EP0939963A1 - Procede d'impregnation d'elements constitutifs - Google Patents

Procede d'impregnation d'elements constitutifs

Info

Publication number
EP0939963A1
EP0939963A1 EP97951185A EP97951185A EP0939963A1 EP 0939963 A1 EP0939963 A1 EP 0939963A1 EP 97951185 A EP97951185 A EP 97951185A EP 97951185 A EP97951185 A EP 97951185A EP 0939963 A1 EP0939963 A1 EP 0939963A1
Authority
EP
European Patent Office
Prior art keywords
impregnating
components
impregnating agent
impregnation
radiation
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.)
Granted
Application number
EP97951185A
Other languages
German (de)
English (en)
Other versions
EP0939963B1 (fr
Inventor
Klaus-Wilhelm Lienert
Rainer Blum
Günter HEGEMANN
Manfred Eichhorst
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.)
Altana Electrical Insulation GmbH
Original Assignee
Beck & Co AG Dr
Drbeck & Co AG
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=7812306&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP0939963(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Beck & Co AG Dr, Drbeck & Co AG filed Critical Beck & Co AG Dr
Publication of EP0939963A1 publication Critical patent/EP0939963A1/fr
Application granted granted Critical
Publication of EP0939963B1 publication Critical patent/EP0939963B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F41/00—Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties
    • H01F41/02—Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for manufacturing cores, coils, or magnets
    • H01F41/04—Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for manufacturing cores, coils, or magnets for manufacturing coils
    • H01F41/12—Insulating of windings
    • H01F41/127—Encapsulating or impregnating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D1/00—Processes for applying liquids or other fluent materials
    • B05D1/18—Processes for applying liquids or other fluent materials performed by dipping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
    • B05D3/02—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by baking
    • B05D3/0209—Multistage baking
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
    • B05D3/02—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by baking
    • B05D3/0254—After-treatment
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
    • B05D3/04—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to gases
    • B05D3/0493—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to gases using vacuum
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
    • B05D3/06—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to radiation
    • B05D3/061—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to radiation using U.V.
    • B05D3/065—After-treatment
    • B05D3/067—Curing or cross-linking the coating

Definitions

  • the invention relates to a method for impregnating components with polymerizable compositions which are liquid at room temperature or liquefiable by heating and which can be hardened by a combined application of heat and high-energy radiation.
  • EP-A-0 643 467 proposes to obtain a pre-gelling and fixing of the impregnating agent and a thermal hardening to improve the impregnating agent distribution in the component during the impregnation via coil heating. At the same time as the thermal hardening on the windings or after the thermal hardening on the windings, those parts of the components that were not reached by the winding heating should be hardened with high-energy, preferably UV radiation.
  • a disadvantage of this method is that with the heating over the windings, only a partial hardening is carried out thermally and that the hardening then takes place with blasting. Since all known components make up have that are not achieved with partial thermal curing and are in the shaded area during post-curing with rays, components that have been treated in accordance with EP-A-0 643 467 always have areas where the impregnating agent is only insufficiently cured. Undesirable emissions then occur from these areas and the impregnant can only insufficiently fulfill its functions there.
  • EP-A-0 643 467 does not contain any teaching on the use of the method in the generally claimed techniques for impregnation.
  • Pre-gelling by winding heating during the impregnation is not sensible because the cavities are filled indefinitely.
  • Preheating the windings to lower the viscosity and thus to accelerate the filling is known in the art, e.g. in the various immersion and flooding processes in which the components are heated in order to achieve a reduction in viscosity and thus better and faster filling. Heating to gelation during impregnation does the opposite, namely an undefined filling of the cavities due to gelation.
  • the polymeric components of known impregnating, casting and coating compositions for electrical components are preferably unsaturated polyesters which are dissolved in vinylically unsaturated compounds, such as styrene, vinyl toluene, allyl phthalate and monomeric or oligomeric acrylic or vinyl esters which are radically (co) polymerized.
  • Impregnating, casting and coating compositions are generally understood to be resin compositions which are used in electrical engineering for impregnating windings, the generally known processes, such as, for example, immersion impregnation, trickling technology, the
  • Dip rolling and flooding are used, these processes possibly being supported by the application of vacuum and / or pressure.
  • the method according to the invention solves the problems mentioned above by partial gelling or partial hardening of the soaked components already in the soaking agent, then allowing the non-gelled impregnating agent portions to run off, if necessary returning these expired soaking agents, if necessary after cooling them, into the soaking agent supply, detaching the component surfaces with high-energy radiation and then thermally curing.
  • the method according to the invention it is possible for the first time to set a largely uniform impregnating agent filling of any filling level practically at any point of the components.
  • the emission of volatile impregnant components is reduced in such a way that there is almost no loss of impregnant.
  • This method is particularly advantageous in immersion impregnation techniques in which virtually no monomers can escape from the immersion system during the partial hardening, which takes place in the immersed state.
  • a large part of volatile monomers are fixed in the resin mass in the immediate vicinity of the heated inner areas of the components.
  • a desired degree of filling of the component can be set by setting the heating rate, temperature and heating time. This method can preferably be used when diving at room temperature and coil heating with electricity shortly before, during or after immersion.
  • the temperature is increased in the impregnating agent. Gelling of the impregnant is initiated only in the immediate vicinity of the heated coils. The main masses of the component and the impregnating agent heat up only slightly, so that there are only a few evaporation losses when they are replaced.
  • the surfaces of the components are irradiated with high-energy radiation, preferably UV light.
  • Patent application P 195 425 64.2 are described, or in the case of epoxy resins, for problem-free, further handling of the impregnated components is necessary. Due to the limitation of the temperature effect to control the degree of filling, the impregnating agent in the interior of the components is generally not yet fully cured, so that thermal post-curing is usually required. As a result of the fact that the residual monomers are largely fixed in the components during this process step and the surfaces of the components are detached, there is only a small amount of evaporation emissions, even if a waiting period is activated before thermal post-curing. Larger components are expediently subsequently cured, for example by further power supply to the winding, while it is often advantageous in the case of smaller components to collect a number and cure them at a later point in time, for example in a heating chamber.
  • Another advantage of the method according to the invention is that it can be carried out on existing or only slightly modified plants, since it is carried out essentially by It is possible to change the control parameters and the sequence of procedures.
  • Impregnants with which the process according to the invention can be carried out are, in particular, the generally known impregnants based on unsaturated polyester resins, which can be radically copolymerized as reactive diluents by preparation with unsaturated monomers.
  • Appropriately selected polyesters are known to the person skilled in the art, as are iid- or amide-modified polyesters which have particularly favorable thermal and mechanical properties.
  • the appropriately selected reactive diluents are also known, styrene, ⁇ -methylstyrene, vinyl toluene, allyl esters, vinyl esters, vinyl ethers and / or (meth) acrylates being used in particular.
  • These polyester resin preparations can be cured thermally and / or with high-energy radiation, preferably UV light, using initiators or catalysts or catalyst mixtures which are likewise known to the person skilled in the art.
  • Further impregnating agents with which the process according to the invention can be carried out contain radically polymerizable monomeric, oligomeric and / or polymeric substances which are also radiation-curable, in particular with UV light.
  • Such substances and combinations of substances are also generally known to the person skilled in the art.
  • they are allylic, vinyl or (meth) acrylic unsaturated substances and / or mixtures of substances.
  • polyepoxy (meth) acrylates, polyurethane (meth) acrylates and / or polyester (meth) acrylates are particularly suitable.
  • Some of the impregnating agents can be thermally polymerized directly, but it is preferred to add free radical initiators for optimal thermal curing at the lowest possible temperatures.
  • free radical initiators are usually added to ensure rapid UV curing.
  • the impregnating agents used can furthermore contain stabilizers to improve the storage stability. Furthermore, the impregnating agents can also contain ionically polymerizable substances, in particular monomeric and / or oligomeric epoxides in conjunction with initiators which can be activated thermally and under UV light.
  • ionically polymerizable substances in particular monomeric and / or oligomeric epoxides in conjunction with initiators which can be activated thermally and under UV light.
  • the process according to the invention avoids the disadvantages of the processes of the known prior art by the specific combination of its process steps, that the distribution of the impregnant and the degree of filling are regulated by controlled heating of the components after the impregnation, still in the impregnation device, until the gelling and impregnation fixation, that the Drip losses are minimized by allowing the non-gelled impregnating agent components to run out after removal from the impregnating device, that these expired impregnating agents, if necessary after cooling, are returned to the soaking agent supply, that the evaporation losses on the component surface and surface stickiness are eliminated by using high-energy radiation and that a complete thermal post-curing then takes place until the impregnant functions optimally.
  • This sequence according to the invention is of great technical, ecological and economic use.
  • the coils are electrically heated until partial gelling.
  • the degree of filling can be regulated very precisely and reproducibly via the speed, amount and duration of this heating.
  • the components are removed from the impregnating agent and the non-gelled impregnating agent is drained off.
  • the draining impregnant can be returned to the impregnation bath, if necessary after cooling.
  • the adhering impregnating agent can also drain off on the outside of the components (laminated cores), on which generally no or only little impregnating agent is desired, this process being supported by the gradually escaping heat flow from the heated areas.
  • the surfaces of the components are sealed by the action of high-energy radiation, preferably UV radiation. Volatile constituents of the impregnating agent are largely fixed in the component by the pre-gelation and on the surface by the radiation. In the subsequent thermal curing, only minimal emissions occur.
  • high-energy radiation preferably UV radiation.
  • the component and impregnating agent have a room temperature of 26 ° C.
  • the component is immersed at 35 mm / minute, dipped again at the same speed after 1 minute, drained over the immersion bath for 20 minutes, then hardened in an oven at 140 ° C for 1 hour, weighed after cooling and then at 140 for 2 hours ° C post-hardened.
  • Comparative Example 4 (according to Example 2 in EP-A-0 643 467) (VB4)
  • the stator is electrically heated to a winding temperature of 60 ° C in 2 minutes, during which the laminated core becomes approx. 32 ° C and the plastic parts of the winding heads become approx. 28 ° C warm. According to the procedure, it is immersed in VB 1, kept immersed for 10 seconds, immersed and drained over the drinking bowl for 5 minutes. Then the winding is heated with electricity to 150 ° C. in 2 minutes and held there for 8 minutes. Already during heating and within the first 3 minutes at 150 ° C, a lot of partially gelled impregnating agent emerges from the stator, which can no longer be returned. After heating, the mixture is allowed to cool for 5 minutes and then exposed according to the procedure in VB 2. After that, the surface is largely tack-free; on the other hand are shaded, but still accessible to the touch,
  • the component and impregnating agent have a room temperature of 26 ° C.
  • the component is immersed at 35 mm / minute, the winding is heated to 160 ° C. in the immersion pool in 30 seconds and held for 1 minute, then it is immersed again at the same speed and allowed to drip over the pool for 20 minutes.
  • the refluxing material is apparently not gelled, almost nothing drips after 20 minutes, and there is evidently good filling in both winding heads.
  • the stator is exposed to UV light according to the procedure in VB 2, with only a few drops of losses occurring.
  • the winding is heated to 180 ° C. by means of electricity and held for 10 minutes. There are no more drip losses.
  • the laminated core becomes approx. 100 ° C and the plastic parts of the winding heads become approx. 85 ° C warm. Laminated core and winding heads are non-sticky, even in shaded areas of the component there is no longer any stickiness. After cooling overnight, the following day is cured for a further 2 hours at 140 °
  • Example 3 (B3) The procedure is as in Example 1 (B1), but is kept in the immersed state for 2 minutes.
  • Bl filling than with Bl
  • B2 filling
  • evaporation and post-curing losses due to the much higher resin absorption are also somewhat higher than with Bl and B2 are.
  • Example 3 The procedure is as in Example 3 (B3), but after the UV curing in the oven, it is first cured for 1 hour at 120 ° C. and then for a further 2 hours at 130 ° C. After cooling overnight, the following day is cured for a further 2 hours at 140 ° C.
  • the stators were sawn to assess the filling.
  • the components according to examples B3 and B4 show a perfect filling of slot and winding, ie approx. 150-160 g are the maximum possible resin absorption. Resin uptake of about 100% filling level cannot be achieved with any other state-of-the-art process. The dripping, evaporating and post-curing losses are low to an extent not previously achieved. It is also possible to adjust the resin absorption to any desired degree of filling, for example for cost reasons, with largely constant low losses.

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Manufacture Of Motors, Generators (AREA)

Abstract

L'invention concerne un procédé pour imprégner des éléments constitutifs avec des agents d'imprégnation polymérisables, qui sont liquides à température ambiante ou peuvent être fluidifiés par chauffage et peuvent être durcis sous l'action combinée de chaleur et de rayonnements puissants. Les éléments constitutifs sont imprégnés à température ambiante ou à l'état préchauffé, sont chauffés après imprégnation dans l'agent d'imprégnation, jusqu'au point de gélification et sont ensuite soumis à un traitement par rayonnement puissant avant durcissement et sont ensuite entièrement durcis thermiquement.
EP97951185A 1996-11-21 1997-11-13 Procede d'impregnation d'elements constitutifs Expired - Lifetime EP0939963B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19648134A DE19648134A1 (de) 1996-11-21 1996-11-21 Verfahren zur Tränkung von Bauteilen
DE19648134 1996-11-21
PCT/EP1997/006325 WO1998022962A1 (fr) 1996-11-21 1997-11-13 Procede d'impregnation d'elements constitutifs

Publications (2)

Publication Number Publication Date
EP0939963A1 true EP0939963A1 (fr) 1999-09-08
EP0939963B1 EP0939963B1 (fr) 2003-05-02

Family

ID=7812306

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97951185A Expired - Lifetime EP0939963B1 (fr) 1996-11-21 1997-11-13 Procede d'impregnation d'elements constitutifs

Country Status (5)

Country Link
US (1) US6146717A (fr)
EP (1) EP0939963B1 (fr)
DE (2) DE19648134A1 (fr)
ES (1) ES2198603T3 (fr)
WO (1) WO1998022962A1 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19939760A1 (de) * 1999-08-21 2001-03-08 Schenectady Int Inc Verfahren und Vorrichtung zur Isolierung elektrotechnischer Bauteile
DE10209511A1 (de) * 2002-03-05 2003-10-02 Siemens Ag Vorrichtung zur berührungsfreien Hochfrequenzübertragung
DE20216113U1 (de) * 2002-10-18 2004-03-18 Baumüller Nürnberg GmbH Tauchlack-beschichteter Kühl-Gehäusemantel für eine elektrische Maschine
US7786635B2 (en) * 2007-12-13 2010-08-31 Regal Beloit Corporation Motor for high moisture applications
DE102008025541A1 (de) * 2008-05-27 2009-12-17 Hexion Specialty Chemicals Gmbh Verfahren zum Herstellen eines rissfestem Gießharztransformators und rissfester Gießharztransformator
US20130095232A1 (en) * 2011-10-18 2013-04-18 GM Global Technology Operations LLC Method of applying varnish to a stator
JP6149750B2 (ja) * 2014-02-07 2017-06-21 トヨタ自動車株式会社 リアクトルの固定方法
FR3070803A1 (fr) 2017-09-07 2019-03-08 Moteurs Leroy-Somer Procede d'impregnation d'une machine electrique
EP3872962A1 (fr) * 2020-02-25 2021-09-01 Siemens Aktiengesellschaft Procédé d'imprégnation, de renforcement ou d'électroisolation d'un corps portant des enroulements mono- ou multicouche
CN115395750A (zh) * 2022-08-19 2022-11-25 天津云齐新材料技术有限责任公司 电机绕组绝缘浸渍处理方法及装置
DE102022125457A1 (de) 2022-10-04 2024-04-04 Bayerische Motoren Werke Aktiengesellschaft Verfahren und Vorrichtung zum Versehen einer Statorwicklung mit einem Harz

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3914467A (en) * 1971-06-22 1975-10-21 Matsushita Electric Industrial Co Ltd Method of making resin encapsulated electric coil
US3937855A (en) * 1974-06-21 1976-02-10 General Electric Company Method of curing vacuum pressure impregnated coils
US4247578A (en) * 1977-01-14 1981-01-27 Henkel Corporation Interpenetrating dual cure resin compositions
BR8406821A (pt) * 1983-12-21 1985-10-29 Gen Electric Processo para aplicar material isolante de revestimento em enrolamento
JPS60210829A (ja) * 1984-04-04 1985-10-23 Toshiba Corp 変圧器の製造方法
JPS61214749A (ja) * 1985-03-15 1986-09-24 Toshiba Corp 回転電機巻線の絶縁処理方法
DE4022235A1 (de) * 1990-07-12 1992-01-16 Herberts Gmbh Verfahren zur fixierung von wickelguetern und verwendung von radikalisch polymerisierbaren massen hierfuer
JPH0767302A (ja) * 1993-08-26 1995-03-10 Toshiba Corp 回転電機巻線の絶縁処理方法
JPH0767300A (ja) * 1993-08-26 1995-03-10 Toshiba Corp 回転電機巻線のワニス処理方法
DE4331086A1 (de) * 1993-09-11 1995-03-16 Herberts Gmbh Verfahren zur Fixierung von Wickelgütern mit radikalisch polymerisierbaren Massen
US5789039A (en) * 1994-09-06 1998-08-04 Herberts Powder Coatings, Inc. Radiation curing of powder coatings on heat sensitive substrates: chemical compositions and processes for obtaining coated workpieces
DE29505650U1 (de) * 1995-04-01 1995-05-24 Sturm, Werner, 45549 Sprockhövel Vorrichtung zum Trennen und Verschweißen von, zumindestens zum Teil, schmelzfähigen Materialien nach dem Verfahren der Ultraschallschneid- und -schweißtechnik, zusammengefaßt in einer Funktionseinheit
DE19542564A1 (de) * 1995-11-15 1997-05-22 Beck & Co Ag Dr Verfahren zur Imprägnierung von elektrisch leitenden Substraten
WO1997020642A1 (fr) * 1995-12-06 1997-06-12 Kansai Paint Co., Ltd. Procede de formation d'un film de peinture
AU708172B2 (en) * 1996-02-26 1999-07-29 Rohm And Haas Company Dual-cure latex compositions

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9822962A1 *

Also Published As

Publication number Publication date
DE59709984D1 (de) 2003-06-05
WO1998022962A1 (fr) 1998-05-28
ES2198603T3 (es) 2004-02-01
US6146717A (en) 2000-11-14
DE19648134A1 (de) 1998-05-28
EP0939963B1 (fr) 2003-05-02

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