# Integrated Damage Sensing in Fibre-Reinforced Composites with Extremely Low Carbon Nanotube Loadings

Authors: Han Zhang; Manabu Kuwata; Emiliano Bilotti; Ton Peijs
Journal: Journal of Nanomaterials
 (2015)

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## Abstract

A nanoengineered hybrid composite system has been developed, with integrated damage sensing capabilities at extremely low carbon nanotube (CNT) contents. The employed simple spray coating technique offers good spatial control and the possibility of localized CNT deposition, especially near the fibre/matrix interface, solving traditional problems associated with the incorporation of nanofillers in fibre-reinforced composite laminates such as increased resin viscosity and filtering effects. Moreover, the employed spraying technology has good potential for industrial scale-up.In situ damage sensing based on standard composite tests has been demonstrated for the first time on hybrid glass fibre/CNT composites using extremely low CNT loadings (below 0.1 wt.%) and shows great potential for localized structural health monitoring by controlled CNT deposition into damage prone zones.


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## Body

## 1. Introduction

Because of the increasing trend of using fibre-reinforced plastics to replace traditional structural materials like metals for various applications including aircraft and automotive, structural health monitoring in composites has become more important than ever. Due to their laminated nature, outstanding in-plane properties are accompanied with relatively weak out-of-plane performance in both glass fibre and carbon fibre-reinforced plastics. Traditional nondestructive testing methods involve the monitoring of internal failure modes typically associated with out-of-plane properties such as delamination or interlaminar shear failure and include techniques such as radiography or ultrasonic scan. Unfortunately, the examination of such part is often associated with a significant downtime and always leads to additional maintenance costs. Hence, thein situ and integrated health monitoring of structural composites is highly desirable for industry.Owing to their excellent mechanical and electrical properties, carbon nanotubes (CNTs) have become one of the most used fillers to enhance composites’ performance [1–5]. The use of CNTs for this purpose has additional benefits as these conductive nanofillers allow for the creation of multifunctional composites with integrated sensing capabilities [6–10], especially for structural health monitoring and damage sensing purposes [11–14]. Various outer stimuli can be sensed by percolated CNT networks within polymer matrices, such as strain [15–18], temperature [8], gas [19, 20], and polymer degradation [21]. Thostenson and Chou [9] have shown that using high shear mixing processes, CNTs can be dispersed in epoxy resins with the aim of sensing damage during a specifically designed tensile test. Traditionally, nanofillers like CNTs are introduced by mixing them into bulk resins such as epoxies before subsequent composite manufacturing, leading to an increase in viscosity of the resins, which interferes with manufacturing processes such as resin transfer moulding (RTM) or prepregging. Moreover, even after dispersion, the CNTs tend to agglomerate over time [22] nullifying their advantage as a nanofiller. In addition, the flow of these CNT modified resins through textile preforms such as woven fabrics can lead to filtering effects [23] by these textile preforms and uneven distribution of the nanofiller throughout the composite part. Hence, spatial control of CNTs in the epoxy matrix is not feasible using such conventional mixing strategies.A solution to this problem comes from coating fibre surfaces with CNTs using techniques such as electrophoresis deposition orin situ growth. Kepple et al. [24] showed improved interlaminar fracture toughness by about 50% with functionalized CNTsin situ grown onto carbon fibre fabrics. Another method is by introducing them into a fibre sizing. Gao et al. [25] introduced CNTs into composite laminates through a CNT modified sizing with the aim ofin situ impact damage sensing. However, the complex processing steps involved and cost of these techniques limit productivity and its ability of scale-up.Spraying techniques are among the simplest methods to deposit and disperse nanomaterials onto substrates, using strong airflows to generate very fine droplets, creating a spray which can be directly delivered onto films, fabrics, or fibres [26]. Very recently, studies based on spraying technique for mechanical reinforcement of fibre-reinforced plastics (FRPs) have been reported [26–28]. Joshi and Dikshit [28] deposited CNTs onto a film and then transferred this onto prepregs for toughening and Yavari et al. [29] sprayed graphene nanoplatelets onto glass fibres for improved fatigue properties, while Thakre et al. [30] have deposited single wall carbon nanotubes onto fibre preforms for interlaminar fracture toughness, although the improvements reported were limited. Zhang et al. utilized this method for CNTs deposition on carbon fibre prepregs and obtained improved mechanical properties [12]. However, to the best of authors’ knowledge, no research works had been performed on utilizing this simple and effective method to deposit CNTs into glass fibre-reinforced plastics (GRP) for damage sensing purposes.In the present work, an airbrushing technique is used for the first time to integrate damage sensing capability into GRP. It is shown that such a spraying technique achieves good CNT distribution, localization, and spatial control. As such the work demonstrates that it is possible to overcome existing processing issues such as increased resin viscosity through the introduction of CNTs in resins, since nanofillers are introduced in the fibre preform rather than in the resin. At the same time spraying provides a cheap and easy scalable method that can be applied to any fibre surface with the possibility of localizing CNTs in damage prone regions.


## 2. Materials and Methods

### 2.1. Materials

The composites system in this study was based on a 2 × 2 twill glass fibre woven fabric (Sigmatex Ltd., UK) and an epoxy resin system RTM6-2 (HexFlow). Nonfunctionalized, high aspect ratio (>150) multiwalled carbon nanotubes (MWCNTs) produced by chemical vapour deposition (CVD) were used as received from Nanocyl S.A. (Product number NC7000), where detailed characterization can be found in [31, 32]. Methanol (Sigma-Aldrich) was used as solvent for CNTs suspension.


### 2.2. Spray Coating Technique

The various steps of the process are schematically depicted in Figure1. Measured amounts of CNTs were dispersed into methanol, using an ultrasonication probe to break down the CNTs agglomerates, with 20% of maximum amplitude and 5000 joules of energy. After sonication, the CNT solution was placed into an airbrush container for spraying deposition. The airbrushing setup (Iwata Performance plus model H4001 HP-CPLUS) was connected with an air compressor (Iwata studio series), providing 30 psi (2.0 bars) of air pressure with 10 cm distance between spraying nozzle and substrate. The spray coating process was repeated with constant pattern to cover complete preform until the prepared CNT suspension has finished.Figure 1
Schematic illustration of CNT spray coating and laminate fabrication process. Glass fibre fabrics are spray-coated on one side and subsequently stacked together for resin infusion using a vacuum assisted resin infusion process.For interlaminar fracture toughness test specimen, six plies of glass fibre fabric all in 0/90° configuration were employed, with five plies single-sided sprayed with 4 mg CNTs on each layer. For interlaminar shear strength (ILSS) test specimen, same spraying procedures were used but here 10 mg instead of 4 mg of CNTs was deposited onto each layer. The spraying process was repeated in a controlled manner until all of the CNT solution was deposited onto the fabric substrate.


### 2.3. Specimen Manufacturing and Preparation

Two parts of epoxy resins were preheated to 80°C before they were mixed with the weight ratio of 59.5 to 40.5 between epoxy and hardener. After degassing the epoxy resin for 30 min in a vacuum oven, the infusion process was carried out under a vacuum of 1 bar at 90°C. Vacuum assisted resin infusion (VARI) was used for the manufacturing of the composite laminates, followed by a typical curing cycle that involved 140°C for 1.5 hrs and a postcure at 180°C for another 2 hrs. After curing, the composite laminates were cut into 135 mm × 20 mm double cantilever beam (DCB) specimens for Mode-I interlaminar testing. The exposed edges at the specimen ends were connected with copper wire and silver paint. Regarding sensing of short beam strength (SBS) specimens for ILSS testing, both in-plane and through-thickness direction were used in the sensing test, as shown in Figure2. Thin copper wire was positioned at both ends of the specimen for in-plane measurements, while, for through-thickness, silver conductive paint was applied to the surface and bottom of specimen, before copper wire was attached by a silver-loaded epoxy adhesive.Figure 2
Illustration ofin situ damage sensing setup for (a) DCB tests and (b) SBS tests.
(a)
(b)


### 2.4. Characterization

For electrical measurements, a digital multimeter (Agilent 34401A) was used to measure the volumetric resistance of each specimen using a two-probe direct current measurement setup. Electrodes were directly connected with copper wires from specimen edges, as shown in Figure2. For interlaminar fracture toughness testing, double cantilever beam tests were performed according to ASTM D5528 [33], using an Instron 5566 universal testing machine at a test speed of 1 mm/min, while, for interlaminar shear strength (ILSS) evaluation, SBS tests were performed in accordance with ASTM D2344 at the same testing machine and a crosshead speed of 1 mm/min.The scanning electron microscope (SEM) used in this work is an Inspect F model from FEI. Morphologies of deposited CNTs on glass fibre surfaces as well as fracture surfaces of specimens after tests were examined under SEM. The fracture surface was gold-coated before examination.


## 2.1. Materials

The composites system in this study was based on a 2 × 2 twill glass fibre woven fabric (Sigmatex Ltd., UK) and an epoxy resin system RTM6-2 (HexFlow). Nonfunctionalized, high aspect ratio (>150) multiwalled carbon nanotubes (MWCNTs) produced by chemical vapour deposition (CVD) were used as received from Nanocyl S.A. (Product number NC7000), where detailed characterization can be found in [31, 32]. Methanol (Sigma-Aldrich) was used as solvent for CNTs suspension.


## 2.2. Spray Coating Technique

The various steps of the process are schematically depicted in Figure1. Measured amounts of CNTs were dispersed into methanol, using an ultrasonication probe to break down the CNTs agglomerates, with 20% of maximum amplitude and 5000 joules of energy. After sonication, the CNT solution was placed into an airbrush container for spraying deposition. The airbrushing setup (Iwata Performance plus model H4001 HP-CPLUS) was connected with an air compressor (Iwata studio series), providing 30 psi (2.0 bars) of air pressure with 10 cm distance between spraying nozzle and substrate. The spray coating process was repeated with constant pattern to cover complete preform until the prepared CNT suspension has finished.Figure 1
Schematic illustration of CNT spray coating and laminate fabrication process. Glass fibre fabrics are spray-coated on one side and subsequently stacked together for resin infusion using a vacuum assisted resin infusion process.For interlaminar fracture toughness test specimen, six plies of glass fibre fabric all in 0/90° configuration were employed, with five plies single-sided sprayed with 4 mg CNTs on each layer. For interlaminar shear strength (ILSS) test specimen, same spraying procedures were used but here 10 mg instead of 4 mg of CNTs was deposited onto each layer. The spraying process was repeated in a controlled manner until all of the CNT solution was deposited onto the fabric substrate.


## 2.3. Specimen Manufacturing and Preparation

Two parts of epoxy resins were preheated to 80°C before they were mixed with the weight ratio of 59.5 to 40.5 between epoxy and hardener. After degassing the epoxy resin for 30 min in a vacuum oven, the infusion process was carried out under a vacuum of 1 bar at 90°C. Vacuum assisted resin infusion (VARI) was used for the manufacturing of the composite laminates, followed by a typical curing cycle that involved 140°C for 1.5 hrs and a postcure at 180°C for another 2 hrs. After curing, the composite laminates were cut into 135 mm × 20 mm double cantilever beam (DCB) specimens for Mode-I interlaminar testing. The exposed edges at the specimen ends were connected with copper wire and silver paint. Regarding sensing of short beam strength (SBS) specimens for ILSS testing, both in-plane and through-thickness direction were used in the sensing test, as shown in Figure2. Thin copper wire was positioned at both ends of the specimen for in-plane measurements, while, for through-thickness, silver conductive paint was applied to the surface and bottom of specimen, before copper wire was attached by a silver-loaded epoxy adhesive.Figure 2
Illustration ofin situ damage sensing setup for (a) DCB tests and (b) SBS tests.
(a)
(b)


## 2.4. Characterization

For electrical measurements, a digital multimeter (Agilent 34401A) was used to measure the volumetric resistance of each specimen using a two-probe direct current measurement setup. Electrodes were directly connected with copper wires from specimen edges, as shown in Figure2. For interlaminar fracture toughness testing, double cantilever beam tests were performed according to ASTM D5528 [33], using an Instron 5566 universal testing machine at a test speed of 1 mm/min, while, for interlaminar shear strength (ILSS) evaluation, SBS tests were performed in accordance with ASTM D2344 at the same testing machine and a crosshead speed of 1 mm/min.The scanning electron microscope (SEM) used in this work is an Inspect F model from FEI. Morphologies of deposited CNTs on glass fibre surfaces as well as fracture surfaces of specimens after tests were examined under SEM. The fracture surface was gold-coated before examination.


## 3. Results and Discussion

A fine percolated network of CNTs onto the glass fibres is observed after spray coating (Figures3(a) and 3(b)). No obvious large CNT aggregates are apparent and localization of CNTs in the damage prone interfacial zone has been achieved. The CNTs deposited by airbrushing are positioned not only at the fibre surface but also near the interfacial or matrix regions in between individual fibres. This is attributed to two main factors: first, the strong airflow during airbrush deposition which directly positions CNTs within the spacing between individual glass fibres and secondly, the infusion process during VARI which allows for some of CNT migration into the glass fibre bundles, especially as a result of through-thickness resin flow.Figure 3
SEM images of (a) percolated CNT network on glass fibre surface and in interfacial regions; (b) higher magnification showing deposited networks on fibre surface; (c) fracture surface of DCB tested specimen with CNTs presented; (d) cross-sectional area of reference specimen after SBS test; and (e) cross-sectional area of CNT/GRP hybrid specimen after SBS test.
(a)
(b)
(c)
(d)
(e)From the SEM fracture surface images of the Mode-I tested composite laminates (Figure3(c)), it can be seen that glass fibres are covered by epoxy, indicating good adhesion between fibres and resin with the presence of CNTs. CNTs could also be found on both fibre surfaces and connected interfacial regions between fibres and matrix, which can contribute to enhanced stress transfer compared to composites based on neat resins. The well-dispersed electrically conductive CNT network within these glass fibre laminates can now be used for damage sensing through the monitoring of resistivity changes with progressive cracking. Figures 3(d) and 3(e) show the cross-sectional areas of GRP reference specimen and hybrid CNT/GRP specimen after SBS tests, respectively, where very clear interlaminar shear failures were observed.Using spray coating technology, a concentration of as little as 0.012 wt.% CNTs is able to introduce electrical conductivity into the composite laminates, indicating excellent network formation. This extremely low CNT loading is chosen due to our previous sensing experience based on percolated networks that sensitivity of the composites upon outer stimuli will be reduced if CNT loading is well above percolation threshold [15, 34]. The obtained electrical conductivity is believed to be not solely attributed to the initial dispersion of CNTs onto the fibre surfaces, but also the result of a “dynamic percolation” process [15, 34] to take place after the infusion process but before complete cross-linking of the epoxy resin.Figure4(a) shows the damage sensing results together with a typical load-displacement curve from the DCB test. The successive drops in the load curve are due to crack propagation. The simultaneously measured resistivity increases with clear steps which directly correlate with the load drops and is due to the percolated CNT network being affected by crack propagation. This correlation confirms that the spray-coated conductive CNT network on the glass fibre fabrics can be used as a sensing tool to detect damage within the composite specimens during mechanical deformation.Figure 4
(a)In situ damage sensing results showing measured volumetric electrical resistivity during DCB testing, accompanied with load-displacement curves; (b) correlation between relative resistivity and load change (in percentage).
(a)
(b)To further confirm the correlation between mechanical performance and electrical sensing signals, the relative force and resistivity change (in percentage) is plotted (Figure4(b)). The relative change of load and resistance was taken from the data separately and plotted as a function of displacement. Excellent correlation between these two signals is observed, indicating the reliability of this technique to detect delamination damage in composite laminates. Although the measured interlaminar fracture toughness (GIC) of the CNT modified laminates (0.52±0.09 kJ/m2) was only slightly higher than that of the reference laminate (0.44±0.05 kJ/m2), the spray coating approach did show some promise in improving interlaminar toughness, taking into account the extremely low CNT concentration (0.012 wt.%) used. Again this stresses the advantage of CNT localization at damage prone zones or interfacial regions to improve its efficiency.Thein situ damage sensing work was also applied to SBS tests to examine its effectiveness under flexure loadings. Both in-plane and through-thickness direction were used to apply an electrical field for sensing; unfortunately, no electrical signals were recorded in through-thickness specimens. This is believed to be due to two main reasons: (i) the relatively low CNT loading in the composites (0.072 wt.%) and (ii) the appearance of resin rich regions near the surface of the specimens leading to higher electrical resistance. Hence, only in-plane sensing results were successfully obtained and employed to analyse the internal damage during the SBS test.Figure5 shows the load curves together with the normalized electrical sensing signals. For the SBS test, the force starts to build up from beginning of the test, until interlaminar shear failure occurs which leads to an obvious drop of the force before the end of the test. Clearly, at the beginning of the test, the sensing signal was not much affected by the applied load but is maintained at its initial starting level. It is worth noting that the electrical resistance was actually slightly reduced with increased loading, which was due to the flexural deformation which involves partly compression of the specimen and a slightly reduced gap between CNTs within the network. This finding is consistent with other researches [16, 35]. When interlaminar shear failure occurs, the network structure of the percolated CNTs is severely affected, leading to a dramatic change in sensing signals. From the enlarged graph near the ultimate failure load (Figure 5(b)), it can be seen very clearly that also here the measured electrical sensing signals correlate well with the applied load, with the highest resistance change occurring near the final failure of the specimen.Figure 5
Damage sensing results for ILSS test: (a) load curve with in-plane sensing results; (b) zoomed in area near the failure load.
(a)
(b)Table1 summarizes the observed mechanical properties of the nanoengineered hybrid composites. As expected, with the extremely low CNT loadings employed in this study, no major improvements in both interlaminar fracture toughness and interlaminar shear strength were observed. However, more importantly, mechanical property levels were sustained at their initial levels while at the same time multifunctionality was introduced through a damage sensing capability.Table 1
Summary table for mechanical properties of glass/epoxy laminates with and without CNT spray coating.
Reference
With CNT spray coating
Relative change (%)
CNT loading  (wt.%)
G
IC (kJ/m2)
0.44 (±0.05)
0.52 (±0.09)
+18%
0.012
ILSS (MPa)
38.35 (±2.12)
40.25 (±0.82)
+5%
0.072


## 4. Conclusions

A hybrid micronanocomposite with integrated damage sensing capabilities was prepared using extremely low CNT concentrations.In situ damage sensing was established based on standard composite tests. An airbrushing technique proved to be a highly effective method to disperse and deposit CNTs onto fibre textile preforms with great spatial control and potential for localization, introducing damage sensing capabilities into glass fibre composite laminates. Apart from its simplicity and versatility, spraying also allows for a relatively easy industrial scale-up. The highly effective percolated CNT networks obtained were utilized to detect interlaminar damage in real time, while simultaneously providing some mechanical property improvement.



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*Source: 785834-2015-06-08.xml*