If carbon is used as the filler material for planarization, etch-back processes may etch the carbon filler material below the bit line damaging magnetic bits. An effective etch-back stop will protect magnetic bits from sub bit line etching during planarization.
In a following description, reference is made to the accompanying drawings, which form a part hereof, and in which is shown by way of illustration a specific example in which the invention may be practiced. It is to be understood that other embodiments may be utilized and structural changes may be made without departing from the scope.
It should be noted that the descriptions that follow, for example, in terms of method to protect magnetic bits during carbon field planarization is described for illustrative purposes and the underlying system can apply to any number and multiple types patterned stacks and planarization processes. In one embodiment, the magnetic bits protection can be configured as a silicon nitride stop layer. In other embodiments the stop layer materials may include other materials for example silicon, silicon oxide, silicon carbide or silicon oxy-nitride. The stop layer may be configured to include adjustable deposition thicknesses.
The thin silicon nitride stop layer 110 may be deposited using processes that may include for example Chemical Vapor Deposition (CVD), Plasma Enhanced Chemical Vapor Deposition (PECVD) and Reactive Ion Beam Deposition (RIBD); Ion Beam Deposition (IBD), Atomic Layer Deposition (ALD), or other processes. The deposition processes apply the thin silicon nitride stop layer 110 over the entire patterned surface of the patterned stack 100. The thicknesses of the thin silicon nitride stop layer 110 can be controlled to match the type of carbon material being used for a carbon fill layer 130 of one embodiment.
The carbon fill layer 130 has a portion of the deposited materials, the carbon field 135, removed in a planarization process 140. The planarization process 140 is used to smooth the surface to the tops of the patterned magnetic bits 120 or bit line. The planarization process 140 may include processes such as a Chemical Mechanical Process (CMP) where the chemical process includes an etching of the carbon fill layer 130 to remove the carbon field 135 or carbon material above the bit line, or other processes that may include for example Reactive Ion Etch (RIE) or Reactive Ion Beam etch (RIBE). A mechanical process may include a polishing process to reduce the height differences of the etching to create the smooth surface of one embodiment.
The chemical etching or etch-back of the carbon materials is stopped from affecting the patterned magnetic bits 120 by the thin silicon nitride stop layer 110. The thin silicon nitride stop layer 110 will not react with the chemicals that may be used in the etch-back process and the magnetic bits are protected during etch-back 150. The protection provided by the thin silicon nitride stop layer 110 preserves the magnetic integrity of the patterned magnetic bits 120 and magnetic film and the intended uses of their magnetic properties on the patterned stack 100. The method to protect magnetic bits during carbon field planarization allows the planarization of carbon backfilling to be used without damaging the magnetic bits and thus increases the quality of a patterned stack 100 such as a bit-patterned or discrete track media of one embodiment.
In another embodiment the thin silicon nitride stop layer 110 may be deposited using for example Chemical Vapor Deposition (CVD). A Chemical Vapor Deposition (CVD) process may include placing the patterned stack 100 in a deposition process chamber 200. The process may include depositing silicon nitride on patterned topography 210 using for example gas compounds that are injected into the deposition process chamber 200. The patterned stack 100 is heated and the injected gas compounds are deposited in thin films on the surfaces of the patterned stack 100 topography including the magnetic bits. A deposition process control of silicon nitride film thickness 220 is accomplished by control of the flow rate of gas compounds, temperature and pressure in the deposition process chamber 200. The deposited thin silicon nitride stop layer 110 forms an etch mask on the patterned stack 100 of one embodiment.
One or more processes may be used to deposit carbon fill layer 230 materials on the patterned stack 100 thin silicon nitride stop layer 110. The carbon fill materials may include one or more types of diamond-like carbon. A pure diamond-like carbon has properties such as hardness close to natural diamond. Other types of diamond-like carbon include other elements or compounds that may adjust the properties for example hardness and wear resistance. The method to protect magnetic bits during carbon field planarization allows the adjustment of the thin silicon nitride stop layer 110 thicknesses and composition to provide a range of protection of the magnetic bits for the various types of carbon fill materials.
The deposit of carbon fill layer 230 may be above the bit line of the magnetic bits and thin silicon nitride stop layer 110. The carbon fill layer 130 is smoothed and reduced in thickness to the bit line using one or more planarization process 140. The planarization process 140 creates smoothness of the contours of the patterned stack 100 topography surface by minimizing the step heights of the materials. The planarization process 140 may include chemical mechanical polishing planarization. A chemical mechanical polishing planarization process is used for smoothing surfaces with the combination of chemical and mechanical forces. The planarization chemical forces may include chemical etching of one embodiment.
The planarization chemical etching or etch-back process 240 may be used to reduce the thickness of the carbon field 135 to the bit line. The etch-back process 240 may result in a carbon field etched to or above bit line 250 or a carbon field etched below the bit line 260. The planarization etch-back process 240 may include for example a reactive ion beam etching of the carbon field 135 using a chemical such as oxygen gas (O2) as the reactive agent of one embodiment.
The method to protect magnetic bits during carbon field planarization provides a structure wherein an etch-back process stops at the thin silicon nitride stop layer 270. The etch-back process stops because the chemical ingredients of the etch-back process 240 do not react with the thin silicon nitride stop layer 110. Magnetic bits are protected during etch-back 150 by the thin silicon nitride stop layer 110. The protection of the patterned magnetic bits 120 of
The chemical vapor deposition (CVD) process may include placing the patterned stack 100 in a deposition process chamber 200 as part of the process of depositing silicon nitride on patterned topography 210. The chemical vapor deposition (CVD) process may include positioning the patterned stack 100 between two electrodes 300. The two electrodes 300 may be used to heat the patterned stack 100 to a temperature suitable for the chemistry chosen for the processing of one embodiment.
The chemical reaction may include gaseous compounds 320 injected through a gas compounds delivery tube 310. The gaseous compounds 320 may include Silane (SiH4), Ammonia (NH3), Tetrachlorosilane (SiCl4) and Dichlorosilane (SiCl2H2). The pressure of the injected gas can be used to regulate the flow rate. The pressure, temperature, concentrations of the gas compounds and their flow rates and exposure times may be used to control the thicknesses of the silicon nitride film depositions. The gaseous compounds 320 in contact with the heated patterned stack 100 create a chemical reaction that deposits silicon nitride films to form the stop layer of one embodiment.
The thicknesses of the thin silicon nitride stop layer 110 of
The deposition of diamond-like carbon (DLC) 500 may be of a thickness that extends above the bit line 400. The portion of the DLC deposited above the bit line 400 forming the carbon field 135 may be removed using the planarization process 140 of
The carbon fill layer 130 of
The properties of the type of diamond-like carbon (DLC) may also differ with added materials such as the amounts and types of diluents added to reduce the cost of production. Other differences in the properties of the type of diamond-like carbon (DLC) may include the fractional content of hydrogen. Diamond-like carbon (DLC) production methods may include the use of hydrogen or methane as a catalyst. This may result in different percentages of hydrogen remaining in the finished DLC material. The variations that may be included in the carbon materials used to in the deposition of diamond-like carbon (DLC) 500 can be accommodated through the adjustments in the thicknesses of the thin silicon nitride stop layer 110 of one embodiment.
The etch-back process 240 may include a reactive ion beam etching process that uses oxygen gas (O2) as a reactive agent. The oxygen gas (O2) reactive agent in the presence of the ion beam removes the carbon field 135 portion of the deposition of diamond-like carbon (DLC) 500. The thin silicon nitride stop layer 110 does not react with the oxygen gas (O2) in reactive ion beam etching process. This stops the reactive ion beam etching at the thin silicon nitride stop layer 110 not allowing the etching to damage the patterned magnetic bits 120 of the patterned stack 100 of one embodiment.
This added protection coverage prevents damage from below bit line etched carbon field 610 results of the etch-back process 240 of
The mechanical polishing may include the removal of the portion 700 of the thin silicon nitride stop layer 110 on top of the patterned magnetic bits 120 to the bit line 400. This will provide the smoothness to the surface of the patterned stack 100. The thin silicon nitride stop layer 110 has prevented damage to the patterned magnetic bits 120. The method to protect magnetic bits during carbon field planarization has provided a cost effective and efficient means of fabricating patterned stack 100 products that may include for example bit-patterned and discrete track media using a carbon fill layer 130 of
The foregoing has described the principles, embodiments and modes of operation. However, the invention should not be construed as being limited to the particular embodiments discussed. The above described embodiments should be regarded as illustrative rather than restrictive, and it should be appreciated that variations may be made in those embodiments by workers skilled in the art without departing from the scope as defined by the following claims.