EP3681969A1 - Élément dissipateur de chaleur - Google Patents

Élément dissipateur de chaleur

Info

Publication number
EP3681969A1
EP3681969A1 EP18778385.7A EP18778385A EP3681969A1 EP 3681969 A1 EP3681969 A1 EP 3681969A1 EP 18778385 A EP18778385 A EP 18778385A EP 3681969 A1 EP3681969 A1 EP 3681969A1
Authority
EP
European Patent Office
Prior art keywords
graphite
pcm
plate
microencapsulated
heat
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.)
Withdrawn
Application number
EP18778385.7A
Other languages
German (de)
English (en)
Inventor
Thomas Koeck
Werner Langer
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.)
SGL Carbon SE
Original Assignee
SGL Carbon SE
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 SGL Carbon SE filed Critical SGL Carbon SE
Publication of EP3681969A1 publication Critical patent/EP3681969A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K5/00Heat-transfer, heat-exchange or heat-storage materials, e.g. refrigerants; Materials for the production of heat or cold by chemical reactions other than by combustion
    • C09K5/02Materials undergoing a change of physical state when used
    • C09K5/06Materials undergoing a change of physical state when used the change of state being from liquid to solid or vice versa
    • C09K5/063Materials absorbing or liberating heat during crystallisation; Heat storage materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D20/00Heat storage plants or apparatus in general; Regenerative heat-exchange apparatus not covered by groups F28D17/00 or F28D19/00
    • F28D20/02Heat storage plants or apparatus in general; Regenerative heat-exchange apparatus not covered by groups F28D17/00 or F28D19/00 using latent heat
    • F28D20/023Heat storage plants or apparatus in general; Regenerative heat-exchange apparatus not covered by groups F28D17/00 or F28D19/00 using latent heat the latent heat storage material being enclosed in granular particles or dispersed in a porous, fibrous or cellular structure
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/61Types of temperature control
    • H01M10/613Cooling or keeping cold
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/62Heating or cooling; Temperature control specially adapted for specific applications
    • H01M10/625Vehicles
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/65Means for temperature control structurally associated with the cells
    • H01M10/651Means for temperature control structurally associated with the cells characterised by parameters specified by a numeric value or mathematical formula, e.g. ratios, sizes or concentrations
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/65Means for temperature control structurally associated with the cells
    • H01M10/653Means for temperature control structurally associated with the cells characterised by electrically insulating or thermally conductive materials
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/65Means for temperature control structurally associated with the cells
    • H01M10/655Solid structures for heat exchange or heat conduction
    • H01M10/6554Rods or plates
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/65Means for temperature control structurally associated with the cells
    • H01M10/659Means for temperature control structurally associated with the cells by heat storage or buffering, e.g. heat capacity or liquid-solid phase changes or transition
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M2220/00Batteries for particular applications
    • H01M2220/20Batteries in motive systems, e.g. vehicle, ship, plane
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/14Thermal energy storage

Definitions

  • the invention relates to a heat dissipation element and its use for temperature control of a Li-ion battery in automobiles, trucks or pedelecs.
  • the object of the present invention is therefore to provide heating elements for Li-ion batteries, which can stabilize the temperature of the Li-ion battery to a predetermined temperature and with which the above-mentioned disadvantages of the prior art are overcome.
  • the object is achieved by the use of at least one heat dissipation element for tempering a Li-ion battery in the automobile, truck or pedelec comprising graphite and microencapsulated phase change material (PCM).
  • at least one heat dissipation element for tempering a Li-ion battery in the automobile, truck or pedelec comprising graphite and microencapsulated phase change material (PCM).
  • the heat dissipation elements are arranged in the Li-ion battery between the so-called pouch cells, so that depending on the structure of the Li-ion battery one or more heat dissipation elements are used.
  • the graphite is selected from the group consisting of natural graphite, synthetic graphite, expanded graphite or mixtures thereof.
  • graphite such as natural graphite is usually mixed with an intercalate such as nitric acid or sulfuric acid and heat-treated at an elevated temperature of, for example, 600 ° C to 1200 ° C. (DE10003927A1)
  • Expanded graphite represents a graphite that is expanded by a factor of 80 or more, for example, compared to natural graphite in the plane perpendicular to the hexagonal carbon layers. Due to the expansion, expanded graphite is characterized by excellent formability and good intermeshability. Expanded graphite may be used in sheet form, preferably using a film having a density of 0.7 to 1.8 g / cm 3 . A film having this density range has thermal conductivities of 150 W / (mK) to 500 W / (mK). The thermal conductivity is determined by the Angstrom method (Angstrom's Method of Measuring Thermal Conductivity, Amy L. Lytle, Physics Department, The College of Wooster, Theses).
  • phase change material is understood as meaning a material which undergoes a phase transition when heat is supplied or discharged. This can be, for example, a transition from the solid to the liquid phase or vice versa.
  • phase transition point is reached, the temperature remains constant until the material is completely transformed.
  • latent heat The heat supplied or removed during the phase transition, which does not cause a temperature change in the material, is called latent heat.
  • the PCM is selected from the group consisting of sugar alcohols, paraffin, waxes, salt hydrates, fatty acids, preferably selected from the group consisting of paraffins, salt hydrates and waxes.
  • sugar alcohols there may be used, for example, pentaerythritol, trimethylolethane, erythritol, xylitol, mannitol, neopentyl glycol, and any mixture thereof.
  • paraffins it is possible to use saturated hydrocarbons having the general empirical formula C n H 2n + 2, where the number n between 18 and 32 can lie. The molar mass of such paraffins is thus between 275 and 600 grams per mole.
  • the salt hydrates used can be, for example, calcium chloride hexahydrate, magnesium chloride hexahydrate, lithium nitrate trihydrate and sodium acetate trihydrate.
  • Capric acid, lauric acid, myristic acid, palmitic acid, stearic acid and any desired mixture thereof can be used as fatty acids, for example.
  • the choice of PCM depends on the temperature range in use.
  • the PCM has a melting range between -20 and 130 ° C, preferably between -10 and 100 ° C, more preferably between 0 and 70 ° C.
  • the temperature stabilization in the melting range of less than -20 ° C and greater than 130 ° C can be realized by phase change materials only by increased effort and weight. In addition, these temperatures are rare, so that the material held almost exclusively without function is carried. To prevent this, the temperature range between -20 ° C and 130 ° C is selected.
  • the temperature of the Li-ion battery is stabilized, for example, the temperature can be stabilized at 6 ° C during cooling at night.
  • phase transition preferably the entire phase transition
  • at least part of the phase transition (preferably the entire phase transition) of the PCM takes place in a temperature range from 20 to 0 ° C. This can be determined calorimetrically by measuring and recording the temperature in the heat sink, exposing the heat sink in a calorimeter to a defined temperature atmosphere, and continuously ramping that temperature 20K above the melting point of the PCM (highest melting point) , 1 K / min decreases, up to one
  • Phase-change microcapsulated phase-change material in this temperature range is available from Mikrotek Laboratories Inc., Dayton, Ohio 43459, and is available under the designations MPCM 6 and MPCM 18. With the help of such PCM is further cooling the battery parked Vehicle delays especially efficiently towards the end of the night and early morning. On many winter mornings, the PCM will then provide exactly the energy that would otherwise have to be supplied to the Li-ion battery prior to startup with active supply of heat with heating elements.
  • PCM microencapsulated phase change material
  • the temperature at which a PCM begins to solidify is at least 8K higher than the temperature at which another PCM, which solidifies at a lower temperature, is completely solidified. Again, this is easily read from the thermogram.
  • the different PCMs are preferably spatially separated, e.g. by being present in different microcapsules.
  • Embodiments with PCMs having different melting ranges achieve the desired improvements in the starting state of the vehicle over a wider range of different ambient temperatures. This is desirable because the lows reached in winter nights can vary widely from night to night.
  • the microencapsulated PCM has a size of ⁇ 5 mm, preferably ⁇ 1 mm, particularly preferably ⁇ 100 ⁇ m.
  • the at least one heat sink is formed as a sheet or foil comprising graphite and microencapsulated PCM or formed as a sheet or foil comprising graphite and microencapsulated PCM, on the sheet or foil at least one layer comprising microencapsulated PCM.
  • the at least one heat-dissipating element or as a graphite foil or graphite plate is formed and comprises at least one applied layer of microencapsulated PCM.
  • the various embodiments of the heat dissipation element can be used in any combination for the temperature control of a Li-ion battery.
  • the proportion of microencapsulated PCM in the plate or film comprising graphite, microencapsulated PCM and additionally binder is 10% by weight to 98% by weight, preferably 20% by weight to 80% by weight, particularly preferably 45% by weight to 70% by weight .%.
  • the proportion of binder on the plate comprising graphite, microencapsulated PCM and additionally binder 2 to 30% by weight, preferably 5 to 20% by weight.
  • the strength of the composite material can be increased and the heat capacity is only slightly affected. In the preferred case, the heat capacity is only reduced by 10%.
  • the binder may be selected from the group consisting of epoxy resins (such as Araldite 2000 (2014)), phenolic resins, silicone resins, acrylate resins, rubber (e.g., Litex SX1014) or thermoplastics.
  • the proportion of microencapsulated PCM of the layer comprising microencapsulated PCM and additionally binder applied to the sheet or foil comprising graphite and microencapsulated PCM is 10 to 98% by weight, preferably 15 to 95% by weight, more preferably 30 to 88% by weight.
  • the proportion of microencapsulated PCM of the layer comprising microencapsulated PCM and additionally binder applied to the graphite foil or graphite plate is 10% to 98% by weight.
  • the amount of binder in the layer comprising microencapsulated PCM and additionally binder applied to the graphite and microencapsulated PCM plate or film is from 1 to 40% by weight, preferably from 2 to 30% by weight, more preferably from 5 to 20 wt.%.
  • the proportion of binder of the layer comprising microencapsulated PCM and additionally binder, which is applied to the graphite foil or graphite plate 1 to 40 wt.%, Preferably 2 to 30 wt.%, Particularly preferably 5 to 20 wt.%.
  • the proportion of binder is no longer sufficient for strength and with more than 40% by weight of binder, the proportion of binder is too high, so that the heat capacity of the layer, due to the microencapsulated PCM, negative being affected.
  • these may also contain a dispersing aid, the proportion being between 0 and 5% by weight.
  • a dispersing agent for example, polyvinylpyrrolidone (PVP) can be used.
  • the binder content ensures a firm and compact layer, whereas with a desired high enthalpy of fusion a correspondingly high proportion of microencapsulated PCM is to be selected.
  • conductive additives may consist, for example, of carbon nanotubes (CNTs), graphene, graphene oxide or hexagonal boron nitride.
  • the layer applied to the plate, foil, graphite plate or graphite foil can be applied to one or more sides of the plate, foil, graphite plate or graphite foil.
  • the at least one layer comprising microencapsulated PCM has a thickness of ⁇ 5 mm, preferably 1 to 3 mm, particularly preferably 100 to 500 ⁇ m. With a thickness of the layer of greater than 5 mm, the flexibility of the composite is negatively influenced by the thickness layer. In addition, there are adhesion problems of the coating on the carrier substrate.
  • the film or graphite foil has a thickness of 10 ⁇ m to 1 mm, preferably 25 to 500 ⁇ m, particularly preferably 25 to 100 ⁇ m. At less than 10 ⁇ m, no appreciable effect occurs due to the graphite foil.
  • the plate or graphite plate has a thickness of> 1 to 5 mm, preferably 2 to 4 mm, particularly preferably 2 to 3 mm. If greater than 5 mm, the effect according to the invention is not achieved.
  • the thermal conductivity of the at least one heat-dissipating element is above 150 W / (m-K).
  • Another object of the invention is a heat sink, which comprises graphite and microencapsulated PCM, wherein the heat dissipation element is formed as a plate or foil and on the plate or foil at least one layer comprising microencapsulated PCM is applied.
  • the present invention will be described purely by way of example with reference to advantageous embodiments and with reference to the accompanying drawings. The invention is not limited by the figures.
  • FIG. 1 shows a heat dissipation element in cross section.
  • FIG. 2 shows a heat dissipation element in cross section.
  • FIG. 3 shows a heat dissipation element in cross section.
  • FIG. 1 shows a heat dissipation element made from a graphite foil (1) and a layer of microencapsulated PCM (3) applied thereon with a binder (2).
  • Figure 2 shows a heat dissipation element as a graphite (4), microencapsulated PCM (3) and binder (2) plate.
  • Figure 3 shows a heat dissipation element as a graphite (4), microencapsulated PCM (3) and binder (2) plate and a microencapsulated PCM (3) and binder (2) layer applied thereto.
  • a heat dissipation element as a graphite (4), microencapsulated PCM (3) and binder (2) plate and a microencapsulated PCM (3) and binder (2) layer applied thereto.
  • a graphite foil with a thickness of 150 ⁇ and a density of 1.3 g / cm 3 (commercially available from SGL Carbon GmbH) is unilaterally with a mixture of
  • microencapsulated PCM (Micronal 28, BASF), a rubber binder and a
  • composition of the mixture is 24.5 g of water, 1.5 g of Litex SX 1014, 10.4 g of microencapsulated PCM (Micronal 28, BASF) and 0.1 g of polyvinylpyrrolidone (PVP).
  • the mixture is dispersed in an ultrasonic bath and applied to a coating system with a doctor blade height 500 ⁇ .
  • the result after drying is a 200 ⁇ thin layer on the graphite foil.
  • Embodiment 2 is a diagrammatic representation of Embodiment 1:
  • a graphite foil with a thickness of 150 ⁇ and a density of 1.3 g / cm 3 (commercially available from SGL Carbon GmbH) is double-sided with a mixture of
  • microencapsulated PCM (Micronal 28, BASF), 5 ⁇ fine graphite powder, a
  • Rubber binder and a dispersing aid coated Rubber binder and a dispersing aid coated.
  • composition of the mixture is 31.5 g of water, 2 g of Litex SX 1014, 20 g of graphite powder, 10.4 g of microencapsulated PCM (Micronal 28, BASF) and 0.1 g of polyvinylpyrrolidone (PVP).
  • the mixture is dispersed in an ultrasonic bath and applied to a coating system at 55 ° C. with a doctor blade height 600 ⁇ m.
  • the result after drying is a 400 ⁇ thin layer on the graphite foil.
  • a plate with microencapsulated PCM (Micronal 28, BASF) for use as a heat sink is as follows: 135 g of graphite powder (50 ⁇ ), 67.5 g of graphite powder (150 ⁇ ), 810 g of microencapsulated PCM (Micronal 28, BASF) and 337.5 g Elastosil M4642A as a binder and Elastosil M4642B as a hardener ,
  • Embodiment 4 The individual mixture components are added in succession in an Eirich mixer and mixed for a total of 10 minutes. Subsequently, the raw mass is pressed in a press in a 5 mm thick plate.
  • Embodiment 4 The individual mixture components are added in succession in an Eirich mixer and mixed for a total of 10 minutes. Subsequently, the raw mass is pressed in a press in a 5 mm thick plate.
  • a plate with microencapsulated PCM (Micronal 28, BASF) for use as a heat dissipation element The composition of the plate is as follows: 135 g of graphite powder (50 ⁇ ), 67.5 g of graphite powder (150 ⁇ ), 810 g of microencapsulated PCM (Micronal 28, BASF) and 337.5 g Elastosil M4642A as a binder and Elastosil M4642B as a hardener ,
  • the individual mixture components are added successively in an Eirich mixer and mixed for a total of 10 minutes and pressed into a 5 mm thick plate. Subsequently, the plate is coated on one side with a mixture of microencapsulated PCM (Micronal 28, BASF), a rubber binder and a dispersing aid.
  • the composition of the mixture is 24.5 g of water, 1.5 g of Litex SX 1014, 10.4 g of microencapsulated PCM (Micronal 28, BASF) and 0.1 g of polyvinylpyrrolidone (PVP).
  • the mixture is dispersed in an ultrasonic bath and applied to a coating system with a doctor blade height 500 ⁇ m.
  • the result after drying is a 200 ⁇ thin layer.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Manufacturing & Machinery (AREA)
  • Electrochemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • General Physics & Mathematics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Dispersion Chemistry (AREA)
  • Algebra (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Secondary Cells (AREA)
  • Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)

Abstract

L'invention concerne un élément dissipateur de chaleur et son utilisation pour la thermorégulation d'une batterie lithium-ion dans des automobiles, des poids lourds ou des vélos à assistance électrique type Pedelec.
EP18778385.7A 2017-09-12 2018-09-12 Élément dissipateur de chaleur Withdrawn EP3681969A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102017216105.1A DE102017216105A1 (de) 2017-09-12 2017-09-12 Wärmeableitelement
PCT/EP2018/074600 WO2019053059A1 (fr) 2017-09-12 2018-09-12 Élément dissipateur de chaleur

Publications (1)

Publication Number Publication Date
EP3681969A1 true EP3681969A1 (fr) 2020-07-22

Family

ID=63683843

Family Applications (1)

Application Number Title Priority Date Filing Date
EP18778385.7A Withdrawn EP3681969A1 (fr) 2017-09-12 2018-09-12 Élément dissipateur de chaleur

Country Status (6)

Country Link
US (1) US20200212522A1 (fr)
EP (1) EP3681969A1 (fr)
JP (1) JP7034268B2 (fr)
KR (1) KR20200052337A (fr)
DE (1) DE102017216105A1 (fr)
WO (1) WO2019053059A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114963655A (zh) * 2022-06-13 2022-08-30 武汉理工大学 低热惯性的锂电池冷却液存储系统

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20210175402A1 (en) * 2019-12-10 2021-06-10 Tintoria Piana, US Inc. Thermoelectric Device with Flexible Heatsink
DE102021134531A1 (de) 2021-12-23 2023-06-29 Audi Aktiengesellschaft Wärmeleitmatte für einen Energiespeicher, Energiespeicher und Verfahren zum Herstellen zumindest eines Teils eines Energiespeichers
CN115036507A (zh) * 2022-06-14 2022-09-09 北京新能源汽车股份有限公司 负极补锂极片及其制备方法与应用

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JPH06293099A (ja) * 1993-04-08 1994-10-21 Kanegafuchi Chem Ind Co Ltd 断熱パッド材およびその製造方法
DE10003927A1 (de) 2000-01-29 2001-08-02 Sgl Technik Gmbh Verfahren zum Herstellen von expandierbaren Graphiteinlagerungsverbindungen unter Verwendung von Phosphorsäuren
US8273474B2 (en) * 2000-02-29 2012-09-25 Illinois Institute Of Technology Battery system thermal management
DE60128727T2 (de) * 2001-01-22 2008-01-31 PARKER HANNIFIN Corporation, Cleveland Rückstandsfrei ablösbares thermisches verbindungsstück mit phasenübergangsmaterial
DE102011081149A1 (de) * 2011-08-17 2013-02-21 Sgl Carbon Se Wärmeableiter und elektrischer Energiespeicher
DE102012202748A1 (de) * 2012-02-22 2013-08-22 Sgl Carbon Se Verfahren zur Herstellung einer Graphitfolie
DE102012203924A1 (de) * 2012-03-13 2013-09-19 Sgl Carbon Se Graphit und Phasenwechselmaterial enthaltende formbare Masse und Verfahren zur Herstellung eines Formkörpers aus der Masse
JP6063819B2 (ja) 2013-05-29 2017-01-18 株式会社イノアックコーポレーション 断熱カバーおよびその製造方法
WO2015095271A1 (fr) * 2013-12-17 2015-06-25 All Cell Technologies, Llc Composite à base d'un matériau à changement de phase flexible pour systèmes de gestion thermique

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114963655A (zh) * 2022-06-13 2022-08-30 武汉理工大学 低热惯性的锂电池冷却液存储系统

Also Published As

Publication number Publication date
JP7034268B2 (ja) 2022-03-11
KR20200052337A (ko) 2020-05-14
JP2020535241A (ja) 2020-12-03
US20200212522A1 (en) 2020-07-02
DE102017216105A1 (de) 2019-03-14
WO2019053059A1 (fr) 2019-03-21

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