Evaluation of the influence of cooling rate on residual strain development in unidirectional carbon fibre/polyphenylenesulfide laminates using embedded fibre Bragg grating sensors
Abstract:This study investigates the influence of cooling rate on the residual strain of the carbon fibre/polyphenylenesulfide unidirectional laminates. Three different cooling rates (−300℃/min, −100℃/min and −10℃/min) were applied to simulate a wide range of cooling conditions. The crystallisation behaviour which depends on the cooling rate was evaluated using differential scanning calorimetry. A process monitoring test was then conducted using embedded fibre Bragg grating sensors. In-plane transverse strain of carbon… Show more
“…tool–part interaction). 14 Three kinds of molding conditions were set. Because the main difference in the three conditions was the cooling rate, they were defined as slow cooling (SC), medium-speed cooling (MC), and fast cooling (FC).…”
Section: Methodsmentioning
confidence: 99%
“…Fiber Bragg grating (FBG) is a type of optical fiber sensors widely applied to in situ process monitoring. [11][12][13][14][15] They are highly sensitive to changes in strain and temperature. The optical fiber used in this current study is made of silica glass coated by polyimide.…”
In thick thermoplastic composite laminates, nonuniform temperature and cooling rate distribution arises in the through-thickness direction during cost-effective high-rate manufacturing processes. Annealing is often carried out after molding to homogenize degree of crystallinity (DOC) and to reduce residual stress. Even though the change in the residual stress/strain distribution occurring inside thick laminates by this heat treatment is practically important, the changing process and the detailed mechanism are not sufficiently clarified. This present study addresses development and redistribution behavior of residual stress through both molding and annealing using multiple optical fiber sensors deployed in the thickness direction. This article begins by explaining about process monitoring of thick laminates to discuss process-induced strain distribution depending on cooling conditions during molding. Next, strain monitoring is performed during annealing, and the strain change caused by cold crystallization is clarified. Finally, the residual stress distribution is evaluated by a transverse three-point bending test, and the validity of the redistribution mechanism deduced from the strain measurement is confirmed.
“…tool–part interaction). 14 Three kinds of molding conditions were set. Because the main difference in the three conditions was the cooling rate, they were defined as slow cooling (SC), medium-speed cooling (MC), and fast cooling (FC).…”
Section: Methodsmentioning
confidence: 99%
“…Fiber Bragg grating (FBG) is a type of optical fiber sensors widely applied to in situ process monitoring. [11][12][13][14][15] They are highly sensitive to changes in strain and temperature. The optical fiber used in this current study is made of silica glass coated by polyimide.…”
In thick thermoplastic composite laminates, nonuniform temperature and cooling rate distribution arises in the through-thickness direction during cost-effective high-rate manufacturing processes. Annealing is often carried out after molding to homogenize degree of crystallinity (DOC) and to reduce residual stress. Even though the change in the residual stress/strain distribution occurring inside thick laminates by this heat treatment is practically important, the changing process and the detailed mechanism are not sufficiently clarified. This present study addresses development and redistribution behavior of residual stress through both molding and annealing using multiple optical fiber sensors deployed in the thickness direction. This article begins by explaining about process monitoring of thick laminates to discuss process-induced strain distribution depending on cooling conditions during molding. Next, strain monitoring is performed during annealing, and the strain change caused by cold crystallization is clarified. Finally, the residual stress distribution is evaluated by a transverse three-point bending test, and the validity of the redistribution mechanism deduced from the strain measurement is confirmed.
“…QEN' is the endothermic heat per unit mass determined by melting fully crystallized neat PPS resin (150.4 J g −1 ). 13 The mass fraction W f of the fibres was measured as 0.66. During the preheat process, Q EN and Q EX were measured to be 13.8 J g −1 and 16.7 J g −1 , respectively.…”
This study investigates the influence of macroscale skin-core residual stress and cooling rate on the impact response of aerospace grade carbon fibre/polyphenylenesulphide (CF/PPS). Numerical simulations are developed which analyse the thermal shrinkage and residual stress development of unidirectional (UD) lay-up configurations. Macroscale skin-core residual stresses are then incorporated into low-velocity impact simulations based on an orthotropic elastic material model. Interlaminar delamination is modelled using a bilinear cohesive traction–separation law, and intralaminar failure is modelled using the Chang–Chang strength-based failure criterion. The simulation results are compared with the results of drop tower impact tests showing qualitative agreement in terms of maximum impact force and delamination. The results of this work highlight the importance of cooling rate on the interlaminar delamination and intralaminar failure of CF/PPS.
“…9 However, it is quite difficult to measure residual stresses in a composite using nondestructive testing directly. 10 Although the residual strain during composite forming can be measured by an in-situ method like that using an optical fiber strain sensor, 11 the residual stresses in an RVE have not been measured to date. Micro FE simulation provides a feasible approach to study micro-residual stresses as long as the methodology and material data are reliable.…”
As the thickness of a composite differs significantly from the size of a representative volume element, composite is studied at both micro- and macroscales. In this study, the synergy between the prescribed displacement boundary and massively parallel computing enables end users to model a composite described in the micro-meter scale and take into account the global influence of the forming process. After validating the software and material models, the residual stresses of a sandwich thermoplastic composite caused by the dynamic thermomechanical forming process were simulated. The results of the macro-micro simulation revealed that the micro structure of a composite consisting of continuous carbon fiber and thermoplastic that have significantly different material properties has a weak impact on temperature distribution throughout the thickness, but exerts a significant influence on the distribution of in-plane stresses. The stresses within a representative volume element at the top and bottom surfaces of the composite layer were further studied to explain the effect of the temperature gradient on the simulated stresses along with the axial and transverse directions of the fiber. The results of this study provide a practical method to reveal actual residual stresses feasibly and efficiently.
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