BACKGROUND
[0001] The present disclosure relates to a transformer arrangement comprising an air duct
element for cooling a coil assembly and/or a core of the transformer arrangement,
a respective air duct element, and a cooling system comprising such an air duct element.
[0002] Transformers are used to convert electricity from a first voltage level to an electricity
at a second voltage level which is either higher or a lower than the first voltage
level. A typical transformer comprises two sets of insulated wire coils - herein also
referred to as "windings" for short- around a ferromagnetic core of the transformer,
namely a high voltage (HV) winding and low voltage (LV) winding. The LV winding often
constitutes an inner winding, and the HV winding an outer winding. When electrical
power is applied to one winding that draws power from a source of voltage, it is then
magnetically transferred to another winding that delivers power to a load at a transformed
voltage. The ratio of turns in one winding to the turns in another winding is the
same as the ratio of the voltage of the source to the voltage of the load.
[0003] In a dry-type transformer, typically used for power distribution networks, no dielectric
liquid is used for insulating the windings. A dry-type transformer performance is
principally highly limited by temperature rise during operation due to losses and
heat dissipation.
[0004] Presently, centrifugal fans with very high air-flow rate are typically used for air-forced
cooling of a dry-type transformer. Fig. 1 schematically shows a centrifugal fan 200
positioned in a lower region of a transformer. The transformer comprises a core 500,
an inner winding 600, and an outer winding 700. Heat-producing parts of the transformer
are primarily its windings and the core. The centrifugal fan 200 generates an airflow
800 directed at the windings 600, 700 and the core 500.
[0005] However, a problem here is that much of the air expelled by the centrifugal fan 200
does not specifically reach those parts of the transformer whose cooling is particularly
important. This results in an airflow waste and a reduced cooling efficiency.
[0006] It is also known to use a fan and an air duct coupled to the fan to direct cooling
air to a dry-type transformer. However, also here only limited efficiency can be achieved
with the known solutions.
[0007] Therefore, there is a need for a technology providing improved cooling of a transformer,
particularly a dry-type transformer.
SUMMARY
[0008] According to the present invention, a transformer arrangement is provided which comprises
a transformer core, defining a longitudinal axis, a coil assembly wound around the
core, the coil assembly comprising a winding, and an air duct element configured and
arranged to direct an airflow portion to a bottom end of the winding and/or along
an inner or outer surface area of the winding and/or to at least one cooling gap provided
in the transformer arrangement for cooling the coil assembly and/or the core, wherein
a distance between the air duct element and the bottom end of the winding is less
than 50 mm.
[0009] The air duct element allows for directing the airflow portion in a particular effective
way to the bottom end of the winding and/or along the inner or outer surface area
of the winding and/or at least one cooling gap for cooling the coil assembly and/or
the core, i.e. to parts of the transformer arrangement whose cooling during operation
of the transformer is of particular importance. In this way, an airflow waste or loss
can be significantly reduced. The air duct element is particularly suited to be adapted
or configured to deliver the airflow portion in a particularly precise manner to respective
areas or parts of the transformer arrangement. Air can be substantially prevented
from flowing to regions where it is not needed for the desired cooling effect. Moreover,
the air duct element can be easily configured such that generation of turbulences
is significantly reduced.
[0010] Various embodiments may implement one or more of the following features:
[0011] The transformer arrangement may comprise a dry-type transformer. The coil assembly
may comprise two or more windings. The windings may comprise at least one low-voltage
winding and at least one high-voltage winding. The low-voltage winding may be an inner
winding and the high-voltage winding may be an outer winding.
[0012] The bottom end of the winding may be the downward facing end of the winding when
the transformer is set up in an operating position.
[0013] The distance is the smallest distance between two parts, e.g., the air duct element
and the bottom end of the winding.
[0014] The distance may be less than 40 mm, less than 30 mm, less than 20 mm, less than
10 mm, or less than 5 mm. Generally, the smaller the distance, the better the guidance
of the airflow. However, a minimum distance is necessary in order not to generate
electrical problems between a fan, which may be provided for generating and delivering
an airflow into the airduct element, and the winding of the transformer arrangement.
This is naturally even more critical in the case of a high-voltage winding than in
the case of a low-voltage winding. Thus, minimum distances may differ for high-voltage
and low-voltage windings. The minimum distance is also dependent on the power of the
transformer arrangement.
[0015] The airduct element may be made from a dielectrical material and/or a nonconductive
material. This is advantageous because it reduces the risk of undesirable electrical
effects being triggered by the airduct element. The airduct element may thus serve
as an electric isolation between the transformer and its windings and the fan or other
air guiding parts.
[0016] The air duct element may be manufactured by additive manufacturing. This particularly
allows for a cheap, easy and fast manufacturing option of the airduct element and
its particularly suitable geometries.
[0017] The air duct element may comprise an airflow portion opening as an outlet of an airflow
portion, wherein the shape of the airflow portion opening matches the shape of an
outer or inner edge of the bottom end of the winding and/or the inner or outer surface
area of the winding, and/or at least one cooling gap provided in the transformer arrangement.
In this way, a particularly precise guidance of the airflow portion is further supported.
High losses of airflow may further be avoided by such matching shape. Reference to
matching shape may be understood as referring to shapes which are aligned to a high
degree as regards their geometry, extension and position. For example, the shape of
the airflow portion opening may, at the side adjacent the outside or inside of a winding,
correspond to the or part of the winding's bottom end's outside or inside geometry.
This may, for example, refer to the two-dimensional shape of said winding, e.g., when
seen at its footprint.
[0018] The airflow portion opening may just cover or be aligned with a segment of the bottom
end of the winding and/or along an inner or outer surface area of the winding and/or
to at least one cooling gap provided in the transformer arrangement for cooling the
coil assembly and/or the core. It may thus extend within a spatial area defined or
limited by two angular legs of an angle α whose angular vertex coincides with the
longitudinal axis, wherein α is between 5° and 350°, preferably between 10° and 270°,
preferably between 20° and 180°, preferably between 25° and 100°. Preferably, the
angle α lies in a plane perpendicular to the longitudinal axis. For example, the edge
of the airflow portion opening may extend in a plane perpendicular to the longitudinal
axis, wherein the angle α lies the same plane as the edge of the airflow portion opening.
[0019] The airflow portion opening may match the shape of the inner or outer edge of the
bottom end of the winding and/or the inner or outer surface area of the winding to
such a degree that at least 80% of the airflow exiting the airflow portion opening,
preferably at least 90% of the airflow, preferably at least 95% of the airflow, even
more preferably at least 98% of the airflow reaches and flows along the inner or outer
surface area of the winding and/or at least one cooling gap provided in the transformer
arrangement.
[0020] The transformer arrangement may further comprise a fan having a fan air outlet, wherein
the fan is configured and arranged to generate an airflow and to deliver the airflow
through the fan air outlet to an air inlet opening of the air duct element. Inner
surfaces of the air duct element for guiding the airflow from the air inlet opening
to the airflow portion opening are preferably smooth and without steps or sharp edges.
This further reduces generation of turbulences in the airflow and contributes to an
efficient cooling.
[0021] According to a further aspect of the invention, an air duct element is provided which
is configured to direct an airflow portion to an outer or inner edge of a bottom end
of a winding of a coil assembly of a transformer and/or along an inner or outer surface
area of a winding of a coil assembly of a transformer and/or to at least one cooling
gap provided in the transformer arrangement. The air duct element comprises an airflow
portion opening for outlet of the airflow portion. Preferably, the shape of the airflow
portion opening matches the shape of an outer or inner edge of the bottom end of the
winding and/or the inner or outer surface area of the winding, and/or at least one
cooling gap provided in the transformer arrangement.
[0022] The airflow portion opening may have a circumferentially closed form extending around
the longitudinal axis. This allows for a particular effective cooling.
[0023] According to a further aspect of the present disclosure an air duct element is provided
which is configured to be attached to a fan air outlet of a fan for cooling a dry-type
transformer, for example an air duct element as described above. The air duct element
is configured to divide an airflow generated by the fan and delivered through the
fan air outlet into at least a first airflow portion and a second airflow portion.
The air duct element is configured to direct the first airflow portion and the second
airflow portion to different individual parts of the transformer. Preferably, the
air duct element comprises a first airflow portion opening for outlet of the first
airflow portion. The first airflow portion opening has two opposing edge regions which
are at least partially curved in an identical direction. Preferably, the air duct
element is configured to divide the airflow generated by the fan and delivered through
the fan air outlet in a controlled manner into at least a first airflow portion and
a second airflow portion.
[0024] By dividing the airflow in a first airflow portion and a second airflow portion,
it is possible to guide cooling air to different specific or individual parts or portions
of the transformer. Since the parts of the transformer that generate particularly
much heat during operation of the transformer, such as the windings and the core,
typically have curved or substantially curved surface areas, the curved opposing edge
regions of the first airflow portion opening allow the cooling air to be directed
in a particularly targeted manner to the areas to be cooled. In this way, a significantly
increased cooling efficiency can be achieved. Moreover, providing the first airflow
portion opening with two opposing edge regions which are at least partially curved
in an identical direction makes it possible to adapt the first airflow portion opening
particularly well to the shape of an area to be cooled, which particularly reduces
formation of turbulences in the airflow within the air duct element. This also contributes
to the increase in efficiency.
[0025] The achievable increase in cooling efficiency allows an increase in transformer power
performance to be achieved. For example, a performance increase of about 10 % can
be achieved.
[0026] Further, the increase in cooling efficiency may allow to reduce the number of airgaps
in a winding, e. g. in an LV winding, and/or to reduce the size of such airgaps.
[0027] Accordingly, also a reduction of the transformer size and weight can be achieved.
[0028] The air duct element is particularly suited for applications where a maximum airflow
is set, such as for example in case of wind turbines.
[0029] The individual parts of the transformer may be selected from a winding of the transformer,
an outer surface area of a winding of the transformer, an inner surface area of a
winding of the transformer, a gap area between two windings or within a winding of
the transformer, and an outer surface area of a core of the transformer. The winding
may be a high voltage winding or a low voltage winding. The low voltage winding may
be an inner winding and the high voltage winding may be an outer winding.
[0030] For example, the air duct element may be configured to direct the first airflow portion
to an outer surface area of an outer winding, and to direct the second airflow portion
to an inner surface area of the outer winding or to a gap area between the outer winding
an inner winding.
[0031] The transformer may have a rated power of for example between 0.5 MVA and 40 MVA.
[0032] The air duct element may be made from a dielectrical material and/or a nonconductive
material. In this way, unwanted electrical interference of the air duct element with
the electrical function of the transformer can be prevented.
[0033] The air duct element may be manufactured by additive manufacturing, for example by
3D-printing. This enables particularly cost-effective production of the air duct element.
Particularly, in this way, the air duct element can be produced quickly and easily
at low cost.
[0034] The air duct element may be configured to be reversibly connectable to the fan air
outlet.
[0035] The first airflow portion opening may comprise an edge extending in a first airflow
portion opening plane.
[0036] The air duct element may comprise an air inlet opening for receiving the airflow
generated by the fan. The air inlet opening may comprise an edge extending in an air
inlet opening plane. The edge of the first airflow portion opening may have a length
that is greater than the distance between the air inlet opening and the first airflow
portion opening. In this way, the distance that the air travels between the air inlet
opening and the first airflow portion opening can be kept comparatively short. In
this way flow losses within the air duct element can be kept particularly low.
[0037] The first airflow portion opening plane and the air inlet opening plane may be parallel.
The edge of the first airflow portion opening may have a length that is greater than
the distance between the first airflow portion opening plane and the air inlet opening
plane.
[0038] Alternatively, the first airflow portion opening plane and the air inlet opening
plane may include an angle which is greater than 0°. This is generally advantageous
with regard to an effective and space-saving arrangement of the fan. The angle may
be less than 25°, preferably less than 20°.
[0039] At least a segment of the first airflow portion opening may extend along an arc of
a first circle. This is a particularly advantageous design because the above-mentioned
individual parts of the transformer are typically shaped at least partially circular-cylindrical.
However, this is as well advantageous, for example, if a winding to be cooled is shaped
so that it has a normal cross-section that is in the form of a square with "rounded
corner areas", since the configuration of the first airflow portion opening may be
such that the first circle matches the shape of one of the corner areas.
[0040] The arc of the first circle may be defined by an angle α of at least 30°, preferably
at least 60°, preferably at least 90°. The first airflow portion opening may have
a circumferential closed form. For example, the angle α may be 360°.
[0041] The first airflow portion opening may have an arcual length S measured along the
first circle and a radial thickness Δr measured perpendicular to the first circle,
wherein the relation S/Δr fulfills 1.2 <_ S/Δr <_ 200, preferably 1.5 <_ S/Δr <_ 150,
preferably 2 <_ S/Δr <_ 100, preferably 2 ≤ S/Δr ≤ 50.
[0042] In principle, it is not mandatory that the first airflow portion opening is shaped
so that it extends along an arc. In such a case, the first airflow portion opening
may extend along a line which is at least partially curved and/or at least partially
straight. In this case, the above relations may apply analogously, wherein the "arcual
length S" is replaced by the "extension of the first airflow portion opening measured
along the line" and the radial thickness Δr is replaced by a thickness perpendicular
to the line. This length may also be briefly referred to as the "edge length" of the
first airflow portion opening.
[0043] The arcual length S or the edge length of the first airflow portion opening may be
larger than the distance between the air inlet opening and the first airflow portion
opening.
[0044] Inner walls of the air duct element for guiding the first airflow portion and the
second airflow portion may be shaped stepless. This substantially contributes to reducing
formation of turbulences.
[0045] The air duct element may further comprise a second airflow portion opening for outlet
of the second airflow portion.
[0046] The first airflow portion opening and the second airflow portion opening may extend
in one plane. Specifically, the edge of the first airflow portion opening and the
edge of the second airflow portion opening may extend in one plane. This allows for
example the two openings to be positioned particularly close to an outer surface area
and an inner surface area of a winding.
[0047] The second airflow portion opening may have two opposing edge regions being at least
partially curved in an identical direction.
[0048] The two opposing edge regions of the first flow portion opening and the two opposing
edge regions of the second airflow portion opening may be curved in the identical
direction. This allows to fit particularly well to corresponding parts pf the transformer.
[0049] At least a segment of the second airflow portion opening may extend along a second
circle. The second circle may have a smaller radius than the first circle. The first
circle and the second circle may be formed so that they share a same center point.
[0050] The second airflow portion opening may be configured analogous to the first airflow
portion opening.
[0051] The second airflow portion opening may have a circumferential closed form.
[0052] The arc of the second circle may be defined by an angle α2 of at least 30°, preferably
at least 60°, preferably at least 90°.
[0053] The second airflow portion opening may have an arcual length S2 measured along the
second circle and a radial thickness Δr2 measured perpendicular to the second circle,
wherein the relation S2/Δr2 fulfills 1.2 ≤ S2/Δr2 ≤ 200, preferably 1.5 ≤ S2/Δr2 ≤
150, preferably 2 ≤ S2/Δr2 ≤ 100, preferably 2 ≤ S2/Δr2 ≤ 50. In the case of a non-circular
extension of the second airflow portion opening, the above relationships apply again
analogously.
[0054] The shape of the first airflow portion opening may be a transformation of the shape
of the second airflow portion opening in form of a centric stretching with respect
to a center.
[0055] The air duct element may be further configured to divide the airflow into a third
airflow portion, wherein the air duct element further comprises a third airflow portion
opening for outlet of the third airflow portion.
[0056] The air duct element may be further configured to divide the airflow into a fourth
airflow portion, wherein the air duct element further comprises a fourth airflow portion
opening for outlet of the fourth airflow portion. A fifth, sixth, seventh, etc. airflow
portion opening may be provided in a corresponding manner.
[0057] The first airflow portion opening and the third airflow portion opening may extend
in different planes. Specifically, the edge of the first airflow portion opening may
extend in a first plane and the edge of the third airflow portion opening may extend
in a second plane, wherein the second plane differs from the first plane. The first
and the second plane may be parallel. In this way, the first airflow portion opening
can be positioned particularly suitably close to a first winding of the transformer
and the third airflow portion opening particularly close to a second winding of the
transformer extending further down than the first winding. For example, the first
airflow portion opening can be positioned particularly suitably close to an outer
surface of an outer winding of the transformer and the third airflow portion opening
particularly close to, for example below an inner winding of the transformer. The
outer winding may be a high voltage winding, and the inner winding may be a low voltage
winding. The inner winding may have at least one internal gap. Alternatively, the
inner winding may have no internal gap.
[0058] The third airflow portion opening may have two opposing edge regions being at least
partially curved in an identical direction.
[0059] The two opposing edge regions of the first airflow portion opening and the two opposing
edge regions of the third airflow portion opening may be curved in the identical direction.
[0060] At least a segment of the third airflow portion opening may extend along a third
circle. The third circle may have a smaller radius than the second circle. The third
circle and the first circle may be formed so that they share a same center point.
The arc of the third circle may be defined by an angle α3 of at least 30°, preferably
at least 60°, preferably at least 90°.
[0061] The third airflow portion opening may be configured analogous to the first airflow
portion opening.
[0062] The third airflow portion opening may have a circumferential closed form.
[0063] The third airflow portion opening may have an arcual length S3 measured along the
third circle and a radial thickness Δr3 measured perpendicular to the third circle,
wherein the relation S3/Δr3 fulfills 1.2 ≤ S3/Δr3 ≤ 200, preferably 1.5 ≤ S3/Δr3 ≤
150, preferably 2 ≤ S3/Δr3 ≤ 100, preferably 2 ≤ S3/Δr3 ≤ 50. In the case of a non-circular
extension of the third airflow portion opening, the above relationships apply again
analogously.
[0064] According to a further aspect of the invention, a cooling system for cooling a dry-type
transformer is provided which comprises a fan and an air duct element according to
the present disclosure. The fan has a fan air outlet and is configured to generate
an airflow and to deliver the airflow through the fan air outlet. The air duct element
is attached to the fan air outlet.
[0065] The air duct element may be directly attached to the fan. The air duct element may
comprise an air inlet opening for receiving the airflow generated by the fan. The
air inlet opening may be attached particularly in an air-tight manner to the fan air
outlet.
[0066] The cooling system may comprise an intermediate piece disposed between the fan and
the air duct element. The intermediate piece may be coupled directly, particularly
in an air-tight mannerto the fan air outlet and to the air inlet opening.
[0067] According to a further aspect of the invention, a dry-type transformer is provided
which comprises a core, a coil assembly wound around the core, and a cooling system
according to the present disclosure or an air duct element according to the present
disclosure. The coil assembly comprises an outermost winding and an innermost winding.
[0068] The outermost winding may be a high-voltage winding. The innermost winding may be
a low-voltage winding.
[0069] The core may comprise a linear core segment, where the outermost winding and the
innermost winding are wound around the linear core segment. The linear core segment
may be oriented vertically.
[0070] The first airflow portion opening of the air duct element may be configured and arranged
to direct the first airflow portion along an outer surface area of the outermost winding.
[0071] The second airflow portion opening of the air duct element may be configured and
arranged to direct the second airflow portion into a gap area formed by the coil assembly
between the outermost winding and the innermost winding or to an inner surface area
of the outermost winding.
[0072] The third airflow portion opening of the air duct element may be configured and arranged
to direct the third airflow portion partially along an outer surface area of the innermost
winding and/or partially along an inner surface area of the innermost coil.
[0073] The distance between the coil assembly and the air duct element may be less than
10 cm, preferably less than 5 cm.
[0074] In particular, the present disclosure comprises the following aspects:
- 1. A transformer arrangement, comprising
a transformer core (50), defining a longitudinal axis (L),
a coil assembly wound around the core (50), the coil assembly comprising a winding
(60, 70), and
an air duct element (2) configured and arranged to direct an airflow portion (62,
64, 66) to a bottom end (69, 79) of the winding (60, 70) and/or along an inner or
outer surface area (72, 74; 65, 67) of the winding (60, 70) for cooling the coil assembly
and/or the core (50),
wherein a distance (δ) between the air duct element (2) and the bottom end (69, 79)
of the winding (60, 70) is less than 50 mm.
- 2. The arrangement of aspect 1, wherein the distance (δ) is less than 40 mm, preferably
less than 30 mm, preferably less than 20 mm, preferably less than 10 mm.
- 3. The arrangement of aspect 1 or 2,
wherein the airduct element (2) is made from a dielectrical material and/or a nonconductive
material; and/or
wherein the air duct element (2) is manufactured by additive manufacturing.
- 4. The arrangement of any of the preceding aspects, wherein the air duct element (2)
comprises an airflow portion opening (10, 20, 30) for outlet of the airflow portion,
wherein the shape of the airflow portion opening (10, 20, 30) matches the shape of
an outer or inner edge of the bottom end (69, 79) of the winding (60, 70) and/or the
inner or outer surface area (72, 74, 65, 67) of the winding, and/or at least one cooling
gap provided in the transformer arrangement.
- 5. The arrangement of aspect 4, wherein the airflow portion opening (10, 20, 30) extends
within a spatial area defined by two angular legs of an angle α whose angular vertex
coincides with the longitudinal axis (L), wherein α is between 5° and 350°, preferably
between 10° and 270°, preferably between 20° and 180°, preferably between 25° and
100°.
- 6. The arrangement of any of aspect 4 or 5, wherein the airflow portion opening (10,
20, 30) matches the shape of the inner or outer edge of the bottom end (69, 79) of
the winding (60, 70) and/or the inner or outer surface area (72, 74, 65, 67) of the
winding to such a degree that at least 80% of the airflow exiting the airflow portion
opening (10, 20, 30), preferably at least 90% of the airflow, preferably at least
95% of the airflow, even more preferably at least 98% of the airflow reaches and flows
along the inner or outer surface area (72, 74, 65, 67) of the winding and/or at least
one cooling gap provided in the transformer arrangement.
- 7. The arrangement of any of the preceding aspects,
further comprising a fan (4) having a fan air outlet (42), the fan (4) being configured
and arranged to generate an airflow (6) and to deliver the airflow (6) through the
fan air outlet (42) to an air inlet opening (22) of the air duct element (2),
preferably wherein inner surfaces of the air duct element (2) for guiding the airflow
(6) from the air inlet opening (22) to the airflow portion opening (10, 20, 30) are
smooth and without steps or sharp edges.
- 8. An air duct element (2), configured to direct an airflow portion (62, 64, 66) to
an outer or inner edge of a bottom end (69, 79) of a winding (60, 70) of a coil assembly
of a transformer and/or along an inner or outer surface area (72, 74, 65, 67) of a
winding (60, 70) of a coil assembly of a transformer and/or to at least one cooling
gap provided in the transformer arrangement,
the air duct element (2) comprising an airflow portion opening (10, 20, 30) for outlet
of the airflow portion (62, 64, 66),
wherein the shape of the airflow portion opening (10, 20, 30) matches the shape of
an outer or inner edge of the bottom end (69, 79) of the winding (60, 70) and/or the
inner or outer surface area (72, 74, 65, 67) of the winding, and/or at least one cooling
gap provided in the transformer arrangement; and/or
wherein the airflow portion opening (10, 20, 30) has a circumferentially closed form
extending around the longitudinal axis (L).
- 9. An air duct element (2) configured to be attached to a fan air outlet (42) of a
fan (4) for cooling a dry-type transformer, preferably the air duct element of aspect
8,
wherein the air duct element (2) is configured to divide an airflow (6) generated
by the fan (4) and delivered through the fan air outlet (42) into at least a first
airflow portion (62) and a second airflow portion (64),
wherein the air duct element (2) is configured to direct the first airflow portion
(62) and the second airflow portion (64) to different individual parts of the transformer.
- 10. The air duct element (2) of aspect 9,
wherein the air duct element (2) comprises a first airflow portion opening (10) for
outlet of the first airflow portion (62), the first airflow portion opening (10) having
two opposing edge regions (12, 14) being at least partially curved in an identical
direction.
- 11. The air duct element of aspect 9 or 10, wherein the individual parts of the transformer
are selected from a winding (60, 70) of the transformer, an outer surface area (72)
of a winding (70) of the transformer, an inner surface area (74) of a winding of the
transformer, a gap area (80) between two windings (60, 70) or within a winding of
the transformer, and an outer surface area (52) of a core (50) of the transformer.
- 12. The air duct element of any of aspects 9 to 11, wherein the air duct element (2)
comprises an air inlet opening (22) for receiving the airflow (6) generated by the
fan (4),
wherein the edge of the first airflow portion opening (10) has a length that is greater
than the distance between the air inlet opening (22) and the first airflow portion
opening (10).
- 13. The air duct element of any of aspects 9 to 12, wherein at least a segment of
the first airflow portion opening (10) extends along an arc of a first circle.
- 14. The air duct element of aspect 13, wherein the arc of the first circle is defined
by an angle α of at least 30°, preferably at least 60°, preferably at least 90°.
- 15. The air duct element of any of aspects 9 to 14, wherein the first airflow portion
opening (10) has a circumferential closed form.
- 16. The air duct element of any of the preceding aspects, comprising the features
of aspect 13, wherein the first airflow portion opening (10) has an arcual length
S measured along the first circle and a radial thickness Δr measured perpendicular
to the first circle, wherein the relation S/Δr fulfills 1.2 ≤ S/Δr ≤ 200, preferably
1.5 ≤ S/Δr ≤ 150, preferably 2 ≤ S/Δr ≤ 100, preferably 2 ≤ S/Δr ≤ 50.
- 17. The air duct element of aspect 16, comprising the features of aspect 10,
wherein the arcual length S of the first airflow portion opening (10) is larger than
the distance between the air inlet opening (22) and the first airflow portion opening
(10).
- 18. The air duct element of any of aspects 9 to 17,
wherein inner walls of the air duct element (2) for guiding the first airflow portion
(62) and the second airflow portion (64) are shaped stepless.
- 19. The air duct element of any of the preceding aspects,
wherein the air duct element (2) further comprises a second airflow portion opening
(20) for outlet of the second airflow portion (64).
- 20. The air duct element of aspect 19, wherein the first airflow portion opening (10)
and the second airflow portion opening (20) extend in one plane.
- 21. The air duct element of aspect 19 or 20, wherein the second airflow portion opening
(20) has two opposing edge regions (22, 24) being at least partially curved in an
identical direction.
- 22. The air duct element of aspect 21, wherein the two opposing edge regions (12,
14) of the first flow portion opening (10) and the two opposing edge regions (22,
24) of the second airflow portion opening (20) are curved in the identical direction.
- 23. The air duct element of any of aspects 19 to 22, wherein at least a segment of
the second airflow portion opening (20) extends along an arc of a second circle.
- 24. The air duct element of any of aspect 23, wherein the first circle and the second
circle are formed so that they share a same center point (M).
- 25. The air duct element of any of aspects 9 to 24, wherein the air duct element (2)
is further configured to divide the airflow (6) into a third airflow portion (66),
wherein the air duct element (2) further comprises a third airflow portion opening
(30) for outlet of the third airflow portion (66).
- 26. The air duct element of aspect 25, wherein the first airflow portion opening (10)
and the third airflow portion opening (30) extend in different planes.
- 27. The air duct element of aspect 25 or 26, wherein the third airflow portion opening
(30) has two opposing edge regions (32, 34) being at least partially curved in an
identical direction.
- 28. The air duct element of aspect 27, wherein the two opposing edge regions (12,
14) of the first airflow portion opening (10) and the two opposing edge regions (32,
34) of the third airflow portion opening (30) are curved in the identical direction.
- 29. The air duct element of any of aspect 25 to 28, wherein at least a segment of
the third airflow portion opening (30) extends along a third circle.
- 30. A cooling system for cooling a dry-type transformer, comprising
a fan (4) having a fan air outlet (42), and being configured to generate an airflow
(6) and to deliver the airflow (6) through the fan air outlet (42), and
at least one air duct element (2) according to any of aspects 9 to 29, attached to
the fan air outlet (42).
- 31. A dry-type transformer, comprising
a core (50),
a coil assembly wound around the core (50), the coil assembly comprising at least
one winding, for example an outermost winding (70) and an innermost winding (60),
and
a cooling system according to aspect 30 or an air duct element (2) according to any
of aspects 9 to 29 for cooling the coil assembly and/or the core (50).
- 32. The dry-type transformer of aspect 31,
wherein the first airflow portion opening (10) of the air duct element (2) is configured
and arranged to direct the first airflow portion (62) along an outer surface area
(72) of the outermost winding (70).
- 33. The dry-type transformer of aspect 31 or 32,
wherein the second airflow portion opening (20) of the air duct element (2) is configured
and arranged to direct the second airflow portion (64) into a gap area (80) formed
by the coil assembly between the outermost winding (70) and the innermost winding
(60).
- 34. The dry-type transformer of any of aspects 31 to 33,
wherein the third airflow portion opening (30) of the air duct element (2) is configured
and arranged to direct the third airflow portion (66) partially along an outer surface
area of the innermost winding (60) and/or partially along an inner surface of the
innermost winding (60).
- 35. The dry-type transformer of any of aspects 31 to 34,
wherein the distance δ between the coil assembly and the air duct element (2) is less
than 10 cm, preferably less than 5 cm.
SHORT DESCRIPTION OF THE DRAWINGS
[0075] The subject-matter of the disclosure will be explained in more detail with reference
to preferred exemplary embodiments which are illustrated in the attached drawings.
Fig. 1 is a schematic view of lower region of a transformer and a fan for cooling
the transformer according to prior art.
Fig. 2 is a view of a lower region of a transformer comprising three coil assemblies,
each coil assembly provided with a cooling system according to the present disclosure.
Fig. 3 is a perspective view of a first one of the cooling systems.
Fig. 4 is an enlarged section of Fig. 3.
Fig. 5 is a schematic cross-sectional view of an air duct element according to the
present disclosure and adjacent portions of a fan and a transformer.
Fig. 6 is a perspective view of a separated air duct element according to the present
disclosure.
Fig. 7 is a rear view of the lower region of the transformer shown in Fig. 2.
Fig. 8a is a schematic sectional view of a core, an inner winding, and outer winding
and an air duct element.
Fig. 8b is a schematic sectional view of a core, an inner winding, and outer winding
and an alternatively shaped air duct element.
Fig. 9 is a schematic cross-sectional view of a lower portion of a transformer arrangement
according to the present invention.
DETAILED DESCRIPTION
[0076] Fig. 2 is a view of a lower region of a dry-type transformer comprising three coil
assemblies 7, 7', 7", each coil assembly provided with a corresponding cooling system
5, 5', 5" according to the present disclosure.
[0077] The transformer comprises a core having three linear core segments, wherein each
coil assembly 7, 7', 7" is wound around a respective linear core segment.
[0078] The cooling systems 5, 5', 5" may be of the same configuration. Therefore, only one
cooling system 5 is described in more detail below. The corresponding linear core
segment is also referred to as "core" in the following for the sake of brevity.
[0079] Fig. 3 is a perspective view of the cooling system 5. The cooling system 5 comprises
a fan 4 and an air duct element 2 attached to the fan 4. Fig. 4 is an enlarged section
of Fig. 3. Fig. 5 shows a corresponding cross-sectional view. The air duct element
2 is preferably made from a dielectric material and may be manufactured by additive
manufacturing, e. g. by 3D printing.
[0080] The fan 4 is configured to generate an airflow 6 and to deliver the airflow 6 through
a fan air outlet 42. The air duct element 2 has an air inlet opening 22 for receiving
the airflow 6 generated by the fan 4. The air duct element 2 may be attached directly
to the fan air outlet 42, as sketched in Fig. 5. This is particularly advantageous
if the edge of the fan air outlet 42 and the edge of the inlet opening 22 of the air
duct element 2 extend at least approximately in the same plane.
[0081] Alternatively, as shown in Fig. 4, the cooling system may further comprise an intermediate
piece or adapter 3 which connects the air duct element 2 to the fan 4. This is for
example advantageous, if the edge of the fan air outlet 42 and the edge of the inlet
opening 22 extend in two different planes which include an angle greater than 0°,
since the intermediate piece 3 may be configured in such a case to connect the fan
air outlet 42 and the air inlet opening 22 of the airduct element 2 by bridging the
corresponding space in between, particularly in an air-tight manner.
[0082] The air duct element 2 is configured to divide the airflow 6 generated by the fan
4 and delivered through the fan air outlet 42 into at least a first airflow portion
62 and a second airflow portion 64. The air duct element 2 is configured to direct
the first airflow portion 62 and the second airflow portion 64 to different individual
parts of the transformer.
[0083] In the example illustrated in Fig. 5, an innermost winding 60 and an outermost winding
70 are wound around a linear core segment or core 50 for short.
[0084] Generally, more than two windings can be provided around each linear core section.
In the example of Fig. 5, the number of windings wound around the core 50, is two
so that here the outermost winding is an outer winding 70 and the innermost winding
is an inner winding 60. The outer winding 70 comprises a bottom end 79 and the inner
winding 60 comprises a bottom end 69.
[0085] Barrier elements 90 may be provided in a gap area 80 formed between the inner winding
60 and the outer winding 70. Typically, such barrier elements show practically no
or at best little relevance with respect to heat generation by the transformer. Accordingly,
the air duct element 2 may be configured not - or at least not specifically - to guide
air to the barrier elements 90.
[0086] The core 50 extends along a longitudinal axis L which is typically oriented vertically.
Fig. 8a shows a schematic cross-sectional view normal to the longitudinal axis L (not
to scale). The windings 60, 70 are wound around the core 50 so that, when viewed in
the normal cross-section, the core 50, the inner winding 60, and the outer winding
70 may share a common center point M.
[0087] In the example illustrated in Fig. 5, the air duct element 2 is configured to direct
the first airflow portion 62 to an outer surface area 72 of the outer winding 70 and
the second airflow portion 64 to an inner surface area 74 of the outer winding 70.
[0088] Fig. 6 shows a perspective view of the separated air duct element 2. The air duct
element 2 comprises a first airflow portion opening 10 for outlet of the first airflow
portion 62. The first airflow portion opening 10 has two opposing edge regions 12,
14 being at least partially curved in an identical direction. In this way, the shape
of the first airflow portion opening 10 can be particularly well adapted to the outer
surface area 72 of the outer winding 70 to be cooled.
[0089] In the example illustrated in Fig. 6, the first airflow portion opening 10 extends
along an arc of a first circle - here having a first radius R1 - defined by an angle
α. Preferably, the angle α is at least 30°. The first airflow portion opening 10 may
have an arcual length S measured along the first circle and a radial thickness Δr
measured perpendicular to the first circle, wherein the relation 2 ≤ S/Δr ≤ 50 is
fulfilled.
[0090] Generally, as sketched exemplarily in Fig. 8a, the angle α may be 360° so that the
first airflow portion opening 10 has a circumferential closed form. In this way a
particularly effective cooling of the respective part of the transformer, for example
the outer surface area 72 of the outer winding70 can be achieved.
[0091] Alternatively, as sketched more simplified in a cross-sectional view in Fig. 8b,
only a (true) first segment σ1 the first airflow portion opening 10 may extend along
an arc of a first circle. A second segment σ2 may extend for example straight. Also
in such a case, the first airflow portion opening 10 may have a circumferential closed
form as sketched exemplarily in Fig. 8b.
[0092] This may be advantageous for example in a case where a corresponding winding shows
a normal cross-section having a shape of a rectangle with "rounded edges", as sketched
in Fig. 8b. In this case, the first circle may match advantageously a corresponding
rounded edge region of the corresponding winding 70. In the example shown in Fig.
8b, the first segment σ1 of the first airflow portion opening 10 is shaped so that
the first circle has a center point M1. A third segment σ3 of the first airflow portion
opening 10 may be shaped so that a corresponding further circle has a further center
point M2, and so on. Thus, in the example shown in Fig. 8b, the first airflow portion
opening 10 has circumferential closed form, however it is not shaped circular.
[0093] However, alternatively and more generally, the first airflow portion opening 10 may
be shaped exclusively straight, for example, it may merely extend along the segment
indicated by reference sign σ2.
[0094] In the example shown in Figures 5 and 6, the edge of the air inlet opening 22 and
the edge of the first airflow portion opening 10 extend in parallel planes.
[0095] It is generally advantageous if the path of the airflow within the air duct element
2 is kept comparatively short. To this end, it is advantageous if the length of the
edge of the first airflow portion opening 10 is larger than the distance D, see Fig.
5, between the air inlet opening plane and the first airflow portion opening plane.
Preferably, the arcual length S of the first airflow portion opening 10 is larger
than the distance D.
[0096] In the example shown in Fig. 6, the air duct element 2 further comprises a second
airflow portion opening 20 for outlet of the second airflow portion 64. The configuration
may be so that the second airflow portion 64 is directed by the air duct element 2
to an inner surface area 74 of the outer winding 70. Advantageously, the first airflow
portion opening 10 and the second airflow portion opening 20 extend in one plane.
The second airflow portion opening 30 may extend along an arc of a second circle,
having a radius R2 which is smaller than the radius R1 of the first circle. The first
and the second circle may share a same center point M.
[0097] The air duct element 2 may comprise wall portions 29 separating the first airflow
portion 62 and the second airflow portion 64. These wall portions 29 may extend to
the plane of the air inlet opening 22. In other words, the air inlet opening 22 may
comprise a first part and a second part (or more parts), the first part being designed
to receive a first portion of the airflow 6 which forms the first airflow portion
62 after entry into the air duct element 2, and the second part being designed to
receive a second portion of the airflow 6 which forms the second airflow portion 64
after entry into the air duct element 2.
[0098] The air duct element 2 may be further configured to divide the airflow 6 into a third
airflow portion 66, wherein the air duct element 2 further comprises a third airflow
portion opening 30 for outlet of the third airflow portion 66. In the example illustrated
in Fig. 5, the third airflow portion opening 30 faces the bottom end 69 of the inner
winding 60. In the normal cross-section, as exemplarily shown in Fig. 8a, the projection
of the third airflow portion opening 30 may include the inner winding 60, specifically,
the bottom end 69 of the inner winding.
[0099] The configuration may be so that the third airflow portion 66 is directed by the
air duct element 2 partially to an outer surface area 65 of the inner winding 60 and
partially to an inner surface area 67 of the inner winding 60. Further, the third
airflow portion opening 30 may be configured to match the shape of the bottom end
69 of the inner winding 60.
[0100] Moreover, the inner winding 60 may comprise at least one internal gap extending parallel
to the longitudinal axis L throughout the vertical length of the inner winding 60,
where the third airflow portion 66 may be directed further through a gap area of the
at least one gap of the internal winding 60.
[0101] As shown for example in Figures 5 and 6, the first airflow portion opening 10 and
the third airflow portion opening 30 may extend in different planes. This is for example
particularly advantageous if the inner winding 60 extends further down than the outer
winding 70, as exemplarily illustrated in Fig. 5. The air duct element 2 may further
comprise wall portions 39 separating the second airflow portion 64 and the third airflow
portion 66. These wall portions 39 may extend - as the wall portions 29 - to the plane
of the air inlet opening 22.
[0102] Fig. 7 shows a variation of an air duct element 2' in which the first airflow portion
opening 10' is formed having a shorter length than in the above example. Furthermore,
this variation differs in that the air duct element 2' further comprises a "further"
first airflow portion opening 10", which is directed towards a further outer surface
area of the outer winding 70. These first airflow portion openings 10', 10" may extend
along two distinct segments of a common circle. These segments may each be defined
by a corresponding angle α as described above. Generally, a plurality of corresponding
segments may be provided.
[0103] This design can be advantageous, for example, if the outer surface of the outer winding
70 has a radially outwardly projecting region, such as for example a dome region 92.
Here, the two first airflow portion openings 10', 10" can advantageously be arranged
on both sides of the radially outwardly projecting region or dome region 92.
[0104] Fig. 9 is a schematic cross-sectional view of a lower portion of a transformer arrangement,
for example the transformer, the front of which is shown exemplarily in Fig. 2 and
the rear of which is shown in Fig. 7. The air duct element 2 may be disposed in the
front as illustrated in Figures 5 and 9, and a further air duct element 2' according
to the above-described variation together with a respective further fan 4' is disposed
in the rear, where the outer winding 70 shows the dome region 92.
[0105] As already described above, an air duct element according to the present disclosure
is particularly advantageous, since it enables guiding cooled air in a very specific
manner to parts of the transformer which need cooling during operation. More specifically,
as shown in Fig. 5, the configuration may be such that a distance δ between the coil
assembly, for example a lower edge or bottom end 79 of the outer winding 70, and the
air duct element 2, for example the edge of the first airflow portion opening 10,
is less than 10 cm, preferably less than 5 cm, even more preferably less than 3 cm,
for example less than 2 cm. In this way a particularly high cooling efficiency can
be achieved.
[0106] Some of the advantages achievable with the invention are listed in the following:
- Cooling air can be guided very precisely and specifically to parts of the transformer
which need to be cooled during operation, such as the windings and the core.
- Cooling air can also be supplied to locations that cannot or cannot suitably be supplied
with cooling air according to the state of the art.
- It can be achieved that the cooling air is practically not lost before it reaches
the parts to be cooled, for example the windings.
- The air can be guided through a confined space up to the very edge of the windings.
- The technology makes it possible, with comparable performance, to reduce the size,
the weight, and the required material of the transformer.
- The disclosed technology is of particular benefit for applications where there are
restrictions in the maximum airflow permitted to cool the transformer, such as for
example in case of wind turbines.
- The transformer according to the present disclosure allows for a significant increase
in the power of the transformer, for example by as much as about 10%.
- The air duct element according to the present disclosure can be easily adapted to
requirements of different transformers.
- A cooling system according to the present disclosure is suited to be implemented in
a large variety of transformers, regardless of whether they have an enclosure or not.
1. A transformer arrangement, comprising
a transformer core (50), defining a longitudinal axis (L),
a coil assembly wound around the core (50), the coil assembly comprising a winding
(60, 70), and
an air duct element (2) configured and arranged to direct an airflow portion (62,
64, 66) to a bottom end of the winding (60, 70) and/or along an inner or outer surface
area (72, 74; 65, 67) of the winding (60, 70) for cooling the coil assembly and/or
the core (50),
wherein a distance (δ) between the air duct element (2) and the bottom end of the
winding (60, 70) is less than 50 mm.
2. The arrangement of claim 1, wherein the distance (δ) is less than 40 mm, preferably
less than 30 mm, preferably less than 20 mm, preferably less than 10 mm.
3. The arrangement of claim 1 or 2,
wherein the airduct element (2) is made from a dielectrical material and/or a nonconductive
material; and/or
wherein the air duct element (2) is manufactured by additive manufacturing.
4. The arrangement of any of the preceding claims, wherein the air duct element (2) comprises
an air flow portion opening (10, 20, 30) for outlet of the airflow portion,
wherein the shape of the air flow portion opening (10, 20, 30) matches the shape of
an outer or inner edge of the bottom end of the winding (60, 70) and/or the inner
or outer surface area (72, 74, 65, 67) of the winding, and/or at least one cooling
gap provided in the transformer arrangement.
5. The arrangement of any of claim 4, wherein the airflow portion opening (10, 20, 30)
matches the shape of the inner or outer edge of the bottom end of the winding (60,
70) and/or the inner or outer surface area (72, 74, 65, 67) of the winding to such
a degree that at least 80% of the airflow exiting the airflow portion opening (10,
20, 30), preferably at least 90% of the airflow, preferably at least 95% of the airflow,
even more preferably at least 98% of the airflow reaches and flows along the inner
or outer surface area (72, 74, 65, 67) of the winding and/or at least one cooling
gap provided in the transformer arrangement.
6. The arrangement of any of the preceding claims,
further comprising a fan (4) having a fan air outlet (42), the fan (4) being configured
and arranged to generate an airflow (6) and to deliver the airflow (6) through the
fan air outlet (42) to an air inlet opening (22) of the air duct element (2),
preferably wherein inner surfaces of the air duct element (2) for guiding the airflow
(6) from the air inlet opening (22) to the airflow portion opening (10, 20, 30) are
smooth and without steps or sharp edges.
7. An air duct element (2), configured to direct an airflow portion (62, 64, 66) to an
outer or inner edge of a bottom end of a winding (60, 70) of a coil assembly of a
transformer and/or along an inner or outer surface area (72, 74, 65, 67) of a winding
(60, 70) of a coil assembly of a transformer and/or to at least one cooling gap provided
in the transformer arrangement,
the air duct element (2) comprising an airflow portion opening (10, 20, 30) for outlet
of the airflow portion (62, 64, 66),
wherein the shape of the air flow portion opening (10, 20, 30) matches the shape of
an outer or inner edge of the bottom end of the winding (60, 70) and/or the inner
or outer surface area (72, 74, 65, 67) of the winding, and/or at least one cooling
gap provided in the transformer arrangement; and/or
wherein the air flow portion opening (10, 20, 30) has a circumferentially closed form
extending around the longitudinal axis (L).
8. An air duct element (2) configured to be attached to a fan air outlet (42) of a fan
(4) for cooling a dry-type transformer, preferably the air duct element of claim 7,
wherein the air duct element (2) is configured to divide an airflow (6) generated
by the fan (4) and delivered through the fan air outlet (42) into at least a first
airflow portion (62) and a second airflow portion (64),
wherein the air duct element (2) is configured to direct the first airflow portion
(62) and the second airflow portion (64) to different individual parts of the transformer.
9. The air duct element of claim 8,
wherein the air duct element (2) comprises a first airflow portion opening (10) for
outlet of the first airflow portion (62), the first airflow portion opening (10) having
two opposing edge regions (12, 14) being at least partially curved in an identical
direction.
10. The air duct element of claim 9, wherein at least a segment of the first airflow portion
opening (10) extends along an arc of a first circle.
11. The air duct element of claim 10, wherein the arc of the first circle is defined by
an angle α of at least 30°, preferably at least 60°, preferably at least 90°.
12. The air duct element of any of claims 9 to 11, wherein the first airflow portion opening
(10) has an arcual length S measured along the first circle and a radial thickness
Δr measured perpendicular to the first circle, wherein the relation S/Δr fulfills
1.2 ≤ S/Δr ≤ 200, preferably 1.5 ≤ S/Δr ≤ 150, preferably 2 ≤ S/Δr ≤ 100, preferably
2 ≤ S/Δr ≤ 50.
13. The air duct element of any of claims 9 to 12, wherein the air duct element (2) further
comprises a second airflow portion opening (20) for outlet of the second airflow portion
(64), preferably
wherein the first airflow portion opening (10) and the second airflow portion opening
(20) extend in one plane.
14. The air duct element of any of claims 9 to 13, wherein the air duct element (2) is
further configured to divide the airflow (6) into a third airflow portion (66), wherein
the air duct element (2) further comprises a third airflow portion opening (30) for
outlet of the third airflow portion (66).
15. The air duct element of claim 14, wherein the first airflow portion opening (10) and
the third airflow portion opening (30) extend in different planes.