in conjunction with the accompanying drawings.
Within a typical damascene interconnect structure, for example, metal vias run perpendicular to the semiconductor substrate (e.g., the substrate thickness) and metal lines run parallel to the semiconductor substrate (e.g., the substrate length). Typically, the metal vias are present beneath the metal lines and both features are embedded within a dielectric material. As the dimensions of integrated circuit shrink in the quest to improve chip performance, the reduction of contact area results in an increase in contact resistance. Moreover, it is generally desirable to reduce contact resistance to improve device performance.
Described herein are methods and structures for forming semiconductor devices with reduced contact resistance utilizing a gas cluster ion beam technique and cleaning process to increase surface area of a contact landing as well as contact structures that are formed from the same, which will now be described in greater detail by referring to the following discussion and drawings that accompany the present application. It is noted that the drawings of the present application are provided for illustrative purposes only and, as such, the drawings are not drawn to scale.
In the following description, numerous specific details are set forth, such as particular structures, components, materials, dimensions, processing steps and techniques, in order to provide a thorough understanding of the present invention. However, it will be appreciated by one of ordinary skill in the art that the present invention can be practiced without these specific details. In other instances, well-known structures or processing steps have not been described in detail in order to avoid obscuring the present invention.
It will be understood that when an element as a layer, region or substrate is referred to as being “on” or “over” another element, it can be directly on the other element or intervening elements can also be present. In contrast, when an element is referred to as being “directly on” or “directly over” another element, there are no intervening elements present. It will also be understood that when an element is referred to as being “connected” or “coupled” to another element, it can be directly connected or coupled to the other element or intervening elements can be present. In contrast, when an element is referred to as being “directly connected” or “directly coupled” to another element, there are no intervening elements present.
Reference is first made to
When the substrate is an insulating material, the insulating material can be an organic insulator, an inorganic insulator or a combination thereof including multilayers. When the substrate is a conducting material, the substrate can include, for example, polysilicon, an elemental metal, alloys of elemental metals, a metal silicide, a metal nitride or combinations thereof including multilayers. When the substrate is a semiconducting material, one or more semiconductor devices such as, for example, complementary metal oxide semiconductor (CMOS) devices can be fabricated thereon.
The interconnect dielectric material 10 can include any middle-of-the-line (MOL) or back-end-of-the-line (BEOL) dielectric including inorganic dielectrics or organic dielectrics. The interconnect dielectric material 10 can be porous or non-porous. Porous dielectric materials generally have a lower dielectric constant than the non-porous counterparts. Some examples of suitable dielectrics that can be used as the interconnect dielectric material 10 include, but are not limited to, SiO2, silsesquixoanes, C doped oxides (i.e., organosilicates) that include atoms of Si, C, O and H, thermosetting polyarylene ethers, or multilayers thereof. The term “polyarylene” is used in this application to denote aryl moieties or inertly substituted aryl moieties which are linked together by bonds, fused rings, or inert linking groups such as, for example, oxygen, sulfur, sulfone, sulfoxide, carbonyl and the like.
In one or more embodiments, the interconnect dielectric material 10 has a dielectric constant that is about 4.0 or less. In one or more other embodiments, the interconnect dielectric material 10 has a dielectric constant of about 2.8 or less. All dielectric constants mentioned in this detailed description are relative to a vacuum unless otherwise noted. Dielectrics having a dielectric constant of about 4.0 or less generally have a lower parasitic crosstalk as compared with dielectric materials that have a higher dielectric constant than 4.0. The thickness of the interconnect dielectric material 10 can vary depending upon the device dimensions, and the dielectric material used as well as the exact number of dielectrics within the interconnect dielectric material 10.
Referring now to
Referring to
Each opening of the plurality of openings 120 can be formed utilizing techniques well known to those skilled in the art. For example, each opening of the plurality of openings can be formed by lithography (i.e., applying a photoresist to the surface of the interconnect dielectric material 102, exposing the photoresist to a desired pattern of radiation, and developing the exposed resist utilizing a conventional resist developer), and etching (dry etching or wet etching) an opening in the interconnect dielectric material 102. The term “dry etching” is used herein to denote an etching technique such as reactive-ion etching, ion beam etching, plasma etching or laser ablation.
When a combined via and line opening is formed, a second iteration of lithography and etching is typically employed. Also, in one or more embodiments, the via can be formed first, followed by the trench such as by a dual damascene process. In one or more other embodiments, the line can be formed first, then the via. In either instance, the via and line are in communication with each other.
Each via opening 120 is an opening that runs perpendicular to the underlying substrate and it generally has a width, w, as measured from one sidewall to another sidewall, of from 10 nm to less than 80 nm. Each line opening which runs parallel to the underlying substrate has a width, w1, which is greater than the width of each via opening 120. Typically, each line opening has a width, w1, measured from one sidewall to another sidewall, of from 15 nm to 80 nm. Each via opening 120 that is formed can have a same or different width and/or height. Each line opening that is formed can have a same or different width and/or height.
Referring to
In the gas cluster ion beam process used to provide the oxidized surface, beams composed of clusters of oxygen atoms can be singly ionized, accelerated, and impact the surfaces of the semiconductor device 100. The gas cluster ion beam process can be performed in a vacuum environment of any conventional ion-beam apparatus. As such, contamination control for the work piece surface can be obtained. The interconnect dielectric 102, which is itself oftentimes an oxygen containing dielectric such as silicon dioxide, will not suffer plasma damage. Likewise, damage to the other materials such as the spacer layers 114 will be minimal at worse and at any rate, of no consequence.
In one or more embodiments, the gas cluster ion beam oxidation process can be performed with a dose from 1×e12 clusters/cm2 to 1×e18 clusters/cm2. In another embodiment, the gas cluster ion beam oxidation can be performed with a dose from 1×e14 clusters/cm2to 1×e18 clusters/cm2. Other doses that are below and/or above the aforementioned ranges can also be employed in embodiments of the present invention.
In one or more embodiments, the gas cluster ion beam oxidation can be performed at a pressure from 10−2 Torr to 10−6 Torr. In one or more other embodiments, the gas cluster ion beam oxidation can be performed at a pressure from 10−3 Torr to 10−6 Torr. Other pressure values that are below and/or above the aforementioned ranges can also be employed in the present invention.
In one or more embodiments, the gas cluster ion beam oxidation that can be performed at a power/energy from 2 keV to 80 keV. In one or more other embodiments, the gas cluster ion beam oxidation that can be employed can be performed at a power/energy from 10 keV to 60 keV. Other power/energy values that are below and/or above the aforementioned ranges can also be employed in embodiments of the present invention.
In one or more embodiments, the gas cluster ion beam oxidation can be performed at a temperature from 20° C. to 500° C. In one or more other embodiments, the gas cluster ion beam oxidation can be performed at a temperature from 20° C. to 400° C. Other temperatures that are below and/or above the aforementioned ranges can also be employed in embodiments of the present invention.
In one or more embodiments, the gas used in the gas cluster ion beam oxidation process is composed of an oxidative reactive gas, including, but not limited to, oxygen and/or an oxygen-containing gas and any combination thereof. The oxidative reactive gas can be used neat (i.e., 100% pure reactive gas), or the oxidative reactive gas can be admixed with a quantity of an inert gas such as, for example, neon (Ne), helium (He), argon (Ar), krypton (Kr) and/or xenon (Xe).
Turning now to
Suitable conductive materials include, for example, polysilicon, a conductive metal, an alloy including at least two conductive metals, a conductive metal silicide or combinations thereof. In one or more embodiments, the conductive material 130 is a conductive metal such as Cu, W or Al. In another embodiment, the conductive material 130 includes Cu or a Cu alloy (such as AlCu).
The conductive material 130 can be formed utilizing a conventional deposition process including, but not limited to, CVD, PECVD, sputtering, chemical solution deposition or plating.
By increasing surface roughness of the contact landing, subsequent filling of the via with a conductive material advantageously reduces the contact resistance, wherein the increased surface roughness increases the surface area that contacts the conductive material. The average surface roughness (Ra) is 1 nanometer (nm) to 10 nm. Surface roughness can be measured in a manner generally known by those skilled in the art. By way of example, surface roughness can be measured microscopically, e.g., transmission electron microscopy.
The cleaning process can be a wet etch process to selectively remove the oxide layer from the contact landing. An exemplary wet etch process includes is by etching using water diluted HF with some buffering agents such as ammonium fluoride.
Optionally, a diffusion barrier (200) can be conformally deposited and patterned before or after the gas cluster ion beam oxidation and cleaning steps The diffusion barrier can include Ta, TaN, Ti, TiN, Ru, RuN, W, WN or any other material that can serve as a barrier to prevent conductive material from diffusing there through. In some embodiments, a combination of the above mentioned diffusion barrier materials, i.e., TiN/Ti or TaN/Ta, can be employed as diffusion barrier. The diffusion barrier can be formed a deposition process such as, for example, atomic layer deposition (ALD), chemical vapor deposition (CVD), plasma enhanced chemical vapor deposition (PECVD), physical vapor deposition (PVD), sputtering, chemical solution deposition, or plating. The thickness of the diffusion barrier 16 can vary depending on the exact means of the deposition process as well as the material employed. Typically, the diffusion barrier has a thickness from 4 nm to 40 nm, with a thickness from 7 nm to 20 nm being more typical.
In some embodiments, especially when Cu or a Cu alloy is employed as the conductive material 130, an optional plating seed layer (not shown) can be formed on the diffusion barrier prior to forming the conductive material. The optional plating seed layer is employed to selectively promote subsequent electroplating of a pre-selected conductive metal or metal alloy. The optional plating seed layer can include Cu, a Cu alloy, Ir, an Ir alloy, Ru, a Ru alloy (e.g., TaRu alloy) or any other suitable noble metal or noble metal alloy having a low metal-plating over potential. Typically, Cu or a Cu alloy plating seed layer is employed, when a Cu metal is to be subsequently formed within the at least one opening. The thickness of the optional seed layer can vary depending on the material of the optional plating seed layer as well as the technique used in forming the same. Typically, the optional plating seed layer has a thickness from 2 nm to 80 nm. The optional plating seed layer can be formed by a conventional deposition process including, for example, CVD, PECVD, ALD, and PVD.
Referring now to
The descriptions of the various embodiments of the present invention have been presented for purposes of illustration, but are not intended to be exhaustive or limited to the embodiments described herein. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the described embodiments. The terminology used herein was chosen to best explain the principles of the embodiments, the practical application or technical improvement over technologies found in the marketplace, or to enable others of ordinary skill in the art to understand the embodiments described herein.
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Number | Date | Country | |
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20180061762 A1 | Mar 2018 | US |