Method for thin film protective overcoat

Abstract

A system and method for improving the durability and reliability of recording media used in hard drives is disclosed. A protective overcoat made by depositing a diamond like carbon (DLC) layer over a magnetic layer and then depleting the DLC protective layer of hydrogen before it is coated with a Perfluoropolyethers (PFPE) using an in-situ vapor lubrication technique.

Description

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to magnetic discs for use in computer disc drives, and, more particularly, to application of the lubricant layer over the magnetic disc

2. Description of the Related Art

Computer disc drives commonly use components made out of thin films to store information. Both the read-write element and the magnetic storage media of disc drives are typically made from thin films.

FIG. 1A is an illustration showing the layers of a conventional magnetic media structure including a substrate 105 , a seed layer 109 , a magnetic layer 113 , a diamond like carbon (DLC) protective layer 117 , and a lube layer 121 . The initial layer of the media structure is the substrate 105 , which is typically made of nickel-phosphorous plated aluminum or glass that has been textured. The seed layer 109 , typically made of chromium, is a thin film that is deposited onto the substrate 105 creating an interface of intermixed substrate 105 layer molecules and seed layer 109 molecules between the two. The magnetic layer 113 , typically made of a magnetic alloy containing cobalt (Co), platinum (Pt) and chromium (Cr), is a thin film deposited on top of the seed layer 109 creating a second interface of intermixed seed layer 109 molecules and magnetic layer 113 molecules between the two. The DLC protective layer 117 , typically made of carbon and hydrogen, is a thin film that is deposited on top of the magnetic layer 113 creating a third interface of intermixed magnetic layer 113 molecules and DLC protective layer 117 molecules between the two. Finally the lube layer 121 , typically made of a polymer containing carbon (C) and fluorine (F) and oxygen (O), is deposited on top of the DLC protective layer 117 creating a fourth interface of intermixed DLC protective layer 117 molecules and lube layer 121 molecules.

The durability and reliability of recording media is achieved primarily by the application of the DLC protective layer 117 and the lube layer 121 . The combination of the DLC protective layer 117 and lube layer 121 is referred to as a protective overcoat. The DLC protective layer 117 is typically an amorphous film called diamond like carbon (DLC), which contains carbon and hydrogen and exhibits properties between those of graphite and diamond. Thin layers of DLC are deposited on disks using conventional thin film deposition techniques such as ion beam deposition (IBD), plasma enhanced chemical vapor deposition (PECVD), magnetron sputtering, radio frequency sputtering or chemical vapor deposition (CVD). During the deposition process, adjusting sputtering gas mixtures of argon and hydrogen varies the concentrations of hydrogen found in the DLC. Since typical thicknesses of DLC protective layer 117 , are less than 100 Angstroms, lube layer 121 is deposited on top of the DLC protective layer 117 , for added protection, lubrication and enhanced disk drive reliability. Lube layer 121 further reduces wear of the disc due to contact with the magnetic head assembly.

A typical lubricant used in lube layer 121 is Perfluoropolyethers (PFPEs), which are long chain polymers composed of repeat units of small perfluorinated aliphatic oxides such as perfluoroethylene oxide or perfluoropropylene oxide. The entire disclosure of U.S. Pat. No. 5,776,577 titled “Magnetic Recording Disk Having A Lubricant Reservoir On The Inner Circumferential Surface,” which discloses PFPE lubricant, is incorporated herein by reference. PFPEs are used as lubricants because they provide excellent lubricity, wide liquid-phase temperature range, low vapor pressure, small temperature dependency of viscosity, high thermal stability, and low chemical reactivity. PFPEs also exhibit low surface tension, resistance to oxidation at high temperature, low toxicity, and moderately high solubility for oxygen. Several different PFPE polymers are available commercially, such as Fomblin Z (random copolymer of CF 2 CF 2 O and CF 2 O units) and Y (random copolymer of CF(CF 3 )CF 2 O and CF 2 O) including Z-DOL and AM 2001 from Montedison, Demnum (a homopolymer of CF 2 CF 2 CF 2 O) from Daikin, and Krytox (homopolymer of CF(CF 3 )CF 2 O).

Lube layer 121 is typically applied evenly over the disc, as a thin film, by dipping the discs in a bath containing mixture of a few percent of PFPE in a solvent and gradually draining the mixture from the bath at a controlled rate. The solvent remaining on the disc evaporates and leaves behind a layer of lubricant less than 100 Angstroms. Recent advances have enabled the application of PFPE using an in-situ vapor deposition process that includes heating the PFPE with a heater in a vacuum lube process chamber. In this system, evaporation occurs in vacuum onto freshly deposited DLC protective layer 117 that has not been exposed to atmosphere, creating a thin uniform coating of PFPE lube layer 121 .

Since it is known in the art that recording media with higher lubricant bonded ratio has better corrosion protection and that an in-situ vapor lubrication process enhances the bonding between lubricants and amorphous carbon, in-situ vapor lubrication has been used to lubricate amorphous carbon layers. In-situ vapor lubrication of recording media is the lubrication of the recording media immediately after a DLC protective layer 117 has been deposited over the magnetic layer 113 without exposing it to atmosphere. FIG. 1B is a flow chart showing the typical steps used in an in-situ vapor lubrication process that deposits PFPE lubricant over a carbon layer. The process begins with step 150 by transferring a partially complete media with substrate 105 , seed layer 109 , and magnetic layer 1113 into a vacuum chamber. In step 155 an amorphous carbon layer is deposited over the partially complete media. Next in step 160 , the amorphous carbon is coated with a lube layer 121 of PFPE using an in-situ vapor lubrication process. Finally, in step 165 the lubed magnetic media is transferred to the next manufacturing operation.

The same technology, however, works less effectively with a DLC protective layer 117 . When a DLC protective layer 117 is applied over the magnetic layer 115 , unpaired carbon electrons pair with hydrogen electrons and dangling carbon bonds are tied up, as illustrated in FIG. 1 C. The termination of the carbon bonds on the surface by hydrogen effectively reduces the reactive sites. As a result, the bonding sites for lubricant molecules are reduced and therefore the lubricant bonded ratio decreases. This effect is particularly strong when lubricant is deposited in-situ after depositing the DLC protective layer 117 , as manifested by the poor adhesion of lube layer 121 to the DLC protective layer 117 . Because of this effect, IBD or PECVD processes, which produce DLC protective layer 117 , and in-situ vapor lubrication processes, which enhances bonding, have not been combined to achieve the maximum performance.

Therefore what is needed is a system and method which overcomes these problems and makes it possible to use IBD or PECVD processes to deposit DLC protective layer 117 and in-situ vapor lubrication processes to deposit lube layer 121 to make a reliable final overcoat.

SUMMARY OF THE INVENTION

In order to improve the adhesion between the diamond like carbon (DLC) protective layer 117 , and the lube layer 121 , deposited with an in-situ lubrication process, the DLC protective layer 117 is depleted of hydrogen prior to the application of lube layer 121 using in-situ vapor lubrication processes. Depletion of hydrogen activates the surface of the DLC protective layer 117 by creating unpaired electrons in the DLC that are ready to react. The unpaired electrons create a strong bond between the DLC protective layer 117 and the lube layer 121 .

The DLC protective layer 117 is depleted of hydrogen by bombarding it with argon ions. The hydrogen atoms are ejected from the surface of the DLC protective layer 117 when the accelerated argon ions collide with them.

The present invention also can be implemented as a computer-readable program storage device which tangibly embodies a program of instructions executable by a computer system to perform a system method. In addition, the invention also can be implemented as a system itself.

These and various other features as well as advantages which characterize the present invention will be apparent upon reading of the following detailed description and review of the associated drawings.

BRIEF DESCRIPTION OF THE INVENTION

FIG. 1A is a block diagram showing a prior art conventional magnetic media structure;

FIG. 1B is a flowchart illustrating the prior art method of using in-situ vapor lubrication on a carbon layer;

FIG. 1C is an illustration of a prior art DLC protective layer ready to be lubed;

FIG. 2 is an illustration of a Hydrogen Depleted DLC (HDDLC) layer, ready for in-situ vapor lubrication, in accordance with an embodiment of the invention;

FIG. 3 is a block diagram showing the HDDLC layer 200 in a magnetic media environment;

FIG. 4 is a flowchart showing the preferred method of depositing the protective overcoat including the HDDLC layer 200 and the lube layer 121 ;

FIG. 5 is a block diagram showing a thin film deposition system used to deposit the magnetic media structure 300 ; and

FIG. 6 is an illustration showing details of surface modifier 520 of system 500 of FIG. 5 .

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

The invention provides a system and method for protecting magnetic media.

FIG. 2 is an illustration of a Hydrogen Depleted DLC (HDDLC) layer 200 , ready for in-situ vapor lubrication, in accordance with one embodiment of the invention. The HDDLC layer 200 includes carbon atoms 210 , hydrogen atoms 220 , carbon-hydrogen bonds 230 , carbon-carbon bonds 240 and free dangling carbon bonds 250 .

The free dangling carbon bonds 250 are created by bombarding the DLC protective layer 117 with charged ions as is furthered described with reference to FIG. 4 below. This bombardment process converts the DLC protective layer 117 into a more reactive HDDLC layer 200 by creating free dangling bonds 250 . This increases the bonding between the DLC protective layer 117 and the lubricant that is deposited over it with an in-situ vapor lube process as is described with reference to FIG. 4 below.

FIG. 3 is a block diagram showing the HDDLC layer 200 in a magnetic media environment 300 including a substrate 105 , a seed layer 109 , a magnetic layer 113 and a lube layer 121 . HDDLC layer 200 protects magnetic media from wear and tear as does DLC protective layer 117 except that it has been modified so that the lube layer 121 adheres to it much better than it otherwise would, providing improved protection.

FIG. 4 is a flow chart showing the preferred steps used to make a protective overcoat including an HDDLC layer 200 and and in-situ lubed layer 121 . Protective overcoats typically include a hard layer such as DLC and a lubrication layer. The process begins with step 405 by transferring a partially complete media having substrate 105 , seed layer 109 , and magnetic layer 113 into a vacuum chamber.

Next in step 410 , a DLC protective layer 117 containing carbon and hydrogen is deposited onto the substrate. The deposition process can be done by various thin film deposition techniques including ion beam deposition (IBD), plasma enhanced chemical vapor deposition (PECVD), magnetron sputtering, radio frequency sputtering or chemical vapor deposition (CVD).

Next in step 415 , the DLC protective layer 117 is activated by exposing the DLC protective layer 117 to argon ions (Ar + ), from an argon ion plasma, which depletes the DLC protective layer 117 of hydrogen atoms. Exposing includes bombarding the DLC protective layer 117 with ions that are accelerated by an electric field as well as allowing atoms, molecules or ions to randomly strike the DLC protective layer 117 in the absence of an electric field. As Ar + ions bombard the DLC protective layer 117 , hydrogen atoms are ejected, reducing the number of hydrogen atoms left on the DLC protective layer 117 , creating an HDDLC layer 200 . The depletion of hydrogen activates the DLC by making it a reactive carbon. The HDDLC is reactive because carbon atoms that were once bonded to hydrogen atoms now have unpaired electrons available for bonding. This preferred process of removing hydrogen atoms from the DLC by Ar + ion bombardment is a mechanical process. Step 415 can be done in the same chamber as that in which the DLC protective layer 117 is deposited or it can be done in a different chamber. If step 415 is performed in a second vacuum chamber then the partially complete media is transferred to a second chamber after the DLC protective layer 117 is deposited. The transferring process is done under vacuum or in an inert environment such as argon.

In the preferred embodiment, the rate at which hydrogen atoms are removed from the DLC protective layer 117 can be adjusted by changing parameters such as voltages, pressures, flow rates, and temperatures. Voltage controls the electric field acting on the Ar + ions and consequently the force with which Ar + ions bombard the DLC protective layer 117 . Bombarding occurs when the ions are accelerated towards the DLC protective layer 117 , because of the electric field acting on the Ar + ions, and collide with the DLC protective layer 117 . Pressure and flow rates control physical properties of the plasma such as the number of Ar + ions available to bombard the DLC protective layer 117 . Temperature controls the kinetic energy at the surface of the DLC protective layer 117 and consequently the amount of energy that must be imparted to the surface to remove hydrogen atoms.

In the preferred embodiment the plasma is made out of ionized argon. Argon is used in the preferred embodiment because it is inert and readily available. However, other inert gases such as helium (He), neon (Ne), krypton (Kr) or xenon (Xe) can also be used to make up the plasma of charged ions, which bombard the DLC protective layer 117 and remove hydrogen atoms from it. Noble gases are preferred because they are inert and do not chemically react with the DLC protective layer 117 . This enables the removal hydrogen atoms from the DLC protective layer 117 by the mechanical process of bombardment. The invention, however, is not limited to only using noble gases because this process can be carried out using non-noble gases which do not chemically react with the DLC protective layer 117 . Additionally, this invention is not limited to the removal of hydrogen atoms from the DLC protective layer 117 by mechanical means only. Other methods such as heating the DLC protective layer 117 or chemically reacting another substance with the DLC protective layer 117 can be used to remove hydrogen atoms from the DLC protective layer 117 .

Next in step 420 , an in-situ vapor deposition technique is used to apply a lubricant onto a partially completed media completing the protective overcoat. In the preferred embodiment PFPE is applied to the partially completed media using an in-situ vapor deposition process that includes heating the lubricant with a heater in a vacuum lube process chamber. In this embodiment, evaporation of PFPE occurs in a vacuum onto HDDLC 200 after the DLC protective layer 117 has been deposited and its surface depleted of hydrogen by exposing it to ionized argon without exposing the HDDLC 200 to atmosphere.

Finally in step 425 the lubed magnetic media is transferred to the next manufacturing operation.

Although the preferred steps used to make a protective overcoat are described in reference to a DLC protective layer 117 and lube layer 121 , those skilled in the art will recognize that the same steps can be used to deposit any two layers, wherein the bonding between the two layers is improved. For example, a first layer, which can be metallic, insulating, semi-conducting or semi-metallic, can be deposited as described with reference to step 410 . The first layer is then activated as described with reference to step 415 . After the first layer is activated, a second layer, which can also be metallic, insulating, semi-conducting or semi-metallic, can be deposited as described with reference to step 420 . The combination of the first layer and second layer can then be transferred to the next manufacturing operation as described in step 425 .

FIG. 5 represents a multilayer thin film deposition system 500 equipped with an in-situ DLC deposition system, a carbon surface modifying system and a vapor lube system. System 500 preferably includes a loader 510 , a DLC depositor 515 , a surface modifier 520 , a vapor luber 525 , an unloader 530 , a controller 535 , a power system 540 , a pumping system 545 and a gas flow system 550 .

Loader 510 and unloader 530 represent conventional load locks that allow substrates to be transferred into and out of a vacuum chamber without venting the entire vacuum system. DLC depositor 515 represents a conventional thin film deposition chamber used to deposit the DLC protective layer 117 . DLC depositor 515 can use ion beam deposition (IBD), plasma enhanced chemical vapor deposition (PECVD), magnetron sputtering, radio frequency sputtering or chemical vapor deposition (CVD) techniques to deposit the DLC protective layer 117 . Surface modifier 520 is used to deplete the top surface of the DLC protective layer 117 of hydrogen, creating HDDLC layer 200 as is further discussed with reference to FIG. 4 above. Vapor luber 525 represents a conventional vapor lubing system used to deposit the lube layer 121 onto the HDDLC layer 200 . Controller 535 is the software and hardware which controls the operation of system 500 . Power system 540 represents power supplies used to power the system 500 and include power supplies for heaters, conveyers, DC magnetrons, rf sources. Pumping system 545 represents all pumps and valves used to evacuate the vacuum chambers including mechanical pumps, turbo pumps, cryogenic pumps and gate valves. Gas flow system 550 represents the gas delivery equipment such as mass flow controllers, valves, piping and pressure gauges.

FIG. 6 is an illustration showing surface modifier 520 depleting hydrogen atoms from the top surface of the DLC protective layer 117 . In one embodiment, surface modifier 520 includes a vacuum chamber 605 , an argon ion plasma 610 , argon ions (Ar + ) 615 , a first voltage V 1 620 , a second voltage V 2 625 and a stage 630 depleting hydrogen atoms from the top surface of the DLC protective layer 117 of a partially completed media.

After depositing the DLC protective layer 117 , as discussed with reference to FIG. 1B , the top surface of the DLC protective layer 117 is exposed to an argon ion plasma 610 consisting of (Ar + ) ions 615 . In step 415 , the partially complete media is moved to a grounded vacuum chamber 605 which is maintained at process pressures ranging from 10-3 torr to 10-2 torr. Power supplies such as the Advanced Energy MDX series manufactured by Advanced Energy of Fort Collins, CO, USA are used to maintain the DLC protective layer 117 at a first voltage V 1 615 and the argon ion plasma at a second voltage V 2 625 . The voltage difference between the plasma and the DLC protective layer 117 creates an electric field 630 that accelerates the Ar + ions towards the DLC protective layer 117 . The actual trajectory 635 of the argon ions depends on many factors including the initial velocity of the ions and the configuration of the electric field, which is determined by the first voltage 620 and the second voltage 625 .

It will also be recognized by those skilled in the art that, while the invention has been described above in terms of preferred embodiments, it is not limited thereto. Various features and aspects of the above-described invention may be used individually or jointly. Further, although the invention has been described in the context of its implementation in a particular environment and for particular applications, those skilled in the art will recognize that its usefulness is not limited thereto and that the present invention can be utilized in any number of environments and implementations.

Claims

1. A method of preparing a layer comprising, the steps of:depositing a first layer having a first layer surface; activating the first layer surface by bombarding the first layer surface with charged atoms; and depositing a second layer directly onto the first layer surface after said first layer surface has been activated.

2. The method of claim 1 wherein depositing is done by ion beam deposition techniques.

3. The method of claim 1 wherein the step of activating the first layer surface is depleting the first layer surface of atoms.

4. The method of claim 1 wherein the step of activating the first layer surface is bombarding the first layer surface with charged ions.

5. A method for preparing a protective overcoat with in-situ vapor lubrication, comprising the steps:depositing a first layer having carbon and hydrogen onto a medium; depleting said first layer of hydrogen; and depositing a second layer onto said first layer using an in-situ vapor deposition process, said second layer having a lubricant.

6. The method of claim 5 wherein the step of depleting hydrogen includes exposing said first layer to ionized argon gas.

7. The method of claim 5 wherein the step of depositing a first layer is done using ion beam deposition.

8. The method of claim 5 wherein the step of depositing a first layer is done using plasma enhanced chemical vapor deposition.

9. The method of claim 5 wherein the step of depleting hydrogen includes a chemical process for depleting hydrogen.