The present disclosure is directed, in general, to power and signal processing and, in particular, to a micromagnetic device and method of forming the same.
A continuing challenge in the design of compact power and signal processing devices for present and future markets is to produce product with smaller sizes and higher operating efficiencies. Prior industrial and research focus has been to produce semiconductor devices with smaller sizes, but has not made comparable progress for micromagnetic devices, which are necessary elements in these circuits. Producing micromagnetic devices, with very small overall dimensions and with low manufacturing costs has been a continuing design challenge.
To meet these challenges, new magnetic alloy compositions should be explored with improved properties and that can accommodate large product runs. New electroplating techniques would also be beneficial to achieve higher levels of magnetic performance and manufacturing repeatability. To achieve a high level of power conversion efficiency in end products, micromagnetic devices with thick winding turns would be advantageous.
A further challenge to produce a micromagnetic device with small dimensions is to avoid the production of pattern edge “horns” that tend to form during a thick electroplating process. Current through-photoresist electroplating approaches produce uneven surface features in magnetic or metallic layers that compromise manufacturing yields and affect product reliability in the field. Accordingly, what is needed in the art is a micromagnetic device that addresses these and other design and manufacturing challenges therefor.
These and other problems are generally solved or circumvented, and technical advantages are generally achieved, by advantageous embodiments of the present disclosure including a micromagnetic device and method of forming the same. In one embodiment, the micromagnetic device includes a substrate, a seed layer over the substrate and a magnetic layer over the seed layer. The magnetic layer includes a magnetic alloy including iron, cobalt, boron and phosphorous, wherein a content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion of the magnetic alloy.
The foregoing has outlined rather broadly the features and technical advantages of the present invention in order that the detailed description of the invention that follows can be better understood. Additional features and advantages of the invention will be described hereinafter, which form the subject of the claims of the invention. It should be appreciated by those skilled in the art that the conception and specific embodiment disclosed can be readily utilized as a basis for modifying or designing other structures or processes for carrying out the same purposes of the present invention. It should also be realized by those skilled in the art that such equivalent constructions do not depart from the spirit and scope of the invention as set forth in the appended claims.
For a more complete understanding of the present invention and the advantages thereof, reference is now made to the following descriptions taken in connection with the accompanying drawings, and which:
Corresponding numerals and symbols in the different figures generally refer to corresponding parts unless otherwise indicated, and cannot be redescribed in the interest of brevity after the first instance. The FIGUREs are drawn to illustrate the relevant aspects of exemplary embodiments.
The making and using of the present exemplary embodiments are discussed in detail below. It should be appreciated, however, that the embodiments provide many applicable inventive concepts that can be embodied in a wide variety of specific contexts. The specific embodiments described herein are merely illustrative of specific ways to make and use a micromagnetic device.
A device will be described herein with respect to exemplary embodiments in a specific context, namely, a broad class of industrial manufacturing processes for manufacturing a micromagnetic device. The specific embodiments are applicable to processes in many fields including, but are not limited to, manufacturing of micromagnetic devices that may include a metallic structure such as a metallic layer or winding and a magnetic structure.
A sequence of steps to produce a micromagnetic device formed according to the principles of the disclosure will now be described. In the interest of brevity, the details of some processing steps well known in the art may not be included in the descriptive material below. For example, without limitation, cleaning steps such as using deionized water or a reactive ionizing chamber may not be described, generally being ordinary techniques well known in the art. The particular concentration of reagents, the exposure times for photoresists, general processing temperatures, current densities for electroplating processes, chamber operating pressures, chamber gas concentrations, radio frequencies to produce ionized gases, etc., are often ordinary techniques well-known in the art, and will not always be included in the description below. Similarly, alternative reagents and processing techniques to accomplish substantially the same result, for example, the substitution of chemical-vapor deposition for sputtering, etc., may not be identified for each processing step, and such substitutions are included within the broad scope of the disclosure. The dimensions and material compositions of the exemplary embodiment described below also may be altered in alternative designs to meet particular design objectives, and are included within the broad scope of the disclosure.
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The power train 110 receives an input voltage Vin at an input thereof and provides a regulated output characteristic (e.g., an output voltage Vout) to power a microprocessor or other load coupled to an output of the power converter. The controller 120 may be coupled to a voltage reference representing a desired characteristic such as a desired system voltage from an internal or external source associated with the microprocessor, and to the output voltage Vout of the power converter. In accordance with the aforementioned characteristics, the controller 120 provides a signal SPWM to control a duty cycle and a frequency of at least one power switch of the power train 110 to regulate the output voltage Vout or another characteristic thereof by periodically coupling the integrated micromagnetic device to the input voltage Vin.
In accordance with the aforementioned characteristics, a drive signal(s) [e.g., a first gate drive signal PG with duty cycle D functional for a P-channel metal-oxide semiconductor field-effect transistor (“MOSFET”) (referred to as a “PMOS”) power switch and a second gate drive signal NG with complementary duty cycle 1-D functional for a N-channel MOSFET (referred to as an “NMOS”) power switch] is provided by the driver 130 to control a duty cycle and a frequency of one or more power switches of the power converter, preferably to regulate the output voltage Vout thereof.
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The power train of the power converter receives an input voltage Vin (e.g., an unregulated input voltage) from a source of electrical power (represented by a battery) at an input thereof and provides a regulated output voltage Vout to power, for instance, a microprocessor at an output of the power converter. In keeping with the principles of a buck converter topology, the output voltage Vout is generally less than the input voltage Vin such that a switching operation of the power converter can regulate the output voltage Vout. A main power switch Qmain, (e.g., a PMOS switch) is enabled to conduct by a gate drive signal PG for a primary interval (generally co-existent with a duty cycle “D” of the main power switch Qmain,) and couples the input voltage Vin to an output filter inductor Lout, which may be advantageously formed as a micromagnetic device. During the primary interval, an inductor current ILout flowing through the output filter inductor Lout increases as a current flows from the input to the output of the power train. An ac component of the inductor current ILout is filtered by an output capacitor Cout.
During a complementary interval (generally co-existent with a complementary duty cycle “1-D” of the main power switch Qmain), the main power switch Qmain is transitioned to a non-conducting state and an auxiliary power switch Qaux (e.g., an NMOS switch) is enabled to conduct by a gate drive signal NG. The auxiliary power switch Qaux provides a path to maintain a continuity of the inductor current ILout flowing through the micromagnetic output filter inductor Lout. During the complementary interval, the inductor current ILout through the output filter inductor Lout decreases. In general, the duty cycle of the main and auxiliary power switches Qmain, Qaux may be adjusted to maintain a regulation of the output voltage Vout of the power converter. Those skilled in the art should understand, however, that the conduction periods for the main and auxiliary power switches Qmain,, Qaux may be separated by a small time interval to avoid cross conduction therebetween and beneficially to reduce the switching losses associated with the power converter.
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Regarding the magnetic layer 340, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The magnetic layer 340 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The magnetic layer 340 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the magnetic layer 340 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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Thus, a micromagnetic device formed with a quaternary alloy with magnetic properties improved over those currently available, and related method, has been introduced herein formed over a substrate. In an advantageous embodiment, the quaternary alloy includes iron, cobalt, boron and phosphorus, and is an amorphous or nanocrystalline magnetic alloy.
In an embodiment, the micromagnetic device (300) includes a substrate (310), an adhesive layer (320) over the substrate (310), a seed layer (330) over the adhesive layer (320), and a magnetic layer (340, e.g., one to fifteen microns in thickness) over the seed layer (330) from a magnetic alloy including iron, cobalt, boron and phosphorous. A content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion (e.g., 70 - 95 atomic percent) of the magnetic alloy.
The magnetic alloy may also include at least one of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, and copper with a concentration in a range of 1 to 1000 parts per million. The magnetic alloy is an amorphous or nanocrystalline magnetic alloy. The adhesive layer (320) may include at least one of nickel, chromium, titanium, and titanium tungsten.
The seed layer (330) may include at least one of copper, gold, titanium, titanium tungsten, nickel, nickel-iron, cobalt, ruthenium, platinum and titanium followed by a thin layer of copper or gold. The seed layer (330) forms a conductive layer onto which the magnetic layer (340) is formed. The micromagnetic device (300) further includes a protective layer (350) over the magnetic layer (340). The protective layer (350) may include at least one of titanium, titanium tungsten, chromium, and nickel.
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Regarding the first magnetic layer 440, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The first magnetic layer 440 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The first magnetic layer 440 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the first magnetic layer 440 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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The thickness of the insulating layer 450 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the insulating layer 450 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The insulating layer 450 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the first magnetic layer 440, which is then hard cured by heating or other means. The insulating layer 450 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the insulating layer 450 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for an insulating layer 450 in the micromagnetic device 400, thereby simplifying the total manufacturing process.
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Thus, a micromagnetic device formed with a quaternary alloy with magnetic properties improved over those currently available, and related method, has been introduced herein formed over a substrate. In an advantageous embodiment, the quaternary alloy includes iron, cobalt, boron and phosphorus, and is an amorphous or nanocrystalline magnetic alloy.
In an embodiment, the micromagnetic device (400) includes a substrate (410), a first adhesive layer (420) and a first seed layer (430) over the substrate (410), and a first magnetic layer (440, e.g., one to fifteen microns in thickness) over the first adhesive layer (420) and first seed layer (430) from a magnetic alloy including iron, cobalt, boron and phosphorous. The micromagnetic device (400) also includes a second adhesive layer (460) and second seed layer (470) over the first magnetic layer (440), and second magnetic layer (480, e.g., one to fifteen microns in thickness) over the second adhesive layer (460) and second seed layer (470) from a magnetic alloy including iron, cobalt, boron and phosphorous. A content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion (e.g., 70 - 95 atomic percent) of the magnetic alloy.
The magnetic alloy may also include at least one of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, and copper with a concentration in a range of 1 to 1000 parts per million. The magnetic alloy is an amorphous or nanocrystalline magnetic alloy. The first and second adhesive layers (420, 460) may include at least one of nickel, chromium, titanium, and titanium tungsten.
The first and second seed layers (430, 470) may include at least one of copper, gold, titanium, titanium tungsten, nickel, nickel-iron, cobalt, ruthenium, platinum and titanium followed by a thin layer of copper or gold. The first and second seed layers (430, 470) form a conductive layer onto which the first and second magnetic layers (440, 480), respectively, are formed.
The micromagnetic device (400) also includes an insulting or semi-insulating layer (450) between the first and second magnetic layers (440, 480). The insulating layer (450, e.g., a polymer, an aluminum oxide or silicon dioxide) can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The micromagnetic device (400) further includes a protective layer (490) over the second magnetic layer (480). The protective layer (490) may include at least one of titanium, titanium tungsten, chromium, and nickel.
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Regarding the magnetic layer 540, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The magnetic layer 540 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The magnetic layer 540 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the magnetic layer 540 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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The thickness of the insulating layer 560 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the insulating layer 560 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The insulating layer 560 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the protective layer 550, which is then hard cured by heating or other means. The insulating layer 560 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the insulating layer 560 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for an insulating layer 560 in the micromagnetic device 500, thereby simplifying the total manufacturing process.
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Thus, a micromagnetic device formed with a quaternary alloy with magnetic properties improved over those currently available, and related method, has been introduced herein formed over a substrate. In an advantageous embodiment, the quaternary alloy includes iron, cobalt, boron and phosphorus, and is an amorphous or nanocrystalline magnetic alloy.
In an embodiment, the micromagnetic device (500) includes a substrate (510), a first adhesive layer (520) over the substrate (510), a first seed layer (530) over the first adhesive layer (520), and a magnetic layer (540, e.g., one to fifteen microns in thickness) over the first seed layer (530) from a magnetic alloy including iron, cobalt, boron and phosphorous. A content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion (e.g., 70 - 95 atomic percent) of the magnetic alloy. The micromagnetic device (500) also includes a metallic layer (590) over the magnetic layer (540). The metallic layer (590) may be about 20 microns thick formed from copper, gold, aluminum, or other electrically conductive metallic material.
The magnetic alloy may also include at least one of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, and copper with a concentration in a range of 1 to 1000 parts per million. The magnetic alloy is an amorphous or nanocrystalline magnetic alloy.
The micromagnetic device (500) also includes a protective layer (550), an insulting layer (560), and a second adhesive layer (570) and a second seed layer (580) between the magnetic layer (540) and the metallic layer (590). The first and second adhesive layers (520, 570) may include at least one of nickel, chromium, titanium, and titanium tungsten. The first and second seed layers (530, 580) may include at least one of copper, gold, titanium, titanium tungsten, nickel, nickel-iron, cobalt, ruthenium, platinum and titanium followed by a thin layer of copper or gold. The first and second seed layers (530, 580) form a conductive layer onto which the magnetic layer (540) and the metallic layer (590), respectively, are formed. The insulating layer (560, e.g., a polymer, an aluminum oxide or silicon dioxide) can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The protective layer (550) may include at least one of titanium, titanium tungsten, chromium, and nickel.
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Regarding the first magnetic layer 620, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The first magnetic layer 620 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The first magnetic layer 620 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the first magnetic layer 620 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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The thickness of the insulating layer 630 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the insulating layer 630 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The insulating layer 630 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the first protective layer 625, which is then hard cured by heating or other means. The insulating layer 630 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the insulating layer 630 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for an insulating layer 630 in the micromagnetic device 600, thereby simplifying the total manufacturing process.
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Regarding the second magnetic layer 650, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The second magnetic layer 650 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The second magnetic layer 650 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the second magnetic layer 650 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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In an embodiment, the micromagnetic device (600) includes a substrate (605), a first adhesive layer (610) over the substrate (605), a first seed layer (615) over the first adhesive layer (610), and a first magnetic layer (620, e.g., one to fifteen microns in thickness) over the first seed layer (615) from a magnetic alloy including iron, cobalt, boron and phosphorous. A content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion (e.g., 70 - 95 atomic percent) of the magnetic alloy. The micromagnetic device (600) includes a metallic layer (645) over the first magnetic layer (620). The metallic layer (645) may be about 20 microns thick formed from copper, gold, aluminum, or other electrically conductive metallic material.
The magnetic alloy may also include at least one of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, and copper with a concentration in a range of 1 to 1000 parts per million. The magnetic alloy is an amorphous or nanocrystalline magnetic alloy.
The micromagnetic device (600) also includes a first protective layer (625), an insulting layer (630), a second adhesive layer (635) and a second seed layer (640) between the first magnetic layer (620) and the metallic layer (645). The micromagnetic device (600) also includes a second magnetic layer (650, analogous to the first magnetic layer 620) above the metallic layer (645), and a second protective layer (655) above the second magnetic layer (650). The first and second adhesive layers (610, 635) may include at least one of nickel, chromium, titanium, and titanium tungsten. The first and second seed layers (615, 640) may include at least one of copper, gold, titanium, titanium tungsten, nickel, nickel-iron, cobalt, ruthenium, platinum and titanium followed by a thin layer of copper or gold. The first and second seed layers (615, 640) form a conductive layer onto which the first magnetic layer (620) and the metallic layer (645), respectively, are formed. The insulating layer (630, e.g., a polymer, an aluminum oxide or silicon dioxide) can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The first and second protective layers (625, 655) may include at least one of titanium, titanium tungsten, chromium, and nickel.
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Regarding the first magnetic layer 720, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The first magnetic layer 720 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The first magnetic layer 720 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the first magnetic layer 720 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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The thickness of the first insulating layer 725 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the first insulating layer 725 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The first insulating layer 725 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the first magnetic layer 720, which is then hard cured by heating or other means. The first insulating layer 725 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the first insulating layer 725 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for a first insulating layer 725 in the micromagnetic device 700, thereby simplifying the total manufacturing process.
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Regarding the second magnetic layer 740, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The second magnetic layer 740 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The second magnetic layer 740 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the second magnetic layer 740 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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The thickness of the second insulating layer 750 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the second insulating layer 750 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The second insulating layer 750 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the protective layer 745, which is then hard cured by heating or other means. The second insulating layer 750 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the second insulating layer 750 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for a second insulating layer 750 in the micromagnetic device 700, thereby simplifying the total manufacturing process.
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Thus, a micromagnetic device formed with a quaternary alloy with magnetic properties improved over those currently available, and related method, has been introduced herein formed over a substrate. In an advantageous embodiment, the quaternary alloy includes iron, cobalt, boron and phosphorus, and is an amorphous or nanocrystalline magnetic alloy.
In an embodiment, the micromagnetic device (700) includes a substrate (705), a first adhesive layer (710) over the substrate (705), a first seed layer (715) over the first adhesive layer (710), and a first magnetic layer (720, e.g., one to fifteen microns in thickness) over the first seed layer (7150 from a magnetic alloy including iron, cobalt, boron and phosphorous. A content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion (e.g., 70 - 95 atomic percent) of the magnetic alloy. The micromagnetic device (700) includes a second magnetic layer (740) analogous to and above the first magnetic layer (720) and a metallic layer (765) over the second magnetic layer (740). The metallic layer (765) may be about 20 microns thick formed from copper, gold, aluminum, or other electrically conductive metallic material.
The magnetic alloy may also include at least one of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, and copper with a concentration in a range of 1 to 1000 parts per million. The magnetic alloy is an amorphous or nanocrystalline magnetic alloy.
The micromagnetic device (700) also includes a first insulting layer (725), a second adhesive layer (730) and a second seed layer (735) between the first magnetic layer (725) and the second magnetic layer (740). The micromagnetic device (700) also includes a protective layer (745), a second insulating layer (750), a third adhesive layer (755) and a third seed layer (760) between the second magnetic layer (740) and the metallic layer (765). The first, second and third adhesive layers (710, 730, 755) may include at least one of nickel, chromium, titanium, and titanium tungsten.
The first, second and third seed layers (715, 735, 760) may include at least one of copper, gold, titanium, titanium tungsten, nickel, nickel-iron, cobalt, ruthenium, platinum and titanium followed by a thin layer of copper or gold. The first, second and third seed layers (715, 735, 760) form a conductive layer onto which the first and second magnetic layers (720, 740) and the metallic layer (765) are formed. The first and second insulating layers (725, 750, e.g., a polymer, an aluminum oxide or silicon dioxide) can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The protective layer (745) may include at least one of titanium, titanium tungsten, chromium, and nickel.
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The thickness of the first insulating layer 825 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the first insulating layer 825 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The first insulating layer 825 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the first metallic layer 820, which is then hard cured by heating or other means. The first insulating layer 825 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the first insulating layer 825 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for the first insulating layer 825 in the micromagnetic device 800, thereby simplifying the total manufacturing process.
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Regarding the first magnetic layer 840, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The first magnetic layer 840 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The first magnetic layer 840 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the first magnetic layer 840 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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The thickness of the second insulating layer 845 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the second insulating layer 845 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The second insulating layer 845 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the first magnetic layer 840, which is then hard cured by heating or other means. The second insulating layer 845 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the second insulating layer 845 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for the second insulating layer 845 in the micromagnetic device 800, thereby simplifying the total manufacturing process.
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The thickness of the third insulating layer 870 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the third insulating layer 870 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The third insulating layer 870 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the protective layer 865, which is then hard cured by heating or other means. The third insulating layer 870 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the third insulating layer 870 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for a third insulating layer 870 in the micromagnetic device 800, thereby simplifying the total manufacturing process.
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Thus, a micromagnetic device formed with a quaternary alloy with magnetic properties improved over those currently available, and related method, has been introduced herein formed over a substrate. In an advantageous embodiment, the quaternary alloy includes iron, cobalt, boron and phosphorus, and is an amorphous or nanocrystalline magnetic alloy.
In an embodiment, the micromagnetic device (800) includes a substrate (805), a first adhesive layer (810) over the substrate (805), a first seed layer (815) over the first adhesive layer (810), and a first metallic layer (820) over the first seed layer (815). The micromagnetic device (800) also includes first and second magnetic layers (840, 860, e.g., one to fifteen microns in thickness) over the first metallic layer (820) from a magnetic alloy including iron, cobalt, boron and phosphorous. A content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion (e.g., 70 - 95 atomic percent) of the magnetic alloy.
The magnetic alloy may also include at least one of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, and copper with a concentration in a range of 1 to 1000 parts per million. The magnetic alloy is an amorphous or nanocrystalline magnetic alloy.
The micromagnetic device (800) also includes a second metallic layer (885) over the second magnetic layer (860). The first and second metallic layers (820, 885) may be about 20 microns thick formed from copper, gold, aluminum, or other electrically conductive metallic material.
The micromagnetic device (800) also includes a first insulting layer (825), a second adhesive layer (830) and a second seed layer (835) between the first metallic layer (820) and the first magnetic layer (840). The micromagnetic device (800) also includes a second insulting layer (845), a third adhesive layer (850) and a third seed layer (855) between the first magnetic layer (840) and the second magnetic layer (860). The micromagnetic device (800) also includes a protective layer (865), a third insulting layer (870), a fourth adhesive layer (875) and a fourth seed layer (880) between the second magnetic layer (860) and the second metallic layer (885). The first, second, third and fourth adhesive layers (810, 830, 850, 875) may include at least one of nickel, chromium, titanium, and titanium tungsten.
The first, second, third and fourth seed layers (815, 835, 855, 880) may include at least one of copper, gold, titanium, titanium tungsten, nickel, nickel-iron, cobalt, ruthenium, platinum and titanium followed by a thin layer of copper or gold. The first, second, third and fourth seed layers (815, 835, 855, 880) form a conductive layer onto which the first and second magnetic layers (840, 860) and the first and second metallic layers (820, 885) are formed. The first, second and third insulating layers (825, 845, 870, e.g., a polymer, an aluminum oxide or silicon dioxide) can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The protective layer (865) may include at least one of titanium, titanium tungsten, chromium, and nickel.
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The thickness of the first insulating layer 925 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the first insulating layer 925 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The first insulating layer 925 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the first metallic layer 920, which is then hard cured by heating or other means. The first insulating layer 925 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the first insulating layer 925 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for the first insulating layer 925 in the micromagnetic device 900, thereby simplifying the total manufacturing process.
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Regarding the first magnetic layer 940, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The first magnetic layer 940 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The first magnetic layer 940 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the first magnetic layer 940 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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The thickness of the second insulating layer 950 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the second insulating layer 950 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The second insulating layer 950 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the first interface layer 945, which is then hard cured by heating or other means. The second insulating layer 950 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the second insulating layer 950 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for the second insulating layer 950 in the micromagnetic device 900, thereby simplifying the total manufacturing process.
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The thickness of the third insulating layer 970 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the third insulating layer 970 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The third insulating layer 970 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the protective layer 965, which is then hard cured by heating or other means. The third insulating layer 970 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the third insulating layer 970 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for a third insulating layer 970 in the micromagnetic device 900, thereby simplifying the total manufacturing process.
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Thus, a micromagnetic device formed with a quaternary alloy with magnetic properties improved over those currently available, and related method, has been introduced herein formed over a substrate. In an advantageous embodiment, the quaternary alloy includes iron, cobalt, boron and phosphorus, and is an amorphous or nanocrystalline magnetic alloy.
In an embodiment, the micromagnetic device (900) includes a substrate (905), a first adhesive layer (910) over the substrate (905), a first seed layer (915) over the first adhesive layer (910), and a first metallic layer (920) over the first seed layer (915). The micromagnetic device (900) also includes first and second magnetic layers (940, 960, e.g., one to fifteen microns in thickness) over the first metallic layer (920) from a magnetic alloy including iron, cobalt, boron and phosphorous. A content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion (e.g., 70 - 95 atomic percent) of the magnetic alloy.
The magnetic alloy may also include at least one of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, and copper with a concentration in a range of 1 to 1000 parts per million. The magnetic alloy is an amorphous or nanocrystalline magnetic alloy.
The micromagnetic device (900) also includes a second metallic layer (985) over the second magnetic layer (960). The first and second metallic layers (920, 995) may be about 20 microns thick formed from copper, gold, aluminum, or other electrically conductive metallic material.
The micromagnetic device (900) also includes a first insulting layer (925), a second adhesive layer (930) and a second seed layer (935) between the first metallic layer (920) and the first magnetic layer (940). The micromagnetic device (900) also includes a first interface layer (945), a second insulting layer (950) and a second interface layer (955) between the first magnetic layer (940) and the second magnetic layer (960). The micromagnetic device (900) also includes a protective layer (965), a third insulting layer (970), a third adhesive layer (975) and a third seed layer (980) between the second magnetic layer (960) and the second metallic layer (985). The first, second and third adhesive layers (910, 930, 970) may include at least one of nickel, chromium, titanium, and titanium tungsten.
The first, second and third seed layers (915, 935, 980) may include at least one of copper, gold, titanium, titanium tungsten, nickel, nickel-iron, cobalt, ruthenium, platinum and titanium followed by a thin layer of copper or gold. The first, second and third seed layers (915, 935, 980) form a conductive layer onto which the first magnetic layer (940) and the first and second metallic layers (920, 985) are formed. The first, second and third insulating layers (925, 950, 970, e.g., a polymer, an aluminum oxide or silicon dioxide) can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The first and second interface layers (945, 955) may include gold, nickel, nickel-iron, cobalt or molybdenum or a combination of consecutive layers of the above. The protective layer (965) may include at least one of titanium, titanium tungsten, chromium, and nickel.
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Regarding the first magnetic layer 1020, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The first magnetic layer 1020 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The first magnetic layer 1020 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the first magnetic layer 1020 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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The thickness of the first insulating layer 1030 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the first insulating layer 1030 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The first insulating layer 1030 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the first protective layer 1025, which is then hard cured by heating or other means. The first insulating layer 1030 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the first insulating layer 1030 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for a first insulating layer 1030 in the micromagnetic device 1000, thereby simplifying the total manufacturing process.
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The thickness of the second insulating layer 1050 can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The thickness of the second insulating layer 1050 can be adjusted using simulation or experimental techniques to produce a die with low residual mechanical stress after completion of micromagnetic device processing.
The second insulating layer 1050 can be formed with a deposition of a patternable layer (e.g., photosensitive photoresist, screen printed polymer or laser patternable coating with no or very low electric conductivity) on top of the metallic layer 1045, which is then hard cured by heating or other means. The second insulating layer 1050 can be a semi-insulating layer such as polypyrrole with a low level of electrical conductivity deposited by an electroplating process. Following electroplating, the second insulating layer 1050 is cured and annealed, which substantially reduces its conductivity. The result is a sufficiently high level of resistivity is obtained for a second insulating layer 1050 in the micromagnetic device 1000, thereby simplifying the total manufacturing process.
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Regarding the second magnetic layer 1065, to provide an alloy with magnetic properties improved over alloys currently available, the quaternary alloy including iron, cobalt, boron and phosphorous is introduced. The second magnetic layer 1065 includes cobalt in the range of 1.0 - 8.0 atomic percent, boron in the range of 0.5 - 10 atomic percent, and iron in the range of 70 - 95 atomic percent. The first magnetic layer 1020 can further include phosphorus in the range of 3.5 - 25 atomic percent, thereby reducing the iron concentration. The alloy may also include trace amounts of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, copper, and/or combinations thereof, with a concentration of each in the range of one (1) to 1000 parts per million (“ppm”), to reduce stress and/or increase resistivity compared to the basic quaternary alloy without these trace elements.
The quaternary alloy employable with the second magnetic layer 1065 advantageously sustains a magnetic saturation flux density of about 1.2 - 2.0 tesla (12,000 - 20,000 gauss), and accommodates a power converter switching frequency of, without limitation, 20 MHz with low loss when electroplated in layers one (1) to fifteen (15) µm thick, each layer separated by an insulation layer (e.g., inorganic materials such as aluminum or silicon oxides and/or organic based materials such as, but not limited to, polymeric films) as set forth below. In comparison, soft ferrites of the past commonly used in the design of switch-mode power converters typically sustain a magnetic saturation flux density of only about 0.3 tesla. The quaternary alloy described herein is readily adaptable to a repeatable and continuing manufacturing process, and can provide long operational life in a typical application environment without substantial degradation of operating characteristics. The quaternary alloy can be electroplated with a sufficiently high current density to accommodate a low-cost manufacturing operation. The quaternary alloy can be readily electroplated in alternating layers with intervening insulating or semi-insulating layers onto a surface patterned, such as with a photoresist, to produce a micromagnetic device operable at a high switching frequency with a low level of power dissipation.
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Thus, a micromagnetic device formed with a quaternary alloy with magnetic properties improved over those currently available, and related method, has been introduced herein formed over a substrate. In an advantageous embodiment, the quaternary alloy includes iron, cobalt, boron and phosphorus, and is an amorphous or nanocrystalline magnetic alloy.
In an embodiment, the micromagnetic device (1000) includes a substrate (1005), a first adhesive layer (1010) over the substrate (1005), a first seed layer (1015) over the first adhesive layer (1010), and a first magnetic layer (1020, e.g., one to fifteen microns in thickness) over the first seed layer (1015) from a magnetic alloy including iron, cobalt, boron and phosphorous. A content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion (e.g., 70 - 95 atomic percent) of the magnetic alloy. The micromagnetic device (1000) also includes a metallic layer (1045) over the first magnetic layer (1020), and a second magnetic layer (1065, analogous to the first magnetic layer 1020) over the metallic layer (1045). The metallic layer (1045) may be about 20 microns thick formed from copper, gold, aluminum, or other electrically conductive metallic material.
The magnetic alloy may also include at least one of sulfur, vanadium, chromium, rhodium, ruthenium, carbon, tin, bismuth, tungsten, and copper with a concentration in a range of 1 to 1000 parts per million. The magnetic alloy is an amorphous or nanocrystalline magnetic alloy.
The micromagnetic device (1000) also includes a first protective layer (1025), a first insulting layer (1030), and a second adhesive layer (1035) and a second seed layer (1040) between the first magnetic layer (1020) and the metallic layer (1045). The micromagnetic device (1000) also includes a second insulting layer (1050), and a third adhesive layer (1055) and a third seed layer (1060) between the metallic layer (1045) and the second magnetic layer (1065). The micromagnetic device (1000) also includes a second protective layer (1065) over the second magnetic layer (1065). The first, second and third adhesive layers (1010, 1035, 1055) may include at least one of nickel, chromium, titanium, and titanium tungsten. The first, second and third seed layers (1015, 1040, 1060) may include at least one of copper, gold, titanium, titanium tungsten, nickel, nickel-iron, cobalt, ruthenium, platinum and titanium followed by a thin layer of copper or gold. The first, second and third seed layers (1015, 1040, 1060) form a conductive layer onto which the first and second magnetic layers (1020, 1065) and the metallic layer (1045) are formed. The first and second insulating layers (1030, 1050, e.g., a polymer, an aluminum oxide or silicon dioxide) can affect residual mechanical stress in the product due to differential thermal expansion of conductive, magnetic, and other layers during device processing steps. The first and second protective layers (1025, 1070) may include at least one of titanium, titanium tungsten, chromium, and nickel.
A process to produce a micromagnetic device formed with thick, metallic winding (or coil) turns on a substrate, such as a thick, copper, spiral winding, employs depositing a photoresist on the substrate. After depositing the photoresist, the substrate is spun to form a thin photoresist layer, and is then dried. Light is directed through a reticle, and is focused with an optical lens on the photoresist to produce a pattern for the copper spiral winding that will be formed to produce the metallic winding. The process of depositing the photoresist, spinning, and drying (i.e., baking and curing the photoresist) is repeated generally at least 2-3 times for a 60-90 micrometers (“µm”) thick photoresist to form the desired thickness for the metallic winding on the substrate.
The aforementioned traditional process for forming metallic winding turns that may be 100 µm thick or more inefficiently adds cost and process time to forming the device. There is no current process to quickly produce and with low cost a thick metallic winding such as a thick copper spiral coil on a substrate. Accordingly, a faster and more cost-effective method of manufacturing thick metallic windings on a substrate compared to traditional photolithographic processes would be beneficial.
A dry, thick-film photolithographic process for constructing devices such as micromagnetic devices will now be described. The process enables production of wafer-level micromagnetic devices having metallic layers (or windings) with a thickness, without limitation, of 100 µm or more, and with spacing between winding segments (or inter-turn separations) that may only be, without limitation, 40 µm or less. The result is a faster and more cost-effective method of manufacturing wafer-level micromagnetic devices on substrates with thick windings, and with high aspect ratio, namely a high ratio of winding segment thickness to spacing between winding segments, compared to traditional photolithographic processes.
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The substrate 1140 on which a metallic layer is to be formed adheres to the photosensitive film 1110 by pressure produced by the rollers 1100, 1130. The rollers 1100, 1130 can be heated as needed or can remain at room temperature. A photolithographic process is then applied to the photosensitive film 1110 that produces the metallic layer (winding or coil) with a high aspect ratio in one efficient processing iteration. There is no need for repeatedly applying, spinning, and drying a photoresist. The photosensitive film 1110 is available in various thicknesses, ranging from 5-300 µm and either a single layer or multiple layers of the photosensitive film can be processed appropriately to accommodate a thickness of the metallic layer very close to the photosensitive film 1110 such as 95 to 98 µm. Thus, the photosensitive film is employed to form metallic layer(s) in reduced processing steps as opposed to repeatedly applying and etching a photoresist to form thick apertures into which the metallic layer(s) will be formed.
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At a second step 1250, the excess photosensitive film is cut to match the wafer shape to provide a laminated substrate 1255. At a third step 1260, a photolithography process using a mask 1265 and ultraviolet (“UV”) radiation is performed on the laminated substrate 1255. This step could be performed for example using a standard I-line UV aligner with an appropriate ultraviolet dosage typically between 20-200 milli-Joules-per-centimeters squared (“mJ/cm2”).
At a fourth step 1270, a pattern from the mask 1265 is transferred to the laminated substrate 1255 by a post exposure bake and photoresist development process. The development process is also chosen appropriate to the type of film chosen. Such developers are typically aqueous, and as an example alkaline (hydroxide) based developers may be used for positive tone films and carbonate based developers maybe chosen for negative tone films. Suppliers and manufacturers of such photosensitive films typically provide guidance on appropriate selection of the type of developer and processing parameters. The result is a patterned laminated substrate 1275.
At a fifth step 1280, features of the micromagnetic device are electroplated and the laminated photosensitive film is removed by, for instance, a wet photoresist stripping process and to form a micromagnetic device 1285. Similar to the choice of developers, typically solutions used for stripping are also suggested by the manufacturer of the photosensitive film, depending on the type of processing employed and contain several components proprietary to the manufacturer such as surfactants and anti-oxidants. For the process of stripping, commercially available aqueous alkaline stripping solutions as described earlier maybe employed at elevated temperatures between 30-80° C. This is typically accompanied by vigorous agitation onto the substrate. Since a significant portion of the photosensitive film and its components may not dissolve in the solution, an inline filtration of the solution to remove particulates and pieces of the photosensitive film that have been removed from the substrate as part of the stripping process may be necessary. It should be noted that
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Thus, a device (such as a micromagnetic device 1300), and related method of forming the same, has been introduced herein (see, e.g.,
The metallic layer (1360) may include another winding segment (1372) electroplated within another aperture (1355) in the photosensitive film (1330). The another aperture (1355) is formed by exposing the photosensitive film (1330) through the reticle to define the pattern (1340) and developing the photosensitive film (1330) to form the another aperture (1355) based on the pattern (1340). An aspect ratio representing a thickness (TH) of the winding segment (1370) to a spacing (SP) between the winding segment (1370) and the another winding segment (1372) is at least one-to-one. It should be noted that the thickness (TH) of the winding segment (1370) and the another winding segment (1372) may be different, and spacing (SP) between multiple winding segments can be different. The winding segment (1370) and the another winding segment (1372) may form at least a portion of a spirally shaped winding. Of course, the device (1300) may include a single winding segment or multiple winding segments.
The device (1300) may also include an insulating layer (1380) formed over the winding segment (1370) and the another winding segment (1372). The device (1300) may further include a magnetic layer (1315) formed between the substrate (1310) and the seed layer (1320), and another magnetic layer (1390) formed over the insulating layer (1380). Of course, the device (1300) may include a single magnetic layer or multiple magnetic layers. The magnetic layer (1315) and/or the another magnetic layer (1390) may include a magnetic alloy including iron, cobalt, boron and phosphorous, wherein a content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion of the magnetic alloy.
In another embodiment, the method of forming the device (such as a micromagnetic device 1300) includes forming a seed layer (1320) over a substrate (1310), laminating a photosensitive film (1330) over the seed layer (1320), and exposing the photosensitive film (1330) through a reticle to define a pattern (1340) on the photosensitive film (1330). The method also includes developing the photosensitive film (1330) to form an aperture (1350) based on the pattern (1340) in the photosensitive film (1330), and electroplating a metallic layer (1360) within the aperture (1350) to produce a winding segment (1370, e.g., having a thickness of at least 10 microns).
The method may also include developing the photosensitive film (1330) to form another aperture (1355) based on the pattern (1340) in the photosensitive film (1330), and electroplating the metallic layer (1360) within the another aperture (1355) to produce another winding segment (1372). An aspect ratio representing a thickness (TH) of the winding segment (1370) to a spacing (SP) between the winding segment (1370) and the another winding segment (1372) is at least one-to-one. It should be noted that the thickness (TH) of the winding segment (1370) and the another winding segment (1372) may be different, and spacing (SP) between multiple winding segments can be different. The winding segment (1370) and the another winding segment (1372) may form at least a portion of a spirally shaped winding. Of course, the device (1300) may include a single winding segment or multiple winding segments.
The method may also include forming an insulating layer (1380) over the winding segment (1370) and the another winding segment (1372). The method may further include forming a magnetic layer (1315) over the substrate (1310) prior to forming the seed layer (1320), and forming another magnetic layer (1390) over the insulating layer (1380). Of course, the device (1300) may include a single magnetic layer or multiple magnetic layers. The magnetic layer (1315) and/or the another magnetic layer (1390) may include a magnetic alloy including iron, cobalt, boron and phosphorous, wherein a content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion of the magnetic alloy.
TABLE 1 below shows in a sequence of columns examples of typical coating time, exposure time, developing time, bake time, strip time, and total processing time to produce a metallic layer (e.g., copper winding) employing a conventional (“spinner”) process and the photolithographic process (“laminator”) introduced herein. Data are compared in TABLE 1 as illustrated in the leftmost column for copper winding thicknesses of 10, 30, 60, and 100 µm. Coating time grows with film thickness for a conventional process, but remains at 0.5 minutes for the laminating process illustrated in
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Thus, a device (such as a micromagnetic device 1400), and related method of forming the same, has been introduced herein (see, e.g.,
The metallic layer (1460) may include another winding segment (1472) electroplated within another aperture (1455) in the first photosensitive film (1430) and the second photosensitive film (1435). The another aperture (1455) is formed by exposing the first photosensitive film (1430) and the second photosensitive film (1435) through the reticle to define the pattern (1440) and developing the first photosensitive film (1430) and the second photosensitive film (1435) to form the another aperture (1455) based on the pattern (1440). An aspect ratio representing a thickness (TH) of the winding segment (1470) to a spacing (SP) between the winding segment (1470) and the another winding segment (1472) is at least one-to-one. It should be noted that the thickness (TH) of the winding segment (1470) and the another winding segment (1472) may be different, and spacing (SP) between multiple winding segments can be different. The winding segment (1470) and the another winding segment (1472) may form at least a portion of a spirally shaped winding. Of course, the device (1400) may include a single winding segment or multiple winding segments.
The device (1400) may also include an insulating layer (1480) formed over the winding segment (1470) and the another winding segment (1472). The device (1400) may further include a magnetic layer (1415) formed between the substrate (1410) and the seed layer (1420), and another magnetic layer (1490) formed over the insulating layer (1480). Of course, the device (1400) may include a single magnetic layer or multiple magnetic layers. The magnetic layer (1415) and/or the another magnetic layer (1490) may include a magnetic alloy including iron, cobalt, boron and phosphorous, wherein a content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion of the magnetic alloy.
In another embodiment, the method of forming the device (such as a micromagnetic device 1400) includes forming a seed layer (1420) over a substrate (1410), laminating a first photosensitive film (1430) and a second photosensitive film (1435) over the seed layer (1420), and exposing (e.g., concurrently or at different steps or time) the first photosensitive film (1430) and the second photosensitive film (1435) through a reticle to define a pattern (1440) on the first photosensitive film (1430) and the second photosensitive film (1435). The method also includes developing (e.g., concurrently or at different steps or time) the first photosensitive film (1430) and the second photosensitive film (1435) to form an aperture (1450) based on the pattern (1440) in the first photosensitive film (1430) and the second photosensitive film (1435), and electroplating a metallic layer (1460) within the aperture (1450) to produce a winding segment (1470, e.g., having a thickness of at least 10 microns).
The method may also include developing the first photosensitive film (1430) and the second photosensitive film (1435) to form another aperture (1455) based on the pattern (1440) in the first photosensitive film (1430) and the second photosensitive film (1435), and electroplating the metallic layer (1460) within the another aperture (1455) to produce another winding segment (1472). An aspect ratio representing a thickness (TH) of the winding segment (1470) to a spacing (SP) between the winding segment (1470) and the another winding segment (1472) is at least one-to-one. It should be noted that the thickness (TH) of the winding segment (1470) and the another winding segment (1472) may be different, and spacing (SP) between multiple winding segments can be different. The winding segment (1470) and the another winding segment (1472) may form at least a portion of a spirally shaped winding. Of course, the device (1400) may include a single winding segment or multiple winding segments.
The method may also include forming an insulating layer (1480) over the winding segment (1470) and the another winding segment (1472). The method may further include forming a magnetic layer (1415) over the substrate (1410) prior to forming the seed layer (1420), and forming another magnetic layer (1490) over the insulating layer (1480). Of course, the device (1400) may include a single magnetic layer or multiple magnetic layers. The magnetic layer (1415) and/or the another magnetic layer (1490) may include a magnetic alloy including iron, cobalt, boron and phosphorous, wherein a content of the cobalt is in a range of 1.0 to 8.0 atomic percent, a content of the boron is in a range of 0.5 to 10 atomic percent, a content of the phosphorus is in a range of 3.5 to 25 atomic percent, and a content of the iron is substantially a remaining proportion of the magnetic alloy.
Although the embodiments introduced herein and its advantages have been described in detail, it should be understood that various changes, substitutions, and alterations can be made herein without departing from the spirit and scope thereof as defined by the appended claims. Also, many of the features, functions, and steps of operating the same can be reordered, omitted, added, etc., and still fall within the broad scope of the various embodiments.
Moreover, the scope of the various embodiments is not intended to be limited to the particular embodiments of the process, machine, manufacture, composition of matter, means, methods and steps described in the specification. As one of ordinary skill in the art will readily appreciate from the disclosure, processes, machines, manufacture, compositions of matter, means, methods, or steps, presently existing or later to be developed, that perform substantially the same function or achieve substantially the same result as the corresponding embodiments described herein can be utilized as well. Accordingly, the appended claims are intended to include within their scope such processes, machines, manufacture, compositions of matter, means, methods, or steps.
This application claims the benefit of U.S. Pat. Application Serial No. 62/704,316, entitled “Micromagnetic Device and Method of Forming the Same,” filed May 4, 2020, U.S. Pat. Application Serial No. 62/706,692, entitled “Micromagnetic Device and Method of Forming the Same,” filed Sep. 3, 2020, and U.S. Pat. Application Serial No. 63/198,718, entitled “Micromagnetic Device and Method of Forming the Same,” filed Nov. 6, 2020, which are incorporated herein by reference.
Filing Document | Filing Date | Country | Kind |
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PCT/US2021/070500 | 5/4/2021 | WO |
Number | Date | Country | |
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63198718 | Nov 2020 | US | |
62706692 | Sep 2020 | US | |
62704316 | May 2020 | US |