2018
DOI: 10.1002/ente.201800111
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Interfacial Thermal Resistance in Magnetocaloric Epoxy‐Bonded La‐Fe‐Co‐Si Composites

Abstract: Magnetocaloric composites made from La−Fe−Co−Si particles and an epoxy binder matrix exhibit mechanical stability and good magnetocaloric properties, but also a large characteristic time for thermal transport. Here, the origin of this large time constant is examined by comparing two measurement techniques, direct and contactless, to finite‐element simulations based on a tomographic dataset of the sample. The combination of the low thermal conductivity of the epoxy matrix and a thermal resistance at the interfa… Show more

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Cited by 13 publications
(5 citation statements)
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“…The constant delay with respect to the field variation, observable for all samples, is due to the characteristic time of the temperature sensor, as described in detail in literature. [ 18,37,38 ] In contrast, the adiabatic temperature change for the composite without TEGO is characterized by a response time to the magnetic field about two times larger ( τ = 0.21 ± 0.03 s) as compared with the composite with TEGO. The same delay has been reported also for epoxy‐bonded composites of LaFeSi ( τ = 0.22 s [ 38 ] ) and MnfePSi ( τ = 0.20 s [ 18 ] ) compounds.…”
Section: Resultsmentioning
confidence: 95%
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“…The constant delay with respect to the field variation, observable for all samples, is due to the characteristic time of the temperature sensor, as described in detail in literature. [ 18,37,38 ] In contrast, the adiabatic temperature change for the composite without TEGO is characterized by a response time to the magnetic field about two times larger ( τ = 0.21 ± 0.03 s) as compared with the composite with TEGO. The same delay has been reported also for epoxy‐bonded composites of LaFeSi ( τ = 0.22 s [ 38 ] ) and MnfePSi ( τ = 0.20 s [ 18 ] ) compounds.…”
Section: Resultsmentioning
confidence: 95%
“…Indeed, it has already been demonstrated that the main cause of the worsening of heat transport in a composite made of metallic powder and an epoxy binder matrix is the interfacial thermal resistance at the powder–matrix interface, which is not considered in the simulated model. [ 38 ]…”
Section: Resultsmentioning
confidence: 99%
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