The thermal conductivity of epoxy resin can be increased by a factor of eight to ten by loading with highly conductive particles. However, higher loadings increase the viscosity of the resin and hamper its use for liquid composite molding processes. Thus, the enhancement of the out-of-plane thermal conductivity of carbon composites manufactured by VARTM and accomplished by matrix filling is limited to about 250%. In order to derive higher increases in out-of-plane thermal conductivity, additional measures have to be taken. These consist of introducing thermally conductive fibers in out-of-plane direction of the preform using a 3D-weaving process. Measured out-of-plane thermal conductivities of 3D-woven fabric composites are significantly increased compared to a typical laminated composite. It has been shown that if introducing highly conductive z-fibers, the use of a particle filled resin is not necessary and furthermore should be avoided due to the manufacturing problems mentioned above. An existing analytical model was altered to predict the effective thermal conductivity as a function of the composite material properties such as the thermal conductivities and volume contents of fibers in in-plane and out-of-plane directions, the thermal conductivity of the loaded resin, the grid-density of the out- of-plane fibers, and material properties of the contacting material. The predicted results are compared with measured data of manufactured samples.
Fiber based composites offer the unique ability to tailor material properties locally. Localized matrix or fiber architecture changes can meet local mechanical, electrical, or thermal loads within a component or vehicle, without the penalty of extra weight or the necessity to resort to additional external structures. Such integral materials reduce the number of components leading to not only more elegant designs, but also to structures that are less costly to manufacture. Local strength, stiffness, toughness, and thermal properties can be tailored by using carbon fibers and/or improved matrices. Numerous attempts have been made to increase the thermal conductivity of the matrix by adding high thermal conductivity solid fillers [
To further enhance the out-of-plane thermal conductivity of a composite plate or part, the fiber architecture has to be altered by introducing highly conductive carbon fibers in the out-of-plane direction. This can be done by different textile technology based procedures [
Tufting;
Stitching;
Z-pinning;
3D-weaving.
Tufting and stitching are used on two-dimensional fabrics and thus are not suitable to introduce greater contents of z-fibers to the preform in the thickness direction without damaging the planar reinforcing fibers. Z-pinning is a technique to insert pins in thickness direction by mechanically forcing pins through the dry 2D-preform [
3D-weaving is the only technology to manufacture a fabric with z-fibers of variable and higher contents (
matrix or the fiber architecture has been altered. A novel approach consists in combining both approaches. Thus, the objective of this research is to evaluate the suitability of the increase of the thermal conductivity by improving matrix conductivity and fiber architecture and its prediction.
The matrix material was a cold-curing HP-E3000GL_SDB_resin with HP-E200GL_ SDB_hardener from HP-Textiles in which aluminum particles with an average diameter of 4 µm were distributed with a weight fraction of 7.5% corresponding with an Al-particle volume fraction of 3.6%. The thermal conductivity of this resin is given as 0.2 W/(m∙K) and of the aluminum as 170 W/(m∙K).
For in-plane fibers, the Tenax®-E HTA40 E13 3K 200 tex fiber with a thermal conductivity of 17 W/(m∙K) is used. The out-of-plane fibers were high-modulus pitch-fibers from Mitsubishi (K13916 3K 2200 tex) with a thermal conductivity of 200 W/(m∙K). It was originally intended to utilize a pitch-fiber from Mitsubishi (K13D2U 2K 365 tex) with a thermal conductivity of 800 W/(m∙K) which was unfortunately not accessible.
A 3D-weaving machine from the company MAGEBA (
pable to lift 160 g. From 1024 available Jacquard-threads, 750 were used to move the same number of the light Tenax-warp-yarns. 14 Jacquard-threads were attached to the 14 heavy pitch-carbon rovings. Preforms were made with attempted preform z-fiber contents 0%, 3% and 6%. The woven fabrics had the dimensions 140 × 140 × 5 mm.
The high modulus pitch fibers used have an ultimate elongation of 0.4%. Thus, they are not primarily suitable to be processed by weaving or stitching due to the small bending radii incorporated by these methods. Braiding is used for a cabling process as known from carpet and tire industries. A supporting polyester thread was braided around the pitch-fiber roving [
Six panels were produced by VARTM. Each panel contained either 0%, 3% or 6% of z-fibers and 0% or 3.6% Al-particles. The entire lay-up was assembled in accordance to
gradually dissipated, and the pressure boundary conditions were maintained until the resin was cured and subsequently post-cured at 65˚C.
It could be noticed that the Al-particles were filtered out within the first 10 mm of the flow path making these panels not worth for further consideration. Thus, a preform with no z-fibers was manufactured, allowing introducing the Al-particles directly into the preform. This preforms was infused as described above.
Four circular specimens with a diameter of 50 mm were cut out of each previously described infused panels by water-jet cutting. The panels had since been milled in order to create plano-parallel surfaces with accessible z-fibers (
The thermal conductivity measurements were performed within a measuring cell (
The thermal conductivity for a particle filled resin can be calculated for particle volume fraction up to 30% with a sufficient accuracy using a model suggested by Maxwell in the 19th century [
with ν P―particle volume fraction.
kp―thermal conductivity of particle.
km―thermal conductivity of matrix.
For a thermal conductivity of a particle much higher than that of the matrix (
More elaborate models have been published by Bruggemann, Cheng-Vachon, and Nielsen.
Bruggemann [
Cheng-Vachon [
with
Nielsen [
with
and
Other, very theoretical models have been developed. However, they are not practical to use [
The out-of-plane thermal conductivity for laminated and woven composites consists of contributions of vertical z-fibers plus the transverse thermal conductivity of the composite without vertical fibers. It can be approximated as a parallel connection of both components [
with δZ-Fibers = νFz/νF.
νFz―fiber volume fraction of z-fibers.
νF―fiber volume fraction of x-, y-, z-fibers.
k33―out-of-plane thermal conductivity of a 3D-woven fabric composite.
k11―longitudinal thermal conductivity of a laminated composite.
k22―transverse thermal conductivity of a laminated composite.
The longitudinal z-fiber contribution can be described according to the longitudinal thermal conductivity modeled by Thornburgh and Pears using the simple rule of mixture [
with kFa―axial fiber thermal conductivity.
The transverse thermal conductivity has been modeled by several researchers. A well accepted model was published by Hatta and Taya [
with kFr―radial thermal conductivity of fiber.
It has been found out that Equation (9) overestimates the thermal conductivities of composite samples with fibers of high thermal conductivity in perpendicular direction [
Distribution of the high conductive areas (number of entry points)
Thermal conductivity of an attaching material to deviate an incoming homogeneous heat flux into an inhomogeneous one (or vice versa for an existing heat flux)
Thickness of composite part or sample
with ξKmat―material factor.
ξTD―thickness-grid density factor.
with kmat―Thermal conductivity of adjacent material.
tsample―thickness of composite part or sample.
drov―diameter of roving.
The thermal conductivity of the loaded resin was calculated using the Equations (2)-(8) with particle volume content of νp = 3.6%. All models delivered quite similar results (
The out-of-plane thermal conductivity k33 can be predicted according to Equations (9)-(14). One key parameter to obtain high k33-values is the z-fiber content, which depends on the distance between the z-fibers as shown in
With the parameters given above, the out-of-plane thermal conductivity was calculated depending on the distance between the z-fibers for a 5 mm thick sample and matrix conductivities for neat resin (km = 0.2 W/m∙K) and resin loaded with 3.6% Al-par- ticles (
Models | ||||
---|---|---|---|---|
Maxwell | Bruggemann | Cheng-Vachon | Nielsen | |
km [W/(m∙K] | 0.215 | 0.223 | 0.235 | 0.211 |
thermal conductivity is about 0.1 W/(m∙K) higher than for neat resin and is thus negligible for higher z-fiber contents. As depicted in
The thermal conductivity measurements yielded the following results as shown in
Measured and predicted thermal conductivity values for the out-of-plane direction correspond quite well. The measured thermal conductivity of the neat resin agrees well with the data given by the manufacturer of the resin of 0.2 W/(m∙K) which proves the accuracy of the measuring device used. The thermal conductivities of the composite samples are slightly lower than predicted which can be caused by fibers not having a proper thermal contact due to an insulating resin film and broken fibers due to the weaving process.
It has been shown that reinforcing fabrics in thickness direction with high thermally conductive pitch carbon fibers is a viable method to increase the out-of-plane thermal conductivity of a carbon composite material. Due to the high impact of the z-fiber conductivity on the out-of-plane conductivity, the influence of a loaded matrix is marginal. Moreover, the infusion of preforms in the usual way with loaded resins is almost not possible due to filtering effects. Thus, it can be concluded that if introducing highly conductive z-fibers, the use of a particle filled resin is not necessary and furthermore should be avoided due to the manufacturing problems mentioned above.
The single models introduced in a combined approach to predict the out-of-plane thermal conductivity of a 3D-woven fabric agree well with the measured values. In case of using the K13D2U 2k fiber from Mitsubishi with a thermal conductivity of 800
Sample Type | Out-of plane thermal conductivity k33 | |
---|---|---|
Measurement [W/(m∙K] | Prediction [W/(m∙K] | |
neat resin | 0.206 ± 0.002 | 0.2 (manufacturer data) |
resin + 3.6% Al-particles | 0.217 ± 0.003 | 0.215 (Maxwell) |
0% z-fibers | 0.420 ± 0.015 | 0.507 |
0% z-fibers + 3.6% Al-particles | 0.619 ± 0.049 | 0.543 |
3% z-fibers | 1.42 ± 0.058 | 1.62 |
6% z-fibers | 3.87 ± 0.053 | 4.15 |
W/(m∙K), which has the same ultimate elongation as the fiber used, an out-of-plane thermal conductivity of more than 15 W/(m∙K) can be predicted while maintaining the same fiber spacing and thus z-fiber volume fraction. This should be proven experimentally once these fibers are accessible.
Using newly developed shuttles, the weaving process with very brittle but cabled pitch fibers was possible. This approach has to be followed and smaller spacings between z-fibers should be produced by 3D-weaving.
Thanks are due to the German Science Foundation (DFG), which supported financially the acquisition of the 3D-weaving machine financially (INST 252/9-1) and the AiF Arbeitsgemeinschaft industrieller Forschungsvereinigungen “Otto von Guericke” e.V. for financial support through the ZIM-project KF2161903PK1 to develop a shuttle for weaving carbon fibers.
Schuster, J., Schütz, M., Lutz, J. and Lempert, L. (2016) Prediction of the Enhanced Out-of-Plane Thermal Conductivity of Carbon Fiber Composites Produced by VARTM. Open Journal of Com- posite Materials, 6, 100-111. http://dx.doi.org/10.4236/ojcm.2016.64010