2021
DOI: 10.1016/j.compositesa.2020.106224
|View full text |Cite
|
Sign up to set email alerts
|

Experimental study and in-situ FBG monitoring of process-induced strains during autoclave co-curing, co-bonding and secondary bonding of composite laminates

Abstract: The geometric stability of bonded structural parts, such as self-stiffened panels, is a critical issue in aeronautics.However, autoclave curing and bonding of large complex integrated primary structures often induce distortions compromising their geometric stability. Composite cure-induced strains and distortions have been extensively studied in the literature but the influence of the adhesive on these distortions has often been overlooked. More experimental data are therefore necessary to properly understand … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
5

Citation Types

2
22
0

Year Published

2021
2021
2024
2024

Publication Types

Select...
10

Relationship

0
10

Authors

Journals

citations
Cited by 30 publications
(24 citation statements)
references
References 36 publications
2
22
0
Order By: Relevance
“…Then, the upper and lower skins and honeycomb core are glued together using a secondary bonding method. Thus, the manufacturing process is complicated, and the manufacturing cost is high [ 15 ]. In contrast, the VARI process could make all the components in a single molding step, resulting in the rapid and low-cost manufacturing of sandwich structures [ 4 , 16 ].…”
Section: Introductionmentioning
confidence: 99%
“…Then, the upper and lower skins and honeycomb core are glued together using a secondary bonding method. Thus, the manufacturing process is complicated, and the manufacturing cost is high [ 15 ]. In contrast, the VARI process could make all the components in a single molding step, resulting in the rapid and low-cost manufacturing of sandwich structures [ 4 , 16 ].…”
Section: Introductionmentioning
confidence: 99%
“…Oliveira et al [ 14 ] investigated influences of four types of tools, including aluminum, steel, carbon composites and carbon foam, on the internal stresses of carbon fiber composites during autoclave curing using embedded fiber Bragg gratings. Moretti et al [ 15 ] used an experimental approach to examine the effect of curing processes, such as co-curing, co-bonding, and secondary bonding, on the geometric stability of composite laminates. However, composite curing experiments are often costly, time-consuming, and not conducive to parametric studies.…”
Section: Introductionmentioning
confidence: 99%
“…It has become the main connection technology for CFRP materials in the aerospace field [12]. In the aerospace industry, the bonding of CFRPs includes co-curing, co-bonding, and secondary bonding [13]. The CFRP laminate is used in co-bonding and secondary bonding [14][15][16][17], so the surface treatment has an important influence on the bonding performance [18,19].…”
Section: Introductionmentioning
confidence: 99%