Open access peer-reviewed chapter

Composite Materials under Extreme Radiation and Temperature Environments of the Next Generation Nuclear Reactors

By Nikolaos Simos

Submitted: November 14th 2010Reviewed: March 23rd 2011Published: July 20th 2011

DOI: 10.5772/21488

Downloaded: 3932

1. Introduction

In the nuclear energy renaissance, driven by fission reactor concepts utilizing very high temperatures and fast neutron spectra, materials with enhanced performance that exceeds are expected to play a central role. With the operating temperatures of the Generation III reactors bringing the classical reactor materials close to their performance limits there is an urgent need to develop and qualify new alloys and composites. Efforts have been focused on the intricate relations and the high demands placed on materials at the anticipated extreme states within the next generation fusion and fission reactors which combine high radiation fluxes, elevated temperatures and aggressive environments. While nuclear reactors have been in operation for several decades, the structural materials associated with the next generation options need to endure much higher temperatures (1200oC), higher neutron doses (tens of displacements per atom, dpa), and extremely corrosive environments, which are beyond the experience on materials accumulated to-date. The most important consideration is the performance and reliability of structural materials for both in-core and out-of-core functions.

While there exists a great body of nuclear materials research and operating experience/performance from fission reactors where epithermal and thermal neutrons interact with materials and alter their physio-mechanical properties, a process that is well understood by now, there are no operating or even experimental facilities that will facilitate the extreme conditions of flux and temperature anticipated and thus provide insights into the behaviour of these well understood materials. Materials, however, still need to be developed and their interaction and damage potential or lifetime to be quantified for the next generation nuclear energy. Based on material development advances, composites, and in particular ceramic composites, seem to inherently possess properties suitable for key functions within the operating envelope of both fission and fusion reactors. In advanced fission reactors composite materials are being designed in an effort to extend the life and improve the reliability of fuel rod cladding as well as structural materials. Composites are being considered for use as core internals in the next generation of gas-cooled reactors. Further, next-generation plasma-fusion reactors, such as the International Thermonuclear Experimental Reactor (ITER) will rely on the capabilities of advanced composites to safely withstand extremely high neutron fluxes while providing superior thermal shock resistance. In addition it will be required by the composite to possess and maintain under severe neutron irradiation extremely high thermal conductivity to enable the flow of the anticipated extreme thermal heat loads generated in the core. The first wall and blanket surrounding the core in the fusion reactor are the two elements where composites are considered leading candidates.

Composites of special interest to both fission and fusion next generation nuclear reactors are carbon-fiber (C/C) and silicon carbide fiber (SiCf/SiC), and more recently, C/SiC composites. These are continuous fiber-reinforced materials of either carbon or silicon carbide fibers infiltrated with a similar matrix. During the last two decades a number of studies have been conducted to address the feasibility and response of the two composites to different radiation environments of fission and fusion reactors and identify their limitations. While these composite structures have a significant advantage over materials used in the same reactor applications (i.e. nuclear graphite, BeO and metal alloys) because of the physical and mechanical properties they possess, they also experience limitations that require quantification. Carbon-fiber composites for example while they can have customized architecture to enhance desired properties, such as thermal conductivity, they too may experience anisotropic dimensional changes and be susceptible to irradiation-induced degradation. SiCf/SiC composites, on the other hand exhibit good fracture resistance and low induced activity due to the irradiation stability of the SiC crystal but their technology is less mature. Critical issues such as cost, fabrication and joining as well as uncertainties due to lack of experience data in performance/survivability and lifetime in the combined extremes of high temperature and high fast neutron fluxes require further evaluation to qualify and quantify their performance.

During the last three decades and driven primarily by the fusion reactor needs (i.e. ITER) a extensive array of neutron-irradiation experiments at high temperatures have been conducted using available test reactors while the technology in composites was maturing. Facilities such as the High Flux Isotope Reactor (HFIR) at Oak Ridge National Laboratory, Japan Materials Testing Reactor (JTMR) as well as test reactors in Europe have been used to irradiate newly developed alloys and composites to anticipated fluence levels in the next generation fusion and fission reactors. As mentioned above, the understanding of the behaviour of reactor materials through studies and experience from the operating low energy neutron reactors may not necessarily transfer to the new materials under a different neutron spectrum. While the peak of the energy spectrum in the fission reactors to-date is ~1 MeV, neutrons in fast-spectrum reactors of the next generation are of several MeV while neutrons from fusion reactions will have energies of ~14 MeV. Based purely on modelling it is anticipated that the induced damage in the microstructure of materials will be similar to the one corresponding to that induced by less than 1 MeV neutrons. While the assumption may be generally correct, there is greater uncertainty with composites which do not form a perfectly oriented structure and are subject to the effects of dissimilar response between the fibre structure and the matrix. In addition, interaction with higher energy neutrons will generate more hydrogen and helium (as a result of nuclear interactions and transmutation products). Helium trapped within basal graphite planes and irradiation-induced defects will form bubbles and degrade the microstructure of the constituents. Therefore understanding how these composite structures behave in the fast neutron environment and what the degradation rate of their key properties (thermal conductivity, expansion, strength, etc.) is important and assessment by means of extrapolation from available data will be risky.

To observe the effects of high energy irradiating particles on composite structures, irradiation studies have been launched using the Brookhaven National Laboratory (BNL) proton linear accelerator and the target station at the isotope production facility (BLIP). The tuneable, ~25 kW (~110 μA peak) accelerator can accelerate protons to energies up to 200 MeV. Irradiation damage studies on graphite, carbon composites and new alloys have been performed in different phases using the proton beam directly on the materials and reaching fluences of ~1021 protons/cm2. Results on the finding following proton irradiations on carbon composites, graphite and composite-like structures are presented in subsequent sections. In a different irradiation mode where the isotope targets completely absorb the 116 MeV protons, a mostly isotropic fast neutron is generated downstream of the isotope targets from the spallation process. This neutron spectrum with mean energy of ~9 MeV is utilized for the irradiation of composites and new alloys. While peak fluences are of the order of 1019 – 1020 neutron/cm2 for each yearly proton beam run (much lower than the ~1021 -1022 n/cm2) expected in the fusion reactor, still the interaction of these new composites with predominantly fast neutrons is expected to provide useful indicators of their stability and resilience to damage. Neutron irradiation studies at BNL BLIP have been completed recently for a number of super alloys and nano-structured coatings (Al2O3, TiO2) on various substrates. Nanostructured coatings, along with AlBeMet, an aluminium-beryllium metal matrix composite, and structures made of fusion-bonded dissimilar materials constitute a special class of composites which are discussed in a subsequent section.

2. Composites and extreme environments

The development of advanced materials to be used in next generation reactors (Zinkle, 2004) has been driven by the need to endure the extreme environment consisting of prolonged, highly damaging radiation fluxes (tens of dpa), extreme temperatures (above 1000º C and up to 1200º C) and high stress conditions, which together can push well-understood and widely used materials beyond their limit. In fusion and fission reactor applications there are certain key properties that the materials which are playing a pivotal role (i.e. first wall and blanket in a fusion reactor) must maintain. These include low activation, structural integrity, dimensional stability, thermal conductivity and inherent ability to absorb thermal shock.

2.1. C/C composites

Carbon fibre reinforced composites (Cf/C) are an attractive choice for use in the extreme environment of the next generation reactors because of some key properties they inherently possess, namely enhanced strength as compared to nuclear graphite, thermal shock resistance because of their unique structure, extremely low thermal expansion, enhanced thermal conductivity due to the presence and directionality of fibres and low neutron activation. Due to their attractive properties carbon-carbon composites have enjoyed widespread use in advanced technologies which have led to the maturity of their technology and fabrication. A wide variety of architectures of the fibre/matrix have been developed as well as fabrication techniques. Most widely used architectures are the two-dimensional (2D Cf/C) and three-dimensions (3D Cf/C) forms. Shown in Figures 1 and 2 are sections of the three-dimensional architecture of the composite (FSI 3D Cf/C) indicating the orderly fibre bundle (thickness of ~265μm) and matrix arrangement.

While carbon composites exhibit enhanced properties when compared to graphite, radiation-induced damage from neutrons or other energetic particles such as protons is far less well understood. To the contrary, nuclear graphite has been extensively studied for radiation-induced degradation for almost sixty (60) years and so the degradation of the key properties as a function of the neutron fluence such as thermal conductivity, dimensional stability and strength has been established thus leading to limitation thresholds for its use in more extreme environments (Gittus, 1975; Maruyama & Harayama 1992; Nikolaenko et al. 1999). Key findings from these studies on graphite are the anisotropic dimensional changes that take place at higher radiation doses and most importantly the degradation of the thermal conductivity. Within the last two decades a body of experimental research work on irradiation damage of carbon-carbon composites has been reported prompted primarily by the need to identify higher performance, low neutron activation for the first wall of fusion reactors such as the International Thermonuclear Experimental Reactor (ITER). Of primary interest in these reported studies (Burchell, 1992, 1994; Burchell et al. 1996; Barabash, et al., 1998) are neutron irradiation induced dimensional changes, thermal conductivity and mechanical properties.

Figure 1.

Image of a 3D Cf/C composite structure using an optical microscope. Shown is the orderly arrangement of the fibre bundles and the matrix

Figure 2.

A closer view of the fibre/matrix configuration of the 3D Cf/C composite and measured fibre bundle thicknesses

Figure 3.

SEM image of the matrix/fibre bundle interface in 3D C/C composite including the presence of voids (left) and closer depiction (right) of one of the pre-existing voids, individual fibres and interface

2.1.1. Shock resistance

One of the important attributes of C/C composites in the fusion reactor environment is their inherent ability to absorb thermal shock. In an effort to quantify the ability of the C/C composite to absorb thermal shock and so be used as the material of choice in a number of high power accelerator applications including accelerator targets for the Long Baseline Neutrino Experiment, Neutrino Factory (LBNE), beam collimating elements for the Large Hadron Collider (LHC) or energetic beam absorbers, experiments have been performed using intense pulses of energetic protons. In these experiments (Simos et al., 2005) performed using the 24 GeV proton beam at the Accelerating Gradient Synchrotron (AGS) at BNL the shock performance of FMI 3D C/C composite targets (16-cm long, 1-cm diameter rods) was measured and compared to that of ATJ graphite. Shown in Figure 4 is the shock test arrangement where 3D C/C composite and ATG graphite targets are instrumented with fibre-optic strain gauges mounted on the surface of the target and measuring extremely fast axial strain transients in the target resulting from its interaction with the 24 GeV proton beam. The response from the intense (3.0 e+12 protons) and focussed (0.3mm x 0.7mm) proton pulses on the ATJ graphite and 3D C/C targets is shown in Figure 5 where the two are compared. It is evident from the comparison that the carbon-carbon composite shows a much lower response to the shock induced by the beam while radial reverberations indicated by the high frequency cycles within each axial cycle are damped out as a result of the impedance interfaces (fibre/matrix) and the voids that are present as shown in Figure 3.

Due the potential implications and applications of high shock resistance in the carbon-carbon composites which stem from the “effective” low thermal expansion coefficient specific studies (Hereil, 1997) have focussed on experimentally verifying the compressive wave velocities in a plate-impact configuration by wave decomposition. As observed in (Simos et al., 2006; Hereil et al, 1997) the problem of shock in materials such as C/C remains very complex due to the anisotropy and the fibre-matrix interfaces as well as the response to dynamic loads of wave propagation in the individual components. In such materials, understanding the behaviour at the mesoscale is important for modelling and implementation of these composites in large-scale designs.

Figure 4.

C/C composite and ATJ graphite target shock test arrangement for the BNL AGS proton beam tests

Figure 5.

Comparison of shock response in terms of axial strain recorded on 3D C/C and ATJ graphite targets

2.1.2. Radiation damage

While radiation damage in the carbon-carbon composites have been studied using neutrons from various reactors such as the High Flux Isotope Reactor (HFIR) at Oak Ridge National Laboratory or the Japan Materials Testing Reactor (JMTR), the radiation damage from very energetic accelerator protons is very limited. Reported in the neutron-induced damage studies (Burchell, 1992, 1996; Bonal et al., 2009) is that the composite undergoes dimensional changes as a function of the fluence (or dpa) with the 3D architecture to exhibit an isotropic behaviour. Under neutron irradiation and for a fluence of 1.0 dpa the thermal conductivity reduces by ~50% (Burchell, 1992) while other studies (Maruyama & Harayama 1992) on CX-2002U carbon-carbon composite suggest (see Figure 6) that there is a dramatic drop of the thermal conductivity even at very low fluences (0.01 dpa) when the irradiation temperature is 200º C and below the threshold where induced vacancies and interstitials become mobile. Initiation of the degradation of the 3D C/C structure following neutron irradiation have been observed (Snead, 2004) and (Bonal et al, 2009) at the 2 dpa dose level leading to serious structural disintegration at about 10 dpa. These reported levels of irradiation damage onset pose a serious limitation on the desired lifetime of C/C plasma facing components in the fusion reactors.

Figure 6.

Thermal conductivity of neutron-irradiated graphite and carbon-carbon composite (Maruyama, 1992)

Figure 7.

C/C composite following irradiation (10 dpa at 800º C) showing serious degradations and anisotropic dimensional change in the form of swelling and shrinkage of fibre bundles (Snead, 2004)

For high power accelerators, while the thermal shock resistance is superior to graphite and so is the retention of thermal conductivity, degradation as a result of energetic proton irradiation can be a serious limiting factor along with the dimensional stability required of critical elements such as primary beam intercepting accelerator target and collimators. Irradiation damage studies have been conducted in recent years ( Simos et al, 2006a , 2006b, 2008) using the BNL 200 MeV Linac beam at the isotope production facility (BLIP). The main objective was to assess the proton-induced damage at energies higher than the thermal and fast neutrons these composite structures have been exposed in test reactors like HFIR and JMTR and qualify the differences stemming from the irradiating species (protons vs. neutrons) and energies (neutron energies a few MEV and proton energies up to 200 MeV).

Two architectural types of the composite were proton-irradiated and studied. A 2D C/C structure (AC-200) made by Toyo Tanso to be used as a primary beam collimating material at the Large Hadron Collider at CERN where 3.5 TeV protons at the beam halo (>6σ) will be intercepted and diverted away from the circulating beam and a 3D C/C architecture made by FMI as a target candidate material for the high power accelerators (LBNE and Neutrino Factory). In the case of the 2-D C/C, dimensional stability in the direction along the fibres was extremely important and so was the thermal conductivity and structural degradation resistance. The first in series of long exposures (>1020 p/cm2 or >0.2 dpa) for these two composites revealed that both architectures experience serious structural degradation. Shown in Figure 8 is the structural degradation of the AC-200 2D C/C of specimens formed normal to the fibre planes and along the fibres. Also shown in Figure 8 (right) is the structural degradation of the FME 3D C/C composite. The peak proton fluence within the damage area is ~5.0 – 7.0 1020 p/cm2 (~0.6-0.8 dpa) a level significantly lower than the one associated with neutron-based irradiation of 2 dpa (Bonal et al, 2009). Subsequent irradiations to similar fluence thresholds verified the damage initiation onset at these low proton fluences. Recent studies of the FMI 3D C/C composite irradiated in an inert gas (argon) environment showed that there exists an environmental factor associated with the damage given that the apparent fluence threshold for structural degradation has increased slightly. Further investigation on this finding is currently under way.

Figure 8.

Irradiation damage induced by 200 MeV (left) protons on AC-200 2D C/C (left) and damage induced by 160 MeV protons on FMI 3D C/C composite

The dimensional stability of the proton-irradiated 2D and 3D carbon composites was measured using a LINSEIS high precision dilatometer in the BNL hot cell facility. Of primary interest were the irradiation effects on the thermal expansion coefficient which represents a crucial parameter in the accelerator applications discussed above. From the precise measurements made it was observed that the fibres in both architectures undergo shrinkage as a result of the irradiation. This is evident in dimensional change data depicted in Figure 9 (left). The 2D C/C in its un-irradiated state will shrink along the directions of the fibres (negative thermal expansion) and expand in the direction normal to the fibre planes acting more like typical graphite. Following irradiation, however, and during the first thermal cycle that was applied to the 2-D specimen made along the fibres there is an accelerated expansion beyond the irradiation temperature (irradiation temperature is depicted as the inflection point in the curve). This is the result of the expansion of the fibres which experienced shrinking during irradiation. Interesting to note is that the composite with progressive upper temperature limit in a series of thermal cycles restores the uni-irradiated behaviour up to that temperature. Observing the dimensional change along the normal direction shown in Figure 9 as a function of fluence one notes the growth that has occurred along the direction due to irradiation indicated by the apparent shrinkage during the thermal cycle when the composite is being restored towards the original configuration rather that expand with increasing temperature. This is evident in Figure 10 (left) which depicts a subsequent thermal cycle where the dimensional behaviour is aiming towards that of the un-irradiated composite. Comparing this restoration along the normal direction with that of irradiated IG-43 graphite, Figure 10 (right), the similarities can be seen which should be anticipated along this normal direction except that for the 2D C/C the growth in the lattice between the planes has occurred at lower irradiation temperatures.

Figure 9.

Dimensional change in 2D C/C composite following proton irradiation and removal of fibre shrinkage (left) with thermal annealing in the fibre direction and growth (right) induced in lattice along the normal to fibre direction as a function of fluence (1 = 6.0 • 1020 p/cm2; 2 = 3.0 • 1020 p/cm2; 3 = 1.0 • 1020 p/cm2)

Figure 10.

Restoration of growth along the normal direction of irradiated 2D C/C fibres through thermal cycling and as a function of proton fluence (left) and of irradiated IG-43 graphite irradiated with fluence 4.0 1020 p/cm2

Figure 11.

Dimensional change and thermal annealing of 3D C/C composite structures following proton irradiation with fluence 4.0 1020 p/cm2

The dimensional changes of irradiated 3D C/C composite are shown in Figure 11. For the 3D architecture the material exhibits a negative CTE in all directions. As seen in Figure 11 for the un-irradiated samples, there is accelerated shrinkage >600º C attributed to the influence of the matrix within the fibre structure. Reversal from shrinkage to growth at these temperatures was observed in previous studies (Burchell, 1994). Measurements of thermal conductivity of the irradiated 3D C/C and IG-43 graphite samples following proton irradiation revealed that thermal conductivity reduced by a factor of three (3) for the 3D C/C for 0.25 dpa fluence and by a factor of six (6) for IG-43 and similar fluence. To address the significantly higher irradiation damage from energetic protons a new irradiation experiment has been initiated where the carbon composite will be exposed to a neutron flux at the BNL BLIP facility which results from the spallation of protons with upstream isotope targets. The goal is to compare the damage at similar fluences of energetic protons and energetic neutrons.

2.2. SiCf/SiC

Silicon carbide fibre reinforced composites (SiCf/SiC), along with the C/C composites, considered as prime candidates for the first wall and blanket structural material in fusion reactors. Due to their low activation and irradiation stability these composites have a clear advantage over the C/C composites especially when the neutron doses are expected to be high as it is the case of fusion reactors where tens of dpa over the lifetime will be accumulated. Its inherent stability stems from the isotropic dimensional change of the cubic SiC crystal (Bonal et al. 2009) which tends to saturate at modest irradiation levels. It also exhibits good fracture resistance and excellent mechanical properties at high temperatures. While the carbon composite technology and manufacturing is more mature than that of the SiC composites, which currently have limited structural applicability outside nuclear reactors. Significant progress has been made in recent years to both eliminate issues of early grades of the composite associated with poor irradiation performance (Snead et al., 1992) and reduce cost through adoption of novel fabrication techniques (Katoh et al., 2010a) such as the nano-infiltrated transient-eutectic (NITE) process (Bonal et al., 2009). For nuclear grade SiCf/SiC composites the costly chemical vapour infiltration technique (CVI) is used.

To assess the neutron irradiation damage of SiCf/SiC composites grades produced by a variety of approaches a number of irradiation experiments have been launched using the HFIR and JTMR reactors (Katoh et al., 2010a). Irradiation of the various grades at HFIR to levels up to 10 dpa and at elevated temperatures of 800º C has also been conducted. The key objective is to assess the strength and stability of the improved composites and the thermal conductivity degradation. In contrast to the early SiCf/SiC grades which suffered significant irradiation damage from de-bonding of fibre matrix interface driven by fibre densification the new grades show minimal degradation of strength and stability of mechanical properties up to 10 dpa (Katoh et al., 2007). Thermal conductivity, however, remains an issue for low irradiation temperatures.

An experimental study on the effects of high temperatures and proton or fast neutron irradiation has been initiated at Brookhaven National Laboratory. The goal is to subject SiCf/SiC composite to similar irradiation fields that the carbon composites have been exposed to and make comparison in the irradiation-induced damage. As discussed in the previous section, significant damage was observed in C/C composites at levels far below the observed limits in neutron irradiation environments. Shown in Figure 12 is an optical image of SiCf/SiC composite section showing the fibre bundle thickness (~128μm) and the SiC matrix thickness (~343μm). Also shown in Figure 12 is the distribution of voids within the architecture. Figures 13 and 14 are SEM images of the fibre/matrix interfaces and of the individual fibres.

Figure 12.

Optical microscope image of a SiCf/SiC structure showing the arrangement of the weaved fibre bundles and the matrix

To assess the effect of high temperature on the SiCf/SiC in terms of dimensional changes, structure and density composite samples were brought to 1000º C in atmosphere and the changes were made with precise instruments at the BNL isotope facility. Dimensional changes were more pronounced along the fibres (shrinkage of ~1%) while in the direction normal to the fibres they were of the order of 0.09%. Density reduction of ~0.8% was also observed (ρrt = 2.4324 g/cc) following the annealing of the sample for one hr at 1000º C. Shown if Figure 17 is dimensional changes obtained for temperatures up to 610º C and are compared with those of 3D C/C. As seen in Figure 17 during the first thermal cycle there is an adjustment in the both structures except more pronounced in SiCf/SiC which expands with increasing temperature in contrast to C/C which shrinks for the selected temperature range. Based on the stabilized thermal expansion, the thermal expansion coefficient (CTE) in the range of 200-600º C was estimated as 3.7 10-6/K. Experimental results (Zhang, 2006) on carbon fibre reinforced SiC (via CVI method) up to 1400º C showed values similar average values in the 200-600º C but with dramatic fluctuations above 800º C. Following the planned proton irradiation of the SiCf/SiC and the fast neutron irradiation using the spallation process at the isotope production facility at BNL the effects on the physio-mechanical properties will be studied and compared with the C/C composites.

Figure 13.

SEM photograph of a SiCf/SiC cut section (left) and of fibre arrangement (right)

Figure 14.

SEM photograph of a fibre bundle (left) and fibre detail (right) of SiCf/SiC

Figure 15.

SEM of a SiCf/SiC section at room temperature (left) and following annealing at 1000º C for one hour (right)

Figure 16.

Close SEM view of a SiC/SiC section at room temperature (left) and following annealing at 1000º C for one hour (right)

Figure 17.

Dimensional change of un-irradiated SiC/SiC composite over two thermal cycles (noted as TC1 and TC2) and comparison with 3D C/C

2.3. Composite-like structures

A number of material structures not adhering to the classical definition of composites involving a matrix with fibre-reinforcement, i.e. C/C, C/SiC, SiCf/SiC, etc., can still be considered composites, or more appropriately composite-like with potential applications in the next generation fusion and fission nuclear reactors. These can be based on (a) the embedment of particles of one material into the lattice of another thus maintaining the individual characteristics, (b) the bonding of dissimilar materials using solid state reaction of chemical vapour deposition with the help of an interface layer, and (c) on deposition of nano-structured coatings on substrates to either enhance the properties of the combined structure or protect the substrate. Because of their potential for use in nuclear reactors, some of these composite-like structures have been studied for radiation damage and extreme temperatures.

2.3.1. AlBeMet

AlBeMet, while by metallurgical definition may be considered an alloy, is in fact a composite of aluminium and beryllium consisting typically of ~62% commercially pure beryllium and 38% of commercially pure aluminium by weight. The two metals involved in forming AlBeMet do not fully mix but instead the beryllium particles are embedded in a pure aluminium lattice. The powder is produced by a gas atomization process yielding a fine beryllium structure. The two granular forms are mixed at temperatures just below the melting points of the two metals and a pressure that prompt the particles to form a stable bond. The result is a non-typical composite with some very appealing thermo-physical properties since it combines the workability of aluminium and, for the most part, the hardness of beryllium. Interest in this special composite has been increased in recent years primarily for use in special components of particle accelerator systems and in particular in the accelerator target envelope characterized by high-radiation, high temperature and thermal shock conditions. The combination of low-Z, good thermal conductivity (210 W/m-K) and low electrical resistivity (3.5e-6 Ohm-cm), combined with its workability and hardness, make it very attractive for special components such as magnetic horns and targets. Unknown was its radiation resistance and dimensional stability which are key parameters for potential applications in nuclear reactor systems. The effects of radiation on the physical and mechanical properties of this unique composite have been studied using direct energetic protons and secondary fast neutrons of the BNL accelerator complex through a series of irradiation experiments. Peak proton fluences of 3.0 1020 p/cm2 at 140 MeV using the 200 MeV proton beam at BNL BLIP and, through a different study, fast neutron fluences of ~1019 n/cm2 were achieved in these accelerator-based irradiation experiments. The arrangement of specially designed test samples of beryllium (similar to AlBeMet samples) in the irradiation space intercepting the proton beam is shown in Figure 18. The numbered tensile specimens (dog-bone) are 42mm long and 1.5mm thick and have a strain gauge length of 6mm. The matching specimens are used for post-irradiation analysis of thermal expansion, electrical and thermal conductivity.

Post-irradiation studies revealed that AlBeMet is dimensionally stable following irradiation and that it resists embrittlement and degradation even at high proton fluences where materials such as graphite and carbon composites have shown to undergo serious degradation. As indicated above, the proton fluences received may be representative of a much more severe irradiation condition when correlated to either thermal or fast neutrons. Depicted in Figure 19 is the thermal expansion of both AlBeMet and beryllium for peak fluence of 1.2 1020 p/cm2 and the measured CTE of AlBeMet as a function of average proton fluence. The effects of proton irradiation on the stress-strain relation of AlBeMet and its comparison with beryllium are shown in Figure 20. While it is confirmed that the ultimate tensile strength of beryllium is higher than that of AlBeMet, the AlBeMet appears to increase its strength following irradiation (as expected in all metals due to the pinning of dislocations) but without loss of the ductility anticipated to accompany the induced hardening. Further tests are planned where AlBeMet will be exposed to higher proton and accelerator-produced fast neutron fluences to explore its mechanical behaviour.

Figure 18.

Arrangement of irradiated test samples of beryllium intercepting the 200 MeV proton beam at BNL isotope production facility.

Figure 19.

Thermal expansion (left) comparison of AlBeMet and beryllium irradiated by 200 MeV protons and peak fluence of 1.2 1020 p/cm2, and coefficient of thermal expansion of AlBeMet (right) at 550º C as a function of proton fluence

Figure 20.

Effects of 140 MeV proton irradiation on AlBeMet (left) and beryllium (right) on the stress-strain relations (range of fluence of irradiated samples 0.4 - 1.2 1020 p/cm2)

2.3.2. Bonded dissimilar materials

Bonding of dissimilar materials to create a “composite-like” structure and ensuring its ability to maintain the integrity of the interfaces under extreme temperature conditions and high radiation fluences is an important challenge. Applications of such composites can be seen in nuclear fuel elements, fusion reactor plasma facing components where high-Z materials such as tungsten with higher erosion resistance will protect low Z materials like carbon or beryllium and particle accelerator targets where the variation of the material atomic number Z from the centre of the intercepted beam is important for both particle-mass interaction and heat removal from the hot central part ( Simos et al., 2006b ). In all applications and due to the dissimilarity of the thermal expansion in the bonded material structure, high stresses can develop at the interfaces leading to micro-cracking or even separation. Such condition can dramatically reduce a key property of the composite layer that controls the primary function such as heat transfer across the interfaces through thermal conduction. Shown in Figure 21 is a schematic of a TRISO-coated particle and pebble bed fuel sphere for Generation-IV Very High Temperature Reactor (VHTR). Maintaining the integrity of the interfaces between the various layers around the fuel kernel under high temperatures and extreme radiation fluxes is crucial. The dimensional changes occurring as a result of the two simultaneous effects do not necessarily coincide in terms of direction (growth or shrinkage) and thus a better understanding of the interface mechanics under such conditions is required.

There is a significant need in the nuclear industry and in particular in the first wall of fusion reactors, of graphite/metals bonding to form a coating or cladding on the low Z materials (i.e. graphite) and reduce the erosion rate. Direct graphite-metal junctions (Brossa et al., 1992) for use in the first wall of fusion reactors are extremely sensitive to thermal cycling due to differences in thermal expansion so techniques have been developed and applied with the introduction of interface agents (such as silver) that will prevent the formation of fragile components and metal dissolution. Thus brazing between stainless steel and graphite, Mo and graphite as well as W and graphite has been produced using vacuum plasma spray (VPS) and chemical vapour deposition (CVD) techniques. To study the resilience to thermal shock, graphite/Mo or graphite/W bonding was achieved by using an intermediate layer of Mo, V, or Mo-Ti and applying a solid state reaction bonding technique (Fukatomi et al., 1985).

Figure 21.

TRISO-coated particle and fuel element for a pebble bed reactor (US DOE, 2006)

To assess the effect of proton irradiation bombarding the muon target at J-PARC facility where a 3 GeV, 333 μA proton beam is intercepted by a graphite target at a rate of 25 Hz an experimental study was initiated at Brookhaven National Laboratory. The study consisted of an irradiation phase using the 200 MeV proton beam of the BNL Linac and of a post-irradiation analysis to observe the degradation of the target-like composite structure that was made for the study. Shown in Figure 22 is a test specimen consisting of three materials (copper and titanium alloy Ti-6Al-4V) and graphite (IG-43) and two interfaces (graphite to titanium and copper to titanium alloy). To form the two interfaces the silver brazing technique in vacuum was applied. Two types of geometry in the 42mm long (4mm x 4mm cross sectional area) specimens was used, one at 45º (as shown) and one with normal or 900 interfaces. Shown in the SEM image of Figure 22 and prior to irradiation is the achieved bonding/interface (extremely faint) between copper and titanium alloy for the 900 interface.

The composite specimens were placed in the proton beam and received peak fluence over the two interfaces of ~8.0 1020 p/cm2. Post-irradiation examination revealed the loss of integrity of the graphite/copper interface and the complete separation. Shown in Figure 23 is the graphite-to-titanium interface zone prior to irradiation and the condition of the composite structure after irradiation. As it has been assessed by focussing on the graphite susceptibility to high energy proton irradiation (elevated irradiation damage due to the nuclear interactions and the accelerated formation of He bubbles trapped in the lattice) as part of the same irradiation study, the degradation of the interface is attributed to graphite radiation damage. The composite dimensional changes, which will inevitably result in interface stresses due to thermal expansion coefficient differences, were studied by analyzing the thermal strain as a function of temperature using the high-sensitivity dilatometer in the hot cell. Shown in Figure 24 are the thermal expansion of the composite structure (graphite/copper/titanium) for both 45 and 90-degree interface orientations and the three components of the composite when all have received the same proton fluence. The dissimilar rates of expansion between the three constituents and the dimensional change reversal of graphite above 600º C (discussed previously) introduce a non-liner thermal expansion trace. Important to note is that subsequent thermal cycles above the 600º C threshold, resulted in a complete failure and fracturing of the irradiated graphite in the composite. This was observed for both interface orientations and attributed to the growth reversal in the graphite leading to fracture of an already compromised graphite strength resulting from radiation damage.

Figure 22.

Graphite-titanium-copper composite sample (left) used for the BNL irradiation studies and SEM image of the copper-titanium interface prior to irradiation

Figure 23.

SEM image (left) of the graphite (top) and titanium interface prior to the 200 MeV proton irradiation and image of the degraded interface following irradiation (right)

The study demonstrated the serious effects that energetic protons at fluences above ~5.0 1020 protons/cm2 have on graphite and thus its interface or bonding with metals. In the fusion reactor, however, composite structures that involve graphite with metal cladding or coating will be exposed to higher fluences of 14 MeV fast neutrons. While for such neutron energies it is anticipated that the cross section of nuclear interaction is similar to that of the 200 MeV protons, confirmatory investigations are necessary. It should be emphasized that nuclear graphite exposed to higher fluences of thermal neutrons (< 1 MeV) than the ones achieved with the 200 MeV protons has shown much greater resilience to irradiation damage. Therefore, to address the potentially different response of such graphite to metal bonding when fast neutrons are the irradiating species (as in the fusion reactor) a radiation damage experiment using the spallation-produced fast neutrons at the BNL isotope facility has been launched. During this irradiation phase fast neutron fluences of ~2.0e+19 n/cm2 and dominated by energies between 1 MeV and 30 MeV will be achieved. While these levels are far below the fusion reactor fluences anticipated for the graphite/metal composite structures, a comparison between proton and neutron irradiation at similar exposure levels can be made.

Figure 24.

Thermal strain of the composite structures and of the three constituents all exposed to the same level of proton fluence (~2.0 1020 protons/cm2).

2.3.3. Nanostructured coatings

While nano-structured coatings on metal substrates form a unique class of materials with a wide range of applications, the combined coating/substrate structure can be also characterized as a composite. These structures exhibit similar behaviour at the interface between the substrate and the coating as fibre-reinforced matrices stemming from the mismatch of thermal expansion coefficient which leads to elevated interface stress fields at high temperatures. With recent advances in the techniques and application of nanocoatings on base materials such as thermal spray deposition (Tsakalakos, 2009), interest has increased for their potential use in nuclear reactor systems and in particular in plasma-facing components of fusion reactors.

In fusion reactor environments where the low Z materials of the plasma-facing wall (carbon or beryllium) require protection from erosion, coatings based on tungsten and its alloys have been explored (Koch, 2007). In such setting, however, extreme radiation damage presents an additional challenge for these relatively untested structures which alters the physio-mechanics of the interaction between the substrate and the coating due to the fact that the rate of change of the thermal expansion (CTE) as a function of the radiation fluence may differ significantly between the distinct materials. Therefore, the potential for micro-cracking and even separation between the substrate and the coating under a combination of extreme temperatures and radiation fluxes requires experimental investigation.

Experimental studies focussing on the radiation and extreme temperature effects on alumina (Al2O3) and titania (TiO2) nano-structured coatings applied on Ti-6Al-4V and 4130 steel alloy substrates were launched to assess their susceptibility. Specifically, 200 μm-thick coatings consisting of 87% Al2O3 and 13% TiO2 (grid-blasted) and 600 μm-thick Al2O3 (thermally sprayed) on Ti-6Al-4V substrates were used along with 600μm-thick Al2O3 and 600 μm-thick amorphous Fe coating on alloy steel 4130 substrates. The behaviour of the interface of the between the substrate and the coating was evaluated for temperatures reaching 1200oC. In addition, the radiation damage from the spallation-based radiation field at BNL BLIP using 116 MeV protons. During irradiation, nano-coated samples received a neutron fluence of ~2.0e+19 n/cm2 with mean energy of 9 MeV. Combined with the neutron fluence, the coatings received a secondary proton fluence of ~3.2e+15 p/cm2 of 23 MeV mean energy, a photon fluence of ~3.0 e+19 γ/cm2 of 1 MeV mean energy and ~2.4e+16 e/cm2 of 1 MeV mean energy. Of primary interest was the effect of irradiation on the thermo-mechanical behaviour of the structures. Shown in Figure 25 are changes that occur at the interface of 600μm-thick Al2O3 on Ti-6Al-4V substrate from room temperature, to 900º C and 1200º C. Demonstrated is the resilience of the composite structure despite the high interface stresses which result in shear failure planes in the substrate (middle image). At higher temperatures (1200º C) the substrate material begins to re-arrange across the shear failure plane. The effect of extreme temperatures on the 600μm-thick Al2O3 layer deposited on alloy steel 4130 substrate is quite different as shown in Figure 26. At elevated temperatures (>600º C) an inter-metallic layer begins to form at the interface eventually leading to complete separation of the nano-structured alumina layer at 1200º C.

Figure 25.

Effect of temperature on the interface of nano-structured alumina coating on Ti-6Al-4V substrate from room temperature (left), to 900º C (middle) and 1200º C (right)

The effects of irradiation on the thermal expansion of the coated samples were studied and are depicted in Figures 27 and 28 where they are compared with their un-irradiated counterparts. Observed in the un-irradiated case is that the coating and substrate adjust at certain temperatures to accommodate for the dissimilarities in thermal expansion coefficient. The adjustment which first occurs at a low temperature (~150º C) re-occurs at a higher temperature in a subsequent thermal cycle. This behaviour in which the two dissimilar materials adjust at a particular temperature is very similar to what has been observed near phase transitions in bcc metals such as tungsten. The radiation effects on the stress-strain behaviour based on specially-designed and irradiated specimens with the fluences mentioned above are currently being evaluated.

Figure 26.

Effect of temperature on the interface of nano-structured alumina coating on 4130 steel alloy substrate from room temperature (left), to 900º C (middle) and 1200º C (right)

Figure 27.

Thermal expansion of Ti-6Al-4V substrate coated with 200μm-thick Al2O3 –TiO2 layer compared with the thermal expansion of the substrate alone for the same temperature range. Shown is the re-adjustment that takes place in the coated sample at different temperatures in the thermal cycles (TC1=1st thermal cycle, TC2=2nd thermal cycle).

Figure 28.

Thermal expansion of Ti-6Al-4V substrate coated with 200 μm-thick Al2O3 –TiO2 layer compared with the thermal expansion of the substrate alone for the same temperature range following irradiation with neutrons of fluence 2.0 e+19 n/cm2.

3. Conclusion

With the development of the new generation composites such as C/C, and SiC/SiC as well as special bonds and coatings rapidly advancing and, in the process, performance in extreme environments is better understood and quantified, there is high degree of confidence that these material structures will be able to support the needs of the next generation reactors. A multitude of efforts world-wide have been aiding in closing the knowledge gap on these very promising materials during the last three decades while, with the adoption of novel processing techniques, have made their fabrication at a large-scale feasible. However, due to the harshness of the nuclear environment of the future reactors, consisting of a combination of extremes in temperature and radiation flux, further work is necessary to qualify these composites since the available data are the results of small-scale experimental efforts. The extensive experience on the constituents of these composites from fission reactors may not necessarily provide a good basis to assess the performance of the integrated composite in the elevated nuclear environments. As some of the irradiation experiments using more energetic particles than the thermal neutrons from fission reactors on materials with well understood behaviour (i.e. graphite) showed is that irradiation-induced damage may occur at a faster rate at much lower thresholds. This emphasizes the need to understand and quantify the performance of both the constituents and the final composite structure under prolonged exposure to higher energy neutrons that make up the flux in the next generation fusion and fission reactors.

Irradiation damage studies to-date focussing on the next generation composites and using the available facilities have shown that it is feasible with these new material forms to achieve the performance required through extrapolation. However, the actual conditions in the fusion and next generation fission reactors are expected to be more severe in terms of flux, fluence and temperature. These may result in a much greater spectrum of changes in the physio-mechanical properties of these materials especially in hydrogen and helium formation. The knowledge of the behaviour of these promising composite materials at these levels, either extrapolated or acquired through tests simulating the anticipated conditions, will still be at a small scale. For application in the large-scale of the fusion or fission reactor environment the small-scale must be extrapolated to the realistic size of the components. Therefore a better handle of the scaling must be achieved with the development and implementation of numerical codes. Because of the variability within their structure the numerical models need to consider spatial variation of the properties. Code benchmarking efforts focussed in the specifically on the prediction of the response of these composites will be necessary. Important attributes that make these composites attractive, such as shock resistance, need special attention and further experimental work due to the enormous complexity of the problem associated with fibre-reinforced composites. The effect of irradiation on the degradation of the physical and mechanical properties that control the response to shock absorption, for example, down to the interface between the fibre and the matrix need to be understood so the performance of the bulk composite can be assessed.

Acknowledgments

The author gratefully acknowledges the input of Dr. H. Ludewig and Dr. H. Kirk for discussions on the subject and for reviewing and commenting on the manuscript, Dr. L. Snead for providing SiC/SiC samples for the study and Prof. T. Tsakalakos for providing the nanostructured coating samples and for discussions on the subject. The help of A. Kandasamy, Dr. A. Stein and Dr. J. Warren for facilitating the optical microscopy and SEM images is much appreciated and acknowledged.

© 2011 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms of the Creative Commons Attribution-NonCommercial-ShareAlike-3.0 License, which permits use, distribution and reproduction for non-commercial purposes, provided the original is properly cited and derivative works building on this content are distributed under the same license.

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Nikolaos Simos (July 20th 2011). Composite Materials under Extreme Radiation and Temperature Environments of the Next Generation Nuclear Reactors, Metal, Ceramic and Polymeric Composites for Various Uses, John Cuppoletti, IntechOpen, DOI: 10.5772/21488. Available from:

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