Comparison of engineered nanocoatings on the combustion of aluminum and copper oxide nanothermites (original) (raw)

2013, Surface and Coatings Technology

Water-repellent nano-coatings for submerged combustion of nano-energetic composite materials were developed. These coatings may have applications for oceanic power generation, underwater ordnance, propulsion, metal cutting, and torch technologies. Nano-coatings were deposited on thermite pellets by a vapor-phase technique. Two types of deposition techniques studied were chemical vapor deposition (CVD) and atomic layer deposition (ALD). A total of six types of nano-coatings were applied on the thermite pellets. Various process parameters to produce the coatings were explored. Characterization of the nano-coatings was carried out using Fourier Transform Infrared Spectroscopy (FTIR), Scanning Electron Microscopy (SEM), Atomic Force Microscopy (AFM), and contact angle goniometry. Submerged combustion tests of the nano-coated thermite pellets were performed as a function of submerged time. The pellets were submerged in de-ionized water for 3, 5, and 10 days. The energy released by the thermite reaction was analyzed and compared to other types of nano-coated pellets. Initial results of a fluorocarbon self-assembled monolayer (FSAM) coating were compared with an ALD coating composed of Al 2 O 3 . Results show that with increasing submerged time, there was a decrease in the ratio of bubble energy to total energy of combustion (K c =K bubble /K combustion ) for all coatings tested. The initial bubble energy of the pellets coated with FSAM and ALD with Al 2 O 3 was 133.3 and 142.2 (KJ/Kg), respectively. After submersion for 10 days, the bubble energy reduced to 10.4 and 15.6 (KJ/Kg), respectively. The value of K c for the FSAM coating decreased by a factor of 12.8 whereas the ALD with Al 2 O 3 coating decreased by a factor of 9.1. The hydrophobic coating is critical for energy generation because without it, the pellets do not ignite, resulting in 100% loss of energy.

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Effect of a superhydrophobic coating on the combustion of aluminium and iron oxide nanothermites

Surface and Coatings Technology, 2011

There is an interest in broadening the range of applications of nanoenergetic composite materials to include their combustion and energy generation in submerged environments. Currently, their use is primarily limited to gas environments. Oceanic power generation, underwater ordnance, propulsion, metal cutting, and torch technologies are examples of applications that would significantly benefit from nanocomposite energetic materials. Recent research on superhydrophobic coatings has made it possible to coat nanoenergetic samples using a vapor-phase deposition process which significantly reduces the detrimental effects of water entering the composite that can occur during wet-chemistry based superhydrophobic processes. In this work, we discuss the process utilized to produce the superhydrophobic coating on nanoenergetic materials. We then analyze the bubble energy produced and compare this value to other energetic formulations. It was found that the ratio of the bubble energy to the total energy of combustion was an order of magnitude higher for the superhydrophobic coated materials compared to energetic composites containing a hydrophobic binder.

Effect of surface coatings on aluminum fuel particles toward nanocomposite combustion

Surface and Coatings Technology, 2013

Flame front velocity (FFV) of three energetic material composites was measured in order to understand the effects of surface functionalization on aluminum reactivity. Composites were prepared using molybdenum trioxide (MoO 3 ) and aluminum (Al) fuel particles with and without surface functionalization. The surface functionalization consisted of a 5-nm-thick layer (35% by weight) of perfluorotetradecanoic acid (PFTD) bonded to the Al 2 O 3 surface of the Al particles. The first composite consisted of Al functionalized with PFTD and MoO 3 , the second consisted of Al with MoO 3 and added PFTD particles to the same weight percentage as in the Al functionalized PFTD, and the third composite consisted of Al with MoO 3 . The results showed a dramatic increase in FFV from 100 to 500 m/s resulting from the surface functionalization. The results of the experiments show that the surface functionalized Al composite (Al-PFTD/MoO 3 ) has a reaction rate 2× than that of the simple Al/MoO 3 and 3.5× than that of the Al/MoO 3 /PFTD composite.

A nanoparticle composite for explosive underwater reaction applications has been designed with a nanomatrix of polytetrafluoroethylene and aluminum

2009

anometer aluminum fuel particles demonstrate orders of magnitude higher ignition sensitivity and reactivity than micrometer aluminum particles. This enhanced ignition sensitivity could enable a submerged reaction to propagate and react to completion without quenching. Energetic composites consisting of micrometer Al fuel particles cannot react submerged because too much energy from the reaction is lost to the surrounding water, causing the reactants to quench. However, Al nanoparticles can be synthesized with significantly higher surface-area-to-volume ratios that enable them to exhibit new and unique combustion properties that are much improved over their micron scale counterparts. One such property is enhanced ignition sensitivity, which has the potential to open a new realm of underwater reaction applications. These could include fuses, propulsion, underwater ordnance, torch or metal cutting technologies, offshore oil drilling, blasting, and welding, as well as alternative power ...

Experimental studies on the burning of coated and uncoated micro and nano-sized aluminium particles

Aerospace Science and Technology, 2007

Two different approaches are used in this work to reduce the burning times of aluminium particles with the ultimate goal to improve the performances of solid propellants. One method is to coat the micro-sized particles by nickel, and the second is to decrease the particle sizes to nano-metric scales.A thin coating of Ni on the surface of Al particles can prevent their agglomeration and at the same time facilitates their ignition, thus increasing the efficiency of aluminized propellants. In this work, ignition and burning of single Ni-coated Al particles are investigated using an electrodynamic levitation setup and laser heating of the particles. The levitation experiments are used to measure the particle ignition delay time and burning time at different Ni contents in the particles.Decreasing the size of Al particles increases their specific surface, and hence decreases the burning time of the same mass of particles. In this investigation, a cloud of Al nano-particles formed in a combustion tube is ignited by an electric spark. The cloud experiments are used to measure comparative flame front propagation velocities for different Al particle sizes with and without organic coating.The results and their analysis show that both methods reduce the Al burning time. Ni coating reduces significantly the ignition time of micro-sized Al particles and hence the total burning time compared to non-coated particles. Nano-sized particle clouds burn faster than micro-sized Al particle clouds.Deux approches sont étudiées pour diminuer le temps de combustion des particules d'aluminium dans le but d'améliorer les performances des propergols solides. Il s'agit d'une part d'enrober les particules de tailles micrométriques dans une fine couche de nickel, et d'autre part, d'utiliser des particules d'aluminium de taille nanométrique.Une mince couche de nickel couvrant les particules d'Al permet d'empêcher leur agglomération et facilite leur allumage. Dans ce travail, l'allumage et la combustion des particules isolées d'Al enrobées dans du Nickel sont étudiés à l'aide du lévitateur électrodynamique du LCSR équipé d'un dispositif d'allumage par laser. Ce dispositif permet de déterminer les temps d'allumage et de combustion des particules en fonction de la composition du milieu gazeux environnant, la pression et le contenu en Nickel de la particule. Les expériences sont conduites notamment dans de l'air et le CO2 jusqu'à 40 bars et des pourcentages en Nickel de la particule de 0 à 15% en masse.Diminuer la taille des particules à des échelles nanométriques augmente leur surface spécifique et par conséquent diminue le temps de combustion d'une même masse d'Al. Dans cette étude, un nuage de nano particules d'Al est formé dans un tube de combustion et allumé par des électrodes. Ces expériences permettent de déterminer les vitesses comparatives de propagation du front de flamme en fonction de la taille des particules et de la nature de leur enrobage (alumine ou des matériaux organiques).Les résultats préliminaires et leurs analyses montrent que les deux méthodes permetent de réduire d'une façon significative les temps de combustion des particules de'aluminium.

Effect of particle coating on the thermal response of mixtures of micro- and nano-aluminum particles with water

Journal of Thermal Analysis and Calorimetry, 2016

Differential scanning calorimetry is used to determine the thermal response of commercially available aluminum powders reacting with an excess of water. Thermal response as a function of ageing, particle coating and heating rate is examined. The effect of the surface-tovolume ratio of the reaction vessel is also examined through the use of a purpose-built ignition apparatus. The work is motivated by the use of metal-water reactions to generate gaseous hydrogen for energy applications. Four powders are considered: nanopowder with preexisting oxide coating (U-ALEX), Viton Ò-coated nanopowder (V-ALEX), nonadecyclic-acid-coated nanopowder (L-ALEX) and oxide-coated micron-sized powder (H-2). The powder is mixed with water prior to testing, facilitated by ultrasonic agitation or the addition of a surfactant as needed. To determine the effect of ageing on the reaction onset temperature, selected samples are aged for 0, 1, 2, 5 and 14 days before being subjected to heat. The lowest and highest reaction onset temperatures were observed for the U-ALEX and L-ALEX powder mixtures, respectively. Coated powders had higher onset temperatures. The coatings offered some protection from oxidation, whereas the uncoated samples oxidized completely within 48 h. H-2, U-ALEX and V-ALEX exhibited similar activation energies and showed a slight decline in reaction onset temperature with ageing. It was not possible to determine an activation energy for L-ALEX. Within the limited range of the study, the surface-to-volume ratio of the reaction vessel had no significant impact on ignition temperature.

Coating Nano-sized Aluminum to Improve Solid Rocket Propellant Performance

In order to improve dispersion degree of nano-fuel in binder matrices and to increase the propellant performance, coating of aluminum particles with HTPB, Viton, SUREL or 8-hydroxyquinoline is considered. The quality of coating is verified by TEM visualizations. DSC/TG analyses show that the use of HTPB leads to the maximal oxidation degree among the coated powders. The same powder used in HTPB/AP propellants causes a burning rate enhancement up to 26% at 40 bar with respect to uncoated ALEX TM containing composition. The most effective coating for SKDM-80/AP-based propellants is 8-hydroxyquinoline, considering burning rate (+ 26%), and condensed combustion products (-45%).

Preparation and characterization of energetic materials coated superfine aluminum particles

Applied Surface Science, 2014

This work is devoted to protect the activity of aluminum in solid rocket propellants by means of solvent/non-solvent method in which nitrocellulose (NC) and Double-11 (shortened form of doublebase gun propellant, model 11) have been used as coating materials. Scanning electron microscopy (SEM) and transmission electron microscopy (TEM) were employed to characterize the morphology of coated Al particles. Other characterization data of coated and uncoated Al particles, such as infrared absorption spectrum, laser particle size analysis and the active aluminum content were also studied. The thermal behavior of pure and coated aluminum samples have also been studied by simultaneous thermogravimetry-differential thermal analysis (TG-DTA) and differential scanning calorimetry (DSC). The results indicated that: superfine aluminum particles could be effectively coated with nitrocellulose and Double-11 through a solvent/non-solvent method. The energetic composite particles have core-shell structures and the thickness of the coating film is about 20-50 nm. The active aluminum content of different coated samples was measured by means of oxidation-reduction titration method. The results showed that after being stored in room temperature and under 50% humidity condition for about 4months the active aluminum content of coated Al particles decreased from 99.8 to 95.8% (NC coating) and 99.2% (Double-11 coating) respectively. Double-11 coating layer had a much better protective effect. The TG-DTA and DSC results showed that the energy amount and energy release rate of NC coated and Double-11 coated Al particles were larger than those of the raw Al particles. Double-11 coated Al particles have more significant catalytic effect on the thermal decomposition characters of AP than that of NC coated Al particles. These features accorded with the energy release characteristics of solid propellant.

Analysis of Liquid Feedstock Behavior in High Velocity Suspension Flame Spraying for the Development of Nanostructured Coatings

Over the last decade the interest in thick nano-structured layers has been increasingly growing. Several new applications, including nanostructured thermoelectric coatings, thermally sprayed photovoltaic systems and solid oxide fuel cells, require reduction of micro-cracking, resistance to thermal shock and/or controlled porosity. The high velocity suspension flame spray (HVSFS) is a promising method to prepare advanced materials from nano-sized particles with unique properties. However, compared to the conventional thermal spray, HVSFS is by far more complex and difficult to control because the liquid feedstock phase undergoes aerodynamic break up and vaporization. The effects of suspension droplet size, injection velocity and mass flow rate were parametrically studied and the results were compared for axial, transverse and external injection. The numerical simulation consists of modeling aerodynamic droplet break-up and evaporation, heat and mass transfer between liquid droplets a...

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