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Hardening matrix

Whatever the fine structure and reactions associated with hydrating cement paste, the permeability of the hardened matrix will depend on the sizes of interconnected capillary openings remaining after hydration. [Pg.87]

This equation says that the critical stress on the slip system can change as a result of the accumulation of plastic strain on the slip system. The accumulation of plastic strain on the slip system is measured in terms of the shear strain yp. The matrix hap is the so-called hardening matrix and is the backbone of a hardening law for single crystal plasticity. One of the dominant tasks facing those who aim to build viable models of plasticity on the basis of insights at the dislocation level is to probe the veracity of expressions like that given above. [Pg.59]

Composites have replaced finished metals in many products. They typically consist of fibrous reinforcement such as glass and carbon or other materials that are encapsulated in a hardened matrix of a resin system. Carbon composite is used in launch vehicles and heat shields for the re-entry phase of spacecraft. Composites have advantages over finished metals. They can be stronger and stiffer than metals per unit weight, highly corrosion resistant, electrically insulating, and much more. [Pg.275]

The flexibilizer markedly modifies the relaxation behaviour of the epoxy resin systems shown in Figs. 20 and 21. Its incorporation results in crosslinked two-phase systems. But the two phases are compatible and therefore not clearly separate. The Tg of the resin-hardener matrix (a relaxation) is smoothly passing into the Tg of the incorporated oligoester (a2 relaxation). The maximum of the relaxation shifts to lower temperatures as the flexibilizer content of the system is increased. The QL2 relaxation always occurs at nearly the same characteristic temperature, as is evident from the modulus decay at about 240 K in Figs. 20 and 21. The reduction in modulus observed in the rubber-elastic state shows the decrease in crosslinking density caused by an increase in flexibilizer content. ... [Pg.19]

Jim for concretes. Therefore, in ordinary concrete, special air-entraining agents are added (cf. Section 4.3.6) to produce an artificial system of spherical air bubbles uniformly distributed in the hardened matrix with spacing factor L equal to 200 pm as a maximum. The spacing factor is the most important parameter characterizing the resistance of cement-based materials to freeze-thaw cycles, but other parameters (e.g. a, A gg) also characterize the air-entrained pore system and their values should be maintained within prescribed limits all are described in detail in Section 6.5. [Pg.404]

As mentioned above, the reduced amount of water and low value of the wic ratio are necessary for the high strength and low porosity which characterize high performance concrete. The excellent workability of fresh mix required is ensured by admixtures. When the wJc is equal to 0.22, it means that the amount of water is limited to that necessary for cement hydration. However, in such a case complete hydration is impossible. On the other hand, any additional amount of water, if not bound to cement, may decrease the strength and increase the porosity of the hardened matrix. [Pg.476]

The enhanced strength and corrosion properties of duplex stainless steels depend on maintaining equal amounts of the austenite and ferrite phases. The welding thermal cycle can dismpt this balance therefore, proper weld-parameter and filler metal selection is essential. Precipitation-hardened stainless steels derive their additional strength from alloy precipitates in an austenitic or martensitic stainless steel matrix. To obtain weld properties neat those of the base metal, these steels are heat treated after welding. [Pg.347]

Both sohd-solution hardening and precipitation hardening can be accounted for by internal strains generated by inserting either solute atoms or particles in an elastic matrix (11). The degree of elastic misfit, 5, produced by the difference, Ai , between the lattice parameter, of the pure matrix and a, the lattice parameter of the solute atom is given by... [Pg.113]

Fig. 17. Structuie of U-700 after piecipitation hardening temperature of 1168 C/4 h + 1079" C/4 h + 843 C/24 h + TGO C/IG h with air cooling from each temperature. A grain boundary with precipitated carbides is passing through the center of the electron micrograph. Matrix precipitates are y -Nij(TiAl). Fig. 17. Structuie of U-700 after piecipitation hardening temperature of 1168 C/4 h + 1079" C/4 h + 843 C/24 h + TGO C/IG h with air cooling from each temperature. A grain boundary with precipitated carbides is passing through the center of the electron micrograph. Matrix precipitates are y -Nij(TiAl).
Epoxidized phenol novolak and cresol novolak are the most common curing agents. The composition of the resin and hardener system is optimized for each specific appHcation eg, incorporating phenol novolaks in the matrix resin can iacrease cure speed. [Pg.531]

Bone, or osseous tissue, is composed of osteocytes and osteoclasts embedded in a calcified matrix. Hard tissue consists of about 50% water and 50% solids. The solids are composed of cartilaginous material hardened with inorganic salts, such as calcium carbonate and phosphate of lime. [Pg.185]

In Ni—P electroless deposits, there can be as much as 10% by weight of phosphoms. The amount depends on the added complexing agents and the pH. The Ni—P deposits are fine-grained supersaturated soHd solutions, which may be precipitation hardened by heat treatment to form dispersed Ni P particles in a nickel matrix. [Pg.528]

Fig. 5. Micrographs of the microstructure of fully hardened and tempered tool steels produced by the powder metallurgy technique, showing uniform distribution and fine carbide particles in the matrix, (a) M-42 (see Table 6) and (b) cobalt-free AlSl T-15 having a higher concentration of fine carbide... Fig. 5. Micrographs of the microstructure of fully hardened and tempered tool steels produced by the powder metallurgy technique, showing uniform distribution and fine carbide particles in the matrix, (a) M-42 (see Table 6) and (b) cobalt-free AlSl T-15 having a higher concentration of fine carbide...
Sohd rocket propellants represent a very special case of a particulate composite ia which inorganic propellant particles, about 75% by volume, are bound ia an organic matrix such as polyurethane. An essential requirement is that the composite be uniform to promote a steady burning reaction (1). Further examples of particulate composites are those with metal matrices and iaclude cermets, which consist of ceramic particles ia a metal matrix, and dispersion hardened alloys, ia which the particles may be metal oxides or intermetallic compounds with smaller diameters and lower volume fractions than those ia cermets (1). The general nature of particulate reinforcement is such that the resulting composite material is macroscopicaHy isotropic. [Pg.4]

Cement and Concrete Concrete is an aggregate of inert reinforcing particles in an amorphous matrix of hardened cement paste. Concrete made of portland cement has limited resistance to acids and bases and will fail mechanically following absorption of crystalforming solutions such as brines and various organics. Concretes made of corrosion-resistant cements (such as calcium aluminate) can be selected for specific chemical exposures. [Pg.2457]

Fig. 20.5. Concrete is a particulate composite of aggregate (60% by volume) in a matrix of hardened cement paste. Fig. 20.5. Concrete is a particulate composite of aggregate (60% by volume) in a matrix of hardened cement paste.
Both thermoplastics and thermosets can be formed by compression moulding (Fig. 24.5). The polymer, or mixture of resin and hardener, is heated and compressed between dies. The method is well suited to the forming of thermosets (casings for appliances, for instance) and of composites with a thermosetting matrix (car bumpers, for example). Since a thermoset can be removed while it is still hot, the cycle time is as short as 10 seconds for small components, 10 minutes for large tliick-walled mouldings. Pressures are lower than for injection mouldings, so the capital cost of the equipment is much less. [Pg.259]

Polymer-matrix composites for aerospace and transport are made by laying up glass, carbon or Kevlar fibres (Table 25.1) in an uncured mixture of resin and hardener. The resin cures, taking up the shape of the mould and bonding to the fibres. Many composites are based on epoxies, though there is now a trend to using the cheaper polyesters. [Pg.264]


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