TECHNICAL FIELD
[0001] The present disclosure relates to a current transformer core and a manufacturing
method thereof. The present disclosure also relates to a device which includes the
current transformer core.
BACKGROUND ART
[0002] Current transformers (CT) are current transforming devices for use in measurement
and are used in, for example, current meters and earth leakage circuit breakers. The
current transformers have a soft magnetic material core (magnetic core) which is used
for a closed magnetic circuit. Patent Document 1 discloses that, as this current transformer
core, a core formed of a ribbon of a Fe-based nanocrystalline alloy is preferred.
The Fe-based nanocrystalline alloy exhibits a higher saturation magnetic flux density
than Permalloy and Co-based amorphous alloys and has a higher magnetic permeability
than Fe-based amorphous alloys.
[0003] Typical compositions of the Fe-based nanocrystalline alloy are disclosed in, for
example, Patent Document 2 and Patent Document 3. A typical example of the manufacturing
method of a core with the use of a Fe-based nanocrystalline alloy includes the steps
of: quenching a melt of material alloy which has a desired composition, thereby producing
an amorphous alloy ribbon; winding this amorphous alloy ribbon into a ring-shaped
core element; and performing a heat treatment so as to crystallize the amorphous alloy
ribbon, thereby obtaining a core which has a nanocrystalline organization.
[0004] Patent Document 4 discloses a magnetic core which is formed by winding a steel ribbon
of a Fe-based nanocrystalline alloy, whose magnetic permeability is greater than 12,000
and smaller than 350,000, of which the ratio of the saturation magnetic flux density
Bs and the residual magnetic flux density Br (Br/Bs) is small, and of which the temperature
dependence of the magnetic permeability is small.
[0005] In this specification, a ring-shaped structure formed of a Fe-based alloy ribbon
on which a heat treatment in a longitudinal magnetic field is not yet finished is
referred to as "core element". This is sometimes strictly distinguished from the "core"
that is formed of a Fe-based nanocrystalline alloy ribbon on which the heat treatment
has been finished.
CITATION LIST
PATENT LITERATURE
[0006]
Patent Document 1: Japanese Patent No. 2501860
Patent Document 2: Japanese Examined Patent Publication No. 4-4393
Patent Document 3: Japanese Examined Patent Publication No. 7-74419
Patent Document 4: Japanese PCT National Phase Laid-Open Publication No. 2002-530854
SUMMARY OF INVENTION
TECHNICAL PROBLEM
[0007] As for the above-described current transformer, further improvement in magnetic permeability
of the core has been demanded for the purpose of size reduction and cost reduction
in a device such as a current meter. This is because improvement in magnetic permeability
of the core not only leads to higher sensitivity to an electric current to be measured
but also enables core size reduction and reduction in the number of turns of a coil
around the core.
[0008] A conventional solution for improvement in magnetic permeability of the Fe-based
nanocrystalline alloy is to apply a magnetic field in a magnetic path direction of
the core element in the step of crystallization by a heat treatment. However, the
core produced in such a way has such a problem that a magnetic deviation is likely
to occur due to a large residual magnetic flux density Br. If the core has a magnetic
deviation, the magnetic permeability at the point of operation decreases so that characteristics
demanded of the current transformer cannot be obtained.
[0009] To adapt itself to variations in the device environment such as the use temperature,
the current transformer also needs to have such an excellent temperature characteristic
that the high magnetic permeability of the core exhibits a small variation within
the use temperature range.
[0010] Embodiments of the present disclosure provide a current transformer core which realizes
the characteristics that are necessary in, for example, uses for sensing of electrical
leakage, a manufacturing method of the core, and a device which includes the core.
SOLUTION TO PROBLEM
[0011] A current transformer core of the present disclosure is a current transformer core
formed by winding or layering a soft magnetic material layer, wherein
the soft magnetic material layer is formed of a Fe-based nanocrystalline alloy ribbon
whose thickness is not more than 15 µm,
[0012] Δµr(100-0) is not more than 0.5 where Δµr(100-0) is |µr(100)-µr(0)|/µr(0), and µr(T)
is an amplitude magnetic permeability of the core measured at a temperature T (°C)
in the presence of an applied AC magnetic field of frequency f=50 Hz and amplitude
H=1.0 A/m, and
the ratio of a residual magnetic flux density Br and a saturation magnetic flux density
Bm, Br/Bm, is less than 0.9 where a magnetic flux density B(80) with magnetic field
H=80 A/m is defined as the saturation magnetic flux density Bm.
[0013] In one embodiment, µr(25) has a value between 0.4×µr(max)(25) and 0.9×µr(max)(25)
where µr(max)(T) is µr(T) achieved by heating a core element to not less than a crystallizing
temperature in the presence of a magnetic field of not less than 100 A/m applied in
a magnetic path direction (longitudinal-field heat treatment), the core element being
formed by shaping a Fe-based amorphous alloy ribbon which has a substantially identical
composition and shape to those of the Fe-based nanocrystalline alloy ribbon so as
to have a substantially identical shape to that of the core.
[0014] In one embodiment, µr(25)≥4×10
5 holds true.
[0015] In one embodiment, µr(100)-µr(0) has a positive value.
[0016] A manufacturing method of a current transformer core according to the present disclosure
includes:
the step of providing a core element formed by winding or layering a Fe-based amorphous
alloy ribbon whose thickness is not more than 15 µm and which can be converted into
nanocrystals;
a longitudinal-field heat treatment step which includes heating the core element to
not less than a crystallizing temperature in the presence of a magnetic field of not
less than 100 A/m applied in a magnetic path direction of the core element, thereby
forming a core; and
a transverse-field heat treatment step which includes, after the longitudinal-field
heat treatment step, heating the core to a temperature less than the crystallizing
temperature in the presence of a magnetic field applied in a direction perpendicular
to the magnetic path direction of the core, thereby forming a current transformer
core,
wherein µr(25) is adjusted by the transverse-field heat treatment step to a value
between 0.4×µr(max)(25) and 0.9×µr(max) (25) where µr(max) (T) is µr(T) achieved by
the longitudinal-field heat treatment step, and µr(T) is an amplitude magnetic permeability
of the core measured at a temperature T (°C) in the presence of an AC magnetic field
of frequency f=50 Hz and amplitude H=1.0 A/m.
[0017] In one embodiment, Δµr(100-0) is not more than 0.5 where Δµr(100-0) is |µr(100)-µr(0)|
|/µr(0) of a manufactured current transformer core.
[0018] A device according to the present disclosure includes: the current transformer core
as set forth in any of the foregoing paragraphs; a coil provided around the current
transformer core; and a sensing circuit coupled with the coil.
ADVANTAGEOUS EFFECTS OF INVENTION
[0019] According to the present disclosure, it is possible to provide a current transformer
core which is formed of a Fe-based nanocrystalline alloy layer that has high magnetic
permeability but is unlikely to undergo a magnetic deviation, and has an excellent
temperature characteristic.
BRIEF DESCRIPTION OF DRAWINGS
[0020]
FIG. 1 is a diagram showing the configuration of a measurement system used in measurement
of the magnetic permeability.
FIG. 2A is a graph illustrating the relationship between the temperature of a longitudinal-field
heat treatment and the magnetic permeability µr(25) of the core in the case where
a core element was formed by winding a Fe-based amorphous alloy ribbon (thickness:
18 µm) which had the composition of Fe74Cu1Nb3Si15.5B6.5.
FIG. 2B is a graph illustrating the relationship between the temperature of a longitudinal-field
heat treatment and the magnetic permeability µr(25) of the core in the case where
a core element was formed by winding a Fe-based amorphous alloy ribbon (thickness:
13 µm) which had the composition of Fe74Cu1Nb3Si15.5B6.5.
FIG. 3 is a graph illustrating the relationship between a longitudinal magnetic field during
the process of a longitudinal-field heat treatment and the magnetic permeability µr(25)
of the core in the case where a core element was formed by winding a Fe-based amorphous
alloy (thickness: 13 µm) which had the composition of Fe74Cu1Nb3Si15.5B6.5.
FIG. 4 is a graph illustrating the temperature characteristic of the magnetic permeability
µr(T) of the core for Sample A where the longitudinal magnetic field illustrated in
FIG. 3 was 19 A/m and Sample B where the longitudinal magnetic field was 230 A/m.
FIG. 5 is a graph illustrating an example of the profiles of the temperature and the magnetic
field intensity of a transverse-field heat treatment in the present embodiment.
FIG. 6 is a graph illustrating B-H curves of respective samples obtained when the duration
for which the heat treatment temperature was retained at 400°C (retention time) was
set to 60 minutes, 90 minutes and 120 minutes among the profiles illustrated in FIG.
5, and B-H curves of a sample before a transverse-field heat treatment.
FIG. 7 is a graph illustrating the magnetic permeability of respective samples obtained
when the duration for which the heat treatment temperature was retained at 400°C (retention
time) was set to 60 minutes, 90 minutes and 120 minutes among the profiles illustrated
in FIG. 5.
FIG. 8 is a graph illustrating the measurement temperature dependence of the magnetic permeability
for one of the samples illustrated in FIG. 7 where the duration for which the heat treatment temperature was retained at 400°C
(retention time) was set to 90 minutes.
FIG. 9 is a graph illustrating the relationship between the magnetic field intensity in
a transverse-field heat treatment and the magnetic permeability µr(25).
FIG. 10 is a flowchart illustrating an example of the manufacturing method of a current transformer
core according to the present disclosure.
FIG. 11A is a perspective view showing an example of the basic structure of a current transformer
100 to which the present disclosure is applicable.
FIG. 11B is a perspective view showing an example where the current transformer 100 is applied to a zero-phase current transformer.
FIG. 12 is a diagram showing a circuit configuration example of an earth leakage circuit
breaker 20 which includes the current transformer 100 shown in FIG. 11B.
DESCRIPTION OF EMBODIMENTS
[0021] Hereinafter, an embodiment of the present disclosure is described in detail with
reference to the drawings. Note that, however, excessively detailed descriptions are
sometimes omitted. For example, well-known matter in the art and descriptions of substantially
equal elements are sometimes omitted. This is for the sake of avoiding the following
descriptions from being unnecessarily redundant and assisting one skilled in the art
to easily understand the descriptions. Note that the present inventor provides the
attached drawings and the following descriptions for the purpose of assisting one
skilled in the art to sufficiently understand the present disclosure. However, the
present inventor does not intend that these drawings and descriptions limit the subject
matter recited in the claims.
(Embodiment)
< Current transformer core >
[0022] The current transformer core of the present embodiment is a current transformer core
formed by winding or layering a soft magnetic material layer. The current transformer
core can be realized by winding a ribbon-like soft magnetic material layer or layering
a plurality of rings punched out from the soft magnetic material layer. The soft magnetic
material layer which is a part of the current transformer core of the present embodiment
is formed of a Fe-based nanocrystalline alloy ribbon whose thickness is in the range
of not less than 8 µm and not more than 15 µm (typically about 13 µm). As will be
described later, it was found from experiments conducted by the present inventor that
the thickness of the Fe-based nanocrystalline alloy ribbon is a significant factor
which strongly influences the characteristics of the current transformer core for
use in sensing of electrical leakage.
< Fe-based nanocrystalline alloy ribbon >
[0023] A Fe-based nanocrystalline alloy used in the current transformer core of the present
embodiment is basically produced by a method which includes the step of quenching
a molten alloy, thereby obtaining an amorphous alloy ribbon which has a predetermined
composition, and the heat treatment step of heating this amorphous alloy ribbon so
as to form nanocrystalline grains. It has been known from the results of analysis
by X-ray diffraction and a transmission electron microscope that the nanocrystalline
grains are Fe in a body-centered cubic structure in which Si or the like is incorporated
such that a solid solution is formed. At least 80 volume% of the alloy is occupied
by nanocrystalline grains whose average grain diameter measured at the maximum dimension
is not more than 100 nm. The other part of the alloy than the nanocrystalline grains
is mainly amorphous. The proportion of the nanocrystalline grains may be substantially
100 volume%.
[0024] The composition of the Fe-based nanocrystalline alloy used in the embodiment of the
present disclosure is represented by the following formula:
FORMULA: (Fe
1-aMa)
100-x-y-z-α-β-γCu
xSi
yB
zM'
αM"
βX
γ (atom%)
[0025] Here, M is Co and/or Ni. M' is at least one element selected from the group consisting
of Nb, W, Ta, Zr, Hf, Ti and Mo. M" is at least one element selected from the group
consisting of V, Cr, Mn, Al, platinum-group elements, Sc, Y, rare earth elements,
Au, Zn, Sn and Re. X is at least one element selected from the group consisting of
C, Ge, P, Ga, Sb, In, As and Be.
[0027] The Fe-based nanocrystalline alloy used in the embodiment of the present disclosure
contains Cu in a proportion of 0.1 to 3 atom%. If Cu is smaller than 0.1 atom%, the
effect of decreasing the core loss and the effect of increasing the magnetic permeability,
which are caused by addition of Cu, are rarely achieved. On the other hand, if Cu
is greater than 3 atom%, there is a probability that the core loss is rather larger
than that which occurs in an alloy to which Cu is not added. Also, the magnetic permeability
deteriorates. In the present disclosure, the particularly preferred content x of Cu
is 0.5 to 2 atom%. Within this range, the core loss is particularly small.
[0028] The causes of decrease of the core loss and increase of the magnetic permeability
by addition of Cu are not elucidated but can be estimated as follows. The interaction
parameter between Cu and Fe is positive, so that the solid solubility is low and Cu
and Fe have a tendency to separate. Therefore, if an alloy in an amorphous state is
heated, Fe atoms or Cu atoms gather together to form a cluster, so that composition
fluctuations occur. Therefore, a large number of local regions are produced which
are likely to undergo crystallization, and these regions serve as cores for generation
of nanocrystalline grains. The major constituent of this crystal is Fe, and Cu is
rarely incorporated so that a solid solution is not formed. Therefore, by crystallization,
Cu is purged from the nanocrystalline grains so that the concentration of Cu increases
in a region surrounding the crystal grains. Thus, it is estimated that the crystal
grains are difficult to grow.
[0029] It is estimated that the effect of reducing the size of crystal grains which is achieved
by addition of Cu is particularly improved by the presence of Nb, Ta, W, Mo, Zr, Hf,
Ti or the like. If Nb, Ta, W, Mo, Zr, Hf, Ti or the like is not present, the size
of crystal grains is not reduced so much. The effect of accelerating the size reduction
is particularly large in the cases of Nb, Ta, Zr, Hf, and Mo. Of these elements, particularly
when Nb is added, an alloy is obtained whose crystal grain size is likely to be reduced
and which also has excellent soft magnetic properties. When Nb is added, a nanocrystalline
phase is produced whose major constituent is Fe. Accordingly, magnetostriction is
small as compared with Fe-based amorphous alloys, and the magnetic anisotropy that
is attributed to the internal stress-strain decreases. These phenomena are estimated
to be ones of the reasons that the soft magnetic properties are improved. These elements
are contained in the range of 0.1 to 5 atom%, preferably in the range of 2 to 5 atom%.
If it is less than 0.1 atom%, there is a probability that the size reduction of the
crystal grains is insufficient. If it exceeds 5 atom%, the decrease of the saturation
magnetic flux density is large.
[0030] Si and B are elements which are particularly useful in reducing the size of crystal
grains of the Fe-based nanocrystalline alloy. The Fe-based nanocrystalline alloy is
obtained by, for example, after an amorphous alloy is obtained by the effect of addition
of Si and B, performing a heat treatment so as to form nanocrystalline grains. The
content of Si is in the range of 10 to 20 atom%. A preferred content of Si is in the
range of 14 to 20 atom%. If the content of Si is less than 10 atom%, the amorphous
formability of the alloy is low, so that it is difficult to stably produce amorphous
matter. Further, decrease of the crystalline magnetic anisotropy of the alloy is insufficient,
and therefore, it is difficult to achieve excellent soft magnetic properties (e.g.,
low coercivity). If the content of Si exceeds 20 atom%, decrease of the saturation
magnetic flux density of the alloy is large, and the resultant alloy is likely to
embrittle. Note that the content of B is in the range of 5 to 10 atom%. B is an element
indispensable for formation of amorphous matter. If the content of B is less than
5 atom%, the amorphous formability is low, so that it is difficult to stably produce
amorphous matter. If the content of B exceeds 10 atom%, decrease of the saturation
magnetic flux density is large. A still preferred content of B is not more than 7
atom%. If the contents of Si and B are excessively large, the saturation magnetic
flux density of the alloy markedly decreases.
[0031] The Fe-based nanocrystalline alloy may contain at least one element selected from
the group consisting of C, Ge, P, Ga, Sb, In, Be and As in a proportion of not more
than 10 atom%. These elements are useful in conversion to amorphous matter in formation
of an amorphous alloy ribbon. When added together with Si and B, these elements assist
the conversion to amorphous matter and provide the effect of adjusting the magnetostriction
and the Curie temperature.
[0032] Elements such as V, Cr, Mn, Al, platinum-group elements, Sc, Y, rare earth elements,
Au, Zn, Sn, Re and the like have the effect of improving the anticorrosiveness, the
effect of improving the magnetic properties, and the effect of adjusting the magnetostriction.
The content of such elements is not more than 10 atom% at the highest. If the content
exceeds 10 atom%, the saturation magnetic flux density markedly decreases. A particularly
preferred content of these elements is not more than 8 atom%. Of these elements, when
at least one element selected from the group consisting of Ru, Rh, Pd, Os, Ir, Pt,
Au, Cr and V is added, the resultant core has particularly excellent anticorrosiveness.
[0033] The major constituent of the remaining part, exclusive of impurities, is substantially
Fe. Part of Fe can be substituted with Co and/or Ni. The content of M (Co and/or Ni)
in the above formula, a, is 0≤a<0.5. If a exceeds 0.3, there is a probability that
the core loss increases. Therefore, preferably 0≤a≤0.3. Here, to achieve high magnetic
permeability, a=0 is preferred.
[0034] Next, an embodiment of the manufacturing method of the current transformer core according
to the present disclosure is described.
[0035] First, an amorphous alloy ribbon, which is to be a soft magnetic material layer,
is formed from a molten alloy which has the above-described composition by a known
liquid quenching method (rapid quenching method) such as single-roll method, double-roll
method, and the like. In the present disclosure, the thickness of the amorphous alloy
ribbon is not more than 15 µm. The lower limit of the thickness can be set to, for
example, 8 µm from the viewpoint of mass production. The peripheral velocity of a
cooling roll can be set to, for example, about 15 to 50 m/sec. The cooling roll can
be made of pure copper that has excellent thermal conductivity or a copper alloy such
as Cu-Be, Cu-Cr, Cu-Zr and Cu-Zr-Cr. In the case of mass production, the cooling roll
can be water-cooled. In formation of the amorphous alloy ribbon, the temperature variation
of the roll is kept small because formation of the amorphous organization of the alloy
can sometimes differ depending on the cooling rate. Note that the thickness of the
amorphous alloy ribbon, t, is a value obtained by a weight conversion method. For
example, the weight M of a sample of 2 m (longitudinal direction)×50 mm (width direction)
is measured from a long amorphous alloy ribbon, and the density d [kg/m
3] is determined by dry density measurement (e.g., measurement with an AccuPyc II 1340
series product manufactured by SHIMADZU CORPORATION) according to a constant volume
expansion method. With the weight M and the density d, thickness t[m]=M/((2×50
-3)×d) can be calculated.
[0036] The length of an amorphous alloy ribbon industrially manufactured by the liquid quenching
method exceeds several kilometers. As such, in a casting process which lasts a long
time, it is important to maintain a sufficient cooling capacity immediately after
ejection of a molten alloy to the cooling roll. That is, due to the sufficient cooling
capacity, an alloy of an amorphous organization can be stably obtained. As for the
thickness of the alloy ribbon to be manufactured, it is estimated that, as the thickness
decreases, cooling is easier and amorphous matter is stably obtained. However, according
to research conducted by the present inventor, it was found that when the alloy ribbon
thickness is not more than 15 µm, high magnetic permeability is stably achieved in
a manufactured core. The reasons for this are not elucidated but can be estimated
as follows. Due to the reduced thickness of the alloy ribbon, an amorphous organization
is obtained extremely stably, and furthermore, in generation of a nanocrystallized
organization by a heat treatment, the crystal grain diameter of the organization is
generally uniform and very small.
[0037] The process of producing an amorphous alloy by the liquid quenching method can be
carried out in air when this alloy does not include an active metal. When the alloy
includes an active metal, production of the amorphous alloy may be carried out in
an inert gas such as Ar or He or in a reduced pressure atmosphere. Quenching may be
carried out in an atmosphere including a nitrogen gas, a carbon monoxide gas or a
carbon dioxide gas. It is advantageous that the surface roughness of the amorphous
alloy solidified by quenching is small. The surface roughness of the amorphous alloy
ribbon (arithmetic average roughness Ra) can be set to, for example, 5 µm or smaller,
preferably 2 µm or smaller, more preferably 1 µm or smaller.
[0038] A ring-shaped structure can be produced by winding or layering the amorphous alloy
ribbon. The thus-produced ring-shaped structure (core element) has such a configuration
that a plurality of amorphous alloy layers are layered. There may be a small gap or
any other material between respective ones of the amorphous alloy layers. The volume
occupancy of the amorphous alloy layers in the core element is, for example, about
70% to 90%.
[0039] In the present embodiment, a core element formed by winding the amorphous alloy ribbon
is provided. However, the present disclosure is not limited to such an example.
[0040] Next, a crystallizing heat treatment is performed as follows. A core element formed
by winding or layering the amorphous alloy layer is heated in a nonreactive atmosphere
gas. According to research conducted by the present inventor and his coworkers, sufficient
magnetic permeability was achieved when the heat treatment was carried out in a nitrogen
gas. The nitrogen gas can be used substantially as the nonreactive gas. An inert gas
can also be used as the nonreactive gas. The heat treatment may be performed in vacuum.
[0041] The temperature of the above-described crystallizing heat treatment can be set within
the range of 510°C to 600°C. The temperature of the crystallizing heat treatment is
preferably set to 550°C to 600°C. If the heat treatment temperature is less than 510°C
or more than 600°C, the magnetostriction is large. The retention time at the above-described
heat treatment temperature (heat treatment duration) can be set within the range of
about 5 minutes to 24 hours. If the heat treatment duration is shorter than 5 minutes,
it is difficult to maintain the entirety of the alloy that forms the core at a uniform
temperature, so that the magnetic properties are likely to vary. On the other hand,
if the heat treatment duration is longer than 24 hours, not only deterioration of
productivity but also deterioration of the magnetic properties is likely to occur
due to excessive growth of crystal grains or generation of crystal grains in uneven
forms.
[0042] In the present embodiment, the crystallizing heat treatment is performed in a DC
or AC magnetic field. Such a heat treatment performed in a magnetic field causes a
magnetic anisotropy in the alloy used in the current transformer core. The magnetic
field may be applied during the entire period of the heat treatment or may be applied
during a portion of the period of the heat treatment. The magnetic field is applied
in the longitudinal direction of the alloy layer in the core element formed by winding
the amorphous alloy layer (the circumferential direction of the ring-shaped core element).
The intensity of the applied magnetic field is set to, for example, 100 A/m or greater
such that the alloy layer reaches magnetic saturation. Such a magnetic field is referred
to as "longitudinal magnetic field". A crystallizing heat treatment performed in the
presence of an applied longitudinal magnetic field is referred to as "longitudinal-field
heat treatment". As the intensity of the longitudinal magnetic field increases, the
magnetic permeability µr(T) increases. When the intensity of the longitudinal magnetic
field increases to some level, µr(T) saturates (see FIG. 3 which will be described
later).
[0043] On the other hand, when a longitudinal magnetic field is applied to the ring-shaped
core element to such an extent that the alloy layer reaches magnetic saturation, the
residual magnetic flux density Br greatly increases, and the ratio of the residual
magnetic flux density Br and the saturation magnetic flux density Bm, Br/Bm, increases.
In the present application, the saturation magnetic flux density Bm is defined as
the magnetic flux density B(80) with the magnetic field H=80 A/m. Br/Bm is also referred
to as "squareness ratio".
[0044] After the longitudinal-field heat treatment, a magnetic field is applied in the vertical
direction of the core. For example, the heat treatment temperature is not less than
200°C. The magnetic field is applied for 20 minutes or longer at a temperature less
than the crystallizing temperature of the amorphous alloy. The intensity of the applied
magnetic field is, for example, not less than 80 kA/m. Such a magnetic field is referred
to as "transverse magnetic field". A heat treatment performed in the presence of an
applied transverse magnetic field is referred to as "transverse-field heat treatment".
The longitudinal magnetic field and the transverse magnetic field may be any of a
DC magnetic field, an AC magnetic field and a pulsed magnetic field. Due to the transverse-field
heat treatment, the residual magnetic flux density Br decreases although the magnetic
permeability decreases and, accordingly, Br/Bm decreases, resulting in a current transformer
core in which a magnetic deviation is unlikely to occur. Since high magnetic permeability
is achieved due to the longitudinal-field heat treatment, the magnetic permeability
of the core after the transverse-field heat treatment is higher than the conventional
level, and the high magnetic permeability is maintained within the use temperature
range, so that the temperature characteristics are excellent.
< Magnetic permeability >
[0045] In the present application, the term "magnetic permeability" has the same meaning
as "relative magnetic permeability". A magnetic permeability measured at temperature
T (°C) in the presence of an applied AC magnetic field of frequency f=50 Hz and amplitude
H=1.0 ampere/meter (A/m) is referred to as "amplitude magnetic permeability", which
is expressed as "magnetic permeability µr(T)" or simply "µr(T)". When the measurement
temperature is not particularly specified, the magnetic permeability means a value
measured at 25°C, i.e., µr(25). For the sake of simplicity, µr(25) is sometimes simply
expressed as "µr" in the drawings.
[0046] The magnetic permeability of a core which is subjected to the longitudinal-field
heat treatment with such a magnetic field intensity that the variation (increase)
of the magnetic permeability is not found any more even when the applied longitudinal
magnetic field is increased is defined as "µr(max)(T)". In the embodiment of the present
disclosure, when the intensity of the longitudinal magnetic field during the crystallizing
heat treatment is 100 A/m, the variation (increase) of the magnetic permeability is
not found at a lower magnetic field intensity (e.g., 90 A/m). Therefore, µr(max)(T)
of the present application means the magnetic permeability of a core which is obtained
when the longitudinal magnetic field intensity during the crystallizing heat treatment
is 100 A/m.
[0047] FIG. 1 is a diagram showing the configuration of a measurement system used in measurement
of the magnetic permeability µr(T). In the shown configuration, the primary side conductor
14 of the current transformer is coupled with a function generator
54 configured to generate an AC voltage signal which has an arbitrary frequency and
an arbitrary waveform, via a digital multimeter (DMM)
52 which is capable of measuring the DC voltage, direct current, AC voltage and electric
resistance over a wide range and a resistance
R. Meanwhile, the secondary side conductor
12 of the current transformer is coupled with another digital multimeter (DMM)
56 that is different from the digital multimeter
52 on the primary side conductor
14 side. In the measurement of the present application, the value of the resistance
R was set to 47 ohms, and digital multimeter 34401A manufactured by Agilent Technologies
was used as the digital multimeters
52 and
56. Multifunction generator WF1973 manufactured by NF CORPORATION was used as the function
generator
54 for generation of an AC voltage signal.
[0048] The magnetic permeability µr(T) is determined by the following formula based on the
result of a measurement at temperature T:

where Vo (V) is the voltage value measured by the digital multimeter (DMM)
56, Ae (m
2) is the effective cross-sectional area of the core, µ0 is the magnetic permeability
in vacuum, f (Hz) is the frequency, and H (A/m) is the intensity of an AC magnetic
field applied by the primary side conductor
14.
[0049] In the present embodiment, the heat treatment is divided into two phases, in which
magnetic fields of different directions are applied. By performing such a distinctive
heat treatment in magnetic fields, a current transformer core which exhibits excellent
magnetic properties can be realized. In the first phase heat treatment in a magnetic
field, the magnetic field is formed in the direction of a magnetic path formed in
a ring-shaped core element ("longitudinal-field heat treatment"). By this heat treatment,
the core element is changed to a core. Then, in the second phase heat treatment in
a magnetic field, the magnetic field is formed in a direction perpendicular to the
direction of the above-described magnetic path and applied to the core ("transverse-field
heat treatment"). By appropriately performing such a two-phase heat treatment in the
magnetic fields, a current transformer core of excellent magnetic properties can be
obtained. This aspect is described in detail in the following section.
< Effects of longitudinal-field heat treatment on magnetic permeability µr(25) >
[0050] As a result of research conducted by the present inventor, it was found that the
magnetic permeability µr(25) after the longitudinal-field heat treatment largely varies
depending on the thickness of the Fe-based nanocrystalline alloy ribbon. First, this
point is described below.
[0051] FIG.
2A is a graph illustrating the magnetic permeability µr(25) in the case where a core
element was formed by winding a Fe-based amorphous alloy ribbon (thickness: 18 µm,
width: 10 mm) which had the composition of Fe
74Cu
1Nb
3S
i15.5B
6.5. In this example, the dimensions of the core were the inside diameter of 20 mm, the
outside diameter of 30 mm, and the height of 10 mm. The heat treatment temperature
(retention temperature) in the process of the longitudinal-field heat treatment was
set to 520°C, 540°C and 560°C. The magnetic permeability µr(25) was evaluated based
on four samples for each of the retention temperatures. The retention time at the
retention temperature was one hour for each sample. The temperature increase rate
up to the retention temperature was 6°C/min. The temperature decrease rate from the
retention temperature was 1.5°C/min. The applied magnetic field was 230 A/m. The magnetic
field was applied over the entire temperature range. By this heat treatment process,
the Fe-based amorphous alloy ribbon was crystallized and changed into a Fe-based nanocrystalline
alloy ribbon.
[0052] As seen from FIG.
2A, when the retention temperature of the longitudinal-field heat treatment was decreased
from 560°C to 520°C, the average of the magnetic permeability µr(25) increased from
about 4×10
5 to about 5.5×10
5, although there was a large variation. Br/Bm calculated from the saturation magnetic
flux density Bm and the residual magnetic flux density Br that were determined from
B-H curves was 0.93 in each sample.
[0053] FIG.
2B is a graph illustrating the magnetic permeability µr(25) in the case where a core
element was formed by winding a Fe-based amorphous alloy ribbon (thickness: 13 µm,
width: 10 mm) which had the composition of Fe
74Cu
1Nb
3S
i15.5B
6.5 (which was the same as that of the above-described 18 µm thick Fe-based amorphous
alloy ribbon). The dimensions of the core and the heat treatment (annealing) conditions
were the same as those of the core of FIG.
2A. The heat treatment temperature (retention temperature) in the process of the longitudinal-field
heat treatment was set to 520°C, 540°C and 560°C. The magnetic permeability µr(25)
was evaluated based on four samples for each of the retention temperatures. By the
process of the longitudinal-field heat treatment, the Fe-based amorphous alloy ribbon
was crystallized and changed into a Fe-based nanocrystalline alloy ribbon.
[0054] As seen from FIG.
2B, the average of the magnetic permeability µr(25) exhibits a value generally equal
to about 9×10
5 irrespective of the temperature of the longitudinal-field heat treatment. Br/Bm calculated
from the maximum magnetic flux density Bm and the residual magnetic flux density Br
that were determined from B-H curves was 0.93 in each sample. Note that Bm is the
magnetic flux density B(80) at the magnetic field H=80 A/m. When a relatively thin,
13 µm thick Fe-based amorphous alloy ribbon was thus used, the magnetic permeability
µr(25) greatly increased and, furthermore, the value of the magnetic permeability
µr(25) was stabilized. On the other hand, irrespective of the thickness of the ribbon,
Br/Bm exceeded 0.9 and was equal to 0.93. High magnetic permeability µr(25) with the
thickness of 13 µm was more than expected. Based on this knowledge, the present disclosure
defines the thickness of the Fe-based nanocrystalline alloy ribbon as one of the means
for improving the magnetic permeability.
[0055] Of the samples shown in FIG.
2B, a sample obtained by the heat treatment at 560°C is hereinafter referred to as "Sample
1". Effects of the intensity of the longitudinal magnetic field on the magnetic properties
were examined using Sample 1.
[0056] FIG.
3 is a graph illustrating the variation of the magnetic permeability µr(25) of such
a core that the dimensions of the core and the heat treatment conditions were the
same as those of Sample 1 except for the intensity of the longitudinal magnetic field.
The intensity of the longitudinal magnetic field was adjusted within the range of
6 A/m to 115 A/m by adjusting a longitudinal magnetic field forming current flowing
through a conductor wire (conductor wire for formation of a longitudinal magnetic
field) which was arranged so as to penetrate through the central opening of a ring-shaped
core element in the longitudinal-field heat treatment. The value of µr (25) of the
core at a longitudinal magnetic field intensity of not less than 75 A/m as shown in
FIG.
3 is about 9.5×10
5. This value is large as compared with the value of µr(25) of Sample 1 shown in FIG.
2B (about 8.7×10
5). Such a difference in value is probably attributed to the variation of the core
samples.
[0057] As seen from FIG.
3, when the intensity of the longitudinal magnetic field is not less than 80 A/m, the
magnetic permeability µr(25) saturates.
[0058] FIG.
4 is a graph illustrating the temperature characteristic of the magnetic permeability
µr(T) of the core for each of Sample A where the longitudinal magnetic field during
the longitudinal-field heat treatment was 19 A/m and Sample B (Sample 1) where the
longitudinal magnetic field during the longitudinal-field heat treatment was 230 A/m.
In the graph, the horizontal axis represents the measurement temperature T, and the
vertical axis represents the magnetic permeability µr (T).
[0059] As seen from FIG.
4, in Sample A for which the longitudinal magnetic field intensity was relatively small,
the magnetic permeability µr (T) sharply decreased as the measurement temperature
T increased. Where the amplitude magnetic permeability of the core measured at 100°C
was represented by µr(100), the amplitude magnetic permeability of the core measured
at 0°C was represented by µr(0), and |µr(100)-µr(0)|/µr(0) was represented by Δµr(100-0),
Δµr(100-0) was about 0.55. On the other hand, in Sample B (Sample 1) for which the
longitudinal magnetic field intensity was relatively large and the magnetic permeability
µr(25) saturated and exhibited the maximum value, the magnetic permeability µr (T)
decreased as the measurement temperature T increased. This tendency was the same as
that of Sample A. However, Δµr(100-0) was a small value, 0.14, and the variation of
the magnetic permeability within the use temperature range of 0°C to 100°C was suppressed,
resulting in excellent temperature characteristics.
[0060] Sample A also exhibited high squareness as Sample B (Sample 1) did, i.e., Br/Bm was
0.93, according to the direct current B-H curve and had such magnetic properties that
a magnetic deviation is likely to occur.
[0061] It was found from the above-described results that Br/Bm cannot be decreased by changing
the longitudinal magnetic field intensity.
[0062] As seen from the foregoing, when the thickness of the Fe-based amorphous alloy is
not more than 15 µm and the longitudinal magnetic field intensity during the crystallizing
heat treatment is set such that the alloy has a sufficient magnetic anisotropy, large
magnetic permeability and excellent temperature characteristics can be achieved. However,
the Br/Bm is not decreased, and a magnetic deviation is likely to occur. Further improvements
are necessary for uses of the current transformer core.
[0063] The present inventor wholeheartedly carried out extensive researches and, as a result,
found that by performing a manufacturing process which will be described below a current
transformer core can be realized of which practically sufficiently high magnetic permeability
is stably achieved within the use temperature range, and Br/Bm is greatly decreased,
although the magnetic permeability is lower than that achieved by the longitudinal-field
heat treatment. That is, firstly, the thickness of the Fe-based amorphous alloy is
controlled to be not more than 15 µm, and the longitudinal magnetic field intensity
during the process of the longitudinal-field heat treatment is set to such an extent
that the alloy has a sufficient magnetic anisotropy (e.g., not less than 100 A/m),
whereby a core is manufactured in which a relatively high value of the magnetic permeability
µr(25) can be realized. Thereafter, an appropriate transverse-field heat treatment
is performed on the core, whereby reduction of Br/Bm is realized. In the following
section, measurement results are described in detail.
[0064] FIG.
5 is a graph illustrating an example of the profiles of the temperature and the magnetic
field intensity of the transverse-field heat treatment in the present embodiment.
In the graph, the temperature profile is represented by a solid line, and the magnetic
field intensity profile is represented by a dotted line. In this example, a transverse
magnetic field of 160 kA/m was applied to the core over a period including the entirety
of the period where the temperature of the core increased, the period where the core
was retained at a predetermined heat treatment temperature, and the period where the
temperature of the core decreased (about 4 hours). In the example of FIG.
5, the heat treatment temperature was 400°C, and the retention time was 1 hour and 30
minutes (90 minutes).
[0065] FIG.
6 is a graph illustrating B-H curves of current transformer cores obtained by further
applying a transverse magnetic field according to the profile illustrated in FIG.
5 to Sample 1 of which the dimensions of the core were the inside diameter of 20 mm,
the outside diameter of 30 mm, and the height of 10 mm, with the duration for which
the core was retained at the heat treatment temperature of 400°C (retention time)
being set to 60 minutes, 90 minutes and 120 minutes, and B-H curves of the core of
Sample 1 before the transverse-field heat treatment. The samples with the retention
time of 60 minutes, 90 minutes and 120 minutes are Example 1, Example 2 and Example
3, respectively. Table 1 presented below shows, for respective samples, the values
of the maximum magnetic flux density Bm, the residual magnetic flux density Br, the
coercivity Hc, and the squareness ratio Br/Bm, which were determined from the B-H
curves of FIG.
6. Bm is the magnetic flux density B(80) at magnetic field H=80 A/m.
[Table 1]
| |
Before transverse-field heat treatment (Comparative Example) |
Retention time 60 minutes (Example 1) |
Retention time 90 minutes (Example 2) |
Retention time 120 minutes (Example 3) |
| Bm (T) |
1. 150 |
1. 167 |
1. 153 |
1. 150 |
| Br (T) |
1. 064 |
0. 797 |
0. 759 |
0. 677 |
| Hc (A/m) |
0. 59 |
0. 67 |
0. 72 |
0. 72 |
| Br/Bm |
0. 93 |
0. 68 |
0. 66 |
0. 59 |
[0066] As seen from FIG.
6 and Table 1, by adding the transverse-field heat treatment, the residual magnetic
flux density Br decreases as compared with that achieved before the heat treatment.
Since the variation of Bm is small, Br/Bm can decrease to be less than 0.9. By elongating
the retention time of the heat treatment, the residual magnetic flux density Br and
Br/Bm are further decreased.
[0067] FIG.
7 is a graph illustrating the relationship between the retention time of the transverse-field
heat treatment (400°C) and µr(25) in Examples 1 to 3. The magnetic permeability µr(25)
after the longitudinal-field heat treatment of the measured core (magnetic field intensity:
100 A/m) saturates with respect to the magnetic field intensity and exhibits the maximum
value. This maximum value, µr(max)(25), was 9.5×10
5. For each retention time, µr(25) of two samples were measured. Table 2 shows the
relationship between the retention time and the magnetic permeability µr(25), µr(25)/µr(max)(25).
[Table 2]
| |
Retention time (min) |
µr(25) (×105) |
µr(25)/µr(max) (25) |
| Example 1 |
60 |
7. 18 |
0. 76 |
| 7. 87 |
0. 83 |
| Example 2 |
90 |
5. 76 |
0. 61 |
| 5. 93 |
0. 62 |
| Example 3 |
120 |
4. 57 |
0. 48 |
| 4. 36 |
0. 46 |
[0068] As seen from FIG.
7 and Table 2, the magnetic permeability µr(25) decreased as the retention time of
the transverse-field heat treatment increased. The magnetic permeability µr(25) monotonically
decreases with respect to the retention time. In this example, the magnetic permeability
can be estimated by the formula of µr(25)=(10.5-0.05×t)×10
5 where µr(25) is the magnetic permeability and t is the retention time (min). In other
words, the magnetic permeability can be adjusted by controlling the retention time
of the transverse-field heat treatment.
[0069] FIG.
8 is a graph illustrating the measurement temperature dependence of the magnetic permeability
of the sample of Example 2, which is one of the above-described samples, where the
duration for which the heat treatment temperature was retained at 400°C (retention
time) was set to 90 minutes.
[0070] As seen from this graph, over a wide range from about -50°C to about 100°C, the magnetic
permeability increases generally monotonically as the measurement temperature increases,
and µr(100)-µr(0) has a positive value. Δµr(100-0) of the current transformer core
measured at temperature T (°C) in the presence of an applied AC magnetic field which
had frequency f=50 Hz and amplitude H=1.0 A/m was about 0.25. Likewise, also in the
samples of Example 1 and Example 3, Δµr(100-0) was not more than 0.5.
[0071] FIG.
9 is a graph illustrating the relationship between the magnetic field intensity in
the transverse-field heat treatment and the magnetic permeability µr(25). A Fe-based
amorphous alloy ribbon (thickness: 13 µm, width: 10 mm) was produced which had the
same alloy composition of Fe
74Cu
1Nb
3Si
15.5B
6.5 as Sample 1 but which was from a different production lot. The alloy ribbon was wound
to form a core element. The core element was subjected to a longitudinal-field heat
treatment under the same conditions as those of Sample 1. Further, a transverse-field
heat treatment was performed on the core which had been subjected to the longitudinal-field
heat treatment. In the heat treatment, the retention temperature was 380°C, and the
retention time was 90 minutes. µr(25) of the respective samples in the cases where
the transverse magnetic field intensity was 80 kA/m (Example 4), 160 kA/m (Example
5), and 320 kA/m (Example 6) are shown in the graph. As the magnetic field intensity
increases, µr(25) monotonically decreases. It is understood that the magnetic permeability
of the core can be adjusted by controlling the transverse magnetic field intensity
in the heat treatment. In each of Examples 4 to 6, the evaluated Br/Bm was less than
0.9. Br/Bm had a tendency to decrease as the magnetic field intensity increases. In
each of Examples 4 to 6, Δµr (100-0) was not more than 0.5. In Examples 4 to 6, µr(25)/µr(max)
was 0.5 to 0.7. Here, the magnetic permeability µr(25) of the core after the longitudinal-field
heat treatment (magnetic field intensity: 100 A/m) saturated with respect to the magnetic
field intensity and exhibited the maximum value. µr(max)(25) was 8×10
5.
[0072] As understood from the foregoing description, a manufacturing method of a current
transformer core according to the present disclosure includes: the step of providing
a core element formed by winding or layering a Fe-based amorphous alloy ribbon whose
thickness is not more than 15 µm and which can be converted into nanocrystals; a longitudinal-field
heat treatment step which includes performing a heat treatment on the core element
in the presence of a magnetic field applied in a magnetic path direction of the core
element so as to crystallize the amorphous alloy, thereby obtaining a core; and a
transverse-field heat treatment step which includes performing a heat treatment on
the core obtained after the longitudinal-field heat treatment step in the presence
of a magnetic field applied in a direction perpendicular to the magnetic path direction
of the core, thereby forming a current transformer core. By the transverse-field heat
treatment step, µr(25) is adjusted to a value between 0.4×µr(max)(25) and 0.9×µr(max)(25)
where µr(T) is the amplitude magnetic permeability measured at temperature T (°C)
in the presence of an applied AC magnetic field of frequency f=50 Hz and amplitude
H=1.0 A/m, and µr(max)(T) is µr(T) after the longitudinal-field heat treatment step
(before the transverse-field heat treatment). As a result, a current transformer core
is obtained which has such excellent temperature characteristics that Δµr(100-0) is
not more than 0.5 and Br/Bm is less than 0.9 where Δµr(100-0) is |µr(100)-µr(0)|/µr(0)
measured after manufacture.
[0073] FIG.
10 is a flowchart illustrating an example of the manufacturing method of a current transformer
core according to the present disclosure. As described above, at step S120, a core
element is provided which is formed by winding or layering a Fe-based amorphous alloy
ribbon whose thickness is not more than 15 µm.
[0074] Then, at step S140, a longitudinal-field heat treatment is performed. The treatment
temperature of the longitudinal-field heat treatment can be set to a temperature not
less than the crystallizing temperature, e.g., within the range of 510 to 600°C. The
retention time of the treatment temperature can be set within the range of 5 minutes
to 24 hours. If it is shorter than 5 minutes, it is difficult to obtain magnetic properties
with small variations among respective cores. If it is longer than 24 hours, the productivity
greatly deteriorates. The intensity of an applied longitudinal magnetic field can
be set within the range of not less than 100 A/m. If the longitudinal magnetic field
intensity is less than 100 A/m, there is a probability that provision of a magnetic
anisotropy is insufficient. If the longitudinal magnetic field intensity exceeds 300
A/m, it is difficult stably carry out the treatment.
[0075] Then, at step S160, a transverse-field heat treatment is performed. The treatment
temperature of the transverse-field heat treatment can be set to a temperature less
than the crystallizing temperature, e.g., within the range of not less than 200°C
and less than the longitudinal-field heat treatment temperature. If it is less than
200°C, there is a probability that the effects of the magnetic field treatment are
insufficient. If it is not less than the longitudinal-field heat treatment temperature,
there is a probability that the effects of the longitudinal magnetic field treatment
greatly decrease, and the effects brought about by a different magnetic field treatment,
i.e., a transverse magnetic field treatment performed after the longitudinal magnetic
field treatment in the present disclosure, cannot be achieved. The retention time
of the treatment temperature can be set within the range of 20 minutes to 120 minutes.
If the retention time is less than 20 minutes, there is a probability that the magnetic
field application effect (provision of a magnetic anisotropy) is insufficient. If
the retention time exceeds 120 minutes, the productivity decreases. The intensity
of the applied transverse magnetic field can be set within the range of 80-320 kA/m.
If the transverse magnetic field intensity is less than 80 kA/m, there is a probability
that provision of a magnetic anisotropy is insufficient. If the transverse magnetic
field intensity exceeds 320 kA/m, a stable magnetic field intensity is unlikely to
be obtained, and the treatment becomes difficult.
[0076] Between step S140 and step S160, the core can be cooled to about the room temperature.
Desirably, application of the transverse magnetic field is continued till the core
is sufficiently cooled to a temperature not more than 200°C.
[0077] Typically, when used, the current transformer core can be housed in a case which
is made of a resin, or the like, for the purpose of protection of the current transformer
core itself and insulation of a coil from the other circuit elements. A core element
formed by winding an alloy ribbon is formed of an elongated ribbon-shaped continuous
alloy layer and is therefore advantageous in terms of handleability. After the current
transformer core of the present embodiment is housed in a case which is made of a
resin or the like, a coil is formed around the core for sensing, whereby a current
transformer can be manufactured.
< Current Transformer >
(Example 7)
[0078] FIG.
11A shows an example of the basic structure of a current transformer
100 to which the present disclosure is applicable. The current transformer
100 typically includes a ring-shaped (cylindrical) core
10 and a secondary side conductor (secondary side coil)
12 coiled around the core
10 such as shown in FIG.
11A. The primary side conductor
14, which is the object of the current measurement, can typically be inserted so as to
extend through the center opening of the core
10. The primary side conductor
14 may be wound around the core
10 so as to make two or more turns as is the secondary side conductor
12. The primary side conductor
14 and the secondary side conductor
12 can be an arbitrary known wire whose surface is covered for insulation.
[0079] In the example of FIG.
11A, only part of each of the primary side conductor
14 and the secondary side conductor
12 is schematically shown. The shown primary side conductor
14 has the shape of a linear stick, although the actual shape of the primary side conductor
14 is not limited to such a shape. Both ends of the primary side conductor
14 are electrically coupled with an unshown wire, circuit, voltage source or current
source.
[0080] When an electric current flows through the primary side conductor
14 shown in FIG.
11A, a magnetic field is produced around the primary side conductor
14, and a closed magnetic path is formed in the ring-shaped core
10 that has high magnetic permeability. When an alternating current is flowing through
the primary side conductor
14, the magnetic flux density in the core
10 periodically varies so that an AC voltage is produced in the secondary side conductor
12. As a result, an electric current flows through an unshown circuit coupled with the
secondary side conductor
12. The electric current flowing through the primary side conductor
14 can be measured based on the voltage or current output to the secondary side conductor
12.
[0081] FIG.
11B shows an example where the current transformer
100 is applied to a zero-phase current transformer (ZCT). In the example of FIG.
11B, the electric currents flowing through the primary side conductors
14 of a single-phase, two-line system are the object of measurement. In the case of
a single-phase, three-line system, three primary side conductors are arranged so as
to extend through the opening of the core
10 although not shown. The zero-phase current transformer is capable of sensing a leakage
current when an abnormal current resulting from electrical leakage flows through the
primary side conductors
14. The configuration of the current transformer
100 can be designed such that, when a leakage current of 30 milliamperes (mA) flows at
the frequency of, for example, 50 Hz through the primary side conductors
14, a voltage of 4 millivolts (mV) is produced in the secondary side conductor
12.
< Earth leakage circuit breaker >
(Example 8)
[0082] FIG.
12 shows a circuit configuration example of an earth leakage circuit breaker
20 which includes the current transformer
100 such as shown in FIG.
11B. This earth leakage circuit breaker
20 includes a current transformer core
10, a secondary side conductor
12 coiled around the core
10, a sensing circuit
16 coupled with the secondary side conductor
12, and a trip device
18 coupled with the sensing circuit
16.
[0083] In the example of FIG.
12, an alternating current from a transformer
30 is supplied to the earth leakage circuit breaker
20 via wires of a single-phase, two-line system. The transformer
30 is coupled with, for example, an electric power system for business purposes or any
other AC power supply. The earth leakage circuit breaker
20 is placed on an electrical path coupled with a load
40. The load
40 can be an electronic device or electric machine which is configured to receive an
AC power for operation. The earth leakage circuit breaker
20 is placed in, for example, a distribution board.
[0084] In a normal state, the sum of electric currents flowing through a pair of primary
side conductors
14 is zero. In this case, the trip device
18 of the earth leakage circuit breaker
20 maintains the electrical path in a conducting state, and the load
40 receives an AC power from the transformer
30. When electrical leakage occurs due to, for example, deteriorated insulation of the
load
40, an ground fault current flows from the load
40. Accordingly, the total of the electric currents flowing through the pair of primary
side conductors
14 exhibits a significant value exceeding zero, and as a result, a voltage is produced
in the secondary side conductor
12. Describing based on the above-described example, the configuration of the current
transformer
100 is designed such that when an alternating current of 30 mA flows at the frequency
of, for example, 50 Hz as a leakage current, a voltage of 4 mV is produced in the
secondary side conductor
12. In this case, the leakage current of 30 mA refers to the difference between the currents
flowing through the pair of primary side conductors
14, rather than each of the currents flowing through the pair of primary side conductors
14.
[0085] The sensing circuit
16 activates the trip device
18 based on the voltage or current produced in the secondary side conductor
12. When the voltage or current produced in the secondary side conductor
12 exceeds a predetermined threshold, the sensing circuit
16 activates the trip device
18 in order to shut off the current flowing from the transformer
30 to the load
40. The earth leakage circuit breaker
20 is configured such that, when an abnormal current which is equal to or greater than
a predetermined value flows through the primary side conductor
14 due to electrical leakage, the earth leakage circuit breaker
20 automatically shuts off the current for a short time period, e.g., not more than
0.1 second.
[0086] The current transformer
100 used in such an earth leakage circuit breaker
20 is required to appropriately sense occurrence of a feeble leakage current. The largeness
of the leakage current to be sensed is defined by the standards of respective countries.
If the magnetic permeability of the core
10 is low, a voltage which is produced in the secondary side conductor
12 when a feeble leakage current is produced is low, so that occurrence of the electrical
leakage cannot be sensed appropriately. The upper limit of the magnetic permeability
of the core
10 can be appropriately set based on the lower limit of the leakage current to be sensed.
For example, when Br/Bm is less than 0.9, the core
10 has high magnetic permeability, and therefore, the earth leakage circuit breaker
20 can have an excellent leakage shut-off function. Further, since the variation of
the magnetic permeability is small within the temperature range of 0°C to 100°C as
previously described, the earth leakage circuit breaker
20 can have an excellent leakage shut-off function, which is stable against variation
in temperature.
[0087] In the foregoing, the embodiment has been described as an example of the technology
disclosed in the present application. However, the technology in the present disclosure
is not limited to the example but is applicable to embodiments to which changes, substitutions,
additions, omissions, or the like, are occasionally made. Alternatively, combining
some of the components described in the above embodiment into a new embodiment is
also possible. The components disclosed in the attached drawings and detailed descriptions
can include not only those which are indispensable in solving the problems but also
those which are simply for the sake of exemplification of the above-described technology
and are not indispensable in solving the problems.
[0088] Thus, it should not be acknowledged that the disclosure of those dispensable components
in the attached drawings and detailed descriptions immediately means that those dispensable
components are indispensable.
INDUSTRIAL APPLICABILITY
[0089] The present disclosure is applicable to a current transformer which can be used in
an earth leakage circuit breaker and to a core which is suitable to the current transformer.
REFERENCE SIGNS LIST
[0090]
- 10
- current transformer core
- 12
- secondary side conductor (secondary side coil)
- 14
- primary side conductor
- 16
- sensing circuit
- 18
- trip device
- 20
- earth leakage circuit breaker
- 30
- transformer
- 40
- load
- 100
- current transformer