Patent Application
20250231259
The present invention belongs to the field of spintronic and concerns a magnetoresistive sensor sensitive to an out-of-plane component of a magnetic field. For ease of the description, the out-of-plane component of magnetic field will be named out-of-plane magnetic field or magnetic field perpendicular to the plane.
Spintronic magnetic field sensors are used in a wide range of automotive, industrial or biomedical applications. (P. P. Freitas, R. Ferreira and S. Cardoso, 2016, “Spintronic Sensors,” in Proceedings of the IEEE, vol. 104, no. 10, pp. 1894-1918).
These types of magnetoresistive sensors present several advantages compared to other alternatives such as Hall sensors, search coils, Giant magneto-impedance sensors, SQUIDs or fluxgates due to their combination of high sensitivity, compact size, low power consumption, compatibility with CMOS integration and low cost.
Spintronic sensors convert a magnetic field variation into a voltage or resistance change under dc or ac bias current. Such resistance change is based on the giant magnetoresistance (GMR) effect in spin-valves (SVs) or the tunnel magnetoresistance (TMR) in magnetic tunnel junctions (MTJs). Both magnetoresistive structures show variation in their electrical resistance as a function of the relative orientation between the reference layer (RL) of fixed magnetization and the sensing layer (SL) magnetization.
Vortex based magnetoresistive sensors are known to exhibit high saturation fields, which constitutes an attractive feature for applications with large dynamic range (Suess, D., Bachleitner-Hofmann, A., Satz, A. et al., 2018, “Topologically protected vortex structures for low-noise magnetic sensors with high linear range”. Nat Electron 1, 362-370).
For certain applications such as speed or current sensors, a large linear range is an important feature since this reduces the required accuracy on the amplitude of the field that the bias magnets generate on the sensor. However, it also goes with a decrease in the sensor sensitivity.
The stability of the vortex structure results from a minimization of the total energy of the system which includes the exchange energy arising from the non-uniformity of the vortex structure, the magneto-static energy from dipolar interactions, the magneto-crystalline anisotropy energy and the Zeeman energy if an external field is applied. For certain geometries, the ground energy state of nanoscale cylinders favors a vortex configuration, as theoretically predicted (Metlov, K. L. and Lee Y., 2008, “Map of metastable states for thin circular magnetic nanocylinders.” Appl. Phys. Lett. 92, 112506 (2008)). At such geometries, the magneto-static energy overpowers the exchange energy, resulting in the formation of the vortex configuration which corresponds to an in-plane curling of the magnetic moments enabling in-plane flux closure with an out-of-plane magnetized vortex core to reduce the exchange energy cost which would be generated by a magnetic singularity at the center of the cylinder. In the common case used in prior art sensor, the thickness of the cylinder is much smaller than its diameter. In this situation, the diameter of the vortex core is given by the exchange length defined by
With commonly used materials such as Permalloy (Ni80Fe20), cobalt, iron, this length is typically of the order of 5 nm. The area of the vortex core is consequently a very small fraction of the disk area. For instance, for a disk of diameter 1 micron, the ratio of the core area to the disk area is of the order of (5/1000)2=2.5 10−5.
Prior art vortex-based sensors are sensitive to the in-plane component of the magnetic field. All along this description, “in-plane” means parallel to the plane of the stack layers of the sensor while “out-of-plane” or “perpendicular to the plane” mean along the normal to this plane.
The magnetic stack 1 successively includes:
The pinned synthetic antiferromagnetic structure 3 comprises successively:
The reference layer 10 is part of a Synthetic Antiferromagnet (“SAF”). The SAF comprises two layers 8 and 10 antiferromagnetically coupled, separated by the metallic spacer 9. The two layers 8 and 10 are respectively considered as a reference (or polarizer) layer 10 and a pinned layer 8. The SAF is associated with the antiferromagnetic pinning layer 7 which provides exchange bias to the magnetic pinned layer 8 of the SAF in contact with it. The SAF is then grown above this antiferromagnetic pinning layer 7. Said pinned synthetic antiferromagnetic structure (AF/SAF) of the form (AF/FM/Ru/Reference) is commonly used as pinned reference electrode, where the layer FM 8 is a ferromagnetic material such as cobalt or an alloy mostly based on Fe, Co, Ni. When the sensor is a metallic spin-valve with a non-magnetic metallic spacer separating the reference layer from the sensing layer, the whole stack has usually a face centered cubic (fcc (111) texture). When the sensor is a magnetic tunnel junction, the spacer between the reference layer and the sensing layer is then an oxide tunnel barrier most often made of MgO bcc (001) texture. In this case, to grow a four-fold symmetry bcc (001) oxide tunnel barrier on top of a three-fold symmetry fcc (111) AF/SAF structure, the reference layer 10 usually consists of a composite trilayer comprising successively:
The synthetic antiferromagnetic (SAF) configuration allows reducing the stray field exerted by this hard reference stack on the sensing layer and provides larger magnetic stability to the reference layer. The ferromagnetic reference layer has an in-plane magnetization and is exchange coupled with the layer of anti-ferromagnetic material. As well-known by a man skilled in the art, the ferromagnetic material layer 8 of the SAF adjacent to the antiferromagnetic layer 7 is pinned in an in-plane direction by annealing the stack and letting it cool down from above the blocking temperature of the antiferromagnetic layer under an externally applied magnetic field in that specific direction to saturate the ferromagnetic layer magnetization in that desired direction.
In vortex-based sensors sensitive to in-plane field, in a certain range of field limited by the vortex annihilation fields, an almost linear variation of resistance versus field is observed due to a lateral vortex core motion in a direction orthogonal to that of the in-plane field to be sensed. State of the art magnetoresistive sensors with a vortex configuration in the sensing layer are attractive due to their linear R(H) characteristics and stability of the vortex configuration.
The mechanism of operation of prior art vortex sensor is depicted in
One particular advantage of such known vortex-based sensors is a large linear range (40 mT) compared to that of single domain elliptical sensors (5 mT) which represents an eight-fold enhancement in sensing range but a decrease in sensitivity by the same factor as reported by Suess, D., Bachleitner-Hofmann, A., Satz, A. et al., 2018, “Topologically protected vortex structures for low-noise magnetic sensors with high linear range”. Nat Electron 1, 362-370.
A drawback of this type of sensor is their noise. This noise results from the trapping of the vortex core in its lateral motion due to local fluctuations of the anisotropy. This can in particular occur in magnetic tunnel junction due to spatial variations of interfacial anisotropy at the interface between the oxide tunnel barrier and sense layer. Indeed, it is known that this anisotropy is very sensitive to parameters such as local oxygen or boron concentration. Since the vortex core has a small area in prior art vortex sensors (typically 5 nm in diameter), the trapping can be very effective even on small defects of the order of a few nm such as grain boundaries. This may induce the equivalent of Barkhausen noise known in domain wall propagation but here for vortex core propagation. This noise impacts the signal to noise ratio of this type of sensors.
In addition, these sensors are sensitive to the component of the field parallel to the pinning direction of the reference layer magnetization, i.e., an in-plane direction. There is thus a limitation in the direction of measurement of the magnetic field.
In this context, the object of the present invention is to provide a vortex based magnetoresistive sensor able to measure the out-of-plane component of the field and presenting an improved signal to noise ratio.
For this purpose, the invention proposes a magnetoresistive sensor sensitive to an out-of-plane applied magnetic field comprising:
Thanks to the invention, it is possible to sense a magnetic field oriented perpendicular to the plane of the sensing layer in which the sensing layer is in a vortex micromagnetic configuration. The sensor principle is based on the expansion or contraction of the out-of-plane magnetized vortex core under the influence of the out-of-plane field to be sensed. By implementing such sensing layer in a magnetic tunnel junction or a spin-valve comprising an out-of-plane magnetized reference layer, this expansion/contraction of the vortex core produces a magnetoresistive signal which can be used to measure the amplitude of the applied field to be sensed. The obtained magnetoresistive sensor displays a large linear range and improved signal to noise ratios compared to prior art vortex-based sensors.
The sensor according to the invention exhibits an almost linear variation of resistance versus the amplitude of the out-of-plane field to be sensed. However, this linear variation is not associated with a lateral motion of the vortex core as in prior art sensor but on the expansion/contraction of the vortex core under the out-of-plane applied magnetic field. Due to the much larger size of the vortex core and the fact that the center of the core does not move laterally during field sensing, the noise of these sensors is much reduced resulting in higher signal to noise ratio compared to prior art vortex sensors.
In the present invention, as we will see further in the description, the ratio of the thickness of the sensing layer divided by the lateral dimension of the sensor is advantageously much larger than in prior art vortex sensor. This results in the vortex core being much wider than in prior art vortex sensor in which the diameter of the vortex core is given by the exchange length.
The sensor according to the invention may also present one or more of the characteristics below, considered individually or according to all technically possible combinations:
The invention has also for object a sensing device comprising a plurality of magnetoresistive sensors according to the invention that are electrically coupled in series and/or in parallel.
Said sensing device may comprise four magnetoresistive sensors according to the invention, said four magnetoresistive sensors being arranged according to a Wheatstone bridge configuration and configured so that the reference layer of the two sensors located in the two opposite branches of the bridge are magnetized in a first out-of-plane direction while the reference layer of the two magnetoresistive located in the two other branches of the bridge are magnetized in the opposite out-of-plane direction.
Other characteristics and advantages of the invention will clearly emerge from the description given below, for indicative and in no way limiting purposes, with references to the attached figures, among which:
a shows a transversal section view of the magnetization reversal of a magnetic element of 60 nm diameter, 60 nm thickness and magnetic saturation of 0.8 MA/m performed by micro magnetic simulations;
b shows 2D view of the Mz component of the uppermost superficial layer at the same external fields applied in
c shows an 1D view of the Mz component of the uppermost superficial layer at y=0;
a and b respectively shows:
a shows experimental hysteretic behavior observed in a sensor due to the vortex core polarity change;
b shows non-hysteretic behavior in a sensor of the invention attributed to the presence of a stray field from the non-fully compensated SAF structure that stabilizes the vortex core polarity in a specific direction;
a and b shows respectively a schematic and detailed representation of a magnetoresistive sensor of the invention with an uncompensated magnetic reference layer magnetized in the direction perpendicular to the plane of the multilayers;
Said sensor 100 is a magnetic stack successively including:
The above magnetic stack has the form of a pillar, the cross section of which having advantageously a circular form.
As mentioned above, the sensing layer 106 has a magnetization vortex configuration. Besides, the sensing layer 106 exhibits an aspect ratio (i.e., thickness divided by in-plane characteristic dimension, here, the diameter) between 0.2 and 2 and advantageously, between 0.2 and 1. In contrast to prior art vortex sensor, the aspect ratio of the sense layer in this sensor is much closer to 1. As a result, the vortex is here much more confined within a narrow cylinder than it is in prior art in-plane sensitive sensors. Unexpectedly, due to this confinement, the vortex core turns out to be significantly larger than in prior art vortex sensors. Moreover, as we will see it with respect to
The reference layer 104 has a fixed mono-domain magnetization perpendicular to the plane of the reference layer 104. The reference layer RL is most often used with a Synthetic Antiferromagnet (“SAF”) 102, as shown at
The sensing layer 106 in vortex configuration is part of a magnetoresistive element. The magnetoresistive element can be either a tunnel junction or a giant magnetoresistance metallic stack. In both cases, the element comprises a top and a bottom electrode so that a current can flow throughout the device in a direction roughly perpendicular to the plane of the layers. As well known by the man skilled in the art, the requirements on the nature of the layers are different in a magnetic tunnel junction and in a fully metallic giant magnetoresistance stack. Indeed, in a tunnel junction, different crystallographic structures are present in the stack (body centered (bcc) close to the tunnel barrier and face centered cubic (fcc) in the bottom part and top part of the stack) whereas in the giant magnetoresistance stack, the structure can remain fcc throughout the whole stack.
In contrast to this prior art, the mechanism of operation of the sensor 100 of
Differently from prior art vortex-based sensors sensitive to in-plane field, the sensor 100 is intended to sense out-of-plane field. From physical point of view, instead of relying on a lateral in-plane shift of the vortex core upon application of an in-plane field, the sensor 100 of the invention relies on the expansion/contraction of the vortex core of the sensing layer 106 under an out-of-plane field Hz (i.e., along the z axis, the Oxy plane being the plane of the different layers of the sensor).
The magnetization response Mz along the z axis of the sensing layer 106 as a function of the out of plane component Hz of an applied magnetic field is depicted in the transfer curve of
As previously mentioned, in prior art vortex sensor, the sensing layer diameter is usually large, of the order of one or a few microns, at least an order of magnitude larger than the thickness of the sensing layer. As a result, the vortex core is quite narrow, with a diameter of a few nanometers given by the exchange length. On the other hand, advantageously, according to the invention, the vortex core diameter gets much wider in cylinders of smaller diameters, when the diameter gets closer to the film thickness. If the field is applied in the out-of-plane direction parallel to the vortex core magnetization, the core diameter tends to increase: this situation is illustrated by the state B compared to the state C where no field is applied. In state B, assuming that the magnetization of the vortex core direction along the z-axis is down (i.e., the z component of the magnetization of the vortex core is negative), the component Hz is parallel and in the same direction (Mz is negative) as the vortex core magnetization and the diameter of the vortex core diameter increases compare to its value at state A without applied field. On the contrary, if the field is applied antiparallel to the core magnetization, its diameter then decreases. One has further to note that, advantageously, the sensor of the invention should be used in its linear response range; in other words, preferably, the applied field should not be used above the annihilation field Ha where the vortex core expands to the whole sensing layer area as shown in state A of
If this sensing layer 106 is implemented in a spin-valve or a magnetic tunnel junction comprising an out-of-plane magnetized reference layer 104, these variations in vortex core diameter of the sensing layer 106 yield a resistance variation in the range of field delimited by the positive and negative vortex annihilation fields. Based on the said variation of the resistance, one can have access to the value of the corresponding out-of-plane component of the applied magnetic field.
If the device is a magnetic tunnel junction, then the tunnel barrier 105 is an oxide or a nitride layer, such as MgO, AlOx, TiOx or AlN, TiN but preferably MgO which is known to provide large TMR signal. To get a large TMR with MgO (large TMR meaning typically a TMR above 80%, preferably above 140%, preferably above 200%), the MgO layer and the two magnetic electrodes sandwiching the MgO layer must have a crystalline bcc structure with (100) texture. As well known by the man skilled in the art, this can be realized by using as magnetic electrodes FeCoB layers which are amorphous as deposited but can recrystallize in bcc structure upon annealing at temperatures typically in the range 250° C. to 400° C.
For this recrystallization to take place, the B or more generally the amorphising element contained in the FeCo based alloy must be expelled from this alloy. For that, a thin layer of a material capable of absorbing this amorphizing element is deposited next to the FeCo based layers on their interfaces opposite to the interfaces with the MgO layer. Such amorphizing element absorbing layer can be made of Ta, W, Mo or Hf for instance.
Taking into account the above consideration, the vortex sensing layer 106 can first comprise a thin FeCoB based layer in contact with the MgO barrier 105. In this layer, B is the amorphizing element. B could be substituted by other amorphizing element such as Zr or Nb. This first layer has typically a thickness in the range 1.5 to 5 nm. This FeCoB is then in contact with a thin layer, a few angstroms thick, able to absorb the amorphizing element upon annealing of the structure. This layer can be made for instance of W, Mo, Ta. The sensing layer 106 further comprises a magnetic layer preferably made of a soft magnetic material such as Permalloy NiFe (composition close to Ni80Fe20) or a soft FeCo layer such as Co90Fe10 or an FeCoB alloy in order to minimize hysteresis in this layer when its micromagnetic configuration changes under the influence of the field to be sensed. This sensing layer 106 can also be a multilayer comprising several of such layers. The sensing layer 106 can also comprise thin laminations (thickness of the order of 0.1 to 0.5 nm) of non-magnetic metals such as W, Mo, Ta, intended to absorb any amorphizing element or to break the grain growth to reduce the top roughness of the sensing layer. If the device is a magnetic tunnel junction, these laminations can also be made of oxide materials such as MgO, TaOx, AlOx, TiOx intended to induce some interfacial perpendicular anisotropy in the sense layer thereby allowing to slightly reduce the thickness of the sense layer. The product of resistance by the area (RA) of these oxide laminations should be then adjusted to values lower than the RA of the main barrier which is providing the tunnel magnetoresistance signal. This will avoid to excessively dilute the magnetoresistive signal due to the increased resistance caused by the introduction of these oxide laminations.
As already explained, the total thickness of this sensing layer is advantageously chosen with an aspect ratio (thickness divided by lateral dimension, here the diameter of the circular sensing layer) between 0.2 and 2 so that its micromagnetic equilibrium configuration is a vortex state with a core diameter significantly larger than the exchange length, preferably at least twice the exchange length (i.e., at least 10 nm for material such as Permalloy or Co90Fe10). Examples of dimensions for the sensing layer are a thickness of the order of 60 nm to stabilize the vortex formation at zero field for diameters ranging between 50 and 200 nm, for instance 60 nm.
Micromagnetic simulations can be used to calculate the range of thicknesses which satisfy the condition of vortex configuration with vortex core diameter at least twice the exchange length.
Concerning the reference layer 104, its magnetization is fixed in the direction perpendicular to the stack of magnetic layers. This perpendicular configuration of the reference layer 104 is required since the measured magnetoresistance variation relies on the variation of the perpendicular magnetization Mz of the vortex-sensing layer 106. If the stack is an MgO based magnetic tunnel junction, this reference layer 104 is preferably made of an FeCoB alloy in contact with the MgO barrier 105. The magnetization of this reference layer 104 is maintained fixed out-of-plane by both the interfacial anisotropy which exists at the FeCoB/MgO interface and by exchange-like coupling with an out-of-plane magnetized multilayer such as (Co/Pt) multilayers. Other multilayers such as Co/X, where X is Pd, Ni or Ir, are well known by the man skilled in the art to provide large PMA (Perpendicular Magnetic Anisotropy) values. Alloys such as CoPt, CoPd or FePt or FePd ordered alloys or some rare earth transition alloys such as TbCo, TbFe can also provide strong PMA. This PMA multilayer or alloy can itself be part of a synthetic antiferromagnetic SAF layer 102 consisting of two antiferromagnetically coupled multilayers such as (Co/Pt) multilayers separated by a non-magnetic spacer typically of Ru or Ir whose thickness is adjusted to provide strong antiferromagnetic coupling between the two adjacent multilayers (typically 0.8 nm for Ru spacer). This type of arrangement is well known by the man skilled in the art. It is also well known that such SAF structure may contain more than two antiferromagnetically coupled multilayers to further reduce the net stray field that the SAF and Reference layer exerts on the sensing layer. Since these PMA multilayers have a fcc structure while FeCoB is bcc after annealing, a thin structural transition layer 103 made of for instance Ta, Mo or W has again to be introduced between the FeCoB layer and the PMA multilayers. This layer 103 is also intended to absorb the amorphising element away from the FeCoB alloy upon annealing. In other words, the texture breaking layer 103 is introduced between the reference layer 104 in FeCoB in contact with the barrier 105 and the rest of the SAF 102 to insure a structural transition between the FeCoB layer which has to be body centred cubic (bcc with 4-fold symmetry) in the final device and the rest of the SAF which has generally a fcc structure with (111 texture) and 3-fold symmetry.
Besides, the SAF layer 102 is grown on a seed layer 101 to promote a (111) texture. The seed layer 101 can be a multilayer of the form Ta/Pt. The material used in the seed layer 101 is also usable for the capping layer 107.
The evolution of the magnetization value along the perpendicular direction Mz for the uppermost superficial layer (1 nm cell) along a diameter of the cylindrical sensing layer is represented in
The characteristic nucleation and annihilation fields can be controlled by varying the sensing layer diameter as shown in the micromagnetic simulations of
The simulations reported in
The sample was subsequently annealed at 300° C. for 10 minutes. The annihilation field represented by gray dots in
The characteristic nucleation and annihilation fields can also be controlled by varying the saturation magnetization Ms of the sensing layer.
The increase of the linear range with increasing Ms is experimentally confirmed as observed in
Another advantage of the vortex sensor according to the invention compared to prior art vortex sensors is its reduced hysteresis. Indeed, in prior art vortex-sensors sensitive to in-plane field, the presence of defects at the interface between the vortex sensing layer and the tunnel barrier that are randomly distributed, modify the vortex core displacement path, as the vortex core gets randomly trapped into energy wells associated with such defects. This effect is particularly pronounced in prior art vortex sensor because the vortex core is very narrow (exchange length˜5 nm) so that the vortex core can easily get trapped by such small defects. In magnetic tunnel junctions, these defects can be due to spatial variations over the MgO/FeCoB interface, of oxygen concentration or Boron concentration or to the diffusion towards the MgO interface of third elements present in the stack such as Ta, Mn, W or Mo. These defects can induce local variations of anisotropy energy which then act as trapping centers for the vortex core.
As a result of this trapping, the transfer curve (Mx versus Hx) can be different depending on the followed path, leading to different resistances of the sensor at each value of external field as shown by S. Dounia, C. Baraduc, and B. Dieny, 2020, EP. U.S. Pat. No. 19,315,026.5.
In contrast, the sensor according to the invention is much less sensitive to the presence of such defects and their trapping. Indeed, the vortex core does not move laterally in the sensor of the invention: it only expands or shrinks while the curled magnetization in the outer part of the device is reversibly pulled out-of-plane or come back to the in-plane direction under the influence of the out-of-plane field to be sensed. Therefore, the vortex deformation under magnetic field is much more reversible with the sensor of the invention than in prior art vortex sensor as schematically depicted in
In an embodiment of the sensor of the invention, the reference layer and the associated SAF layer can be compensated, meaning that they exert no field or only a very small field (i.e., a field negligible against the field required to reverse the vortex core polarity). In such a case, a possible drawback of the sensor of the invention could be a change of vortex core polarity when a magnetic field larger than the annihilation field is applied in the direction opposite to the vortex core polarity. Such change in vortex polarity would produce an undesired hysteresis as already observed in
This problem can be avoided by limiting the range of fields to which the sensor is exposed. The field values should remain below the vortex annihilation field. However, a risk of accidental switching of the vortex core polarity still exists in this case if the sensor is accidentally exposed to an excessively large field.
To better circumvent this issue of accidental switching of the vortex core polarity, a second embodiment is proposed in which the reference layer is coupled to an associated PMA multilayer or a SAF layer, said reference layer and said PMA multilayer (or respectively said reference layer and said SAF layer) being uncompensated. As a result, they create an out-of-plane stray field on the sense layer magnetization. Thanks to this out-of-plane stray field, the vortex always nucleates back with the same polarity, independently of the saturation field direction (positive or negative). This yields the optimal response, which is shown in
Such a sensor 200 with a reference layer and PMA multilayer that are not compensated is illustrated in
Said sensor 200 is a magnetic stack successively including:
Except the PMA multilayer 202, the other layers 201, 203, 204, 205, 206 and 207 can be identical to the layers illustrated in the sensor of
As mentioned above, in this case, the reference layer does not have to be coupled to a SAF layer as in
Another possible embodiment aiming at stabilizing the vortex core polarity consists in coupling the sensing layer to an antiferromagnetic layer to provide an out-of-plane exchange bias to the vortex core. Such a sensor 300 is illustrated in
Said sensor 300 is a magnetic stack successively including:
Except the added exchange biasing layer 308, the other layers 301, 302, 303, 304, 305, 306 and 307 can be identical to the respective layers 101, 102, 103, 104, 105, 106 and 107 illustrated in the sensor of
The exchange biasing layer 308 is above and in contact with the vortex sensing layer 306. Said exchange biasing layer 308, made of an antiferromagnetic material (AF) such as iridium manganese (IrMn) or platinum manganese (PtMn) alloys at the interface of the sensing layer opposite to the tunnel barrier, can be used for this purpose. A unidirectional magnetic anisotropy arises at the interface between the ferromagnetic sensing layer 306 and the AF layer 308, caused by the exchange coupling between the two layers. To provide the exchange bias, the stack must be annealed above the antiferromagnetic layer blocking temperature and cooled down in a magnetic field in the field direction perpendicular to the plane of the layers. As well known by the man skilled in the art, the intensity of the exchange bias can be adjusted by inserting at the interface between the sensing layer 306 and the antiferromagnetic layer 308 a thin layer (not represented) of a non-magnetic element such as Cu, W, Mo or Ta. The main advantage of the sensor of
The sensing device D in Wheatstone bridge configuration comprises four elementary sensors R1, R2, R3 and R4 of the invention configured so that R1 and R4 have their reference layer and vortex core magnetization in the sensing layer oriented in a first out-of-plane direction while R2 and R3 have their reference layer and vortex core magnetization in the sensing layer oriented in the opposite out-of-plane direction.
The sensors R1 and R4 have each an inverse response compared to the sensors R2 and R3. In other words, R1 and R4 (sensors located on opposite branches) have the same response and have their reference layer and vortex core magnetization in the sense layer oriented in a first out-of-plane direction while R2 and R3 have also the same response and their reference layer and vortex core magnetization in the sense layer oriented in the opposite out-of-plane direction.
A sense current is supplied between contacts C1 and C2, Iin representing the entering current into the bridge and Iout the outgoing current. In such Wheatstone bridge configuration D, the elementary sensors are configured so that under an applied magnetic field to be sensed, the resistances of two of the elementary sensors located on opposite branches (here R1 and R4) increases (respectively decreases) while the resistance of the two other sensors (in that example R2 and R3) decreases (respectively increases). Advantageously, this makes it possible to measure a potential difference Voutput between the two contacts C3 and C4, which is directly related to the external out-of-plane magnetic field to be sensed.
According to the embodiment of
In an alternative embodiment, the sensors R1, R2, R3, R4 can be formed by several individual sensors connected in series or in parallel. In that case, all the individual sensors constituting one of the resistances Ri (i from 1 to 4) will be configured identically by just applying a saturation field in the up or in the down direction.
Of course, the sensor according to the invention is not limited to the embodiments that have just been described for indicative and in no way limiting purposes with reference to the figures.
In all the above disclosed embodiments, the sensors according to the invention is of the “bottom” configuration, meaning that the sensing layer is above the tunnel barrier and the reference layer is below the tunnel barrier. However, the invention is of course not limited to a “bottom” configuration; the sensor of the invention may be alternatively in the “top” configuration. This means that the stack may be grown in bottom pinned or top pinned configuration i.e. the sensing layer can be above or below the tunnel junction while correspondingly the reference layer is below or above the tunnel barrier. Since the sensing layer is preferably rather thick in the sensor, it may be advantageous to grow it above the tunnel barrier in order not to create a large roughness for the growth of the tunnel barrier.
Besides, while the detailed embodiments of the sensor according to the invention have been made for a sensor based on magnetic tunnel junction, the man skilled in the art knows that the embodiments described above can also be adapted to the case of a fully metallic magnetoresistive sensor based on giant magnetoresistance. In this case, the tunnel barrier would be replaced by a non-magnetic metallic spacer such as Cu. From a material point of view, these metallic stacks are easier since all the involved material can have an fcc structure so fewer materials issues need to be considered than in magnetic tunnel junctions where some parts of the stack are fcc while others are bcc.
Moreover, the detailed embodiments have been disclosed assuming that the sensor of the invention has a cylindrical shape with a circular cross-section so that the sensing layer dimensions were characterized by its diameter and thickness. The invention would however apply for any type of shape which allows stabilizing the vortex configuration of the sense layer. This is among other true for square shape, square shape with rounded corners, slightly rectangular shape (long side not exceeding twice the short side) possibly with rounded corners, elliptical shape with moderate ellipticity (not exceeding a ratio of 2 between long axis and short axis) or any other shape in which the vortex state can be stabilized. For all these shapes, the sense layer aspect ratio is defined by the ratio of its thickness by the shortest in-plane dimension. If the sense layer has a disk shape, this characteristic dimension is its diameter. If it is a square or close to a square, this is the length of the square side. If it is a rectangle, it is the short side of the rectangle. For an ellipse, it is the short axis.
These devices can be fabricated using a manufacturing process very similar to that of prior art TMR sensors. This process involves the steps of depositing all the layers by physical vapor deposition, etching the sensing layer by reactive or ion beam etching and etching the other layers by ion beam etching. In this process, it is known that ion beam etching of magnetic material often leads to tapered pillars especially in the present case where pillars of high aspect ratio are etched. The presence of such tapered shape is acceptable and will not hamper the working principle of the sensor.
Besides, as well known by the man skilled in the art, several sensors of the invention can be connected in series and/or in parallel to increase the signal to noise ratio of the overall sensor.
| Number | Date | Country | Kind |
|---|---|---|---|
| 22305459.4 | Apr 2022 | EP | regional |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/EP2023/058767 | 4/4/2023 | WO |
