2015
DOI: 10.1016/j.ast.2015.03.013
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Fabrication of a thermoplastic matrix composite stiffened panel by induction welding

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Cited by 69 publications
(57 citation statements)
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“…The melting point of PPS is relatively high (285 °C), and PPS molding takes place at high temperature . As a result, in order to avoid the degradation of the polymer, it is highly desirable to have a process for molding PPS during a minimum of molding time.…”
Section: Pps Processingmentioning
confidence: 99%
See 1 more Smart Citation
“…The melting point of PPS is relatively high (285 °C), and PPS molding takes place at high temperature . As a result, in order to avoid the degradation of the polymer, it is highly desirable to have a process for molding PPS during a minimum of molding time.…”
Section: Pps Processingmentioning
confidence: 99%
“…The melting point of PPS is relatively high (285 °C), and PPS molding takes place at high temperature. [92][93][94][95][96][97][98][99][100][101] As a Adapted with permission. [86] Copyright 1992, Springer.…”
Section: Pps Processingmentioning
confidence: 99%
“…1,2 The high-efficiency assembly and connection technology of the thermoplastic composite components are becoming increasingly critical in the industrial manufacturing field. 4,5 Fusion bonding technologies of the thermoplastic composites commonly include laser welding, 6-8 induction welding, [9][10][11] ultrasonic welding, [12][13][14] resistance welding, and so on. 4,5 Fusion bonding technologies of the thermoplastic composites commonly include laser welding, 6-8 induction welding, [9][10][11] ultrasonic welding, [12][13][14] resistance welding, and so on.…”
Section: Introductionmentioning
confidence: 99%
“…The development of manufacturing technique for curved composite panels by using the Integrated Structural Assembly of Advanced Composites (ISSAC) robot at NASA Langley Research Center. Also, the innovative manufacturing technologies of the integrated stiffened composite panel such as through-thickness stitching followed by resin film infusion [8], vacuum assisted resin transfer molding and Pi-joining [7], continuous induction welding [9] and the pultruded rod stitched efficient unitized structure (PRSEUS) concept [10], etc. All of these techniques make it possible to manufacture integrated stiffened composite panel attached by curved composite stiffeners to satisfy various constraints in the aircraft wings and fuselage design.…”
Section: Introductionmentioning
confidence: 99%