2019
DOI: 10.1016/j.compstruct.2019.01.079
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Smart cure cycles for fiber metal laminates using embedded fiber Bragg grating sensors

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Cited by 33 publications
(27 citation statements)
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“…The tensile strength is between 500 and 700 MPa, with a yield strength of 210 MPa and a Young's modulus of 200 GPa. Due to its good mechanical and durability properties, the alloy is used in aircraft construction and automotive engineering, and has been used in multiple previous studies on fibre metal laminates [8,[23][24][25][26][27].…”
Section: Materials and Specimen Preparationmentioning
confidence: 99%
“…The tensile strength is between 500 and 700 MPa, with a yield strength of 210 MPa and a Young's modulus of 200 GPa. Due to its good mechanical and durability properties, the alloy is used in aircraft construction and automotive engineering, and has been used in multiple previous studies on fibre metal laminates [8,[23][24][25][26][27].…”
Section: Materials and Specimen Preparationmentioning
confidence: 99%
“…In the infusion process, integrated sensors can not only be used to determine the degree of cure, because a sufficiently dense network additionally allows the detection of the flow front [1] in advance of the curing reaction. A comparatively new topic is represented by so-called smart cure cycles [2,3], in which residual stress states are to be reduced by lowering the temperature of the curing component when the gel point is reached. In this way, a stress-free temperature closer to the actual service temperature of the component is achieved and residual stresses decrease while the load-bearing capacity of the component is increased.…”
Section: Introductionmentioning
confidence: 99%
“…In this way, a stress-free temperature closer to the actual service temperature of the component is achieved and residual stresses decrease while the load-bearing capacity of the component is increased. While Kim et al still predicted the gel point using simulations based on DSC data [3], Prussak et al instead used integrated fibre Bragg sensors [2], which determine the point at which a mechanical interaction between the epoxy resin and the surrounding laminate begins.…”
Section: Introductionmentioning
confidence: 99%
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“…Furthermore, they can initiate cracks in the fiber-matrix interface which can result in delamination and premature component failure [2]. The stresses depend on the process history and can be influenced by the curing process itself [5,6]. In the initial state, the matrix usually behaves like a liquid.…”
Section: Introductionmentioning
confidence: 99%