US20030049496A1 - Thin film protective layer with buffering interface - Google Patents

Thin film protective layer with buffering interface Download PDF

Info

Publication number
US20030049496A1
US20030049496A1 US09/952,872 US95287201A US2003049496A1 US 20030049496 A1 US20030049496 A1 US 20030049496A1 US 95287201 A US95287201 A US 95287201A US 2003049496 A1 US2003049496 A1 US 2003049496A1
Authority
US
United States
Prior art keywords
thin film
overcoat
nitrogen
protective layer
layer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US09/952,872
Inventor
Daryl Pocker
Jan-Ulrich Thiele
Bond-Yen Ting
Richard White
Bing Yen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GlobalFoundries Inc
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US09/952,872 priority Critical patent/US20030049496A1/en
Assigned to INTERNATIONAL BUSINESS MACHINES CORPORATION reassignment INTERNATIONAL BUSINESS MACHINES CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: THIELE, JAN-ULRICH, POCKER, DARYL J., TING, BOND-YEN, WHITE, RICHARD LONGSTRETH, YEN, BING K.
Publication of US20030049496A1 publication Critical patent/US20030049496A1/en
Priority to US10/756,556 priority patent/US6969447B2/en
Assigned to GLOBALFOUNDRIES U.S. 2 LLC reassignment GLOBALFOUNDRIES U.S. 2 LLC ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: INTERNATIONAL BUSINESS MACHINES CORPORATION
Assigned to GLOBALFOUNDRIES INC. reassignment GLOBALFOUNDRIES INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GLOBALFOUNDRIES U.S. 2 LLC, GLOBALFOUNDRIES U.S. INC.
Abandoned legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/34Sputtering
    • C23C14/3435Applying energy to the substrate during sputtering
    • C23C14/345Applying energy to the substrate during sputtering using substrate bias
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/0641Nitrides
    • C23C14/0658Carbon nitride
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B5/00Recording by magnetisation or demagnetisation of a record carrier; Reproducing by magnetic means; Record carriers therefor
    • G11B5/62Record carriers characterised by the selection of the material
    • G11B5/72Protective coatings, e.g. anti-static or antifriction
    • G11B5/726Two or more protective coatings
    • G11B5/7262Inorganic protective coating
    • G11B5/7264Inorganic carbon protective coating, e.g. graphite, diamond like carbon or doped carbon
    • G11B5/7268Inorganic carbon protective coating, e.g. graphite, diamond like carbon or doped carbon comprising elemental nitrogen in the inorganic carbon coating
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B5/00Recording by magnetisation or demagnetisation of a record carrier; Reproducing by magnetic means; Record carriers therefor
    • G11B5/74Record carriers characterised by the form, e.g. sheet shaped to wrap around a drum
    • G11B5/82Disk carriers
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B5/00Recording by magnetisation or demagnetisation of a record carrier; Reproducing by magnetic means; Record carriers therefor
    • G11B5/84Processes or apparatus specially adapted for manufacturing record carriers
    • G11B5/8408Processes or apparatus specially adapted for manufacturing record carriers protecting the magnetic layer
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F41/00Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties
    • H01F41/32Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for applying conductive, insulating or magnetic material on a magnetic film, specially adapted for a thin magnetic film
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B5/00Recording by magnetisation or demagnetisation of a record carrier; Reproducing by magnetic means; Record carriers therefor
    • G11B5/012Recording on, or reproducing or erasing from, magnetic disks

Definitions

  • the invention relates to thin film protective layers and to methods for the deposition of thin film protective layers and more particularly to films comprising carbon and nitrogen (CNx) and even more particularly to such films as used on magnetic thin film media.
  • CNx carbon and nitrogen
  • FIG. 1 A typical prior art head and disk system 10 is illustrated in FIG. 1.
  • the magnetic transducer 20 is supported by the suspension 13 as it flies above the disk 16 .
  • the magnetic transducer 20 usually called a “head” or “slider,” is composed of elements that perform the task of writing magnetic transitions (the write head 23 ) and reading the magnetic transitions (the read head 12 ).
  • the electrical signals to and from the read and write heads 12 , 23 travel along conductive paths (leads) 14 which are attached to or embedded in the suspension 13 .
  • the magnetic transducer 20 is positioned over points at varying radial distances from the center of the disk 16 to read and write circular tracks (not shown).
  • the disk 16 is attached to a spindle 18 that is driven by a spindle motor 24 to rotate the disk 16 .
  • the disk 16 comprises a substrate 26 on which a plurality of thin films 21 are deposited.
  • the thin films 21 include ferromagnetic material in which the write head 23 records the magnetic transitions in which information is encoded.
  • the thin film protective layer (not shown in FIG. 1) is typically the last or outermost layer.
  • the conventional disk 16 typically has a substrate 26 of AlMg or glass.
  • the thin films 21 on the disk 16 typically include a chromium or chromium alloy underlayer that is deposited on the substrate 26 .
  • the magnetic layer in the thin films 21 is based on various alloys of cobalt, nickel and iron. For example, a commonly used alloy is CoPtCr. However, additional elements such as tantalum and boron are often used in the magnetic alloy.
  • FIG. 2 illustrates one common internal structure of thin films 21 on disk 16 .
  • the protective overcoat layer 37 is used to improve wearability and corrosion.
  • the materials and/or compositions which are optimized for one performance characteristic of an overcoat are rarely optimized for others.
  • the most commonly used protective layer materials for commercial thin film disks have been carbon, hydrogenated carbon (CHx), nitrogenated carbon (CNx) and CNxHy.
  • CHx hydrogenated carbon
  • CNx nitrogenated carbon
  • CNxHy CNxHy
  • Efforts to optimize overcoat properties have included use of a layer structure using different materials and/or compositions for each of two or more layers in the overcoat structure. For example, U.S. Pat. No. 5,942,317 issued to R.
  • White describes the use of a graded CHx protective layer wherein the hydrogen content is highest at the film's surface to take advantage of the lower polar surface energy characteristic of higher hydrogen levels (which improves corrosion resistance) and is lowest at the interface with the magnetic layer to optimize the adhesion properties.
  • the midlevel of the CHx film is likewise optimized by having an intermediate hydrogen concentration which has a high hardness to improve wearability.
  • the variations in the hydrogen content can be continuous or discrete.
  • a protective layer structure with three sublayers with lower hydrogen concentration nearest the magnetic layer, intermediate hydrogen concentration in the middle sublayer and high hydrogen concentration at the surface is suggested in White '317. Hardness and density are reduced by the presence of hydrogen in certain percentage ranges; thus, the overcoat structure of White '317 is hardest and densest at the interface with the magnetic layer.
  • U.S. Pat. No. 6,086,730 to Liu, et al. describes a method for sputtering a carbon protective layer with a high sp 3 content which involves applying relatively high voltage pulses to the carbon target. Liu '730 asserts that the resulting carbon overcoat has good durability and corrosion resistance down to low thicknesses.
  • the protective overcoat 37 must be made as thin as possible to reduce the separation from the magnetic transducer 20 and the magnetic thin film 33 while maintaining the protective function.
  • the applicants disclose a method for sputtering a protective layer which allows the protective layer to be ultra-thin with improved durability over prior art films.
  • the method reduces the kinetic energy of the impinging ions during the initial period of deposition to form a buffering interface which reduces the interpenetration of the atoms of the protective layer into the underlying film.
  • the lower energy ions form a less dense and softer film than do higher energy ions.
  • the sputtering of the overcoat preferably begins with zero (or very low) bias voltage applied to the underlying film. This “low energy” phase of the deposition results in minimal ion implantation in the underlying film.
  • the “low energy” deposition continues only as long as it takes to form a buffer layer of the overcoat material on the underlying film.
  • the buffer layer deposited in this phase is relatively soft and is, therefore, not sufficient for a complete overcoat.
  • the “high energy” phase of the process begins with increases in the magnitude of the negative bias voltage applied to the underlying film.
  • the higher energy imparted to ions in the plasma result in a denser and harder film being formed over the initial buffer layer.
  • the initial buffer layer reduces the interpenetration of the higher energy ions into the underlying film.
  • the protective layer preferably comprises carbon and nitrogen.
  • the protective layer structure of the invention is preferably used over a magnetic layer on thin film magnetic media.
  • the protective film produced by the method of the invention has a relatively lower density at the interface with the underlying film and a relatively higher density at the surface.
  • FIG. 1 is a symbolic illustration of the prior art showing the relationships between the head and associated components in a disk drive.
  • FIG. 2 is an illustration of a layer structure for a magnetic thin film disk according to the invention.
  • FIG. 3 is a graph of the anticipated distribution of the depth of 50 ev carbon ion implantation into a CoPtCr magnetic film.
  • FIG. 2 illustrates a cross section of a magnetic thin film disk embodying the protective layer structure of the invention.
  • the film structure illustrated contains only one magnetic layer 33 and one underlayer 31 .
  • the protective layer structure of the invention is not dependent on any particular underlying film structure so long as the final layer below the overcoat is conductive.
  • the protective layer of the invention therefore, may be used on any combination of multiple magnetic layers, underlayers and seed layers.
  • the interface 42 between the magnetic layer 33 and the protective layer 37 is the region of the protective layer 37 that has the lowest density (indicated by the spacing of the small circles in the drawing) and the surface of the protective layer 37 has the highest density.
  • the preferred material for the protective layer 37 is CNx.
  • Other elements such as hydrogen may be added to the film in relatively small atomic percentages.
  • the preferred method of depositing the protective layer 37 of the invention is by sputtering using known techniques for forming a CNx film with the exceptions noted below.
  • a graphite target is used and nitrogen is introduced into the sputtering chamber as a gas.
  • the relative concentration of nitrogen in the deposited film is controlled by modulating the partial pressure of the nitrogen gas in the chamber. Lower partial pressures of nitrogen result in lower concentrations of nitrogen in the film as would be expected.
  • the precise partial pressures of nitrogen and the working gas typically argon
  • the preferred embodiment of the invention has from 5 to 25 at. % nitrogen in the protective layer.
  • the preferred thickness of the protective layer is from 2 to 9 nanometers.
  • the method of the invention includes modulating the bias voltage applied to underlying film.
  • the use of negative bias voltages applied to metallic substrates is well known. The larger the magnitude of the voltage, the more kinetic energy is imparted to the positive ions as they are accelerated toward the substrate. Higher energy ions result in a denser, harder and smoother overcoat film due, at least in part, to resputtering effects. The higher energy ions also interpenetrate the underlying film to a greater depth than do lower energy ions. This interpenetration is considered to be negligible for many applications since the depth of penetration is small in comparison to the film thickness.
  • FIG. 3 is a graph of the anticipated distribution of the depth of 50 ev carbon ion implantation into a CoPtCr magnetic film.
  • the initial bias voltage is essentially zero which reduces the average energy of the impinging ions to a few electron volts.
  • the interpenetration of the overcoat atoms into the magnetic film is negligible at this energy level.
  • a second batch of otherwise identical disks was prepared using the method of the invention to sputter 2.5 nm CNx overcoats.
  • the particular sputtering setup required approximately four (4) seconds to deposit 2.5 nm of CNx.
  • no voltage bias was applied to the underlying CoPtCr film.
  • the underlying film was then subjected to ⁇ 50 v dc bias for the remainder of the deposition.
  • This second batch of disks was then burnished and tested for flyability. These disks passed the flyability test 87% of the time representing nearly a six-fold increase in yield over the prior art disks.
  • the bias was rapidly switched from 0 to ⁇ 50 v dc after the initial period in which the lower density CNx material for the buffering interface was formed.
  • the bias can also be increased gradually, as long as the low and high density portions of the film are given adequate time to form.
  • the preferred range of dc bias voltages for the high voltage period is from ⁇ 50 v to ⁇ 400 v.
  • the method of the invention can also be used with dual cathode pulsed sputtering techniques.
  • this technique the pulsing of opposing targets provides considerable ion bombardment of the films deposited on grounded substrates, therefore, for this embodiment the preferred bias voltages are in the range of 0 (ground) to ⁇ 200 v.
  • the contact points for delivery of the bias voltage to the conductive film on which the protective layer of the invention is to be formed must not have been shadowed during the deposition of the conductive film(s). This condition is satisfied if the disk is held at different points during the deposition of the overcoat other than the points at which the disk was held during the deposition of the conductive film. A small rotation of the disk after the deposition of the conductive film is sufficient to move the contact points to locations where the conductive has been adequately formed. Since the magnetic thin films in question are on the order of ten's of nanometers thick care must be taken not to overheat the thin film through which the bias current flows.

Abstract

A method for sputtering a thin film protective layer that allows the protective layer (overcoat) to be ultra-thin with improved durability over prior art films is disclosed. The method reduces kinetic energy of the ions of the overcoat material during the initial period of deposition to form a buffering interface which reduces the interpenetration of the atoms of the protective layer into the underlying film. In the method of the invention the sputtering of the overcoat preferably begins with zero (or very low) voltage applied to the underlying film resulting in minimal ion implantation in the underlying film. The “high energy” phase of the process begins with increases in the magnitude of the negative bias voltage applied to the underlying film. The higher energy imparted to ions in the plasma result in a denser and harder film being formed over the initial buffer layer. The protective layer preferably comprises carbon and nitrogen. The protective layer structure of the invention is preferably used over a magnetic layer on thin film magnetic media.

Description

    FIELD OF THE INVENTION
  • The invention relates to thin film protective layers and to methods for the deposition of thin film protective layers and more particularly to films comprising carbon and nitrogen (CNx) and even more particularly to such films as used on magnetic thin film media. [0001]
  • BACKGROUND OF THE INVENTION
  • A typical prior art head and [0002] disk system 10 is illustrated in FIG. 1. In operation the magnetic transducer 20 is supported by the suspension 13 as it flies above the disk 16. The magnetic transducer 20, usually called a “head” or “slider,” is composed of elements that perform the task of writing magnetic transitions (the write head 23) and reading the magnetic transitions (the read head 12). The electrical signals to and from the read and write heads 12, 23 travel along conductive paths (leads) 14 which are attached to or embedded in the suspension 13. The magnetic transducer 20 is positioned over points at varying radial distances from the center of the disk 16 to read and write circular tracks (not shown). The disk 16 is attached to a spindle 18 that is driven by a spindle motor 24 to rotate the disk 16. The disk 16 comprises a substrate 26 on which a plurality of thin films 21 are deposited. The thin films 21 include ferromagnetic material in which the write head 23 records the magnetic transitions in which information is encoded. The thin film protective layer (not shown in FIG. 1) is typically the last or outermost layer.
  • The [0003] conventional disk 16 typically has a substrate 26 of AlMg or glass. The thin films 21 on the disk 16 typically include a chromium or chromium alloy underlayer that is deposited on the substrate 26. The magnetic layer in the thin films 21 is based on various alloys of cobalt, nickel and iron. For example, a commonly used alloy is CoPtCr. However, additional elements such as tantalum and boron are often used in the magnetic alloy.
  • FIG. 2 illustrates one common internal structure of [0004] thin films 21 on disk 16. The protective overcoat layer 37 is used to improve wearability and corrosion. The materials and/or compositions which are optimized for one performance characteristic of an overcoat are rarely optimized for others. The most commonly used protective layer materials for commercial thin film disks have been carbon, hydrogenated carbon (CHx), nitrogenated carbon (CNx) and CNxHy. Efforts to optimize overcoat properties have included use of a layer structure using different materials and/or compositions for each of two or more layers in the overcoat structure. For example, U.S. Pat. No. 5,942,317 issued to R. White describes the use of a graded CHx protective layer wherein the hydrogen content is highest at the film's surface to take advantage of the lower polar surface energy characteristic of higher hydrogen levels (which improves corrosion resistance) and is lowest at the interface with the magnetic layer to optimize the adhesion properties. The midlevel of the CHx film is likewise optimized by having an intermediate hydrogen concentration which has a high hardness to improve wearability. The variations in the hydrogen content can be continuous or discrete. For example, a protective layer structure with three sublayers with lower hydrogen concentration nearest the magnetic layer, intermediate hydrogen concentration in the middle sublayer and high hydrogen concentration at the surface is suggested in White '317. Hardness and density are reduced by the presence of hydrogen in certain percentage ranges; thus, the overcoat structure of White '317 is hardest and densest at the interface with the magnetic layer.
  • In U.S. Pat. No. 5,679,431 Chen, et al., describe the use of a bilayer protective overcoat in which the initial sublayer is carbon, titanium or chromium and the surface sublayer is CHx or CNx. The problem being addressed in Chen '431 is diffusion of nitrogen or hydrogen into the magnetic layer over time. The initial sublayer is intended to act as a diffusion barrier. [0005]
  • U.S. Pat. No. 6,086,730 to Liu, et al., describes a method for sputtering a carbon protective layer with a high sp[0006] 3 content which involves applying relatively high voltage pulses to the carbon target. Liu '730 asserts that the resulting carbon overcoat has good durability and corrosion resistance down to low thicknesses.
  • In order to improve the performance of magnetic thin film media the [0007] protective overcoat 37 must be made as thin as possible to reduce the separation from the magnetic transducer 20 and the magnetic thin film 33 while maintaining the protective function.
  • SUMMARY OF THE INVENTION
  • The applicants disclose a method for sputtering a protective layer which allows the protective layer to be ultra-thin with improved durability over prior art films. The method reduces the kinetic energy of the impinging ions during the initial period of deposition to form a buffering interface which reduces the interpenetration of the atoms of the protective layer into the underlying film. The lower energy ions form a less dense and softer film than do higher energy ions. In the method of the invention the sputtering of the overcoat preferably begins with zero (or very low) bias voltage applied to the underlying film. This “low energy” phase of the deposition results in minimal ion implantation in the underlying film. The “low energy” deposition continues only as long as it takes to form a buffer layer of the overcoat material on the underlying film. The buffer layer deposited in this phase is relatively soft and is, therefore, not sufficient for a complete overcoat. The “high energy” phase of the process begins with increases in the magnitude of the negative bias voltage applied to the underlying film. The higher energy imparted to ions in the plasma result in a denser and harder film being formed over the initial buffer layer. The initial buffer layer reduces the interpenetration of the higher energy ions into the underlying film. The protective layer preferably comprises carbon and nitrogen. The protective layer structure of the invention is preferably used over a magnetic layer on thin film magnetic media. The protective film produced by the method of the invention has a relatively lower density at the interface with the underlying film and a relatively higher density at the surface. [0008]
  • BRIEF DESCRIPTION OF THE FIGURES
  • FIG. 1 is a symbolic illustration of the prior art showing the relationships between the head and associated components in a disk drive. [0009]
  • FIG. 2 is an illustration of a layer structure for a magnetic thin film disk according to the invention. [0010]
  • FIG. 3 is a graph of the anticipated distribution of the depth of 50 ev carbon ion implantation into a CoPtCr magnetic film.[0011]
  • DETAILED DESCRIPTION OF THE INVENTION AND THE PREFERRED EMBODIMENTS
  • FIG. 2 illustrates a cross section of a magnetic thin film disk embodying the protective layer structure of the invention. The film structure illustrated contains only one [0012] magnetic layer 33 and one underlayer 31. However, the protective layer structure of the invention is not dependent on any particular underlying film structure so long as the final layer below the overcoat is conductive. The protective layer of the invention, therefore, may be used on any combination of multiple magnetic layers, underlayers and seed layers. The interface 42 between the magnetic layer 33 and the protective layer 37 is the region of the protective layer 37 that has the lowest density (indicated by the spacing of the small circles in the drawing) and the surface of the protective layer 37 has the highest density.
  • The preferred material for the [0013] protective layer 37 is CNx. Other elements such as hydrogen may be added to the film in relatively small atomic percentages. The preferred method of depositing the protective layer 37 of the invention is by sputtering using known techniques for forming a CNx film with the exceptions noted below. In the typical process for forming a CNx film a graphite target is used and nitrogen is introduced into the sputtering chamber as a gas. The relative concentration of nitrogen in the deposited film is controlled by modulating the partial pressure of the nitrogen gas in the chamber. Lower partial pressures of nitrogen result in lower concentrations of nitrogen in the film as would be expected. As is well known to those in the sputtering arts, the precise partial pressures of nitrogen and the working gas (typically argon) are derived empirically for each unique combination of equipment used in the sputtering process.
  • The preferred embodiment of the invention has from 5 to 25 at. % nitrogen in the protective layer. The preferred thickness of the protective layer is from 2 to 9 nanometers. [0014]
  • The method of the invention includes modulating the bias voltage applied to underlying film. The use of negative bias voltages applied to metallic substrates is well known. The larger the magnitude of the voltage, the more kinetic energy is imparted to the positive ions as they are accelerated toward the substrate. Higher energy ions result in a denser, harder and smoother overcoat film due, at least in part, to resputtering effects. The higher energy ions also interpenetrate the underlying film to a greater depth than do lower energy ions. This interpenetration is considered to be negligible for many applications since the depth of penetration is small in comparison to the film thickness. However, in applications such as magnetic thin film media, the films are sufficiently thin that the interpenetration of atoms into the lattice of magnetic materials is undesirable. FIG. 3 is a graph of the anticipated distribution of the depth of 50 ev carbon ion implantation into a CoPtCr magnetic film. Using the method of the invention the initial bias voltage is essentially zero which reduces the average energy of the impinging ions to a few electron volts. The interpenetration of the overcoat atoms into the magnetic film is negligible at this energy level. [0015]
  • Moreover, for ultra-thin overcoats (for example, 0.5 to 2.5 nm) the performance of the overcoat depends critically on the nature of the interface with the underlying film. Although negative voltage bias improves the overcoat itself, it has been found by the applicants to degrade the interface for overcoats on the order of 2.5 nm thick. [0016]
  • In an experiment performed by the applicants, prior art sputtering techniques using −50 v bias were used to deposit 2.5 nm CNx overcoats on a batch of thin film magnetic disks. The disks were then subjected to the finishing and testing process that is normally used for large scale manufacturing of magnetic disks which includes burnishing the surface of the disks using special heads with leading edges designed to cut off the higher protrusions. To be commercially usable the overcoat on the disks must be able to withstand this burnishing and still present a surface to the slider of the magnetic transducer over which the slider can “fly” without excessive disturbance. In the experiment 85% of the prior art disks with 2.5 nm CNx overcoats failed to provide a flyable surface after burnishing, i.e., the usable yield was 15%. [0017]
  • A second batch of otherwise identical disks was prepared using the method of the invention to sputter 2.5 nm CNx overcoats. The particular sputtering setup required approximately four (4) seconds to deposit 2.5 nm of CNx. For the initial one (1) second, no voltage bias was applied to the underlying CoPtCr film. The underlying film was then subjected to −50 v dc bias for the remainder of the deposition. This second batch of disks was then burnished and tested for flyability. These disks passed the flyability test 87% of the time representing nearly a six-fold increase in yield over the prior art disks. [0018]
  • In the experiment described above the bias was rapidly switched from 0 to −50 v dc after the initial period in which the lower density CNx material for the buffering interface was formed. The bias can also be increased gradually, as long as the low and high density portions of the film are given adequate time to form. The preferred range of dc bias voltages for the high voltage period is from −50 v to −400 v. [0019]
  • The method of the invention can also be used with dual cathode pulsed sputtering techniques. With this technique the pulsing of opposing targets provides considerable ion bombardment of the films deposited on grounded substrates, therefore, for this embodiment the preferred bias voltages are in the range of 0 (ground) to −200 v. [0020]
  • Applying bias to disks with conductive substrates such as the NiP coated AlMg substrates is a straightforward process. The edges of the disk are held during sputtering by conductive material to which the bias voltage is applied. Whether the points of electrical contact are blocked or shadowed during the deposition is irrelevant since the substrate itself is conductive. However, for nonconductive substrates such as glass the bias voltage must be applied to a conductive film on the disk, so shadowing must be taken into account. There are several different types of mechanical systems used to load and support disks while they are being sputtered. Regardless of what type of system is being used, the contact points for delivery of the bias voltage to the conductive film on which the protective layer of the invention is to be formed must not have been shadowed during the deposition of the conductive film(s). This condition is satisfied if the disk is held at different points during the deposition of the overcoat other than the points at which the disk was held during the deposition of the conductive film. A small rotation of the disk after the deposition of the conductive film is sufficient to move the contact points to locations where the conductive has been adequately formed. Since the magnetic thin films in question are on the order of ten's of nanometers thick care must be taken not to overheat the thin film through which the bias current flows. [0021]
  • The atomic percent compositions given above are given without regard for the small amounts of contamination that invariably exist in sputtered thin films as is well known to those skilled in the art. [0022]
  • The invention has been described with respect to use on thin film magnetic disks, but other uses and applications which can benefit from the properties of the protective layer structure of the invention will be apparent to those skilled in the art. [0023]

Claims (20)

1. An article with a thin film layer structure comprising:
a conductive thin film; and
a protective layer formed on the conductive thin film, the protective layer comprising carbon and nitrogen and having a lower density nearer the conductive thin film and a higher density nearer a surface of the protective layer.
2. The article of claim 1 wherein the conductive film is ferromagnetic.
3. The article of claim 2 wherein the atomic percentage of nitrogen is from 5 to 25 atomic percent.
4. The article of claim 2 wherein the protective layer is from 0.5 to 9 nanometers thick.
5. The article of claim 2 wherein the conductive thin film is an alloy of cobalt.
6. A method of depositing thin films comprising the steps of:
depositing a conductive thin film layer on an article;
depositing a buffer layer on the conductive thin film layer comprising carbon and nitrogen while applying a bias voltage from zero to a first negative voltage applied to the conductive thin film layer for a first time period;
changing the bias voltage to a second negative voltage, the second negative voltage being greater in magnitude than the first negative voltage; and
depositing a thin film layer comprising carbon and nitrogen on the buffer layer while the bias voltage is the second negative voltage for a second time period.
7. The method of claim 6 wherein the conductive thin film layer is ferromagnetic.
8. The method of claim 7 further comprising the steps of applying holding the article at a first set of points while depositing the conductive thin film layer and applying bias voltage through a second set of points different from the first set of points while depositing the thin film layer comprising carbon and nitrogen.
9. The method of claim 8 further comprising the steps of rotating the article after depositing the conductive thin film layer and before depositing the buffer layer and applying the second negative voltage to the conductive film through the second set of points where the conductive thin film layer was not subject to shadowing during deposition.
10. The method of claim 7 wherein the second negative voltage is a dc voltage from −50 v to −400 v.
11. The method of claim 7 wherein the second negative voltage is a pulsed voltage from ground to −400 v.
12. The method of claim 7 wherein a thickness of layers comprising carbon and nitrogen is from 0.5 to 9 nm.
13. The method of claim 7 wherein the second time period is longer than the first time period.
14. The method of claim 13 wherein the second time period is approximately four times as long as the first time period.
15. The method of claim 6 wherein a thickness of layers comprising carbon and nitrogen is from 0.5 to 9 nm, the second negative voltage is a dc voltage from −50 v to −400 v and the method further comprises the step of applying the second negative voltage to the conductive thin film layer at one or more points where the conductive thin film layer was not subject to shadowing during deposition.
16. A disk drive comprising:
a magnetic transducer including a read and a write head for reading and writing magnetic transitions;
a spindle; and
a thin film disk mounted on the spindle to rotate in a confronting position in relation to the magnetic transducer, the thin film disk including magnetic material in which the magnetic transducer writes magnetic transitions; and
a overcoat comprising carbon and nitrogen over the magnetic material, the overcoat having a buffer layer of a lower density adjacent to the magnetic material and layer of higher density at a surface of the overcoat.
17. The disk drive of claim 16 wherein the atomic percentage of nitrogen in the overcoat is from 5 to 25 atomic percent.
18. The disk drive of claim 16 wherein the overcoat is from 0.5 to 9 nanometers thick.
19. The disk drive of claim 16 wherein the magnetic material is an alloy of cobalt.
20. The disk drive of claim 16 wherein the atomic percentage of nitrogen in the overcoat is from 5 to 25 atomic percent and the overcoat is from 0.5 to 9 nanometers thick.
US09/952,872 2001-09-11 2001-09-11 Thin film protective layer with buffering interface Abandoned US20030049496A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US09/952,872 US20030049496A1 (en) 2001-09-11 2001-09-11 Thin film protective layer with buffering interface
US10/756,556 US6969447B2 (en) 2001-09-11 2004-01-12 Thin film protective layer with buffering interface

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/952,872 US20030049496A1 (en) 2001-09-11 2001-09-11 Thin film protective layer with buffering interface

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US10/756,556 Division US6969447B2 (en) 2001-09-11 2004-01-12 Thin film protective layer with buffering interface

Publications (1)

Publication Number Publication Date
US20030049496A1 true US20030049496A1 (en) 2003-03-13

Family

ID=25493307

Family Applications (2)

Application Number Title Priority Date Filing Date
US09/952,872 Abandoned US20030049496A1 (en) 2001-09-11 2001-09-11 Thin film protective layer with buffering interface
US10/756,556 Expired - Fee Related US6969447B2 (en) 2001-09-11 2004-01-12 Thin film protective layer with buffering interface

Family Applications After (1)

Application Number Title Priority Date Filing Date
US10/756,556 Expired - Fee Related US6969447B2 (en) 2001-09-11 2004-01-12 Thin film protective layer with buffering interface

Country Status (1)

Country Link
US (2) US20030049496A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115261774A (en) * 2022-08-26 2022-11-01 集美大学 Gradient superhard composite film layer of high-speed blanking die cutting edge of aluminum alloy pop can cover and preparation method thereof

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4005976B2 (en) * 2004-03-03 2007-11-14 Tdk株式会社 Magnetic recording medium
JP4382843B2 (en) * 2007-09-26 2009-12-16 株式会社東芝 Magnetic recording medium and method for manufacturing the same

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2830544B2 (en) 1991-10-25 1998-12-02 松下電器産業株式会社 Magnetic recording media
US5773124A (en) 1993-02-22 1998-06-30 Hitachi, Ltd. Magnetic recording medium comprising a protective layer having specified electrical resistivity and density
US6330131B1 (en) 1993-09-17 2001-12-11 Read-Rite Corporation Reduced stiction air bearing slider
JP3058066B2 (en) * 1995-11-06 2000-07-04 富士電機株式会社 Magnetic recording medium and method of manufacturing the same
US5808832A (en) 1996-02-27 1998-09-15 International Business Machines Corporation Ultrathin silicon wear coating for a slider and thin film magnetic head elements at an ABS
US5855746A (en) 1996-02-28 1999-01-05 Western Digital Corporation Buffered nitrogenated carbon overcoat for data recording disks and method for manufacturing the same
DE19651615C1 (en) 1996-12-12 1997-07-10 Fraunhofer Ges Forschung Sputter coating to produce carbon layer for e.g. magnetic heads
US5942317A (en) 1997-01-31 1999-08-24 International Business Machines Corporation Hydrogenated carbon thin films
US6069769A (en) 1997-09-30 2000-05-30 International Business Machines Corporation Air bearing slider having rounded corners
US6086949A (en) 1998-02-25 2000-07-11 International Business Machines Corporation Thin film protective coating with two thickness regions
US6303214B1 (en) 1999-04-14 2001-10-16 Seagate Technology Llc Magnetic recording medium with high density thin dual carbon overcoats
US6086730A (en) 1999-04-22 2000-07-11 Komag, Incorporated Method of sputtering a carbon protective film on a magnetic disk with high sp3 content

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115261774A (en) * 2022-08-26 2022-11-01 集美大学 Gradient superhard composite film layer of high-speed blanking die cutting edge of aluminum alloy pop can cover and preparation method thereof

Also Published As

Publication number Publication date
US20040170871A1 (en) 2004-09-02
US6969447B2 (en) 2005-11-29

Similar Documents

Publication Publication Date Title
US6565719B1 (en) Magnetic disk comprising a first carbon overcoat having a high SP3 content and a second carbon overcoat having a low SP3 content
EP0293662B1 (en) A process for making a thin film metal alloy magnetic recording disk with a hydrogenated carbon overcoat
US6358636B1 (en) Thin overlayer for magnetic recording disk
US5567512A (en) Thin carbon overcoat and method of its making
US6368425B1 (en) Ion treatments for magnetic recording heads and magnetic recording media
US7169488B2 (en) Granular perpendicular media with surface treatment for improved magnetic properties and corrosion resistance
KR100894790B1 (en) Granular magnetic recording media with improved corrosion resistance by cap layer and pre-overcoat etching
US6902773B1 (en) Energy gradient ion beam deposition of carbon overcoats on rigid disk media for magnetic recordings
US5942317A (en) Hydrogenated carbon thin films
US4900397A (en) Production of magnetic recording media
US7175926B2 (en) Dual-layer carbon-based protective overcoats for recording media by filtered cathodic ARC deposition
US5871621A (en) Method of fabricating a textured magnetic storage disk
US6613422B1 (en) Nitrogen -implanted, high carbon density overcoats for recording media
US7147943B2 (en) Magnetic recording medium, the manufacturing method and magnetic recording apparatus using the same
US6969447B2 (en) Thin film protective layer with buffering interface
US9159353B2 (en) Plasma polish for magnetic recording media
US5078846A (en) Process for forming hafnia and zirconia based protective films on longitudinal magnetic recording media
US8946651B2 (en) Multiple anode ion source
US6416881B1 (en) Media with a metal oxide sealing layer
US6576328B2 (en) Magnetic thin film media with a protective layer of CNx having a plurality of compositions
US20060153975A1 (en) Magnetic recording medium, the manufacturing method and magnetic recording apparatus using the same
US11508405B1 (en) Magnetic recording media with plasma-polished pre-seed layer or substrate
JP2000082210A (en) Target for ground surface film and magnetic recording medium
US6586070B1 (en) Thin film TiSixNy protective layer
JPH06187634A (en) Magnetic recording medium

Legal Events

Date Code Title Description
AS Assignment

Owner name: INTERNATIONAL BUSINESS MACHINES CORPORATION, NEW Y

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:POCKER, DARYL J.;THIELE, JAN-ULRICH;TING, BOND-YEN;AND OTHERS;REEL/FRAME:012175/0061;SIGNING DATES FROM 20010820 TO 20010904

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION

AS Assignment

Owner name: GLOBALFOUNDRIES U.S. 2 LLC, NEW YORK

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:INTERNATIONAL BUSINESS MACHINES CORPORATION;REEL/FRAME:036550/0001

Effective date: 20150629

AS Assignment

Owner name: GLOBALFOUNDRIES INC., CAYMAN ISLANDS

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:GLOBALFOUNDRIES U.S. 2 LLC;GLOBALFOUNDRIES U.S. INC.;REEL/FRAME:036779/0001

Effective date: 20150910