2013
DOI: 10.1088/0957-0233/24/9/095005
|View full text |Cite
|
Sign up to set email alerts
|

Preliminary experimental study on the electrical impedance analysis forin-situmonitoring of the curing of carbon/epoxy composite material for aeronautical and aerospace structures

Abstract: This paper concerns the electrical characterization of T700/M21 unidirectional composite materials using sensors developed specifically for this study. It proposes a reliable and reproducible protocol for the characterization of the material during curing. Prior to the characterization, an analysis was carried out to assess the impact of parasitic access elements (resistance of the electrode/fibre interface or of the feed wire), which was reduced to a minimum by appropriate dimensioning of the electrodes. A st… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

0
15
0

Year Published

2015
2015
2022
2022

Publication Types

Select...
6
1

Relationship

1
6

Authors

Journals

citations
Cited by 11 publications
(15 citation statements)
references
References 33 publications
0
15
0
Order By: Relevance
“…In our current work, electrical impedance (Z) measurements were developed because of their extremely high sensitivity to any change in the composite material during its curing. Effectively, as shown in our previous papers [109][110][111] unidirectional composite laminates behave as an electrical resistance in L direction (according carbon fibers axis) and as the association of a capacitance and a resistance in the two other directions (T for transverse and Z for through-thickness). This is illustrated in Figure 2 where a schematic representation of T700/M21 carbon/epoxy laminates microstructure is given.…”
Section: Impedancemetry For Monitoring Carbon/epoxy Laminates Behaviomentioning
confidence: 63%
See 2 more Smart Citations
“…In our current work, electrical impedance (Z) measurements were developed because of their extremely high sensitivity to any change in the composite material during its curing. Effectively, as shown in our previous papers [109][110][111] unidirectional composite laminates behave as an electrical resistance in L direction (according carbon fibers axis) and as the association of a capacitance and a resistance in the two other directions (T for transverse and Z for through-thickness). This is illustrated in Figure 2 where a schematic representation of T700/M21 carbon/epoxy laminates microstructure is given.…”
Section: Impedancemetry For Monitoring Carbon/epoxy Laminates Behaviomentioning
confidence: 63%
“…The through-thickness (in Z direction -see Figure 2) absolute value of impedance |Z z | and its argument θ z are real-time recorded as a function of current frequency f (Hz) (see eq. 1, 2 and 3) showing thus the capability to detect both the gelation and the vitrification of the epoxy matrix during cure Figure 3 [111]. The maximum changes in the impedance are obtained for a frequency at 10 kHz.…”
Section: Impedancemetry For Monitoring Carbon/epoxy Laminates Behaviomentioning
confidence: 93%
See 1 more Smart Citation
“…Depending on the geometrical parameters (such as thickness, diameter, etc.) and the mechanical properties of the monitored electrical component, the resolution of stress monitoring can differ for the same loading conditions [19] . From the point of view of applicability of such sensors for structural health monitoring the usability is limited due to free vibrations of the tested electronic components.…”
Section: Introductionmentioning
confidence: 99%
“…The designed system is applied for impact monitoring and damage detection for a supporting structure of a sailplane. Another active sensing technique is based on electromechanical impedance (EMI) [2,8], which can be applied on a composite material [12]. The theoretical model for the EMI method was first established by Liang et al [13].…”
mentioning
confidence: 99%