BACKGROUND OF THE INVENTION
(FIELD OF THE INVENTION)
[0001] The present invention relates to a winding element fixing bracket which fixes a winding
element to a predetermined member and a winding element with the fixing bracket which
includes the winding element fixing bracket.
(DESCRIPTION OF THE RELATED ART)
[0002] As a winding element which is formed by winding an elongated conductor member, a
reactor which introduces a reactance to a circuit or a transformer which transmits
energy between a plurality of coils using an electromagnetic induction is known. The
reactor is used in, for example, various electric circuits or electronic circuits
so as to prevent a harmonic current in a power factor improving circuit, to smooth
a current pulsation in a current inverter or a chopper control, and to boost a DC
voltage in a converter. Further, since the transformer is used to convert a voltage,
match impedance, or detect a current, the transformer is used in various electric
circuits or electronic circuits.
[0003] In general, the winding element is used while being attached to a predetermined
member such as a loading member or a mounting member. Then, when power is supplied
to the winding element, the winding element generates heat in a general case, and
hence there is a need to attach the winding element to a predetermined member having
a function of a heat sink in consideration of a heat radiation performance. A reactor
which is devised in consideration of the heat radiation performance is disclosed in,
for example, Japanese Patent Application Laid-Open No.
2009-147041.
[0004] FIGS. 9A and 9B are perspective vies illustrating an attachment aspect of the reactor
disclosed in Japanese Patent Application Laid-Open No.
2009-147041. FIG. 9A illustrates a first attachment aspect and FIG. 9B illustrates a second attachment
aspect.
[0005] In FIGS. 9A and 9B, a reactor 1001 includes an annular core 1002 which is formed
by linear portions facing each other and a U-shaped portion connecting the ends of
the respective linear portions to each other and a coil 1003 which is wound on each
linear portion of the core 1002. Then, in the first attachment aspect disclosed in
Japanese Patent Application Laid-Open No.
2009-147041, as illustrated in FIG. 9A, the reactor 1001 is interposed between a flat heat radiation
portion 1004 which is formed by alumina and a loading portion L, for example, a bottom
plate of a casing or a seat of a heat sink, and both ends of a heat conduction member
1005 as a leg-shaped member disposed at each of four corners of the heat radiation
portion 1004 are respectively fixed to each of the heat radiation portion 1004 and
the loading portion L by, for example, welding, adhering, and threading, so that the
reactor 1001 is fixed to the loading portion L. Further, in the second attachment
aspect disclosed in Japanese Patent Application Laid-Open No.
2009-147041, as illustrated in FIG. 9B, a heat conduction member 1006 as a plate-like member
formed upright on the loading portion L by, for example, welding or adhering is inserted
through a gap between the facing coils 1003 of the reactor 1001, and the heat radiation
portion 1004 is fixed to the upper side of the heat conduction member 1006 by, for
example, adhering or threading, so that the reactor 1001 is fixed to the loading portion
L.
[0006] Incidentally, the attachment surface attached with the winding element may be set
in the inclination direction or the vertical direction (the direction intersecting
or substantially perpendicular to the attachment surface may intersect the gravity
action direction in which the gravity acts). In the first and second attachment aspects
disclosed in Japanese Patent Application Laid-Open No.
2009-147041, since the loading portion L is set in the horizontal direction (the direction perpendicular
to the attachment surface is parallel to the gravity action direction), the reactor
1001 is loaded on the loading portion L by the own weight thereof. Accordingly, there
is no need to support the reactor 1001 by the heat radiation portion 1004 and the
heat conduction member 1005 of the first attachment aspect or the heat radiation portion
1004 and the heat conduction member 1006 of the second attachment aspect. Further,
in Japanese Patent Application Laid-Open No.
2009-147041, a case is assumed in which the loading portion L is set in the vertical direction.
[0007] Further, in a case where the core is a compact core, since the compact core is manufactured
by compact molding and heating at a temperature less than a sintering temperature,
powders are caulked. For this reason, when the winding element is dropped by mistake,
there is a concern that the compact core may be damaged by the impact load generated
by the dropping impact.
SUMMARY OF THE INVENTION
[0008] The present invention is made in view of the aforementioned circumstances, and in
an aspect of the present invention, provided are a winding element fixing bracket
and a winding element with the fixing bracket which includes the winding element fixing
bracket, which enable reliable attachment of a winding element even when an attachment
surface is set in the vertical direction and protection of a core even in the event
of dropping by mistake.
[0009] The present inventor figured out that the aforementioned object may be attained by
aspects of the present invention based on various examinations. That is, according
to an aspect of the present invention, there is provided a winding element fixing
bracket which fixes a winding element with a coil and a core accommodating the coil
to a predetermined member, the winding element fixing bracket including: a band plate-shaped
body which includes a through hole, a pair of leg portions which is formed upright
from respective both ends of the body, and a pair of fixation portions which is formed
upright from respective both ends of the respective leg portions.
[0010] The longitudinal sectional shape of the winding element fixing bracket with such
a configuration becomes a hat shape (where the longitudinal sectional shape is

or Π in the side view), and an attachment member, for example, a bolt is inserted
through the through hole of the body, so that the winding element fixing bracket is
attached to the winding element so as to embrace the winding element. Then, the pair
of fixation portions of the winding element fixing bracket is fixed to a predetermined
member, for example, a heat sink. In this way, since the winding element fixing bracket
with the aforementioned configuration is attached to the winding element so as to
embrace the winding element and the pair of fixation portions is fixed to the predetermined
member, the winding element may be reliably attached even when the predetermined member
is set in the vertical direction. Then, since the winding element fixing bracket with
the aforementioned configuration is attached to the winding element so as to embrace
the winding element in this way, it is possible to protect the core even in the event
of dropping by mistake.
[0011] Further, according to another aspect, there is provided the aforementioned winding
element fixing bracket, in which, when the winding element is attached to the body
and is placed on the predetermined member, a gap is formed between a bottom surface
of the fixation portion and the predetermined member.
[0012] When the winding element fixing bracket is fixed to the predetermined member by the
fixation portion, the gap is removed, so that the bottom surface of the fixation portion
abuts against the predetermined member. For this reason, the winding element fixing
bracket generates a biasing force which presses the winding element against the predetermined
member. Accordingly, the winding element is further reliably pressed by the winding
element fixing bracket using the biasing force. As a result, when the predetermined
member has a function of the heat sink, the heat generated by the winding element
is further reliably transferred to the predetermined member, and hence the heat radiation
performance may be improved.
[0013] Further, according to another aspect, there is provided the aforementioned winding
element fixing bracket, in which, when respective points where the pair of leg portions
is respectively formed upright from the body are denoted by A and B and respective
points where the pair of fixation portions is respectively formed upright from the
pair of leg portions are denoted by C and D, a length between A and B, a length between
C and A, and a length between D and B are set so that respective maximum stresses
which are generated when a biasing force and a predetermined dropping impact load,
which are generated when thicknesses and band widths of the body, the pair of leg
portions, and the pair of fixation portions are predetermined and when the winding
element fixing bracket is fixed onto the predetermined member without the gap respectively,
act on the winding element fixing bracket are smaller than a yielding point of a material
forming the winding element fixing bracket or a physical property value equal to the
yielding point.
[0014] The winding element fixing bracket with such a configuration is not broken even in
the event where the biasing force or the predetermined dropping impact load acts.
[0015] Further, according to another aspect, there is provided the aforementioned winding
element fixing bracket, in which, when the respective points where the pair of leg
portions is respectively formed upright from the body are denoted by A and B, the
respective points where the pair of fixation portions is respectively formed upright
from the pair of leg portions are denoted by C and D, a length between A and B is
denoted by c, and a length between C and A and a length between D and B are denoted
by k; at least an inequation of 0.0236 x k
-1.07 ≤ c/k ≤ 0.0079 x k
-1.9 is satisfied in the range of 0.02 ≤ k ≤ 0.07 [m].
[0016] In the winding element fixing bracket with such a configuration, when the gap between
the bottom surface of the fixation portion and the predetermined member upon attachment
of the winding element to the body to be disposed on the predetermined member is set
to 0.2 [mm] or less as an upper limit value, it is possible to withstand the dropping
impact of 5 G (five times of the gravity) generated in the event of dropping by mistake.
[0017] Further, according to another aspect, there is provided the aforementioned winding
element fixing bracket, in which, when the respective points where the pair of leg
portions is respectively formed upright from the body are denoted by A and B, the
respective points where the pair of fixation portions is respectively formed upright
from the pair of leg portions are denoted by C and D, a length between A and B is
denoted by c, and a length between C and A and a length between D and B are denoted
by k; at least an inequation of 7275.4 x k
2 - 592.14 x k + 14.612 ≤ c/k ≤ 0.0053 x k
-2 is satisfied in the range of 0.02 ≤ k ≤ 0.07 [m].
[0018] In the winding element fixing bracket with such a configuration, when the gap between
the bottom surface of the fixation portion and the predetermined member upon attachment
of the winding element to the body to be disposed on the predetermined member is set
to 1.5 [mm] or less as an upper limit value, it is possible to withstand the dropping
impact of 5 G generated in the event of dropping by mistake.
[0019] Further, according to another aspect, there is provided the aforementioned winding
element fixing bracket, in which, the body, the pair of leg portions, and the pair
of fixation portions are formed by a band-shaped member of a tempered aluminum alloy
of any one of H12 to H38.
[0020] Since the winding element fixing bracket with such a configuration is formed by the
aluminum alloy of JIS H12 to H38 which has a non-magnetic property and is hardly plastically
deformed, the characteristics of the winding element are not influenced, and hence
even when the predetermined member is set in the vertical direction, the winding element
may be attached in a pressed manner against the predetermined member.
[0021] Further, according to another aspect of the present invention, there is provided
a winding element with a fixing bracket including: a winding element which includes
a coil and a core accommodating the coil, and any one of the aforementioned winding
element fixing bracket; in which the core of the winding element includes a core through
hole which penetrates the core from a top surface to a bottom surface thereof, and
in which the winding element is fastened to the winding element fixing bracket by
a through bolt which is inserted through the through hole of the winding element fixing
bracket and the core through hole.
[0022] Since the winding element with the fixing bracket with such a configuration includes
any one of the aforementioned winding element fixing brackets, the winding element
may be reliably attached even when the attachment surface is set in the vertical direction,
and hence the core may be protected even in the event of dropping by mistake.
[0023] The winding element fixing bracket and the winding element with the fixing bracket
according to the present invention enable reliable attachment of the winding element
even when the attachment surface is set in the vertical direction, and hence protection
of the core even in the event of dropping by mistake.
BRIEF DESCRIPTION OF THE DRAWINGS
[0024]
FIG. 1 is a perspective view illustrating a configuration of a winding element with
a fixing bracket of an embodiment of the present invention.
FIG. 2 is a perspective view illustrating a configuration of the winding element in
the winding element with the fixing bracket of the embodiment.
FIG. 3 is a perspective view illustrating a configuration of a core member in the
winding element with the fixing bracket of the embodiment.
FIGS. 4A and 4B are diagrams illustrating stresses which are generated in each portion
of a winding element fixing bracket in the winding element with the fixing bracket
of the embodiment.
FIGS. 5A and 5B are diagrams illustrating a maximum stress which is obtained by dividing
a maximum stress by the Young's modulus in a case of an aluminum alloy of which a
displacement amount a is 0.2 mm.
FIGS. 6A and 6B are diagrams illustrating a maximum stress which is obtained by dividing
a maximum stress by the Young's modulus in a case of an aluminum alloy of which a
displacement amount a is 1.5 mm.
FIG. 7 is a diagram illustrating a maximum stress which is obtained by dividing a
maximum stress by the Young's modulus in a case of stainless steel (SUS304) of which
a displacement amount a is 0.75 mm.
FIG. 8 is a diagram illustrating a range of a length k and an aspect ratio ζ when
the winding element fixing bracket of the embodiment is formed by an aluminum alloy
(A5052-H38).
FIGS. 9A and 9B are perspective views illustrating an attachment aspect of a reactor
disclosed in Japanese Patent Application Laid-Open No.2009-147041.
DESCRIPTION OF THE PREFERRED EMBODIMENT
[0025] Hereinafter, an embodiment according to the present invention will be described based
on the drawings. Furthermore, the constituents that are denoted by the same reference
signs in the respective drawings indicate the constituents which have the same configuration,
and the description thereof may be appropriately omitted. Further, in the present
specification, the general constituent is indicated by the reference sign without
the suffix, and the individual constituent is indicated by the reference sign with
the suffix.
[0026] FIG. 1 is a perspective view illustrating a configuration of a winding element with
a fixing bracket of an embodiment of the present invention. FIG. 2 is a perspective
view illustrating a configuration of a winding element of the winding element with
the fixing bracket of the embodiment. FIG. 3 is a perspective view illustrating a
configuration of a core member in the winding element with the fixing bracket of the
embodiment. FIGS. 4A and 4B are diagrams illustrating a stress which is generated
in each portion of the winding element fixing bracket in the winding element with
the fixing bracket of the embodiment. FIG. 4A is a diagram illustrating a stress which
is generated by removing a gap between a bottom surface of a fixation portion and
an attachment surface, and FIG. 4B is a diagram illustrating a stress which is generated
by the action of the gravity
[0027] In FIG. 1, a winding element with a fixing bracket 1 includes a winding element 20
and a winding element fixing bracket 10 which fixes the winding element 20 to a predetermined
member 30, and the winding element 20 is attached to the winding element fixing bracket
10 by an attachment member 40.
[0028] For example, as illustrated in FIG. 2, the winding element 20 includes one coil 21
which has a pair of first and second terminals (an inlet drawn wire, a drawn wire,
and an electrode wire) 25 (25-1 and 25-2) and a core 22 through which a magnetic flux
generated by the coil 21 when supplying (feeding) power to the coil 21 passes and
serves as, for example, a reactor. Furthermore, the winding element 20 may be a multi-phase
reactor which includes a plurality of coils or a transformer which includes a plurality
of coils. In this way, the winding element may be provided with one or a plurality
of the coils 21.
[0029] The coil 21 is formed by winding an elongated conductor member a predetermined number
of times in an insulated state and generates a magnetic field by supplying power thereto.
For example, the coil 21 may be formed by winding an insulation-coated elongated conductor
member having a circular cross-sectional shape (O-shape) or a rectangular cross-sectional
shape (square shape). However, in this embodiment, from the viewpoint of a reduction
in a so-called eddy current, the coil 21 is formed in a manner such that a band-like
conductor member having an oblong cross-sectional shape (isosceles trapezoid shape)
is wound in an insulated state by interposing, for example, an insulation coating
or an insulation sheet in the wound band-like conductor member so that the width direction
of the conductor member faces the direction of the axis AX of the coil 21. In this
way, the coil 21 of this embodiment is a flatwise type coil of a so-called flatwise
winding structure.
[0030] Furthermore, the band shape indicates a case where the width (axial length) Cw is
larger than the thickness (radial length) Ct of the conductor member, that is, a relation
of Cw > Ct (Cw/Ct > 1) is established between the width Cw and the thickness Ct.
[0031] The first and second terminals 25-1 and 25-2 are terminals which are used to electrically
connect an external circuit to the coil 21 (the conductor member). The first and second
terminals 25-1 and 25-2 may be formed by attaching a conductor wire to both ends of
the conductor member by, for example, welding or soldering. However, in this embodiment,
the first and second terminals 25-1 and 25-2 are portions which prevent the peeling
caused by the external force or the heating and ensure the higher reliability, for
example, in a manner such that the end of the coil 21 (the conductor member) is bent
in a direction of intersecting a plane perpendicular to the axial direction of the
coil 21 (for example, see Japanese Patent Application Laid-Open No.
2011-205056). Then, the first and second terminals 25-1 and 25-2 are formed as multi-structures
by bending the wires in the axial direction from the viewpoint of a decrease in the
size and a decrease in the electric resistance. For example, the first and second
terminals 25-1 and 25-2 are formed as four-layered structures.
[0032] The core 22 is a member through which a magnetic flux caused by a magnetic field
generated in the coil 21 when supplying power to the coil 21 passes, and has magnetic
(for example, permeable) isotropy. For example, as illustrated in FIGS. 2 and 3, the
core 22 includes first and second core members 23 and 24 which have the same configuration
except that first and second terminal through holes for inserting the first and second
terminals 25-1 and 25-2 therethrough are provided in one core member. For example,
the first and second core members 23 and 24 are respectively formed by continuously
forming cylindrical portions 23b and 24b having the outer peripheral surfaces with
the same diameters as those of the disk portions 23a and 24a in the plate surfaces
of the disk portions 23a and 24a with disk shapes. In the example illustrated in FIG.
2, the first and second terminal through holes (which are illustrated in FIG. 2 and
are not illustrated in FIG. 3) are formed so as to penetrate the disk portion 23a
of the first core member 23 in a direction along the direction in which the first
and second terminals 25-1 and 25-2 are drawn from the coil 21 (in this embodiment,
the disk portion 23a in the axial direction of the coil 21). Then, twenty first and
twenty second attachment member through holes 23e and 24e are formed by penetrating
in the axial direction at the substantially middle positions (center positions) of
the disk portions 23a and 24a of the first and second core members 23 and 24 so that
the attachment member 40 passes through the attachment member through holes.
[0033] The core 22 is formed by overlapping the end surfaces of the respective cylindrical
portions 23b and 24b of the first and second core members 23 and 24 with such a configuration,
and a space which accommodates the coil 21 therein is formed inside the core 22. Then,
a second attachment member through hole 26 through which the attachment member 40
is inserted is formed from one surface of the core 22 to the other surface thereof
by the communication between the twenty first and twenty second attachment member
through holes 23e and 24e.
[0034] Then, in the example illustrated in FIG. 3, first and second protrusions 23f and
24f which protrude into the air core S are formed at a position facing the air core
S of the coil 21 in the core 22 when accommodating the coil 21 in the core 22. More
specifically, the first protrusion 23f which has a truncated cone shape and protrudes
into the air core S is formed at a position facing the air core S of the coil 21 in
the inner bottom surface of the first core member 23 when accommodating the coil 21
in the core 22, and the second protrusion 24f which has a truncated cone shape and
protrudes into the air core S is formed at a position facing the air core S of the
coil 21 in the inner bottom surface of the second core member 24 when accommodating
the coil 21 in the core 22. Accordingly, it is possible to further improve the inductance
of the winding element 20 by forming the first and second protrusions 23f and 24f.
Further, it is possible to adjust the inductance value of the winding element 20 by
adjusting the gap length between the respective protrusions 23f and 24f. Further,
the first and second protrusions 23f and 24f may be formed in an arbitrary shape so
as to control the inductance characteristic, and the shape is not limited to the truncated
cone shape and may be, for example, a columnar shape.
[0035] Then, in the first and second core members 23 and 24, the respective end surfaces
of the cylindrical portions 23b and 24b which overlap each other are provided with
convex portions 23c and 24c for the positioning operation and concave portions 23d
and 24d corresponding to the convex portions 23c and 24c. Furthermore, the convex
portions 23c and 24c and the concave portions 23d and 24d may not be provided. For
example, as illustrated in FIG. 3, the respective end surfaces of the cylindrical
portions 23b and 24b in the first and second core members 23 and 24 are provided with
first convex portions 23c-1 and 23c-2 and second convex portions 24c-1 and 24c-2 which
are arranged at the interval of 180° (at the opposite positions) in a substantially
columnar shape and the first concave portions 23d-1 and 23d-2 and the second concave
portions 24d-1 and 24d-2 which are arranged at the interval of 180° (at the opposite
positions) in a substantially columnar shape so that the first convex portions 23c-1
and 23c-2 and the second convex portions 24c-1 and 24c-2 with a columnar shape are
fitted thereinto. Then, the first convex portions 23c-1 and 23c-2, the second convex
portions 24c-1 and 24c-2, the first concave portions 23d-1 and 23d-2, and the second
concave portions 24d-1 and 24d-2 are respectively provided at the interval of 90°.
Furthermore, in FIG. 3, one of the first and second core members 23 and 24 is illustrated
(the first and second terminal through holes are not illustrated). Since the positioning
convex portions 23c and 24c are further provided in the respective end surfaces of
the cylindrical portions 23b and 24b, the first and second core members 23 and 24
may further reliably abut against each other.
[0036] The first and second core members 23 and 24 have a predetermined magnetic characteristic.
It is desirable that the first and second core members 23 and 24 be formed by the
same material from the viewpoint of a decrease in cost. The first and second core
members 23 and 24 may be pure iron subjected to the surface insulation process, but
in this embodiment, the first and second core members are formed by molding a soft
magnetic powder, for example, from the viewpoint whether a desired magnetic characteristic
(a comparatively high permeability) is easily realized and a desired shape is easily
molded.
[0037] The soft magnetic powder is a ferromagnetic metal powder. More specifically, for
example, a pure iron powder, an iron-base alloy powder (Fe-Al alloy, Fe-Si alloy,
sendust, permalloy, and the like) and an amorphous powder, and an iron powder of which
a surface is provided with an electric insulating film such as a phosphoric acid chemical
conversion coating film may be exemplified. The soft magnetic powder may be formed
by, for example, an atomizing method. Further, in general, the saturated magnetic
flux density is large in the same permeability. For this reason, it is desirable that
the soft magnetic powder be, for example, metal such as a pure iron powder, an iron-base
alloy powder, and an amorphous powder. The first and second core members 23 and 24
may be formed, for example, by powder-compacting the soft magnetic powder using an
existing general method.
[0038] Then, the winding element 20 is formed in a manner such that the coil 21 is accommodated
in an internal space formed by abutting the first and second core members 23 and 24
against each other so that the first and second terminals 25-1 and 25-2 are drawn
to the outside from the first and second terminal through holes. In this way, the
winding element 20 of this embodiment is a so-called pod type element in which the
coil 21 is built in the core 22. Furthermore, as illustrated in FIGS. 1 and 2, the
winding element 20 of this embodiment is formed by enclosing the entire coil 21 in
the core 22 so as to reduce the leaking magnetic flux, but an opening may be formed
in a portion corresponding to the peripheral surface of the coil 21 in the core 22.
[0039] The winding element fixing bracket 10 which fixes the winding element 20 having the
core 22 disposed at the outer periphery of the coil 21 to the predetermined member
30 includes a band plate-shaped body 10a which has a first attachment member through
hole 10d, a pair of plate-like leg portions 10b-1 and 10b-2 which is respectively
formed upright from both ends of the body 10a in the substantially perpendicular direction,
and a pair of plate-like fixation portions 10c-1 and 10c-2 which is respectively formed
upright outward from the respective ends of the respective leg portions 10b-1 and
10b-2 in the substantially perpendicular direction.
[0040] The first attachment member through hole 10d of the body 10a is a hole through which
the attachment member 40 is inserted, and is substantially formed at the center in
the length direction in consideration of the symmetry. Then, the respective fixation
portions 10c-1 and 10c-2 are respectively provided with fixation member through holes
10e-1 and 10e-2 to be attached with a fixation member (not illustrated) which fixes
the winding element fixing bracket 10 to the predetermined member 30. The fixation
member is a fastening member such as a screw and a bolt, and a screw groove may be
formed in the inner surfaces of the fixation member through holes 10e-1 and 10e-2.
[0041] The winding element fixing bracket 10 with such a configuration may be formed by,
for example, a bending process of bending a band-shaped member and a through hole
forming process of forming each through hole by punching. In this forming method,
the body 10a, the respective leg portions 10b-1 and 10b-2, and the respective fixation
portions 10c-1 and 10c-2 are integrally formed with each other, the respective leg
portions 10b-1 and 10b-2 are formed so as to be continuous to the body 10a, and the
respective fixation portions 10c-1 and 10c-2 are formed so as to be continuous to
the respective leg portions 10b-1 and 10b-2.
[0042] Then, in the winding element 20 and the winding element fixing bracket 10 with such
a configuration, for example, the attachment member 40 such as a through bolt is inserted
through the first attachment member through hole 10d of the winding element fixing
bracket 10 through a first washer and is inserted through the second attachment member
through hole 26 in the core 22 of the winding element 20 through a second washer.
Then, the other end is fastened by, for example, a fastening member such as a nut
through a third washer, so that the winding element fixing bracket 10 is attached
and fixed to the winding element 20. Accordingly, the winding element with the fixing
bracket is formed. Next, the winding element with the fixing bracket is disposed at
the installation position in the predetermined member (the loading member and the
mounting member) 30 attached with, for example, the winding element 20 of a circuit
board or a heat sink. Then, for example, a fastening member such as a screw is fastened
and fixed to the predetermined member 30 through the fixation member through holes
10e-1 and 10e-2 of the respective fixation portions 10c-1 and 10c-2 of the winding
element fixing bracket 10. Accordingly, the winding element 20 is fixed to the predetermined
member 30 by the winding element fixing bracket 10.
[0043] The winding element fixing bracket 10 with such a configuration is formed so that
the longitudinal section is formed in a hat shape (

in the side view), and is attached to the winding element 20 so as to embrace the
winding element 20 by inserting, for example, the attachment member 40 such as a bolt
through the first attachment member through hole 10d of the body 10a. Then, the winding
element fixing bracket 10 is fixed to the predetermined member 30 of, for example,
a heat sink by the pair of fixation portions 10c-1 and 10c-2. In this way, the winding
element fixing bracket 10 with such a configuration is attached to the winding element
20 so as to embrace the winding element 20 and is fixed to the predetermined member
30 by the pair of fixation portions 10c-1 and 10c-2. Accordingly, even when the predetermined
member 30 is set in the vertical direction, the winding element 20 may be reliably
attached. Then, since the winding element fixing bracket 10 with the aforementioned
configuration is attached to the winding element 20 so as to embrace the winding element
20 in this way, the core 22 may be protected even when the winding element is dropped
by mistake.
[0044] Then, the winding element fixing bracket 10 of this embodiment is formed so that
a gap of, for example, a sub-millimeter order is formed between the bottom surface
of the fixation portion 10c and the surface of the predetermined member 30 when attaching
the winding element 20 to the body 10a of the winding element fixing bracket 10 by
the attachment member 40 so as to be placed on the predetermined member 30. That is,
the respective lengths of the pair of leg portions 10b-1 and 10b-2 and the respective
thicknesses of the pair of fixation portions 10c-1 and 10c-2 are adjusted so that
the bottom surface of the core 22 of the winding element 20 protrudes in relation
to the respective bottom surfaces of the pair of fixation portions 10c-1 and 10c-2
when attaching the winding element 20 to the body 10a of the winding element fixing
bracket 10 by the attachment member 40. In other words, the respective lengths of
the pair of leg portions 10b-1 and 10b-2 and the respective thicknesses of the pair
of fixation portions 10c-1 and 10c-2 are adjusted so that the distance (length) from
the inner surface of the body 10a to the bottom surface of the fixation portion 10c
becomes shorter than the thickness of the core 22 (which includes the thickness of
the second washer when the second washer is interposed between the body 10a and the
core 22).
[0045] In the winding element fixing bracket 10 with such a configuration, when the winding
element fixing bracket 10 is fixed to the predetermined member 30 by the respective
fixation portions 10c-1 and 10c-2, the gap is removed, so that the respective bottom
surfaces of the respective fixation portions 10c-1 and 10c-2 abut against the surface
of the predetermined member 30. For this reason, a biasing force which presses the
winding element 20 against the predetermined member 30 is generated in the winding
element fixing bracket 10 within the elastic range. Accordingly, the winding element
20 is further reliably pressed against the predetermined member 30 by the winding
element fixing bracket 10 with the biasing force. As a result, when the predetermined
member 30 has a function of a heat sink, the heat which is generated by the winding
element 20 is further reliably transmitted to the predetermined member 30, and hence
a heat radiation performance may be improved.
[0046] Here, in order to maintain the spring function of the winding element fixing bracket
10 even when the biasing force is generated, there is a need to determine the material
of the bracket and the plate thickness, the plate width, and the length of the leg
portion so that plastic deformation does not occur.
[0047] When the length (dimension) of the gap is denoted by a in a case where the biasing
force is generated, as illustrated in FIG. 4A, the biasing force is equal to a force
F1 applied to the center position P so as to deform the body 10a outward by the length
a in the direction perpendicular to the body 10a at the center position P of the body
10a while only the winding element fixing bracket 10 is fixed to the predetermined
member 30 by the respective fixation portions 10c-1 and 10c-2. Accordingly, in order
to prevent the damage of the winding element fixing bracket 10 even when the biasing
force is generated, the maximum stress which is generated in the winding element fixing
bracket 10 needs to be smaller than the yielding point of the material of the winding
element fixing bracket 10 or the physical property value equal to the yielding point
(the deformation of the winding element fixing bracket 10 needs to be within the elastic
range) even when the center position P is displaced by the displacement amount a by
the action of the force F1.
[0048] Meanwhile, when the winding element 20 is attached to the attachment surface set
in the inclination direction or the vertical direction, as illustrated in FIG. 4B,
a force F2 generated by the gravity in the direction is applied to the center position
P of the first attachment member through hole 10d attached with the winding element
20 by the attachment member 40, so that the force F2 becomes maximal when the attachment
surface is set in the vertical direction. Accordingly, the maximum stress which is
generated in the winding element fixing bracket 10 by the force F2 needs to become
smaller than the yielding point of the material of the winding element fixing bracket
10 or the physical property value equal to the yielding point.
[0049] For this reason, when the winding element fixing bracket 10 is fixed to the predetermined
member 30 by the respective fixation portions 10c-1 and 10c-2 so that the winding
element 20 is attached to the center position P as described above, the spring constant
K1 in the direction of the force F1 needs to be decreased and the spring constant
K2 in the direction of the force F2 needs to be increased so as to decrease the stress
generated in the winding element fixing bracket 10. Accordingly, when the respective
points (respective bending points) where the respective leg portions 10b-1 and 10b-2
are formed upright from the body 10a are denoted by A and B and the respective points
(respective bending points) where the respective fixation portions 10c-1 and 10c-2
are formed upright from the respective leg portions 10b-1 and 10b-2 are denoted by
C and D, the length c between A and B needs to be lengthened and the respective lengths
k between C and A and between D and B need to be shortened in order to suppress the
plastic deformation of the winding element fixing bracket 10 when the force F1 and
the force F2 act on the winding element fixing bracket 10. As a result, an appropriate
range exists in the aspect ratio ζ (= c/k) of the winding element fixing bracket 10.
[0050] More specifically, the range of the aspect ratio ζ and the length k not causing the
plastic deformation even when the force F1 and the force F2 act on the winding element
fixing bracket 10 may be obtained as below.
[0051] To begin with, firstly, the force F1 acts on the winding element fixing bracket 10
so as to cause the deformation indicated by the two-dotted chain line of FIG. 4A when
the force F1 acts on the winding element fixing bracket 10. As a result, the maximum
stress σ
CA (1)/E which is obtained by dividing the maximum stress by the Young's modulus E and acts
on a position between C and A, that is, a position on the leg portion 10b-1 of the
winding element fixing bracket 10 is expressed by the following equation (1), and
the maximum stress σ
AP (1)/E which is obtained by dividing the maximum stress by the Young's modulus E and acts
on a position between A and P, that is, a portion from one end A of the body 10a of
the winding element fixing bracket 10 to the center position P is expressed by the
following equation (2). Furthermore, t is the thickness (plate thickness) of the winding
element fixing bracket 10.
[0052] [Equation 1]

[0053] [Equation 2]

[0054] As understood from Equation (1) and Equation (2), the maximum stress σ
CA (1) and the maximum stress σ
AP (1) are functions of the Young's modulus E, the displacement amount a, and the shape
(t, c, and k) of the winding element fixing bracket 10.
[0055] Further, secondly, the force F2 acts on the winding element fixing bracket 10 so
as to cause the deformation indicated by the two-dotted chain line of FIG. 4B when
the force F2 acts on the winding element fixing bracket 10. As a result, the maximum
stress σ
CA (2) which acts on a position between C and A is expressed by the following equation (3),
the maximum stress σ
AP (2) which acts on a position between A and P is expressed by the following equation (4),
and the maximum stress σ
PB (2) which acts on a position between P and B, that is, a portion from the center position
P of the body 10a of the winding element fixing bracket 10 to the other end B is expressed
by the following equation (5). Then, the maximum stress σ
BD (2)/E which acts on a position between B and D, that is, the leg portion 10b-2 of the
winding element fixing bracket 10 is expressed by the following equation (6). Furthermore,
b is the width (the plate width and the band width) of the winding element fixing
bracket 10.
[0056] [Equation 3]

[0057] [Equation 4]

[0058] [Equation 5]

[0059] [Equation 6]

[0060] Furthermore, the respective maximum stresses σ
CA, σ
AP, σ
PB, and σ
BD generated between C and A, between A and P, between P and B, and between B and D
are respectively generated at the point C, the point P, the point P, and the point
D.
[0061] As understood from Equation (3) to Equation (6), the maximum stress σ
CA (2), the maximum stress σ
AP (2), the maximum stress σ
PB (2), and the maximum stress σ
BD (2) are functions of the force F2 and the shape (t, b, c, and k) of the winding element
fixing bracket 10.
[0062] Here, in a case where the force F1 and the force F2 act on the winding element fixing
bracket 10, the respective stresses generated by the force F1 and the force F2 are
added when the bending directions are equal to each other in the respective regions,
and the respective stresses generated by the force F1 and the force F2 are counterbalanced
when the bending directions are opposite to each other. Accordingly, referring to
the modified aspect indicated by the two-dotted chain line of FIG. 4A and the modified
aspect indicated by the two-dotted chain line of FIG. 4B, the respective stresses
caused by the force F1 and the force F2 between C and A are added, the respective
stresses caused by the force F1 and the force F2 between A and P are counterbalanced,
the respective stresses caused by the force F1 and the force F2 between P and B are
added, and then the respective stresses caused by the force F1 and the force F2 between
B and D are counterbalanced. Accordingly, the maximum stress caused by the force F1
and the force F2 is generated at the point P or the point C, the maximum stress of
the point P is expressed by the addition of Equation (1) and Equation (5), and the
maximum stress of the point C is expressed by the addition of Equation (2) and Equation
(3).
[0063] Then, in order to search for the aforementioned range in the winding element fixing
bracket 10, the right sides of Equation (1), Equation (2), Equation (3), and Equation
(5) are expressed by using the length k and the aspect ratio ζ based on the relation
of the aspect ratio ζ = c/k, and the length k and the aspect ratio ζ are changed so
as to calculate the maximum stress σ
AP (1 + 2) at the point P and the maximum stress σ
CA (1 + 2) at the point C when the forces F1 and F2 act simultaneously.
[0064] FIGS. 5A and 5B are diagrams illustrating the contour lines of the maximum stresses
σ
AP (1 + 2)/E and σ
CA (1 + 2)/E which are obtained by dividing the maximum stress by the Young's modulus of the
aluminum alloy of which the displacement amount a is 0.2 mm when ζ is changed in the
range from 0 to 3 and k is changed in the range from 0.02 to 0.07. FIGS. 6A and 6B
are diagrams illustrating the contour lines of the maximum stresses σ
AP (1 + 2)/E and σ
CA (1 + 2)/E which are obtained by dividing the maximum stress by the Young's modulus of the
aluminum alloy of which the displacement amount a is 1.5 mm when ζ and k are changed
in the range of FIGS. 5A and 5B. FIG. 7 is a diagram illustrating the contour lines
of the maximum stresses σ
AP (1 + 2)/E and
σCA
(1 + 2)/E which are obtained by dividing the maximum stress by the Young's modulus of non-magnetic
stainless steel SUS304 of which the displacement amount a is 0.75 mm when ζ and k
are changed in the range of FIGS. 5A, 5B, 6A, and 6B. FIGS. 5A, 6A, and 7 illustrate
the calculation result of σ
AP (1 + 2)/E at the point P, and FIGS. 5B and 6B illustrate the calculation result of
CA (1 + 2)/E at the point C. In FIGS. 5A to 7, the horizontal axis indicates k expressed by
the unit m and the vertical axis indicates ζ.
[0065] The calculation condition is as below. In FIGS. 5A to 7, the length k is set to the
range from 0.02 to 0.07 [m] and the aspect ratio ζ is set to the range from 0 to 3.
Here, it is desirable that the winding element fixing bracket 10 have a non-magnetic
property so as not to influence the characteristic of the winding element 20 since
the winding element fixing bracket is used for the winding element. As the non-magnetic
material, for example, aluminum or stainless steel may be exemplified. The Young's
modulus E of aluminum is 70 [GPa], and the Young's modulus E of non-magnetic stainless
steel (SUS304) is 205 [GPa].
[0066] Further, the displacement amount a is defined as below. The winding element 20 is
used in various temperature environments, and when power is supplied to the winding
element, the coil 21 generally generates heat, so that the temperature of the winding
element increases. When the temperature of the winding element 20 increases, the temperature
of the winding element fixing bracket 10 also increases, so that the winding element
fixing bracket 10 is thermally expanded in a general case. Accordingly, in order to
generate the biasing force, for example, the gap length (displacement amount) a needs
to be a positive value (a value larger than 0) in the minimum use temperature defined
by the specification. For example, the use temperature of the winding element 20 is
set to the temperature range of -20 [°C] to +150 [°C] in consideration of, for example,
the use temperature at midwinter and the heatproof temperature of the insulating material.
When the use temperature range and the dimension tolerance of ± 0.2 [mm] of the winding
element 20 are considered, the displacement amount a becomes the range from 0.2 to
1.5 [mm] (0.2 ≤ a ≤ 1.5).
[0067] Further, the force F2 is defined as below. Since the dimension of the winding element
fixing bracket 10 increases depends on the winding element 20, the weight of the winding
element 20 is obtained by considering that the height and the diameter of the winding
element 20 are equal to the length k and the length c of the winding element fixing
bracket 10. The gravity F2 which acts on the winding element 20 is set to the range
from 0.1 [N] to 926.7 [N] by a change in k and ζ. Then, the force F2 may be only the
gravity (mg) acting on the winding element 20, but in this embodiment, a dropping
impact is considered. Then, the load of the dropping impact is set to five times (5
G) the gravity.
[0068] Then, the yielding point of stainless steel SUS304 and the bearing force (elastic
limit) of aluminum 5052 alloy are set as listed in Table 1.
[0069]
[Table 1]
|
E (GPa) |
σ0.2(MPa) |
σ0.2/E |
SUS304 |
205 |
284 |
1.4E-03 |
A5052-O |
70 |
90 |
1.3E-03 |
A5052-H32 |
70 |
195 |
2.8E-03 |
A5052-H34 |
70 |
215 |
3.1E-03 |
A5052-H36 |
70 |
240 |
3.4E-03 |
A5052-H38 |
70 |
255 |
3.6E-03 |
[0070] In Table 1, regarding SUS304 and tempered aluminum alloys (5052 alloys) of O, H32,
H34, H36, and H38 based on JIS, the respective values of the Young's modulus E [GPa],
the yielding point, or the bearing forces σ
0.
2 [MPa] and σ
0.
2/E are described.
[0071] The calculation result based on the conditions are illustrated in FIGS. 5A to 7.
In FIGS. 5A and 5B, a result is illustrated in the case where the winding element
fixing bracket 10 is formed by aluminum having a thickness of 2.0 [mm] and the displacement
amount a is 0.2 [mm] at minimum. In FIGS. 6A and 6B, a result is illustrated in the
case where the winding element fixing bracket 10 is formed by aluminum having a thickness
of 2.0 [mm] and the displacement amount a is 1.5 [mm] at maximum. Then, in FIG. 7,
a result is illustrated in the case where the winding element fixing bracket 10 is
formed by SUS304 having a thickness of 2.0 [mm] and the displacement amount a is 0.75
[mm]. Furthermore, the explanatory notes of at the right side of each drawing illustrate
the values of the contour lines of σ
AP (1 + 2)/E and σ
CA (1 + 2)/E, the contour lines illustrated in FIGS. 5A and 5B and FIGS. 6A and 6B illustrate
only a range which is smaller than the value σ
0.2/E obtained by dividing the elastic limit of the tempered aluminum 5052 alloy of H38
with the highest elastic limit by the Young's modulus of the aluminum alloy, and the
contour line illustrated in FIG. 7 illustrates only a range which is smaller than
the value σ
0.2/E obtained by dividing the yielding point of SUS304 by the Young's modulus of SUS304.
[0072] When the dimensions, the shapes, and the conditions of the winding element fixing
brackets 10 are the same, in the winding element fixing bracket 10 of SUS304, the
spring constant K1 in the direction of the force F1 increases and the stress generated
in the winding element fixing bracket 10 increases. For this reason, as understood
from FIGS. 5A to FIG. 7, in the condition in which the plastic deformation of the
winding element fixing bracket 10 does not occur (the condition in which the maximum
stress is less than the yielding point or the bearing force of σ
0.
2), the range of the length k and the aspect ratio ζ substantially does not exist in
SUS304, where the range slightly exists in the vicinity of k = 0.04 [m] and ζ = 3.
Accordingly, it is desirable that the winding element fixing bracket 10 be formed
by aluminum (including an alloy thereof).
[0073] For this reason, regarding aluminum, when the range of the length k and the aspect
ratio ζ in which σ
AP (1 + 2)/E, and σ
CA (1 + 2)/E obtained by dividing the maximum stresses σ
AP (1 + 2) and σ
CA (1 + 2) generated at the points P and C in the event of the force F1 and the force F2 by
the Young's modulus E of aluminum simultaneously become smaller than the bearing force
σ
0.2/E of aluminum is obtained from the results of FIGS. 5A and 5B and FIGS. 6A and 6B,
the range of the length k and the aspect ratio ζ is illustrated as the hatching of
FIG. 8 in the case of, for example, A5052-H38 based on JIS.
[0074] FIG. 8 is a diagram illustrating a range of the length k and the aspect ratio ζ when
the winding element fixing bracket of the embodiment is formed by aluminum alloy (A5052-H38).
In FIG. 8, the horizontal axis indicates the length k and the vertical axis indicates
the aspect ratio ζ.
[0075] As illustrated in FIG. 8, when the displacement amount a is a minimum value of 0.2
[mm], it is necessary to satisfy at least the inequation of 0.0236 x k -1.07 ≤ ζ (=
c/k) ≤ 0.0079 x k - 1.9 in the range of 0.02 ≤ k ≤ 0.07 [m]. Then, when the displacement
amount a is a maximum value of 1.5 [mm], it is necessary to satisfy at least the inequation
of 7275.4 x k
2 - 592.14 x k + 14.612 ≤ c/k ≤ 0.0053 x k
-2 in the range of 0.02 ≤ k ≤ 0.07 [m].
[0076] Furthermore, in the description above, the result of A5052-H38 is illustrated in
FIG. 8, but even in the other tempered A5000 series or A3000 series, the result obtained
according to the same method. Regarding aluminum, there is a range of the length k
and the aspect ratio in which σ/E at the point P and σ/E at the point C in the event
of the force F1 and the force F2 simultaneously become smaller than the bearing force
σ
0.2/E of aluminum. For this reason, it is desirable to use tempered aluminum H12 to H38
of A3000 series or A5000 series.
[0077] In this way, the length c between A and B, the length k between C and A, and the
length k between D and B in the body 10a, the pair of leg portions 10b, and the pair
of fixation portions 10c of the winding element fixing bracket 10 of this embodiment
are set so that the respective maximum stresses σ which are generated when a biasing
force and a predetermined dropping impact load generated when fixing the winding element
fixing bracket onto the predetermined member 30 without the gap of the dimension a
respectively act on the winding element fixing bracket 10 are smaller than the yielding
point of the material forming the winding element fixing bracket 10 or the physical
property value equal to the yielding point in a state where the thicknesses t and
the band widths b of the body 10a, the pair of leg portions 10b, and the pair of fixation
portions 10c are given. For this reason, the winding element fixing bracket 10 of
this embodiment is not broken even when the biasing force or the predetermined dropping
impact load acts in the range of the design.
[0078] Furthermore, in the description above, the longitudinal sectional shape of the winding
element fixing bracket 10 is a hat shape of

in the side view so that the respective fixation portions 10c-1 and 10c-2 are substantially
formed upright outward in the perpendicular direction from the respective leg portions
10b-1 and 10b-2, but may be a hat shape of Π. In such a case, the winding element
fixing bracket 10 is formed so that the distance between the respective ends of the
pair of fixation portions 10c-1 and 10c-2 becomes longer than the diameter of the
winding element 20 to be fixed. The winding element fixing bracket 10 in such a case
may be analyzed as described above. Further, although it is not illustrated in the
drawings, the region AB may be used in a flat state or may be provided with an opening
so as to reduce the bending rigidity. Accordingly, when a displacement a is generated
at the point P, the stress which is generated between the region A and B due to the
force F1 may be reduced. Further, the bending rigidity may be improved by forming
an uneven portion in the region CA and the region DB. Accordingly, there is an effect
that the stress generated between the regions CA and DB due to the force F2 may be
reduced.
[0079] The present invention has been appropriately and sufficiently described through the
embodiment while referring to the drawings in the description above in order to express
the present invention, but it should be understood by the person skilled in the art
that the aforementioned embodiment may be easily modified and/or improved. Accordingly,
unless the modified aspects or the improved aspects which are made by the person skilled
in the art depart from the scope of claims, it is considered that the modified aspects
or the improved aspects are included in the scope of claims.
The present invention provides a winding element fixing bracket and a winding element
with the fixing bracket that enable reliable attachment of a winding element to an
attachment surface even if the surface is set in the vertical direction and protection
of a core even in the event of dropping by mistake. A winding element fixing bracket
of the present invention is the winding element fixing bracket which fixes a winding
element with a coil and a core accommodating the coil to a predetermined member, and
includes a band plate-shaped body which includes a first attachment member through
hole, a pair of leg portions which is formed upright from both ends of the body, and
a pair of fixation portions which is formed upright outward from respective ends of
the respective leg portions.