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WO2024170196A1 - Générateur de flux d'air - Google Patents

Générateur de flux d'air Download PDF

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Publication number
WO2024170196A1
WO2024170196A1 PCT/EP2024/051048 EP2024051048W WO2024170196A1 WO 2024170196 A1 WO2024170196 A1 WO 2024170196A1 EP 2024051048 W EP2024051048 W EP 2024051048W WO 2024170196 A1 WO2024170196 A1 WO 2024170196A1
Authority
WO
WIPO (PCT)
Prior art keywords
air
airflow generator
multiplier
spiral
transformer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/EP2024/051048
Other languages
English (en)
Inventor
Ulf Sand
Lokman HOSAIN
Rebei Bel Fdhila
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Energy Ltd
Original Assignee
Hitachi Energy Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hitachi Energy Ltd filed Critical Hitachi Energy Ltd
Priority to CN202480010161.0A priority Critical patent/CN120569792A/zh
Priority to KR1020257025255A priority patent/KR20250126837A/ko
Publication of WO2024170196A1 publication Critical patent/WO2024170196A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F27/00—Details of transformers or inductances, in general
    • H01F27/02—Casings
    • H01F27/025—Constructional details relating to cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/02—Units comprising pumps and their driving means
    • F04D25/08—Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/14—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid
    • F04F5/16—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid displacing elastic fluids
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F27/00—Details of transformers or inductances, in general
    • H01F27/08—Cooling; Ventilating
    • H01F27/10—Liquid cooling
    • H01F27/12—Oil cooling

Definitions

  • the present disclosure relates to an airflow generator, and to a transformer assembly comprising such an airflow generator for cooling of a heat exchanger provided externally of the transformer for cooling of the transformer.
  • a power transformer is equipment used in an electric grid of a power system. Power transformers transform voltage and current in order to transport and distribute electric energy. Power transformers involve high currents; therefore, production of heat is inevitable. This heat propagates in oil inside a transformer tank. It is important to release this heat to the surroundings for the normal operation of transformers. An important part of oil-cooling is carried out by placing external devices by the transformer, such as radiators, cooler banks etc., through which the transformer oil is circulated and get cooled.
  • State-of-the art air-cooling for a transformer is performed using conventional fans, i.e. , bladed fans, or using natural convection.
  • the state-of-the-art cooling systems using bladed fans typically produce high noise, have complex structure, are heavy, and are difficult to maintain. For high-power transformers, natural convection is not enough to cool the transformer, and therefore, forced cooling is needed.
  • External transformer cooling generally uses a one or more radiators external to the transformer, said radiators allowing oil to circulate from the transformer and out to the radiators, where heat is dissipated from the oil to surrounding ambient air.
  • the cooling process typically uses natural convection or forced convection to move ambient air past the radiator.
  • This disclosure concerns cooling systems using forced convection. Forced convection is typically achieved using one or more large fans blowing air through or onto the radiator(s). Cooling efficiency is dependent on airflow rate and consequently on the power consumption of the fans.
  • an object of the present disclosure is to provide a compact and power-efficient airflow generator cooling arrangement for a transformer.
  • the air flow generator is suitable for cooling an oi l-to-air external heat exchanger of a transformer.
  • the airflow generator comprises an electrically powered ducted fan provided with an inlet and an outlet, a fluid conduit, and an air multiplier for discharging air along a first axis.
  • the air multiplier comprises an inlet and an outlet.
  • the fluid conduit fluidly connects the outlet of the ducted fan to the inlet of the air multiplier.
  • the air multiplier comprises a spiral-shaped portion extending around the first axis.
  • the spiral may comprise one or more portions having a smooth curvature, and/or it may comprise one or more straight portions.
  • An alternative spiral shape is shown in fig. 8.
  • the fan provides an airflow into the fluid discharge device.
  • the fluid discharge device By providing the fluid discharge device with an air multiplier, a much larger amount of air than the amount of air supplied by the fan, is discharged by the air discharge device. This reduces power-consumption as compared to use of conventional fans directly blowing air. Also, noise emitted from the fan and air multiplier combination is lower than a corresponding noise level emitted from a fan achieving the same air flow.
  • Prior art air multipliers are often shaped as rings with a central opening though which air is accelerated by air discharged from the air multiplier. The flow velocity of air flowing through the ring is higher closer to the ring and lower further from the ring.
  • the air multiplier By making the air multiplier spiral-shaped, the air multiplier discharges air over a larger portion of the cross-section of the airflow provided by the air discharge device, thereby improving control of flow velocity over the whole cross-section of the airflow emitted by the air discharge device.
  • the provision of one spiral-shaped air multiplier enables fluid supply to the air multiplier at one location only, rather than at each separate air multiplier.
  • the simplified structure promotes a more even airflow past the air discharge device, since no additional fluid conduits need be provided to each discrete air multiplier.
  • the spiral-shaped portion may be substantially planar.
  • the fluid discharge device is very compact.
  • the spiral-shaped portion may be inclined along the first axis.
  • the spiral-shaped portion may be helix-shaped.
  • the transformer arrangement comprises an airflow generator according to any one of the alternatives defined above, and a transformer provided with an oil-to-air external heat exchanger.
  • the airflow generator is configured to discharge air towards the oil-to-air heat exchanger.
  • Transformers provided with oil-to-air heat exchangers are known. By providing such transformers with the claimed airflow generator, an energy efficient and compact cooling system for the transformer is achieved.
  • Fig. 1a shows a prior art airflow generator comprising an air multiplier.
  • Fig. 1 b shows a side view of the prior art airflow generator also shown in fig. 1 a (shown without the ducted fan and without the fluid conduit).
  • Fig. 2a shows another prior art airflow generator plurality of air multipliers concentrically aligned and arranged in a planar fashion.
  • Fig. 2b shows a side view of the prior art airflow generator also shown in fig. 2a (shown without the ducted fan and without the fluid conduit).
  • Fig. 3a shows a first embodiment of an airflow generator according to the present disclosure, provided with an air multiplier comprising a spiral-shaped portion extending around the first axis in a substantially planar fashion.
  • Fig. 3b shows a side view of airflow generator also shown in fig. 3a.
  • Fig. 4a shows a second embodiment of an airflow generator according to the present disclosure, provided with an air multiplier comprising a spiral-shaped portion extending around the first axis and being inclined along the first axis in a downstream direction.
  • Fig. 4b shows a side view of airflow generator also shown in fig. 4a.
  • Fig. 5a shows a second embodiment of an airflow generator according to the present disclosure, provided with an air multiplier comprising a spiral-shaped portion extending around the first axis and being inclined along the first axis in an upstream direction.
  • Fig. 5b shows a side view of airflow generator also shown in fig. 4a.
  • Fig. 6 shows a perspective view of a cross-section of one of the air multipliers. All air multipliers are based on the same general cross-sectional design.
  • Fig. 7 shows a transformer arrangement comprising the airflow generator also shown in fig. 4a, and a transformer provided with an external oil-to-air heat exchanger.
  • Fig. 8 shows an alternative shape of the spiral-shape of the air multiplier, having a combination of straight portions and rounded corners.
  • Fig. 1 shows a prior art airflow generator comprising an electrically powered ducted fan 2 provided with an inlet 3 and an outlet 4.
  • the airflow generator 1 further comprises a fluid conduit 5 and an air multiplier 7 for discharging air along a first axis A.
  • the air multiplier 7 comprises an inlet 8 and an outlet.
  • the fluid conduit 5 fluidly connects the outlet 4 of the ducted fan 2 to the inlet 8 of the air multiplier 7.
  • Air multiplier is used in the prior art and thus should be known to the skilled person.
  • Air multipliers are nozzles typically used in bladeless fans.
  • the term air multiplier may to refer to any type of air discharge device/nozzle designed to discharge air through an outlet, typically in the form of one or more elongate slits, such that air around the discharge device is brought along by the air discharged from the outlet at a rate of at least 5-15 times the amount of air discharged by the outlet.
  • Another term which could be used instead of air multiplier is Coanda effect air flow multiplier.
  • Such air discharge devices can vary greatly in design but are often shaped like an extruded hollow profile, an example of which is shown in fig. 6, although any other suitable shape is possible.
  • the profile usually has an elongate cross-sectional shape, and the outlet is typically configured to discharge air in a direction along a longitudinal axis extending along the length of the elongate cross-sectional shape, as shown in fig. 6.
  • the profile may have an aerodynamic foil shape.
  • the outlet may be provided anywhere suitable along the length of the cross-sectional shape of the profile, such as at a leading portion of the profile (facing incoming ambient air as in fig. 6), or at a trailing portion of the profile, facing in the discharge direction of the air multiplier, or somewhere between the leading and trailing portions of the profile.
  • the profile may be straight but is typically bent to form a ring circumscribing an inner cross- sectional area of the air multiplier.
  • the air multiplier may be provided with a convex curved wall portion wherein the outlet may be provided such that air is discharged adjacent the curved portion, along the curved portion, wherein the discharged air ‘adheres’ to the curved wall portion. This leads to increased suction effect acting on ambient air on the opposite side of the discharged airflow with respect to the curved wall portion.
  • the airflow generator 1 also shown in fig. 1a is shown without the ducted fan 2 and without the fluid conduit 5.
  • the fan 2 provides an airflow into the air multiplier 7.
  • the ducted nature of the fan 2 enables it to efficiently pressurize the fluid conduit 5.
  • an airflow generator 1 By providing the airflow generator 1 with an air multiplier 7, a much larger amount of air than the amount of air supplied by the fan 2, is discharged towards an object, such as the oi l-to-air heat exchanger 6 shown in fig. 7.
  • the airflow generator 1 may thus be able to output an airflow of ten to fifteen times the airflow produced by the fan 2. This reduces power-consumption as compared to use of conventional fans directly blowing air against an object to be cooled, such as an oi l-to-air heat exchanger 6 provided on a transformer 11 .
  • Such air multipliers 7 are typically configured as rings with a central opening though which air is moved along by air discharged from the air multiplier along a first axis A.
  • the flow velocity of air flowing through the ring is higher closer to the ring and lower further from the ring, as indicated by the broken-line arrows of fig. 1 whose length indicate a strength of local airflow.
  • FIG. 2a and 2b Another embodiment of a prior art airflow generator is shown in figs. 2a and 2b.
  • the airflow generator 1 of figs. 2a and 2b corresponds to the airflow generator 1 of fig. 1 , but is provided with additional air multipliers, provided radially inside of the larger outer air multiplier 7.
  • the air multipliers 7, are arranged in a same plane as indicated in fig. 2a.
  • the total cross-sectional area inside the larger air multiplier 7 is limited by the thickness of the two inner air multipliers, and only allows air to flow through the passages indicated by arrows d1 and d2.
  • the additional inner air multipliers provide increased airflow and improved control of airflow over the cross-sectional area inside the largest air multiplier 7.
  • the additional air multipliers lead to reduced energy efficiency of the airflow generator 1.
  • the present disclosure proposes to use one air multiplier configured with a spiral shaped portion, as shown in figs. 3a, 3b, 4a, 4b, 5a, and 5b.
  • one inlet is sufficient for supplying air into the air multiplier, thereby mitigating the need of additional fluid conduits to supply air to each air multiplier as in the fig. 2a prior art device in which the additional fluid conduits locally restrict airflow and create additional turbulence.
  • the spiral shaped portion improves control of the discharged airflow over a greater portion of the cross-sectional area of the discharged airflow as compared to the prior art device of fig. 1 a.
  • the air multipliers 7, may be configured such that a discharge direction of the air multiplier 7, is parallel to the first axis, or at least essentially parallel to the first axis, such as within a range of 0-20 degrees, or within 0-15 or 0-10 degrees. It should be understood that the local direction of movement of surrounding air moved through the air multipliers (by the Coanda effect), is naturally different from the discharge direction, and locally varies over the cross-section of the airflow generator 1.
  • the air multipliers may be shaped from an extruded profile bent to its intended final shape, such a profile will be open ended and thus needs to be closed at any open ends to limit air leaks leading to undesired pressure-drop in the air multiplier 1 .
  • open ends are capped with an end cap or closed in any other suitable way, such as with a plug.
  • a free end of an air multiplier having the cross-sectional shape shown in fig. 5 would have to be closed to enable air to be forced through the outlet opening 9 rather than through the open end.
  • the fluid conduit is formed by a portion of a housing in which the ducted fan is provided, wherein the housing forms the duct of the fan and wherein the housing also provided the conduit needed to route air to the inlet of the air multiplier 7.
  • the fluid conduit 5 able to route air from the ducted fan to the air multipliers 7, could alternatively be used instead, such as a pipe or tube extending from a ducted fan provided remotely from the air multiplier 7.
  • the spiral-shaped portion is substantially planar. By arranging the spiral such that it extends in a plane, the fluid discharge device is very compact.
  • the spiral-shaped portion is inclined along the first axis A, either downstream, as shown in fig. 4a, or upstream, as shown in fig. 5a.
  • a distance between adjacent loops of the spiral will be increased, as compared to a planar spiral. The increased distance easier air flow past the fluid discharge device.
  • the spiral-shaped portion of the embodiments of figs. 4a, 4b, 5a, and 5b is helixshaped.
  • a distance between adjacent loops of the spiral will be increased, as compared to a planar spiral.
  • the increased distance enables easier air flow past the fluid discharge device.
  • the spiral extends such that the spiral has a component extending along the flow direction axis, thereby contributing to the inclined nature of the spiral-shape.
  • the airflow generator 1 of the present disclosure is especially useful for providing an airflow directed towards a heat exchanger 6 mounted externally on a transformer 11 .
  • the present disclosure proposes to a transformer arrangement 10 schematically illustrated in fig. 7.
  • the transformer arrangement 10 comprising an airflow generator 1 as described above, comprising an air multiplier 7.
  • the transformer arrangement 10 further comprises a transformer 11 provided with an oi l-to-air external heat exchanger 6.
  • the airflow generator 1 is configured to discharge air towards the oi l-to-air heat exchanger 6.
  • the oi l-to-air external heat exchanger 6 is external in the sense that it is mounted externally on the transformer 11 , thereby able to radiate and conduct heat to surrounding air.
  • oil from inside the transformer 11 is pumped through the oil-to-air heat exchanger 6, wherein the oil transports heat generated within the transformer 11 out to the heat exchanger 6, such that the airflow from the airflow generator 1 cools the heat exchanger 6.

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)

Abstract

La présente divulgation concerne un générateur de flux d'air (1) et un agencement de transformateur, le générateur de flux d'air (1) et un transformateur (11) comportant un échangeur de chaleur externe huile-air (6), ledit générateur de flux d'air (1) étant conçu pour évacuer l'air vers l'échangeur de chaleur huile-air (6). Le générateur de flux d'air comprend : une soufflante à alimentation électrique (2) ayant une entrée (3) et une sortie (4), un conduit de fluide (5) ; et un multiplicateur d'air (7) pour évacuer l'air le long d'un premier axe (A). Le multiplicateur d'air (7) comprend une entrée (8) et une sortie (9), ledit conduit de fluide (5) reliant de manière fluidique la sortie (4) de la soufflante (2) à l'entrée (8) du multiplicateur d'air (7). Le multiplicateur d'air (7) comprend en outre une partie en forme de spirale s'étendant autour du premier axe (A).
PCT/EP2024/051048 2023-02-13 2024-01-17 Générateur de flux d'air Ceased WO2024170196A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN202480010161.0A CN120569792A (zh) 2023-02-13 2024-01-17 气流发生器
KR1020257025255A KR20250126837A (ko) 2023-02-13 2024-01-17 기류 발생기

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP23156276.0A EP4415007A1 (fr) 2023-02-13 2023-02-13 Générateur de flux d'air
EP23156276.0 2023-02-13

Publications (1)

Publication Number Publication Date
WO2024170196A1 true WO2024170196A1 (fr) 2024-08-22

Family

ID=85227220

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2024/051048 Ceased WO2024170196A1 (fr) 2023-02-13 2024-01-17 Générateur de flux d'air

Country Status (4)

Country Link
EP (1) EP4415007A1 (fr)
KR (1) KR20250126837A (fr)
CN (1) CN120569792A (fr)
WO (1) WO2024170196A1 (fr)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010203444A (ja) * 2009-03-04 2010-09-16 Dyson Technology Ltd ファン組立体
AU2013203399B2 (en) * 2010-12-10 2014-07-10 Soliton Holdings Corporation, Delaware Corporation Renewable stream energy use
WO2019062625A1 (fr) * 2017-09-28 2019-04-04 青岛海尔空调器有限总公司 Unité intérieure de climatiseur mural
US20190280562A1 (en) * 2016-01-20 2019-09-12 Soliton Holdings Corporation, Delaware Corporation Generalized Jet-Effect and Generalized Generator
US20190280561A1 (en) * 2016-01-20 2019-09-12 Soliton Holdings Corporation, Delaware Corporation Generalized Jet-Effect and Method for Computational Fluid Dynamics

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010203444A (ja) * 2009-03-04 2010-09-16 Dyson Technology Ltd ファン組立体
AU2013203399B2 (en) * 2010-12-10 2014-07-10 Soliton Holdings Corporation, Delaware Corporation Renewable stream energy use
US20190280562A1 (en) * 2016-01-20 2019-09-12 Soliton Holdings Corporation, Delaware Corporation Generalized Jet-Effect and Generalized Generator
US20190280561A1 (en) * 2016-01-20 2019-09-12 Soliton Holdings Corporation, Delaware Corporation Generalized Jet-Effect and Method for Computational Fluid Dynamics
WO2019062625A1 (fr) * 2017-09-28 2019-04-04 青岛海尔空调器有限总公司 Unité intérieure de climatiseur mural

Also Published As

Publication number Publication date
EP4415007A1 (fr) 2024-08-14
KR20250126837A (ko) 2025-08-25
CN120569792A (zh) 2025-08-29

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