FABRICATION OF TRAPEZOIDAL POLE FOR MAGNETIC RECORDING

Abstract

A method for forming a magnetic write pole with a trapezoidal cross-section is described. The method consists of first forming a magnetic seedlayer on a base followed by depositing a removable material layer on the seedlayer, and then a resist layer on the removable material layer. A trench is then formed in the resist, and the resist is heated to cause the cross-sectional profile of the trench to assume a trapezoidal shape. The resist is then capped with another resist layer and further heated to cause the width of the trapezoidal trench to become narrower. The cap layer and removable material layer at the bottom of the trench are then removed and the trench filled with magnetic material by electroplating. The resist and seedlayer external to the trench are finally removed to form a write pole with a trapezoidal cross-section.

Description

FIELD OF THE INVENTION

The invention relates to magnetic recording heads and more particularly to the fabrication of a trapezoidal write pole.

BACKGROUND

Magnetic recording heads have utility in a magnetic disc drive storage system. Most magnetic recording heads used in such systems today are “longitudinal” magnetic recording heads. Longitudinal magnetic recording in its conventional form has been projected to suffer from superparamagnetic instabilities at densities above approximately 40 Gbit/in². It is believed that reducing or changing the bit cell aspect ratio will extend this limit up to approximately 100 Gbit/in². However, for recording densities above 100 Gbit/in², different approaches will likely be necessary to overcome the limitations of longitudinal magnetic recording.

An alternative to longitudinal recording that overcomes at least some of the problems associated with the superparamagnetic effect is “perpendicular” magnetic recording. Perpendicular magnetic recording is believed to have the capability of extending recording densities well beyond the limits of longitudinal magnetic recording. Perpendicular magnetic recording heads for use with a perpendicular magnetic storage medium may include a pair of magnetically coupled poles, including a main write pole having a relatively small bottom surface area and a flux return pole having a larger bottom surface area. A coil having a plurality of turns is located adjacent to the main write pole for inducing a magnetic field between the pole and a soft underlayer of the storage media. The soft underlayer is located below the hard magnetic recording layer of the storage media and enhances the amplitude of the field produced by the main pole. This in turn allows the use of storage media with higher coercive force. Consequently, more stable bits can be stored in the media. In the recording process an electrical current in the coil energizes the main pole, which produces a magnetic field. The image of this field is produced in the soft underlayer to enhance the field strength produced in the magnetic media. The flux density that diverges from the tip into the soft underlayer returns through the return flux pole. The return pole is located sufficiently far apart from the main write pole such that the material of the return pole does not affect the magnetic flux of the main write pole, which is directed vertically into the hard layer and the soft underlayer of the storage media.

A magnetic recording system such as, for example, a perpendicular magnetic recording system may utilize a write pole with a square or rectangular cross-section. Under certain circumstances, the increased magnetic field concentration at the sharp corners can cause writing or erasure on adjacent tracks.

Another development that overcomes at least some of the problems associated with the superparamagnetic effect is heat assisted magnetic recording (HAMR), sometimes referred to as optical or thermal assisted recording. Heat assisted magnetic recording generally refers to the concept of locally heating a recording medium to reduce the coercivity of the recording medium so that the applied magnetic writing field can more easily direct the magnetization of the recording medium during the temporary magnetic softening of the recording medium caused by the heat source. The heat assisted magnetic recording allows for the use of small grain media, which is desirable for recording at increased aerial densities, with a larger magnetic anisotropy at room temperature and assuring a sufficient thermal stability.

More specifically, super paramagnetic instabilities become an issue as the grain volume is reduced in order to control media noise for high aerial density recording. The superparamagnetic effect is most evident when the grain volume V is sufficiently small that the inequality K_uV/k_bT>40 can no longer be maintained. K_u, is the magnetic crystalline anisotropy energy density of the material, k_b is Boltzman's constant, and T is absolute temperature. When this inequality is not satisfied, thermal energy demagnetizes the individual grains and the stored data bits will not be stable. Therefore, as the grain size is decreased, in order to increase the aerial density, a threshold is reached for a given material K_u, and temperature T such that stable data storage is no longer feasible.

The thermal stability can be improved by employing a recording medium formed of a material with a very high K_u. However, with the available materials, the recording heads are not able to provide a sufficient or high enough magnetic writing field to write on such a medium. Accordingly, it has been proposed to overcome the recording head field limitations by employing thermal energy to heat a local area on the recording medium before or at about the time of applying the magnetic write field to the medium. By heating the medium, the K_u, or the coercivity is reduced such that the magnetic write field is sufficient to write to the medium. Once the medium cools to ambient temperature, the medium has a sufficiently high value of coercivity and assures thermal stability of the recorded information. When applying a heat or light source to the medium, it is desirable to confine the heat or light to the track where writing is taking place, and to generate the write field in close proximity to where the medium is heated to accomplish high aerial density recording. The separation between the heated spot and the write field spot should be minimal or as small as possible so that the writing may occur while the medium temperature is substantially above ambient temperature. This also provides for the efficient cooling of the medium once the writing is completed.

Accordingly, there is identified a need for an improved write pole with a shape and dimensions that overcome the limitations and shortcomings of known magnetic recording heads and heat assisted magnetic recording heads.

SUMMARY

In one aspect of the invention, a method of forming a magnetic write pole with a trapezoidal cross-section is presented. The method comprises forming a magnetic seedlayer on a base, forming a removable material layer on the seedlayer, forming a resist layer on the removable layer and forming a trench in the resist and heating the structure for a first amount of time at a first temperature to form a predetermined slope in the first and second sidewalls of the trench. The method further comprises capping the trench with another resist layer and heating the capped trench for a second amount of time at a second temperature to shrink the separation of the first and second sidewalls of the trench, removing the cap layer and the removable material at the bottom of the trench, electroplating a magnetic material in the trench and removing the resist by stripping the resist and finally removing the seed material outside the pole area by ion-beam etching to form the magnetic pole.

In accordance with another aspect of the invention, a magnetic write pole with a multilayer structure and a trapezoidal cross-section comprises a base and a multilayer magnetic seedlayer on the base. A magnetic layer on the seedlayer has a trapezoidal cross-section, a bottom width W_b less than or equal to about 100 nm, a top width of about 1.25 to 3 times W_b, a height h, and an aspect ratio h/W_b of about 1:1 to about 10:1.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1A is a cross-sectional view from the air bearing surface (ABS) plane showing a prior art HAMR write pole.

FIG. 1B is a cross-sectional view from the ABS plane showing a trapezoidal write pole of the current invention.

FIG. 2 is a diagram illustrating the steps to form a trapezoidal pole.

FIG. 3 is a cross-sectional view of a trench in a resist layer on a substrate before (A) and after (B) a thermal bake process.

FIG. 4 is a cross-sectional view of a capped trench in a resist layer on a substrate before (A) and after (B) a thermal shrink process. The resist cap is removed in (C).

FIG. 5A are SEM images showing different trench profiles achieved at different temperatures during thermal bake process. FIG. 5B is a graph showing bottom and top spacing and beveled angle as a function of bake temperature.

FIG. 6A are SEM images showing different trench profiles after baking for different times. FIG. 6B is a graph showing bottom and top spacing and beveled angle as a function of bake time.

FIG. 7 are SEM images showing trench profiles after combinations of thermal bake (Process A) and thermal shrink (Process B).

FIG. 8 are SEM images showing trench profiles after combinations of thermal bake (Process B) and thermal shrink (Process A).

FIG. 9 is a cross-sectional view of resist layer 300 on easily removable resist layer 290 on magnetic seed layer 210 on substrate 220 (not to scale).

FIG. 10A are magnetic hysteresis loops for a 1000 Å single CoNiFe layer.

FIG. 10B are magnetic hysteresis loops for a 1000 Å laminated seedlayer with a Ni₈₀Fe₂₀ cap layer.

FIG. 11 is a chart of corrosion resistance of CoNiFe seedlayers with and without Ni₈₀Fe₂₀ cap layer.

FIG. 12 are SEM images of 100 nm wide plated trapezoidal poles using (a) a CoNiFe seedlayer and (b) a CoNiFe seedlayer with Ni₈₀Fe₂₀ anti corrosion cap layer.

FIG. 13 is a diagram illustrating the steps to electroplate magnetic trapezoidal pole.

FIG. 14 is a schematic of an Ms gradient trapezoidal pole configuration.

FIG. 15 is a cyclic voltammetry plot of current density versus applied potential for the single bath electrolyte shown in Table 2.

FIG. 16 is a graph showing how composition and magnetic moment of a plated pole can be tailored by adjusting plating current density for the single bath electrolyte shown in Table 2.

FIG. 17 are SEM images of the microstructures of 0.5T NiCu (left) and 0.3T NiCu (right) plated from the single bath shown in Table 2.

FIG. 18 are magnetic hystresis loops of a plated graded Ms stack containing a CoNiFe laminate seed.

FIG. 19A is a schematic of a trapezoidal pole before seed removal.

FIG. 19B is a schematic of a trapezoidal pole after seed removal.

FIG. 20 is a FIB-SEM image of a cross-sectioned trapezoidal pole after seed removal.

FIG. 21 is a schematic of a static ion beam etch method.

FIG. 22 is a SEM image of a cross-sectioned trapezoidal pole after seed removal by static ion beam etch.

FIG. 23 is a SEM image of a cross-sectioned trapezoidal pole after backfilling with Comptech sputtered alumina.

FIG. 24 is a SEM image of a cross-sectioned trapezoidal pole after backfilling with IBD aluminum.

FIG. 25 are SEM images of sectioned (top row) and unsectioned (bottom row) trapezoidal poles with three different designs.

DETAILED DESCRIPTION

The present invention relates to the problem of side writing or erasure on adjacent tracks due to magnetic field concentrations at sharp corners in prior art write poles with rectangular cross-sections as seen from the air bearing surface (ABS) of a recording media. FIG. 1A shows a cross-section of prior art write pole 10 as seen from the ABS. Write pole 10 has three sections, 20, 30, and 40. The shading on FIG. 1 illustrates magnetic field concentrations capable of side writing or erasure. The embodiment of the invention is to replace sections 20 and 30 with a single pole 50 having a trapezoidal cross-section with a bottom spacing 70 at its tip and a top spacing 80 to form write pole 60 as shown in FIG. 1B. Furthermore, by making the spacing of section 90 in FIG. 1B equal to top spacing 80, the corners responsible for magnetic field leakage are eliminated. In another embodiment of the invention, the aspect ratio H/W of the trapezoidal pole 50 is about 1:1 to about 10:1 to keep the wider portions away from the bottom edge (front edge) of the pole that does the writing. In another embodiment of the invention, the magnetization of the trapezoidal pole 50 is graded to ensure that the field from the top of the pole is lower than the field from the bottom of the pole since writing is done at the bottom of the pole.

Prior art trapezoidal poles have been fabricated using high angle ion-beam etching with masking to create the trapezoidal shape. This process is not compatible with the process used to form heat assisted magnetic recording (HAMR) heads. A process that is compatible with the HAMR process is electroplating in a resist trench with a trapezoidal shape.

The disclosed invention solves the following issues. 1) The trench has a trapezoidal shape. 2) The trench width at the bottom is less than 100 nm. 3) The aspect ratio W/H is about 1:1 to about 10:1. 4) Removing the seedlayer without leaving a footing or redepositing seedlayer material on the sides of the pole. 5) Backfilling with alumina without leaving voids in the alumina. 6) The process needs to be compatible with standard processes in industry fabs.

The invention discloses how to form a narrow trench with a controlled trapezoidal shape and controllable top and bottom separations. In summary the method is a hybrid thermal flow process consisting of a resist post-development thermal bake treatment process that allows a sub-100 nm high aspect ratio trench with a trapezoidal shape to be formed that can then be used as a template for electroplating writer pole materials.

Lithographic Process

The steps to form a magnetic pole with a trapezoidal cross-section are given in FIG. 2. First, a substrate is provided (step 100). The substrate can be a ceramic composite used to form sliders such as an aluminum oxide/titanium oxide composite or other materials known in the art. A plating seedlayer is deposited on the substrate (step 102). Suitable seedlayers are selected from a group but are not limited to FeCo, NiFe, CoNiFe, Ru, Ta, CoZrTa, CoNbTa, and Cu.

A thin, easily removable, resist layer is deposited on the seedlayer (step 104). The removable layer is preferably about 10 nm to about 30 nm thick and is preferably a polymethylglutarimide (PMGI) layer. The removable layer is then given a post-apply bake (step 106). A thicker top resist layer is then deposited on the PMGI layer with a thickness of from about 0.5 μm to about 4.0 μm depending on the requirements for the top pole design (step 108). The resist is then given a post-apply bake (step 110). The resist is then exposed using e-beam or other lithographic tools e.g. G-line, I-line, DUV, 193 nm scanner, electron beam direct write, EUV, x-ray lithography or others (step 112). The exposed wafer is then given a post exposure bake (step 114). The exposed wafer is then developed in standard tetramethyl ammonium hydroxide (TMAH) developer to form a rectangular trench (step 116). The developed wafer is then put through a hybrid thermal flow process, described later, to produce the proper trapezoidal shape and spacing of the trench (step 118). Magnetic material is then electroplated in the trench to form a magnetic trapezoidal pole (step 120).

Hybrid Thermal Flow Process

The hybrid thermal flow process is composed of two processes, a thermal bake process and a thermal shrink process. In the thermal bake process, the resist is baked at a temperature close to the glass transition temperature, Tg, of the resist. This causes the walls of the trench to slope into a trapezoidal cross-section as shown in FIG. 3. FIG. 3A shows resist layer 220 with trench 221 on substrate 230 before thermal bake process. FIG. 3B shows resist layer 220 after thermal bake. Trench 221 with rectangular cross-section has transformed into trench 222 with trapezoidal cross-section after the bake.

The thermal shrink process is illustrated in FIG. 4 where resist layer 240 on substrate 230 with a rectangular trench is capped with resist layer 242. Resist layer 242 is applied by spin coating and fills the trench during the process. The spacing of the trench is “a”. The resist is then baked at a temperature less than, equal to, or greater than that used for the thermal bake process. This thermal shrink process causes the separation of the two walls of the trench to decrease giving an added dimension to the control of the trapezoidal trench forming process. The new spacing is “b” where b<a. The thermal shrink process can be repeated at will to obtain the required trench separation. The thermal bake process and thermal shrink process can be interchanged as needed to obtain required trapezoidal trench shapes and dimensions. By combining the two processes, trenches with high aspect ratios of 1:1 to 10:1 and sub-100 nm spacing have been produced. The process is very manufacturable. The addition of the hybrid thermal bake process to an overall manufacturing process can be done using resist development track tools that are standard in most industry fabs. The actual time it takes to incorporate these processes into the lithographic step is minimal compared to the results that can be achieved. In addition, the cost of the added material is attractively small in relation to the cost of updating and maintaining advanced lithographic equipment such as DUV, 193 nm scanners, electron beam direct write, or EUV tools that are needed to reduce trench dimensions to the sub-100 nm regime. It should be mentioned that this method or process is not limited to the application of magnetic pole fabrication. In principle it can be used in any device fabrication in the case where a narrow trapezoidal trench pattern is needed.

An example of how a trapezoidal shape is formed in a 1.3 μm thick resist with a rectangular trench during a thermal bake is shown in FIG. 5A. Scanning electron microscope (SEM) images of the trench are shown at different temperatures after a 60 second bake at different temperatures in FIG. 5A. The bottom and top spacing, of the trench as well as the bevel angle are shown in FIG. 5B as a function of temperature for a 60 second baking time. The top spacing and bevel angle are smoothly varying functions of temperature while the bottom spacing remained constant.

FIGS. 6A and 6B show the time dependence of the thermal bake process at 145° C. on trench dimensions in a 1.3 μm thick resist. The top spacing and bevel angle are smoothly varying functions of time while the bottom spacing remained constant. Combinations of the thermal bake process and the thermal shrink process can give considerable latitude to the shaping of a trapezoidal trench.

FIG. 7 shows SEM images of trenches in a 1.3 μm thick resist given three exposures (increasing from top to bottom). Process A was a thermal bake at 155° C. for 60 seconds and process B was a thermal shrink process at 120° C. for 90 seconds. The shrinking of the wall separation after multiple thermal shrink treatments (A+B, A+2B, A+3B, and A+4B) is evident. Other combinations of treatments were carried out with similar results.

FIG. 8 shows trapezoidal shape formation in a 1.3 μm thick resist given three exposure levels again. In this case the originals were given two thermal shrink treatments (Process B) of 60 seconds each at 120° C. and then given one thermal bake treatment (Process A) for 90 seconds at 130° C., 140° C., and 150° C. The large control over the shape of the trench is obvious.

Plating Process

The plating process to form a trapezoidal pole starts with step 102 in FIG. 2, deposit seedlayer. Although the seedlayer used in this process is described in detail, other seedlayers and combinations of seedlayers can be used. A schematic showing the layer structure of the seed and resist layers is shown in FIG. 9 where the relative dimensions are not to scale. All layers in seedlayer 310 can be formed by physical vapor deposition (PVD), e-beam vapor deposition, sputtering and other means known to those in the art. The seedlayer has two characteristics, a laminated layer structure and an anticorrosion cap. Seedlayer 310 is shown on substrate 320 and includes first or bottom layer 330 on substrate 320. First layer 330 is NiFe about 15 Å thick. Second layer 340 is CoNiFe about 350 Å thick. Third layer 350 on CoNiFe layer 340 is Ta about 12 Å in thickness. Fourth layer 360 includes three NiFe layers about 15 Å thick each. Fifth layer 370 on NiFe layer 360 is CoNiFe about 250 Å thick. Sixth or cap layer 380 is Ni₈₀Fe₂₀ about 50 Å thick and is added for anticorrosion protection as will be discussed below. Easily removable resist layer 390 is on cap layer 380. Layer 390 is preferably a PMGI layer about 10 nm to 30 nm thick and is applied to protect the seedlayer at the base of the trench during subsequent thermal processing. Thick resist layer 400 is on thin easily removable layer 390. Resist layer 400 is from 0.5 μm to 4.0 μm thick depending on the requirements of the pole design.

Magnetic properties of laminate seedlayer 310 are compared with a single CoNiFe layer in FIGS. 10A and 10B. FIG. 10A shows B versus H hysteresis loops for a solid 1000 Å CoNiFe film and FIG. 10B shows B versus H hysteresis loops for a 1000 Å laminate film. The hard axis loop of the laminate shows almost no hysteresis.

In another embodiment of this invention, the magnetization of each magnetic layer in the seedlayer can be different such that the seedlayer exhibits a vertical magnetization gradient which can contribute to the magnetization gradient in the write pole.

FIG. 11 shows the corrosion resistance of a capped seedlayer to be superior to that of an uncapped layer. This corrosion protection is important in defining the shape of the pole. The formation of the trapezoidal resist shape as shown earlier involves thermal baking and shrinking which results in undercut features at the resist/seedlayer interface. During the pre-plate and plating processes, the corrosive plating solution can be trapped in this crevice and cause corrosion. This is evident in FIG. 12 which shows SEM images of 100 nm wide plated trapezoidal poles using a CoNiFe seedlayer without (a) and with (b) Ni₈₀Fe₂₀ anticorrosion cap 280. The SEM images on the right were taken after the poles were sectioned to show the trapezoidal shape. With the Ni₈₀Fe₂₀ cap layer 280, the corrosive solution trapped in the photoresist could not visibly corrode the seedlayer. Since the plating process is on top of an intact (uncorroded) seedlayer, the pole morphology is visibly improved and the depression in the center of the pole is eliminated.

Trapezoidal Pole Plating

The plating process flow to form a trapezoidal pole is shown in FIG. 13 which shows the steps to electroplate a magnetic trapezoidal pole. At step 500, removable layer 390 at the bottom of the trench is removed to expose the seedlayer. This is carried out by O₂ reactive ion etching to clear trench bottom. Next, etching removes surface oxide on the seedlayer (step 502). An acid spray etch performs this process. At step 504, the trench is filled with magnetic material by electroplating. Solid FeCoNi, FeCo and graded magnetization poles can be formed. Following electroplating, the plated trench is rinsed and dried to remove plating solution (step 506). In the next step, the photoresist is removed by oxygen ashing and solvent stripping (step 508). As discussed later, in the final step, the exposed seedlayer is removed by ion beam etching (step 510).

The solid CoNiFe pole is electroplated using the parameters shown in Table 1.

TABLE 1
Solid CoNiFe trapezoidal pole plating chemistry and parameters.
Chemical              Concentration (g/l) and parameters
NiCl2•6H2O            40
CoCl2•6H2O            31
FeCl2•4H2O            4
H3BO3                 40
NH4Cl                 40
STJ additive          0.65
Sodium LaurlelSulfate 0.1
(SLS)
PH                    2.8
Current               2.8-3 mA/cm2

Referring to Table 1, the organic STJ additive acts as a leveling agent and plays an important role in controlling the grain size and surface morphology of the plated pole. Its adsorption to the narrow trench surface can be preferentially enhanced due to radial transportation at the current crowding points thereby increasing plating uniformity. Due to the trapezoidal profile of the trench cross-section, the accessibility of the small trench by the diffusing metal ions can be increased. This improves the uniformity of the plated pole cross-section along the length of the pole.

Graded Ms Poles

As illustrated in FIG. 1A, prior art poles 10 are solid, plated, high Ms CoFeNi material for sections 20, 30, and 40. This high Ms configuration results in a magnetic field spike at the back of the pole 10. In order to reduce this field spike, trapezoidal poles with an Ms gradient can be employed. A schematic of a trapezoidal graded Ms pole is shown in FIG. 14.

Three different pole materials with different magnetization can be plated to form this pole. For example, in the current seedlayer configuration (sputtered Si on substrate)/NiFe 15 Å/CoNiFe 250 Å/Ta 12 Å/NiFe 15 Å)₃/CoNiFe 250 Å/Ni₈₀Fe₂₀ 50 Å, it is possible to subsequently plate 100 nm of IT NiFe layer using a regular NiFe bath, and 50 nm of 0.5T NiCu on the IT NiFe layer, and 50 nm of 0.3T NiCu layer on the 0.5T NiCu layer using another bath.

The 0.3T and 0.5T NiCu layers can be plated from a single bath using the novel developed bath chemistry shown in Table 2.

TABLE 2
0.3T and 0.5T NiCu plating chemistry and parameters.
Chemical                 Concentration (g/l) and parameters
NiCl2•6H2O               119
CuSO4•5H2O               0.5
Sodium citrate dehydrate 29.4
H3BO3                    25
STJ additives            0.6
SLS                      0.1
PH                       55
Current (0.3T/0.5T)      2.5/10 mA/cm2

In the single bath method, deposition is carried out using a single electrolyte while varying deposition parameters such as voltage or current to produce compositional, structural and magnetic modulations of the plated structure. For example, current density is shown as a function of applied voltage in cyclic voltammetry measurements made using the bath given in Table 2 where ions of two metals, Cu and Ni, with Cu being more noble than Ni, are present. At certain potentials (or currents) that are sufficiently negative, Cu will be reduced and Ni will not. In this region, region I in FIG. 15, Cu will be plated and Ni will not. As the potential is decreased into region II, both Cu and Ni will plate and the amounts of each will depend on the applied potential. As shown in FIG. 15, a 0.3T NiCu alloy will plate at a current density of about −2.5 mA/cm² and a 0.5T NiCu alloy will plate at a current density of −10.0 mA/cm². Since the deposition rate of Cu is diffusion limited and hence constant, by varying the potential (or current) during plating, composition and magnetic modulations of the plated structure can be achieved.

The current control technique is employed in the wafer scale embodiment described here. FIG. 16 shows the composition and magnetic moment variation in NiCu plated layers as a function of plating current. As shown in the figure, the magnetic moment, Bs, can be conveniently tailored by adjusting the plating current. Specifically, 2.5 and 10 mA/cm² currents can be applied to obtain 0.3T and 0.5T NiCu. The composition uniformity (1a) for 0.5T and 0.3T NiCu plated layers are 0.1 ^at/₀ (0.5T) and 0.7 ^at/₀ (0.3T) respectively.

The microstructure of the 0.5T and 0.3T NiCu are shown in FIG. 17 as characterized by scanning electron microscopy (SEM). The surface looks sound and glossy and the grains are refined due to the use of the STJ organic additive in the bath. The magnetic hysteresis loop of an actual rated Ms stack is shown in FIG. 18. The stack consists of 50 nm of 0.3T NiCu on 50 nm of 0.5T NiCu on 100 nm of IT NiFe on 100 nm of CoNiFe laminate seed.

Seed Removal and Pole Backfilling

FIG. 19A is a schematic of the trapezoidal pole before ion beam etching. FIG. 19B is a schematic of the trapezoidal pole after ion beam etching. FIG. 19B indicates that the seed material redeposits on the sidewalls of the pole when standard rotating ion mill etching procedures are used. FIG. 20 shows a focused ion beam scanning electron micrograph (FIB-SEM) of a cross-sectioned trapezoidal pole after seed removal by the standard rotating beam ion mill etching process. The redeposited layer is indicated by the dashed lines.

A seed removal method that works best is a static etch with the wafer stationary with the poles at a 30° angle with respect to the ion beam (i.e. α=30°) as shown in FIG. 21. In another embodiment, the wafer can be swept through a range of angles e.g. from about 20° to about 40°. As shown in the figure, the wafer is also set at 50° (i.e. θ=50°) to the ion beam.

Successful seed removal using this process is shown in FIG. 22. FIG. 22 is an SEM image of a seed with an 86° wall angle with no redeposited seed material on the wall of the seed. The bottom, middle and top widths of the pole are 90 nm, 130 nm and 185 nm respectively.

Conventional sputtering such as with Alcatel Comptech equipment cannot be used to backfill the pole with alumina. FIG. 23 is an SEM image of a pole that was backfilled with sputtered alumina using Comptech equipment. There are voids along the sides of the pole as indicated by the arrows. However, ion beam deposition can be used to backfill the pole. FIG. 24 shows two magnifications of SEM images of a pole backfilled with 1.2 μm of ion beam deposited (IBD) alumina deposited at θ=60° with the wafer rotating. There are no voids in the alumina.

EXAMPLE

SEM images of three trapezoidal poles with different dimensions that have been fabricated by the invention disclosed herein are shown in FIG. 25. The top images are end-on views of vertical cross-sections of the poles. The bottom images are perspective views of the unsectioned poles. The bottom and top widths (i.e., critical dimension or CD) are indicated on the figure.

In summary, a novel hybrid thermal flow method to form trapezoidal shape resist trench structures has been invented that allows the production of trapezoidal write poles by electroplating. This process has been used to manufacture heat-assisted magnetic recording heads (HAMR).

Although the present invention has been described with reference to preferred embodiments, workers skilled in the art will recognize that changes may be made in form and detail without departing from the spirit and scope of the invention.

Claims

1. A method of forming a magnetic write pole, the method comprising: forming a magnetic seedlayer on a base;forming a removable material layer on the seedlayer;forming a resist layer on the removable layer;forming a trench in the resist and heating the structure for a first amount of time at a first temperature to form a predetermined slope in the first and second sidewalls of the trench;capping the trench with another removable layer;heating the capped trench for a second amount of time at a second temperature to shrink the separation of the first and second sloped sidewalls of the trench;removing the cap layer;removing the removable material at the bottom of the trench;electroplating a magnetic material in the trench; andremoving the resist and seed material outside the pole area.

2. The method of claim 1, wherein the magnetic seedlayer is a multilayer seedlayer formed of magnetic and nonmagnetic layers.

3. The method of claim 2, wherein the magnetic seedlayer comprises a first NiFe layer on the base, a second CoNiFe layer on the first NiFe layer, a third Ta layer on the second CoNiFe layer, a fourth NiFe layer on the third Ta layer, and a fifth CoNiFe layer on the fourth NiFe layer.

4. The method of claim 3, wherein the first NiFe layer has a thickness between about 5 Å and about 25 Å, the second CoNiFe layer has a thickness between about 150 Å and about 350 Å, the third Ta layer has a thickness between about 5 Å and about 20 Å, the fourth CoNiFe layer has a thickness between about 15 Å and about 60 Å, and the fifth CoNiFe layer has a thickness between about 200 Å and about 300 Å.

5. The method of claim 3, wherein the magnetic seedlayer comprises a sixth corrosion protection layer on the fifth CoNiFe layer.

6. The method of claim 5, wherein the sixth layer comprises Ni80Fe20.

7. The method of claim 6, wherein the sixth layer has a thickness between about 25 Å and about 75 Å.

8. The method of claim 2, wherein the magnetic layers in the magnetic seedlayer have different magnetizations such that the magnetic seedlayer exhibits a magnetization gradient perpendicular to the base.

9. The method of claim 1, wherein the removable layer on the magnetic seedlayer is a removable positive tone resist such as polymethylglutarimide (PMGI) layer having a thickness of from about 10 nm to about 30 nm.

10. The method of claim 1, wherein the trench is formed in the resist by a photolithographic process.

11. The method of claim 1, wherein the first temperature is close to the glass transition temperature of the resist and the second temperature is lower than, about equal to or higher than the first temperature.

12. The method of claim 1, wherein the magnetic pole material in the trench is formed by electroplating and is one of a homogeneous magnetic pole material or a magnetic pole material with a graded magnetic structure.

13. The method of claim 12, wherein the graded magnetic pole material is formed by current controlled electroplating.

14. The method of claim 12, wherein the graded magnetic material is formed by sequentially plating layers of magnetic material from different plating baths.

15. The method of claim 12, wherein the magnetic pole material is at least one of FeCo, CoNiFe, NiFeCu, and NiFe.

16. The method of claim 12, wherein the graded magnetic pole material is a multilayer structure comprised of a first layer comprising a IT NiFe layer having a thickness from about 25 nm to about 200 nm on the seedlayer, a second layer comprising a IT NiCu layer having a thickness of from about 25 nm to about 100 nm on the first layer, and a 0.3T NiCu layer having a thickness of from about 25 nm to about 100 nm on the second layer.

17. The method of claim 16, wherein the first layer is comprised of a high moment alloy comprising at least one of FeCo or CoNiFe and having a thickness of from about 25 nm to about 300 nm.

18. The method of claim 16, wherein the first layer is absent and the seedlayer is a high moment multilayer magnetic structure.

19. The method of claim 1, wherein the write pole has a trapezoidal cross-section with a bottom width Wb less than or equal to about 100 nm, a top width about 1.25 to about 5 times the bottom width, a height h and an aspect ratio h/Wb about 1:1 to about 10:1.

20. The method of claim 1, wherein the seed material outside the pole area is removed by ion milling.

21. The method of claim 20, wherein the ion milling is one of static ion milling wherein the target is stationary or dynamic ion milling wherein the target is oscillated through an angle range of less than 40°.

22. A magnetic write pole comprising: a base;a magnetic seedlayer on the base; anda magnetic layer on the seedlayer with a trapezoidal cross-section, the magnetic layer having a bottom width Wb less than or equal to about 300 nm, having a top width of about 1.25 to about 3 times Wb, having a height h, and having an aspect ratio h/Wb, of about 1:1 to about 10:1.

23. The magnetic write pole of claim 22, wherein the magnetic seedlayer is a multilayer seedlayer formed of magnetic and nonmagnetic layers.

24. The magnetic write pole of claim 23, wherein the magnetic seedlayer comprises a first NiFe layer on the base, a second CoNiFe layer on the first NiFe layer, a third Ta layer on the second CoNiFe layer, a fourth NiFe layer on the third Ta layer, and a fifth CoNiFe layer on the fourth NiFe layer.

25. The magnetic write pole of claim 24, wherein the first NiFe layer has a thickness between about 5 Å and about 25 Å, the second CoNiFe layer has a thickness between about 150 Å and about 350 Å, the third Ta layer has a thickness between about 5 Å and about 20 Å, the fourth CoNiFe layer has a thickness between about 15 Å and about 60 Å, and the fifth CoNiFe layer has a thickness between about 200 Å and about 300 Å.

26. The magnetic write pole of claim 24, wherein the magnetic seedlayer comprises a sixth corrosion protection layer.

27. The magnetic write pole of claim 26, wherein the sixth layer comprises Ni80Fe20.

28. The magnetic write pole of claim 23, wherein the magnetic layers in the magnetic seedlayer have different magnetizations such that the magnetic seedlayer exhibits a magnetization gradient perpendicular to the base.

29. The magnetic write pole of claim of claim 22, wherein the magnetic layer on the seed layer is a homogeneous magnetic pole or a magnetic pole with a graded magnetic structure.

30. The magnetic write pole of claim 29, wherein the homogeneous magnetic pole material is at least one of FeCo, CoNiFe, NiFeCu, and NiFe.

31. The magnetic write pole of claim 29, wherein the graded magnetic pole material is a multilayer structure comprised of a first layer comprising a 1T NiFe layer having a thickness from about 25 nm to about 200 nm on the seedlayer, a second layer comprising a 1T NiCu layer having a thickness of from about 25 nm to about 100 nm on the first layer, and a 0.3T NiCu layer having a thickness of from about 25 nm to about 100 nm on the second layer.

32. The magnetic write pole of claim 31, wherein the first layer is comprised of a high moment alloy comprising at least one of FeCo or CoNiFe and having a thickness of from about 25 nm to about 300 nm.

33. The magnetic write pole of claim 32, wherein the first layer is absent and the seedlayer is a high moment multilayer magnetic structure.