Composite magnetic member and method of manufacturing same
10083784 ยท 2018-09-25
Assignee
Inventors
Cpc classification
C21D10/00
CHEMISTRY; METALLURGY
International classification
C21D8/12
CHEMISTRY; METALLURGY
C21D10/00
CHEMISTRY; METALLURGY
Abstract
A composite magnetic member configured so a nonmagnetic portion different from conventional ones is formed in part of a magnetic member and includes: a base portion including a mother material containing a ferrite phase; and a nonmagnetic portion having an austenite phase that is formed by solid solution of nitrogen (N) into a part of the mother material, the nonmagnetic portion having saturated magnetization less than that of the base portion. The nonmagnetic portion can be obtained by irradiating a high energy beam to a surface portion of stainless steel or the like while relatively moving the beam. This beam is near-ultraviolet nanosecond pulse laser having a short wavelength within a near-ultraviolet range and a pulse width of 10 ps to 100 ns. By adjusting the amount of N introduced and to form a solid solution due to the modification process, the nonmagnetization ratio of the member can be controlled.
Claims
1. A composite magnetic member comprising: a base portion comprising a mother material that contains a ferrite phase; and a nonmagnetic portion having an austenite phase wherein the nonmagnetic portion is formed by irradiating, in a nitrogen-containing atmosphere, laser light to a part of the mother material so that particles of the mother material are released from the irradiated part of the mother material due to ablation, where the released particles along with nitrogen from the nitrogen-containing atmosphere form a solid solution of nitrogen (N) that fills the part of the mother material that was ablated, the nonmagnetic portion having saturated magnetization smaller than that of the base portion, and the nonmagnetic portion has a width of 1 mm or less, the width being a length in a direction orthogonal to a longitudinal direction.
2. The composite magnetic member as recited in claim 1, wherein the nonmagnetic portion contains 0.2 mass % or more of N when whole of the nonmagnetic portion is 100 mass %.
3. The composite magnetic member as recited in claim 1, wherein the nonmagnetic portion has an austenitization ratio of 30 vol % or more, wherein the austenitization ratio is a ratio of the austenite phase to whole metallic structure of the nonmagnetic portion.
4. The composite magnetic member as recited in claim 1, wherein the nonmagnetic portion has a nonmagnetization ratio (phi) of 20% or more, wherein the nonmagnetization ratio (phi) is defined as:
(phi)=100(B0B1)/B0 where B0 represents a saturated magnetization of the base portion and B1 represents a saturated magnetization of the nonmagnetic portion.
5. The composite magnetic member as recited in claim 1, wherein the mother material is an iron alloy that contains 0.1 mass % or more of chromium (Cr) when whole of the mother material is 100 mass %.
6. The composite magnetic member as recited in claim 1, wherein the nonmagnetic portion has a depth from an outermost surface of 10 micrometers or more, the depth of the nonmagnetic portion being a length from the outermost surface to the deepest part at which the N amount is larger than that of the base portion.
7. A method of manufacturing a composite magnetic member, the method comprising an irradiation step of irradiating a high energy beam of a laser to a target portion in an atmosphere containing nitrogen while relatively moving the high energy beam so that particles are released from the target portion due to ablation, thereby to mix the released particles and the nitrogen in the atmosphere to form a solid solution of nitrogen (N), the target portion being a part of a mother material that contains a ferrite phase, wherein a nonmagnetic portion as recited is formed in the target portion; wherein the nonmagnetic portion is formed by the released particles along with nitrogen from the nitrogen-containing atmosphere forming a solid solution that fills the part of the mother material that was ablated, the nonmagnetic portion having saturated magnetization smaller than that of the base portion, and the nonmagnetic portion has a width of 1 mm or less, the width being a length in a direction orthogonal to a longitudinal direction.
Description
BRIEF DESCRIPTION OF DRAWINGS
(1)
(2)
(3)
(4)
DESCRIPTION OF EMBODIMENTS
(5) The contents described herein may be applied not only to the composite magnetic member of the present invention but also to a method of manufacturing the same. One or more features freely selected from the description herein may be added to the above-described features of the present invention. Here, features regarding the manufacturing method, when understood as product-by-process, may also be features regarding a product. Which embodiment is the best or not is different in accordance with objectives, required performance and other factors.
(6) <<Mother Material>>
(7) The mother material according to the present invention comprises pure iron or iron alloy that forms a gamma phase in which the introduced nitrogen forms a solid solution. The iron alloy may take a variety of possible compositions, but may preferably be an iron alloy that contains at least chrome (Cr). When Cr is contained in the mother material, N can readily form a solid solution so that the alpha phase transforms stably to the gamma phase. Unduly small amount of Cr in the mother material may make the effect poor. Therefore, when the whole of the mother material is 100 mass %, it is preferred that the content of Cr is 0.1 mass % (which may simply be represented by %) or more in an embodiment, 0.3% or more in another embodiment, 0.5% or more in still another embodiment, and 0.8% or more in a further embodiment. It is also preferred that the content of Cr is 8% or more in an embodiment, 10% or more in another embodiment, and 12% or more in a further embodiment, because in such a case a composite magnetic member having excellent corrosion resistance can be obtained. The upper limit of the content of Cr may ordinarily be, but is not limited to, 30% or less in an embodiment, and 20% or less in another embodiment. Examples of such a Cr-containing iron alloy include carbon steel (such as JIS SCM steel and SCr steel) and stainless steel. The stainless steel to be the mother material according to the present invention may be enough if it is other than an austenite-based stainless steel which is entirely nonmagnetic. Ferrite-based stainless steel is particularly preferred.
(8) <<Manufacturing Method>>
(9) (1) High Energy Beam
(10) The type of the high energy beam is not limited as long as the high energy beam causes ablation at the target portion of the mother material to form a reaction field in which the released particles generated by the ablation and nitrogen in the atmosphere are mixed together. Examples of the high energy beam include pulse laser and electron beam.
(11) To generate ablation, the target portion of the mother material may have to be imparted with a high energy at a moment. In other words, the target portion of the mother material need be exposed to a high energy beam that has a higher energy density (fluence) than an ablation threshold. Pulse laser having a short pulse width may be preferred as such a high energy beam.
(12) When the operating conditions, such as output power and oscillating frequency, of a laser oscillator are fixed, laser light having a higher fluence can be irradiated to the target portion as the pulse width decreases. In addition, as the pulse width decreases, thermal diffusion to outside of the irradiated area is suppressed and it is possible to promote the ablation and suppress the thermal influence to the mother material. Specifically, it is preferred that the pulse width of the pulse laser is 10 ps to 100 ns in an embodiment, and 1 to 50 ns in another embodiment, for example. If the pulse width is unduly large, it will be difficult to obtain a fluence necessary for ablation, while if the pulse width is unduly small (e.g., 150 fs at which multiphoton absorption occurs), the reaction field necessary for the modification process according to the present invention may not be generated because the energy imparting form by laser will vary.
(13) It is preferred that the output density (fluence) of the pulse laser is 0.3 MW/cm.sup.2 to 30 GW/cm.sup.2 in an embodiment, and 3 MW/cm.sup.2 to 3 GW/cm.sup.2 in another embodiment, for example. The output density affects the depth of the nonmagnetic portion. A small output density causes the nonmagnetic portion to be shallow, while a large output density has a significant thermal influence to the mother material. Note that the output density can be obtained by dividing the laser output by the laser spot area.
(14) As the wavelength of the pulse laser decreases, the absorptivity of laser light by the mother material increases to promote the ablation and suppress the deterioration or the like of the non-ablation portion. The wavelength of the pulse laser may be appropriately adjusted thereby to allow the nonmagnetic portion to readily be formed with a sufficient depth. It is preferred that such a wavelength of the pulse laser is shorter than an infrared range in an embodiment, and within an ultraviolet range (including near-ultraviolet range), which is shorter than a visible range, in another embodiment. Specifically, it is preferred that the wavelength of the pulse laser is 700 nm or less in an embodiment, 550 nm or less in another embodiment, and 380 nm or less in a further embodiment. It is also preferred that the wavelength of the pulse laser is 190 nm or more in an embodiment, and 320 nm or more in another embodiment. If the wavelength of the pulse laser is unduly short, absorption of laser by the atmosphere gas will occur, which may be undesirable.
(15) Specific examples of such pulse laser include: excimer laser which utilizes excimer (excited dimer), such as F.sub.2 (wavelength of 157 nm), ArF (wavelength of 193 nm), KrF (wavelength of 248 nm), XeCl (wavelength of 308 nm) and XeF (wavelength of 351 nm); and YAG laser which can oscillate at a short wavelength.
(16) (2) Irradiation Step
(17) The irradiation step is a step of irradiating the high energy beam to the surface portion of the mother material in accordance with a desired form of the nonmagnetic portion while moving the irradiated area.
(18) When pulse laser is used as the high energy beam, a continuous nonmagnetic portion can readily be formed through partially superposing (overlapping) the irradiated areas by pulse light beams that oscillate contiguously. The ratio of superposing the irradiated areas by the pulse waves (pulse lap ratio) may be adjusted such as by the oscillating frequency of the pulse laser, the relative movement speed to the target portion (which may be referred to as a scanning speed), and the size of the irradiated area at the outermost surface of the target portion (or the focal position of the pulse laser). Depending also on the characteristics of the pulse laser, the pulse lap ratio may preferably be 10% or more and less than 100% in an embodiment, and 20% to 95% in another embodiment, for example. Unduly small pulse lap ratio makes it difficult to form a continuous nonmagnetic portion. Unduly large pulse lap ratio makes it difficult to efficiently perform the modification process and form a uniform nonmagnetic portion.
(19) The pulse lap ratio is calculated as (r/d)100(%), where d represents the beam diameter and r represents an overlapping diameter of contiguous pulse waves. Here, the beam diameter (d) is represented by a width (diameter) that is measured on an orthogonal plane to the laser axis when the beam intensity is at 1/e.sup.2 level relative to the peak intensity value. The overlapping diameter (r) of contiguous pulse waves is represented by dR, where R is a distance between the centers of contiguous beams.
(20) Conditions such as oscillating frequency, scanning speed and focal position may be adjusted on the basis of the pulse lap ratio. Exemplary conditions are mentioned as below. The oscillating frequency may preferably be 1 to 500 kHz in an embodiment, and 2 to 100 kHz in another embodiment, for example. If the oscillating frequency is unduly low, the scanning speed may have to be reduced and the process cannot be efficiently performed. If the oscillating frequency is unduly high, the laser fluence will be reduced in general, and it may be difficult to form a uniform nonmagnetic portion.
(21) The scanning speed may preferably be 0.1 to 5,000 mm/s in an embodiment, and 1 to 1,000 mm/s in another embodiment, for example. If the scanning speed is unduly low, the process cannot be efficiently performed, while if the scanning speed is unduly high, it may be difficult to form a uniform nonmagnetic portion as with the case in which the correlative oscillating frequency is unduly high.
(22) The irradiated range by each pulse light beam varies depending on the focal position of the pulse laser. The focal position may be located on the outermost surface of the target portion of the mother material, or may also be shifted from the outermost surface. However, as the focal position deviates from the irradiated part by the pulse laser (outermost surface part of the target portion), the output density at the irradiated part decreases to affect the stability of the process in the vicinity of the irradiated part and the depth of the nonmagnetic portion, etc. This tendency is remarkable when the laser is converged to form a fine spot diameter on the irradiated part.
(23) (3) Atmosphere
(24) As previously described, the atmosphere in which the irradiation step is carried out may be a nitrogen-containing atmosphere that allows active nitrogen to be generated due to ablation when the high energy beam is irradiated. Such an atmosphere may be appropriately selected depending on the type of the high energy beam.
(25) The irradiation step may be carried out in a closed atmosphere such as in a chamber, but may also be carried out in an open atmosphere. When laser is used as the high energy beam, the irradiation step is possible even in the air atmosphere of ordinary temperature and ordinary pressure which is an open atmosphere. However, in order to control the amount of nitrogen to form the solid solution while avoiding generation or the like of unnecessary compounds, the irradiation step may preferably be carried out in a nitrogen gas atmosphere or in a mixture gas atmosphere obtained by diluting nitrogen gas with inert gas. Specifically, it is preferred to blow nitrogen gas or the like from above the target portion or from the side of the target portion. The blowing direction of the gas may be adjusted such as for the purpose of suppression of debris caused from the ablation. For example, the blowing direction may be set coaxially with the optical axis of the high energy beam thereby to improve the controllability of the nitrogen-containing atmosphere and uniformity of the nonmagnetic portion.
(26) <<Intended Use>>
(27) The composite magnetic member according to the present invention can be utilized in a variety of electromagnetic devices. For example, the composite magnetic member according to the present invention may preferably be a component that constitutes a magnetic circuit, such as in a motor, actuator (electromagnetic valve, electromagnetic rod, etc.), magnetic sensor, memory, marker, and generator.
(28) When the composite magnetic member according to the present invention operates in a high frequency magnetic field (e.g., 1 kHz to 1 MHz), it is preferred that the nonmagnetic portion is formed in the vicinity of the outermost surface (e.g., with a depth of 0.1 to 1 mm). In consideration of the skin effect, the nonmagnetic portion can exert sufficient effects such as shielding effect even with a shallow (thin) form.
EXAMPLES
First Example
(29) Preparation of Sample
(30) (1) Sample Material (Mother Material)
(31) A plurality of sample materials (15.76.510.0 mm) were prepared by being cut out from commercially available ferrite-based stainless steel (JIS SUS430).
(32) (2) Irradiation Step (Nonmagnetization Process, Nitriding Process)
(33) The high energy beam was prepared as pulse laser having a wavelength within a near-ultraviolet range and a pulse width of nanosecond level (this laser will be referred simply to as near-ultraviolet nanosecond laser). This laser was used and irradiated to the target portion of each sample material while nitrogen-containing gas was blown to the target portion. Irradiation conditions were as follows: wavelength of 355 nm; pulse width of <20 ns; output of 0.6 W (output density of 150 MW/cm.sup.2); and focal position on the outermost surface of the target portion of the sample material (defocus distance of 0 micrometers, i.e., just focused). The irradiation conditions were finely tuned for each sample material.
(34) Blowing the gas to the target portion was performed from above along the optical axis of the near-ultraviolet nanosecond laser. During this operation, mixture gas obtained by diluting nitrogen gas with argon gas (diluent gas) was used. The concentration of nitrogen to be introduced into the sample material (amount of N to form a solid solution) was adjusted by appropriately varying the nitrogen concentration in the gas.
(35) The laser irradiation was performed such that the pulse lap ratio calculated by the previously-described method was to be 85% and the trace of the irradiated area of each laser light beam was to form parallel multiple straight lines at an interval of 3 to 7 micrometers on the surface of the target portion. This was to allow the target portion to be modified across the whole surface due to the laser irradiation. Each sample was thus obtained as listed in Table 1. A part of the samples was to remain as a sample material for comparison without performing the nitriding process.
(36) Analysis of Target Portion
(37) (1) EPMA
(38) The target portion of each of samples except for Sample C2 was analyzed using an electron probe microanalyzer (EPMA). The N concentration (amount of N to form a solid solution) in each target portion obtained through the analysis is also listed in Table 1.
(39) (2) XRD
(40) The target portion of each sample (specifically a part located at a depth of 10 micrometers from the outermost surface) was analyzed using an XRD (FeK-alpha radiation source).
(41) In addition, the fcc (gamma phase) peak and the bcc (alpha phase) peak appearing in the X-ray diffraction profile of each sample were used to quantify the ratio of the gamma phase (fcc transformation ratio) in the target portion of each sample. This calculation of the fcc transformation ratio was performed using the Rietvelt method. Specifically, the fcc transformation ratio was calculated using Rietvelt analysis software: RIETAN-FP on the assumption of a 2-phase mixture model of alpha and gamma phases. For this calculation, an extended and divided pseudo-Voigt function was used as the fitting function. The fcc transformation ratio thus obtained of each sample is also listed in Table 1.
(42) (3) Saturated Magnetization
(43) Saturated magnetization (B1) of the target portion of each sample was measured using a VSM. Saturated magnetization (B0) of Sample C2 was also measured in the same manner. The nonmagnetization ratio ((phi)=100(B0B1)/B0) calculated for each sample is also listed in Table 1.
(44) Evaluation
(45) (1) As understood from
(46) Referring also to the X-ray diffraction profiles shown in
(47) As apparent from
(48) (2) As understood from
(49) Referring also to
Second Example
(50) (1) Preparation of Sample
(51) As substitute for the stainless steel used in the first example, three types of sample materials were prepared each comprising an FeCr binary alloy of a different Cr amount. For each sample material, the irradiation step was carried out as with the case of the first example to perform the nitriding process for the target portion, and samples were thus obtained. The composition of each sample material was 0.5%, 1.1% or 14% of Cr and the balance of Fe when the whole of the mother material was 100 mass %.
(52) (2) Analysis/Evaluation of Target Portion
(53) The target portion of each sample was analyzed as with the case of the first example. In all of the samples, the N concentration was (1.30.2) mass % and the fcc transformation ratio was >95%. It has also been confirmed from the XRD profiles that the N in the target portion was in a state of forming a solid solution.
(54) When the fcc transformation ratio is close to 100%, the fitting necessary for the Rietvelt analysis may be difficult, and highly accurate calculation of the fcc transformation ratio is not easy. In the present description, therefore, when the bcc peak is at a noise level and only the fcc peak is observed, the fcc transformation ratio is represented as >95% even if the fcc transformation ratio is substantially 100%. In any case, it has been found that the above-described nitriding process allows almost 100% of the target portion to be austenitized in the stainless steel as well as in a mother material of a low concentration of Cr.
(55) [Supplementation]
(56) The target portion treated with the nitriding process through the above-described laser irradiation is not only austenitized or made nonmagnetic by solid solution of nitrogen but also provided with a structure (nitrogen solid solution fine structure) comprising fine crystal grains. Specifically, the average crystal grain diameter can be 10 micrometers or less in an embodiment, 5 micrometers or less in another embodiment, and 1 micrometer or less in a further embodiment, for example. The lower limit of the average crystal grain diameter is not limited, but may be 50 nm or more or 100 nm or more, for example.
(57) The average crystal grain diameter as referred to herein may be specified as follows. First, the cross-sectional structure of the target portion is observed using an electron microscope (TEM). On the assumption that the cross-sectional shape of the observed grain is ellipsoidal, an average value of the long axis (longest) and the short axis (shortest) is determined as one crystal grain diameter. For 5 points randomly sampled within the observed structure cross-section, the crystal grain diameters are in turn calculated to obtain a simple average (arithmetic average), which is determined as the average crystal grain diameter.
(58) Specifically, when the above-described nitriding process was performed for a Cr-free carbon steel (JIS S45C) and a Cr-containing carbon steel (JIS SUS304: 18 mass % of Cr), for example, the N concentration was over 0.9% and the average crystal grain diameter was less than 1 micrometer in both cases. Note that the average crystal grain diameter of an ordinary FeCr alloy not treated with the above-described nitriding process is about several tens of micrometers.
(59) Thus, the target portion (nonmagnetic portion) according to the present invention is not only simply made nonmagnetic due to the solid solution of nitrogen but has a fine structure and can be uniform. According to the present invention, therefore, there can be obtained a composite magnetic member having a nonmagnetic portion that is uniformly made nonmagnetic in a desired form, regardless of whether the target portion (nonmagnetic portion) is wide or narrow and whether Cr is contained or not. As will be understood, such a nonmagnetic portion can be treated with a thermal process thereby to adjust the average crystal grain diameter (coarsen to several to several tens of micrometers).
(60) TABLE-US-00001 TABLE 1 Nitrogen fcc transformation Nonmagnetization Sample concentration ratio ratio No. (mass %) (vol %) (%) 1 0.9 >95 >98 2 0.6 79 53 C1 0.1 22 0 C2 0 0 (not modified) (reference)