The effect of thermal cycling on the properties of a carbon fibre reinforced magnesium composite

Russell-Stevens, M.; Todd, Richard I.; Papakyriacou, M.

doi:10.1016/j.msea.2005.02.025

Cited by 47 publications

(18 citation statements)

References 19 publications

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“…Types of internal damage observed in MMCs include progressive interfacial reaction, microvoid, and microcrack formation at the interface, interfacial bonding and sliding, fibre fracture and plastic deformation of the matrix leading to dimensional instability. Some types of internal damages are known to cause considerable degradation in composite thermo-physical properties [6].…”

Section: Thermal Expansionmentioning

confidence: 99%

“…Mg matrix and HM carbon fibres have a different coefficient of thermal expansions and thermal conductivity. The CTE of magnesium matrix is large positive 25 × 10 −6 K −1 [13] and that of fibres is even negative -1.5 × 10 −6 K −1 [6,8]. As Rudajevova described in [14] a mismatch in the coefficients of thermal expansion (CTEs) between the metal matrix and the ceramic reinforcements causes large residual thermal stresses that may be influenced by a large difference between the thermal conductivity of the matrix and the reinforcement during the preparation of Mg/C composite.…”

Section: Thermal Expansionmentioning

confidence: 99%

“…Important MMC applications in the ground transportation (auto and rail), thermal management, aerospace, industrial, recreational and infrastructure industries have been enabled by improved functional properties that include high structural efficiency, excellent wear resistance, and attractive thermal and electrical characteristics [5]. MMCs have also been identified as potential candidate materials for primary structural element applications in high-precision space-based system [6]. New magnesium composites are being developed for applications in various branches of industry, mainly for the automotive industry as lightweight structural materials.…”

Section: Introductionmentioning

confidence: 99%

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The microstructure and thermal expansion of Mg/C composite prepared by gas pressure infiltration

BERONSKA¹,

IŽDINSKÝ²,

ŠTEFÁNIK³

et al. 2016

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The interface and thermal expansion behaviour of magnesium matrix composite (Mg--2Al) unidirectionally reinforced with continuous high modulus and high thermal conductivity carbon fibres Thornel K1100 prepared by gas pressure infiltration technique was studied. The structure of the fibre-matrix interface was analysed using light microscopy, SEM, EDS, and TEM. Composite samples were subsequently thermally cycled at the heating/cooling rate of 3 • C min −1 in the temperature range of 30 to 350 • C in an argon atmosphere to reveal their thermal expansion behaviour. K e y w o r d s : metal matrix composites (MMCs), Mg/C interface, thermal expansion, CTE

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Section: Thermal Expansionmentioning

confidence: 99%

Section: Thermal Expansionmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

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The microstructure and thermal expansion of Mg/C composite prepared by gas pressure infiltration

BERONSKA¹,

IŽDINSKÝ²,

ŠTEFÁNIK³

et al. 2016

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“…It was due to the interface debonding and the increase in density of epoxy matrix. The young's modulus of composites decreases significantly by increasing the number of cycles due to external stresses [6,13,16]. No obvious defect or delamination is shown in aluminum-lithium alloy based fiber metal laminates after 1000 cycles.…”

Section: Introductionmentioning

confidence: 99%

Effect of Thermal Cycling on the Tensile Behavior of CF/AL Fiber Metal Laminates

Noor

Pasha

Wakeel

et al. 2017

Adv. Sci. Technol. Res. J.

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The objective of this research work was to estimate the effect of thermal cycling on the tensile behavior of CARALL composites. Fiber metal laminates (FMLs), based on 2D woven carbon fabric and 2024-T3 Alclad aluminum alloy sheet were manufactured by pressure molding technique followed by hand layup method. Before fabrication, aluminum sheets were anodized with phosphoric acid to produce a micro porous alumina layer on surface. This microporous layer is beneficial to produce a strong bond between the metal and fiber surfaces in FMLs. The effect of thermal cycling (-65 to +70ºC) on the tensile behavior of Cf/Al based FML was studied. Tensile strength was increased after 10 thermal cycles, but it was decreased slightly to some extent after 30 and 50 thermal cycles. Tensile modulus also show similar behavior as that of tensile strength.

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“…Thermal cycling led to mechanical damage via microcracks, microvoids and fiber protrusion by interfacial sliding. [17] II. EXPERIMENTAL…”

Section: Introductionmentioning

confidence: 99%

Effects of Thermal and Cryogenic Conditionings on Flexural Behavior of Thermally Shocked Cu-Al2O3 Micro and NanoComposites

Dash

Panda

Ray

2013

Metall Mater Trans A

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The effect of thermal cycling on the properties of a carbon fibre reinforced magnesium composite

Cited by 47 publications

References 19 publications

The microstructure and thermal expansion of Mg/C composite prepared by gas pressure infiltration

The microstructure and thermal expansion of Mg/C composite prepared by gas pressure infiltration

Effect of Thermal Cycling on the Tensile Behavior of CF/AL Fiber Metal Laminates

Effects of Thermal and Cryogenic Conditionings on Flexural Behavior of Thermally Shocked Cu-Al2O3 Micro and NanoComposites

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